SISTEMA E MÉTODO PARA MOVER UMA CARGA ÚTIL

Description

SYSTEM AND METHOD FOR MOVING A PAYLOAD FIELD OF THE INVENTION

[001] The present invention relates to transport equipment, in particular to means and methods for moving a payload, specifically to a system and method for moving a payload that are based on the use of aircraft apparatus, self-propelled modules and payloads and also to an aircraft apparatus, self-propelled module and payload, each of which can be used in such system and method individually or in combination with each other. BACKGROUND OF THE INVENTION

[002] To date, a plurality of various scalable automated transport systems have been developed for transporting or delivering a payload. Despite the acceptable speed and payload capacity of such automated transport systems, existing automated transport systems have a significant disadvantage, as it is impossible to automatically redistribute a payload during transport or delivery to a destination point.

[003] There is therefore a need to develop methods and systems for moving a payload.

[004] In particular, various transport systems that rely on the use of scalable automated aircraft or other types of self-propelled devices that have various housing designs and are equipped with propulsion units enabling movement and navigation in airspace have become widespread.

[005] For example, U.S. Patent Application No. 20220144431 (hereinafter referred to as U.S. 20220144431) published on May 12, 2022 provides a system for moving a payload in the form of a means of Petition 870250091550, dated 07 / 10 / 2025, page 16 / 180 2 / 154 group transport, the system of which comprises aircraft units detachably anchored to each other, each of which has a housing provided with air propulsion units that enable the movement of such group transport means through the air and provided with docking modules that enable detachable connection of the housing of said aircraft unit to that of another aircraft unit while anchoring said aircraft units to each other, wherein said housing is further provided with a control module configured to receive control commands in order to enable detachable docking of the housing of said aircraft unit to that of at least one other aircraft unit.

[006] It should be noted that in the system for moving a payload in the form of a grouping transport means disclosed in US document 20220144431, the payload may be in a fixed position relative to the housing of a particular aircraft apparatus forming said grouping aircraft apparatus, a fact which also makes it impossible to redistribute the payload in said transport means.

[007] Thus, the main disadvantage of the known system for moving a payload in the form of a grouping transport means disclosed in US document 20220144431 is that it is impossible to redistribute a payload in said transport means.

[008] Thus, there is an obvious need for further improvement of known systems, methods, aircraft apparatus and / or self-propelled modules for moving a payload, in particular to enable the redistribution of a payload.

[009] Therefore, the technical problem solved by the present invention is to create a system, method, aircraft apparatus and self-propelled module for moving a payload, in each of which at least the disadvantage of Petition 870250091550, dated 07 / 10 / 2025, page 17 / 180 3 / 154 The known system for moving a payload above the limit, which makes it impossible to redistribute a payload, is at least partially mitigated. DISCLOSURE

[010] The objective of the present invention is to create a self-propelled system, method, aircraft and module for moving a payload, each solving at least the aforementioned technical problem of the prior art, as well as expanding the range of means for moving a payload.

[011] The task at hand is solved in the first aspect of the present invention by the fact that the aircraft apparatus in question comprises: (i) an aircraft apparatus housing which housing is provided with one or more air propulsion units enabling the movement of the aircraft apparatus through the air and one or more docking modules configured, each to detachably connect said housing to the housing of another aircraft apparatus while anchoring said aircraft apparatus to each other; and (ii) a control module configured to receive control commands so as to enable the docking of said aircraft apparatus to at least one other aircraft apparatus; (a) the aircraft apparatus housing is further provided with one or more guides, each of which is configured to mount or suspend a payload thereon and to move said mounted payload along thereon;and (b) at least one of said guides is configured to connect or anchor in a detachable manner to one or more guides of said connected housing of another aircraft device to form a grouping guide.

[012] Furthermore, the task at hand is solved in the second aspect of the present invention by the fact that the aircraft apparatus in question comprises: (i) an aircraft apparatus housing which housing is provided with one or more air propulsion units enabling the Petition 870250091550, dated 07 / 10 / 2025, p. 18 / 180 4 / 154 movement of the aircraft apparatus through the air and a control module; (a) the aircraft apparatus housing is further provided with one or more guides, each of which is configured to mount or suspend a payload thereon and to move said payload along the same; (b) at least one of said guides is configured to connect or anchor in a detachable manner to one or more guides of the housing of another aircraft apparatus to form a grouping guide while anchoring said aircraft apparatus to each other; and (c) the control module is configured to receive control commands so as to enable the anchoring of said aircraft apparatus to each other.

[013] Furthermore, the task at hand is solved in the third aspect of the present invention by the fact that the grouping aircraft apparatus in question comprises: (i) two or more aircraft apparatuses anchored to each other in accordance with the first aspect of the present invention; (a) the control module further enables the undocking of at least one of said anchored aircraft apparatuses in order to enable the formation of a grouping guide of the guides of the remaining anchored aircraft apparatuses and / or enables the anchoring of yet another aircraft apparatus in accordance with the first aspect of the present invention to one of said anchored aircraft apparatuses in order to enable the formation of a grouping guide of the guides of said anchored aircraft apparatuses.

[014] Furthermore, the task at hand is solved in the fourth aspect of the present invention by the fact that the grouped aircraft apparatus in question comprises: (i) two or more aircraft apparatuses anchored to each other in accordance with the second aspect of the present invention; (a) the control module also enables the undocking of at least one of said apparatuses. Petition 870250091550, dated 07 / 10 / 2025, p. 19 / 180 5 / 154 aircraft devices anchored to each other, so as to enable the formation of a grouping guide of the guides of the remaining aircraft devices anchored to each other and / or enables the anchoring of yet another aircraft device according to the second aspect of the present invention, to one of said aircraft devices anchored to each other, so as to enable the formation of a grouping guide of the guides of said aircraft devices anchored to each other.

[015] Furthermore, the task at hand is solved in the fifth aspect of the present invention by the fact that the payload in question comprises: (i) a payload housing which housing is provided with one or more docking modules, at least one of which is configured to interact with at least one guide of the aircraft apparatus or self-propelled module so as to enable movement of the payload housing along said at least one guide and / or provided with one or more guides, at least one of which is configured to interact with at least one docking module of the aircraft apparatus or with at least one docking module of the self-propelled module so as to enable movement of said aircraft apparatus or said self-propelled module along said at least one guide.

[016] Furthermore, the task at hand is solved in the sixth aspect of the present invention by the fact that the self-propelled module in question comprises: (i) a housing for the self-propelled module provided with one or more air propulsion units enabling the movement of the aircraft apparatus through the air and provided with one or more additional means of movement; and (ii) a control unit configured to control the operation of said air propulsion units and to actuate at least one of said additional means of movement; (a) the housing for the module Petition 870250091550, dated 07 / 10 / 2025, page 20 / 180 The 6 / 154 self-propelled unit is further supplied with one or more docking modules, each of which is configured to enable the mounting or suspension of said self-propelled module on a guide and to enable the movement of said self-propelled module along said guide and / or supplied with one or more guides, at least one of which is configured to interact in a detachable manner with the docking module of the aircraft apparatus or the docking module of a payload.

[017] Furthermore, the task in question is solved in the seventh aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more aircraft devices according to the first aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the first aspect of the present invention or one or more aircraft devices grouped together according to the third aspect of the present invention by detachably connecting the anchoring modules thereof to each other, so as to enable the movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together;or (ii) one or more aircraft devices grouped together according to the third aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the first aspect of the present invention or one or more aircraft devices grouped together according to the third aspect of the present invention by detachably connecting the anchoring modules thereof to each other so as to enable the movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together.

[018] Furthermore, the task at hand is resolved in the eighth aspect of Petition 870250091550, dated 07 / 10 / 2025, p. 21 / 180 7 / 154 present invention by the fact that the method of moving a payload in question comprises the steps of: (i) anchoring at least one of one or more aircraft devices according to the first aspect of the present invention, or one or more aircraft devices in a group according to the third aspect of the present invention, to one or more additional aircraft devices according to the first aspect of the present invention, or one or more additional aircraft devices in a group according to the third aspect of the present invention, by connecting the anchoring modules of said aircraft devices to be anchored together to form a grouping guide of the guides of said aircraft devices to be anchored together; and (ii) moving the payload along said grouping guide formed on at least one of said anchored aircraft devices.

[019] One method is possible, in which, before the anchoring stage, the aircraft housing is rotated in relation to the guide.

[020] Furthermore, the task in question is solved in the ninth aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more aircraft devices according to the first aspect of the present invention or one or more aircraft devices grouped together according to the third aspect of the present invention; and (iii) one or more payloads according to the fifth aspect of the present invention, at least one of which is anchored to at least one of said aircraft devices by placing at least one of the guides of said at least one payload in interaction with at least one anchoring module of said at least one aircraft device so as to enable the movement of said at least one aircraft device along the Petition 870250091550, dated 07 / 10 / 2025, p. 22 / 180 8 / 154 referred to by at least one payload guide or by placing at least one of the anchoring modules of said payload in interaction with at least one guide of said at least one aircraft apparatus so as to enable the movement of said at least one payload along said at least one guide of the aircraft apparatus, or (ii-ii) one or more payloads according to the fifth aspect of the present invention,at least one of which is anchored to at least one of said grouped aircraft devices by placing at least one of the guides of said at least one payload in contact with at least one anchoring module of said at least one grouped aircraft device so as to enable the movement of said at least one grouped aircraft device along said at least one payload guide or by placing at least one of the anchoring modules of said payload in interaction with at least one guide of said at least one grouped aircraft device so as to enable the movement of said at least one payload along said at least one guide of the grouped aircraft device.

[021] One method is possible, in which, before the anchoring stage, the aircraft housing is rotated in relation to the guide.

[022] Furthermore, the task at hand is solved in the tenth aspect of the present invention by the fact that the method of moving a payload in question comprises the steps of: (i) anchoring one or more payloads according to the fifth aspect of the present invention, each to at least one of one or more aircraft devices according to the first aspect of the present invention or one or more aircraft devices in a group according to the third aspect of the present invention by placing at least one of the guides of said payload in interaction with the anchoring module of Petition 870250091550, dated 07 / 10 / 2025, p. 23 / 180 9 / 154 referred to as at least one aircraft device in order to enable the movement of said aircraft device and aircraft devices anchored to it along said payload guide or by placing at least one of the anchoring modules of said payload in interaction with the guide of said at least one aircraft device in order to enable the movement of the payload along said aircraft device guide.

[023] One method is possible, in which, before the anchoring stage, the aircraft housing is rotated in relation to the guide.

[024] Furthermore, the task in question is solved in the eleventh aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more aircraft devices according to the first aspect of the present invention, or at least one aircraft device in a group according to the third aspect of the present invention;and (ii) one or more self-propelled modules according to the sixth aspect of the present invention, at least one of which is anchored to at least one of said aircraft devices according to the first aspect of the present invention, or to at least one of the aircraft devices that form said at least one aircraft device in a group according to the third aspect of the present invention, by placing at least one of the guides of said self-propelled module in interaction with the anchoring module of said at least one aircraft device so as to enable the movement of said aircraft device and aircraft devices anchored thereto along said at least one guide of the self-propelled module or by placing at least one of the anchoring modules of said self-propelled module in interaction with the guide of said at least one aircraft device so as to enable the movement of the module; Petition 870250091550, dated 07 / 10 / 2025, p. 24 / 180 10 / 154 self-propelled along the aforementioned aircraft guide.

[025] Furthermore, the task at hand is solved in the twelfth aspect of the present invention by the fact that the method of moving a payload in question comprises the steps of: (i) anchoring one or more self-propelled modules in accordance with the sixth aspect of the present invention,each to at least one of one or more aircraft devices according to the first aspect of the present invention or one or more aircraft devices in a grouping according to the third aspect of the present invention by placing at least one of the guides of said self-propelled module in interaction with the anchoring module of said at least one aircraft device so as to enable the movement of said aircraft device and aircraft devices anchored thereto along said at least one guide of the self-propelled module or by placing at least one of the anchoring modules of said self-propelled module in interaction with the guide of said at least one aircraft device so as to enable the movement of the payload along said guide of the aircraft device.

[026] One option is possible, in which, before the anchoring stage, the housing of the self-propelled module is rotated in relation to the guide.

[027] Furthermore, the task in question is solved in the thirteenth aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more payloads according to the fifth aspect of the present invention; and (ii) one or more self-propelled modules according to the sixth aspect of the present invention, at least one of which is detachably anchored to at least one of said payloads by placing at least one of the guides of said self-propelled module in Petition 870250091550, dated 07 / 10 / 2025, p. 25 / 180 11 / 154 interaction with the anchoring module of said at least one payload in order to enable the movement of said payload along said at least one guide of the self-propelled module or by placing at least one of the anchoring modules of said self-propelled module in interaction with the guide of said at least one payload in order to enable the movement of said at least one self-propelled module along said at least one guide of the payload.

[028] Furthermore, the task at hand is solved in the fourteenth aspect of the present invention by the fact that the method of moving a payload in question comprises the steps of: (i) anchoring one or more self-propelled modules according to the sixth aspect of the present invention, each to at least one of one or more payloads according to the fifth aspect of the present invention, by placing at least one of the guides of said self-propelled module in interaction with the anchoring module of said at least one payload so as to enable the movement of said payload along said at least one guide of the self-propelled module or by placing at least one of the anchoring modules of said self-propelled module in interaction with the guide of said at least one payload so as to enable the movement of the self-propelled module along said payload guide.

[029] One method is possible, in which, before the anchoring stage, the aircraft housing is rotated in relation to the guide.

[030] Furthermore, the task at hand is solved in the fifteenth aspect of the present invention by the fact that the aircraft apparatus in question comprises: (i) an aircraft apparatus housing which housing is provided with one or more air propulsion units Petition 870250091550, dated 07 / 10 / 2025, page 26 / 180 12 / 154 enabling the movement of the aircraft apparatus through the air; and (ii) a control module; (a) the aircraft apparatus housing is further provided with one or more guides, each of which is configured to mount or suspend a payload thereon so as to enable the simultaneous movement of said payload along said guide and the movement of said guide relative to said housing; and (b) at least one of said guides is configured to connect or anchor in a detachable manner to one or more guides of the housing of another aircraft apparatus to form a grouping guide while anchoring said aircraft apparatus to each other.

[031] Furthermore, the task at hand is solved in the sixteenth aspect of the present invention by the suit in which the grouping aircraft apparatus in question comprises: (i) two or more aircraft apparatuses anchored to each other in accordance with the fifteenth aspect of the present invention; wherein (a) the control module further enables the undocking of at least one of said anchored aircraft apparatuses in order to enable the formation of a grouping guide of the guides of the remaining anchored aircraft apparatuses and / or enables the anchoring of yet another aircraft apparatus in accordance with the fifteenth aspect of the present invention, to one of said anchored aircraft apparatuses in order to enable the formation of a grouping guide of the guides of said anchored aircraft apparatuses;wherein (b) the control module further enables the movement of the payload along said grouping guide and the movement of at least a portion of said grouping guide in relation to at least one of the housings of the aircraft devices docked together.;

[032] Furthermore, the task at hand is solved on the seventeenth Petition 870250091550, dated 07 / 10 / 2025, p. 27 / 180 13 / 154 aspect of the present invention by the fact that the aircraft apparatus in question comprises: (i) an aircraft apparatus housing which housing is provided with one or more air propulsion units enabling the movement of the aircraft apparatus through the air and one or more docking modules configured, each to detachably connect said housing to the housing of another aircraft apparatus while anchoring said aircraft apparatus to each other; and (ii) a control module configured to receive control commands so as to enable the docking of said aircraft apparatus to at least one other aircraft apparatus; (a) the aircraft apparatus housing is further provided with one or more guides, each of which is configured to mount or suspend a payload thereon so as to enable the simultaneous movement of said payload along said guide and the movement of said guide relative to said housing;and (b) at least one of said guides is configured to connect or anchor in a detachable manner to one or more guides of said connected housing of another aircraft device to form a grouping guide.

[033] Furthermore, the task at hand is solved in the eighteenth aspect of the present invention by the suit in which the grouping aircraft apparatus in question comprises: (i) two or more aircraft apparatuses anchored to each other in accordance with the eighteenth aspect of the present invention; wherein (a) the control module further enables the undocking of at least one of said anchored aircraft apparatuses in order to enable the formation of a grouping guide of the guides of the remaining anchored aircraft apparatuses and / or enables the anchoring of yet another aircraft apparatus in accordance with the eighteenth aspect of the present invention to one of said anchored aircraft apparatuses. Petition 870250091550, dated 07 / 10 / 2025, p. 28 / 180 14 / 154 si, in order to enable the formation of a grouping guide for the guides of said aircraft devices anchored to each other; wherein (b) the control module further enables the movement of the payload along said grouping guide and the movement of at least a portion of said grouping guide in relation to at least one of the housings of the aircraft devices anchored to each other.

[034] Furthermore, the task in question is solved in the nineteenth aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more aircraft devices according to the second aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the second aspect of the present invention or one or more aircraft devices grouped together according to the fourth aspect of the present invention by detachably connecting the guides thereof to each other, so as to enable the movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together;or (ii) one or more aircraft devices grouped together according to the fourth aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the second aspect of the present invention or one or more aircraft devices grouped together according to the fourth aspect of the present invention by detachably connecting the guides thereof to each other so as to enable the movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together.

[035] Furthermore, the task at hand is solved in the twentieth aspect of the present invention by the fact that the motion method in question of a Petition 870250091550, dated 07 / 10 / 2025, p. 29 / 180 15 / 154 payload comprises the steps of: (i) anchoring at least one of one or more aircraft devices according to the second aspect of the present invention, or one or more aircraft devices grouped together according to the fourth aspect of the present invention, to one or more additional aircraft devices according to the second aspect of the present invention, or one or more additional aircraft devices grouped together according to the fourth aspect of the present invention, by detachably connecting the guides of said aircraft devices to be anchored together to form a grouping guide of the guides of said aircraft devices to be anchored together; and (ii) moving the payload along said grouping guide formed on at least one of said anchored aircraft devices.

[036] One option is possible, in which, before the payload movement stage, the payload is rotated in relation to the grouping guide.

[037] Furthermore, the task in question is solved in the twenty-first aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more aircraft devices according to the fifteenth aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the fifteenth aspect of the present invention, or one or more aircraft devices grouped together according to the sixteenth aspect of the present invention, by detachably connecting the guides thereof to each other so as to enable the simultaneous movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together and the movement of at least a portion of said grouping guide in relation to one or more housings of Petition 870250091550, dated 07 / 10 / 2025, p. 30 / 180 16 / 154 said aircraft devices anchored to each other, or (ii) one or more aircraft devices grouped together according to the sixteenth aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the fifteenth aspect of the present invention, or one or more aircraft devices grouped together according to the sixteenth aspect of the present invention, by detachably connecting the guides thereof to each other, so as to enable simultaneous movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together and movement of at least a portion of said grouping guide in relation to one or more housings of said aircraft devices anchored together.

[038] Furthermore, the task at hand is solved in the twenty-second aspect of the present invention by the fact that the method of moving a payload in question comprises the steps of: (i) anchoring at least one of one or more aircraft devices according to the fifteenth aspect of the present invention, or one or more aircraft devices in a group according to the sixteenth aspect of the present invention, to one or more additional aircraft devices according to the fifteenth aspect of the present invention, or one or more additional aircraft devices in a group according to the sixteenth aspect of the present invention, by detachably connecting the guides of said anchored aircraft devices to each other to form a grouping guide of the guides of said anchored aircraft devices;and (ii) simultaneously move at least a portion of said grouping guide formed in relation to one or more housings of said aircraft devices anchored together and move the payload along said grouping guide formed in relation to; Petition 870250091550, dated 07 / 10 / 2025, p. 31 / 180 17 / 154 minus one of the aforementioned aircraft devices docked together.

[039] Furthermore, the task in question is solved in the twenty-third aspect of the present invention by the fact that the system for moving a payload in question comprises: (i) one or more aircraft devices according to the seventeenth aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the seventeenth aspect of the present invention, or one or more aircraft devices grouped together according to the eighteenth aspect of the present invention, by detachably connecting the anchoring modules thereof to each other so as to enable the simultaneous movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together and the movement of at least a portion of said grouping guide in relation to one or more housings of said aircraft devices anchored together,or (ii) one or more aircraft devices grouped together according to the eighteenth aspect of the present invention, at least one of which is detachably anchored to one or more additional aircraft devices according to the seventeenth aspect of the present invention, or one or more aircraft devices grouped together according to the eighteenth aspect of the present invention, by detachably connecting the anchoring modules thereof to each other so as to enable simultaneous movement of the payload along a grouping guide formed from the guides of said aircraft devices anchored together and movement of at least a portion of said grouping guide in relation to one or more housings of said aircraft devices anchored together.

[040] Furthermore, the task at hand is solved in the twenty-fourth aspect of the present invention by the fact that the motion method in Petition 870250091550, dated 07 / 10 / 2025, p. 32 / 180 18 / 154 issue of a payload comprises the steps of: (i) anchoring at least one of one or more aircraft devices according to the seventeenth aspect of the present invention, or one or more aircraft devices in a group according to the eighteenth aspect of the present invention, to one or more additional aircraft devices according to the seventeenth aspect of the present invention, or one or more additional aircraft devices in a group according to the eighteenth aspect of the present invention, by detachably connecting the anchoring modules of said anchored aircraft devices together to form a grouping guide of the guides of said anchored aircraft devices together;and (ii) simultaneously move at least a portion of said grouping guide formed in relation to one or more housings of said aircraft devices anchored together and move the payload along said grouping guide formed on at least one of said aircraft devices anchored together.

[041] The above aspects of the present invention, from the first to the twenty-fourth, each provide a technical result of increasing the efficiency of redistributing a payload through the use of guides. The above technical advantage of the claimed group of technical solutions is not limiting. Additional advantages of the claimed group of technical solutions and individual technical solutions within said group, including particular embodiments thereof, will become apparent to those skilled in the art from the following detailed description of the present invention and the accompanying drawings.

[042] In addition, the above aspects of the present invention each provide an additional technical result of expanding the range of means for moving a payload. BRIEF DESCRIPTION OF THE DRAWINGS Petition 870250091550, dated 07 / 10 / 2025, page 33 / 180 19 / 154

[043] The accompanying drawings, which are included to provide further understanding of the principles of the present invention, constitute a part of this document and are incorporated into the present invention to illustrate the embodiments and aspects of the present invention below. The accompanying drawings, together with the description below, serve to explain the principles of the present invention. In the drawings: Fig. 1 is a first illustrative embodiment of the system for moving a payload according to the present invention; Fig. 2 is a second illustrative embodiment of the system for moving a payload according to the present invention; Fig. 3.1 is one of the illustrative embodiments of the self-propelled module according to the present invention; Fig. 3.2 is another illustrative embodiment of the self-propelled module according to the present invention; Fig. 3.3 is another illustrative embodiment of the self-propelled module according to the present invention, and of the grouped self-propelled module according to the present invention; Fig. 4 is a schematic view of one of the illustrative examples of the process of anchoring a payload to an aircraft device and a self-propelled module; Fig. 5 is a schematic view of one of the illustrative examples of the process of anchoring an aircraft unit to an aircraft unit supplied to a payload mounted on a self-propelled module; Fig. 6 is a schematic view of one of the illustrative examples of the process of replacing an aircraft apparatus with an aircraft apparatus in a group supplied to a payload mounted in a module. Petition 870250091550, dated 07 / 10 / 2025, page 34 / 180 20 / 154 self-propelled by another aircraft apparatus and also a view of the process of replacing a self-propelled module supplied to a payload with a self-propelled module in cluster; Figures 7.1 and 7.2 are schematic views of an illustrative example of the system comprising an aircraft apparatus in cluster with a cluster guide and multiple payloads configured to move along the cluster guide; Fig. 8 is a flow diagram of the first embodiment of the method for moving a payload; Fig. 9 is a flow diagram of the second embodiment of the method for moving a payload; Fig. 10 is a flow diagram of the third embodiment of the method for moving a payload; Fig. 11 is a flow diagram of the fourth embodiment of the method for moving a payload; Fig. 12 is a flow diagram of the fifth embodiment of the method for moving a payload; Fig. 13 is a flow diagram of the sixth embodiment of the method for moving a payload; and Fig. 14 is a flow diagram of the seventh embodiment of the method for moving a payload. DETAILED DESCRIPTION

[044] Several exemplary embodiments of the present invention are described below with reference to the accompanying drawings; however, it should be understood that the description below does not define or limit the scope of the present invention.

[045] In the following description, a detailed description of functions and Petition 870250091550, dated 07 / 10 / 2025, page 35 / 180 21 / 154 known projects will be omitted, as this unimportant information may obscure the concept of the present invention.

[046] It should be understood that in the following description terms such as first, second, top, bottom, side, front, back, etc. are used for convenience only and should not be interpreted as limiting terms. In particular, as used in the present invention, unless explicitly stated otherwise in the description in the present invention, the terms first, second, third or similar are used to distinguish elements, components, parts, assemblies, modules, blocks, embodiments or similar, to which they belong, from one another and are not intended to describe any particular relationship between them.Thus, for example, it should be understood that the use of the terms first group of self-propelled modules and second group of self-propelled modules is not intended to imply any particular order, type, chronology, hierarchy, or classification (for example) of / between groups of self-propelled modules within a plurality of self-propelled modules, nor is their use (by itself) intended to imply that a third group of self-propelled modules, a fourth group of self-propelled modules, etc., may still exist. Furthermore, as discussed in the present invention in other contexts, reference to a first group and a second group does not preclude in the present invention that the two groups are groups of the same elements. Thus, for example, in some cases, self-propelled modules in a first group of self-propelled modules and in a second group of self-propelled modules may coincide in terms of design, while in other cases they may differ in terms of design.

[047] References to an item in the singular should be understood as including such items in the plural and vice versa, unless explicitly stated otherwise or clear in the context of the present invention. Petition 870250091550, dated 07 / 10 / 2025, p. 36 / 180 22 / 154

[048] Grammatical conjunctions are intended to express any and all disjunctive and conjunctive combinations of conjunctive clauses, sentences, words and the like, unless otherwise indicated or clear from the context. Thus, the term or should be understood as generally meaning and / or and so forth.

[049] The citation of value ranges in the present invention is not intended to be limiting, referring individually to any and all values ​​that fall within the range, unless otherwise indicated in the present invention, and each separate value within such range is incorporated into the description as if it were recited individually in the present invention.

[050] The words about, approximately, or similar, when accompanying a numerical value, should be interpreted as including any deviation as would be understood by a person skilled in the art to operate satisfactorily for an intended purpose. Ranges of values ​​and / or numerical values ​​are provided in this document only as examples and do not constitute a limitation on the scope of the embodiments described.

[051] Any and all examples provided in the present invention, or at least a portion thereof, as well as the corresponding phrases (“for example”, “such as”, “in particular” or the like), are used only to facilitate understanding of the principles of the present invention and to provide sufficient disclosure of the present invention; however, these phrases do not impose any limitation on the embodiments of the present invention, for the description of which embodiments are used in the present invention, in particular they do not limit practical implementations of elements, components, parts, assemblies, modules, blocks, devices, means and / or the like used to disclose the design and operating principles of the present invention. TERMS AND DEFINITIONS USED IN THE DESCRIPTION OF THE PRESENT INVENTION Petition 870250091550, dated 07 / 10 / 2025, page 37 / 180 23 / 154

[052] The term illustrative means a non-limiting example, case, or illustration. Similarly, the terms for example and by way of example used in the present invention establish lists of one or more non-limiting examples, instances, or illustrations. As used in the present invention, the circuit assembly is “configured” to perform a function whenever the circuit assembly comprises the hardware and code necessary (if any) to perform the function, regardless of whether the performance of the function is blocked or prohibited (for example, by an operator-configurable setting, factory setting, etc.).

[053] As used in the present invention, the term correspondence and its derivatives (i.e., adjective, verb, adverb) does not necessarily mean exact conformity or exact equality in / to / between anything in any respect, but may imply a departure or deviation from said equality within specified limits. For example, the term corresponding coordinates, unless the description in the present invention clearly indicates otherwise, means not only that these coordinates may be exactly equal to each other or may coincide exactly with each other, but also implies that said equality or coincidence of coordinates may be established with some error (for example, with the operating error of a GPS system) or within the boundaries of a predetermined geographical region involving an exact geographical point or region to which these coordinates belong, or an exact geographical location to which these coordinates belong.

[054] In the context of the present invention, the term self-propelled module, unless the description in the present invention clearly indicates otherwise, refers to a structurally independent apparatus or device assembled from parts, elements, blocks, Petition 870250091550, dated 07 / 10 / 2025, p. 38 / 180 24 / 154 typical or standard (commercially available) sets, devices and / or similar items capable of moving under their own power through the air, over land (soil), over water, under water and / or over the surface of a stationary or mobile physical object, at least partially located in at least one airspace, land space, surface space and underwater space.

[055] As used in the present invention, the term unmanned aerial vehicle (UAV), unless the description in the present invention clearly indicates otherwise, refers to an unmanned aircraft that is configured to fly or is capable of moving through the air in automatic mode, i.e., without involving a human being or external control sources, or that is capable of moving through the air in semi-automatic mode, i.e., receiving at least a portion of the control commands from a human (e.g., a pilot, an operator, or the like) or an external source (e.g., a control panel, control server, external control device, or the like) through predetermined communication channels. Unlimited examples of UAVs are various multirotor UAVs, e.g., multicopter drones; single-rotor UAVs, e.g., unmanned helicopters; hybrid UAVs, e.g., rotary-wing drones; and the like.

[056] In the context of the present invention, the term housing, unless the description in the present invention clearly indicates otherwise, refers to a structure, skeleton, enclosure, panel, fuselage, load-bearing structure or body of an inanimate physical object, each of which may be formed from a single load-bearing element or a combination of load-bearing elements connected together, wherein the type, shape, overall dimensions, design features and / or material of such housing are not specifically limited in any way. Petition 870250091550, dated 07 / 10 / 2025, page 39 / 180 25 / 154

[057] In the context of the present invention, the term payload, unless the description in the present invention clearly indicates otherwise, refers to persons or living beings (in particular, persons or living beings as such or persons or living beings placed in a capsule, cabin, accommodation module, cryomodule, rescue module, life compartment, life block and the like) or merchandise (merchandise as such or merchandise placed in crates, boxes, packages, bags, containers, reservoirs, vessels, tanks, cans, receptacles, barrels, cisterns, cylinders, vessels, reservoirs, packaging, bottles, flasks, glass containers, cylinders, cases, storage modules and the like) that can be accommodated in the housing of the means of transport performing the carrier function and are intended for the delivery, shipment or transport of persons, various living beings and / or various merchandise by air, land, water and / or underwater.

[058] As used in the present invention, the term module, unless the description in the present invention clearly indicates otherwise, refers to a functional element or a combination of functional elements of a device in the form of a part, node, block, or other assembly unit that performs certain technical functions that provide the operation of the device. The module can generally be implemented in practice using a combination of known structural elements, a combination of known structural elements and known hardware, a combination of known structural elements and known software and hardware, or a combination of known hardware and known software. Therefore, for example, the control module can be implemented using hardware and software.As used in the present invention, the integrated control module can be a physical device, an apparatus, or a plurality of modules implemented using hardware, for example, using a circuit. Petition 870250091550, dated 07 / 10 / 2025, page 40 / 180 26 / 154 application-specific integrated circuit (ASIC) or a field-programmable gate array (FPGA), or a combination of hardware and software, for example, using a microprocessor system and an instruction set that implements the functionality of the control unit, which (when executed) transforms the microprocessor system into an application-specific device or system (e.g., autopilot). Furthermore, each of the modules described in the present invention, or at least one of them, can be implemented in the form of a combination of hardware and software, wherein some of the functionalities described in the present invention in relation to one of the modules can be implemented by means of hardware alone, while other functionalities described in the present invention in relation to the same module or another module can be implemented by using hardware in combination with software.Furthermore, in the context of the present invention, the docking module can be configured to interact in a detachable manner with at least one unmanned aerial vehicle, wherein the docking module can be implemented using a combination of known structural elements, a combination of known structural elements and hardware, a combination of structural elements and software and hardware, or a combination of hardware and software.

[059] As used in the present invention, the term navigation command, unless the description in the present invention clearly indicates otherwise, refers to an instruction directed to aircraft devices and / or self-propelled modules that are part of the system for moving a payload. Navigation commands may be presented or provided by the motion control system of the self-propelled module or by the motion control system of the aircraft device in the form of digital or analog data, instructions, control signals or the like. Navigation commands Petition 870250091550, dated 07 / 10 / 2025, page 41 / 180 27 / 154 can be initially generated by, without limitation, an automatic operator, an operator (whether locally or remotely located) and / or an obstacle avoidance system. In the case of aircraft devices, navigation commands can be communicated, for example, to a control unit to control an aircraft device or the steering system of an aircraft device, while, in the case of self-propelled modules, navigation commands can be communicated, for example, to a control unit to control a self-propelled module or the steering system of a self-propelled module.

[060] As used in the present invention, the term manual control, unless the description in the present invention clearly indicates otherwise, refers not only to control using only human hands, but also using human feet, fingers, voice, pupils, or any suitable combination thereof. Thus, as used in the present invention, the term manual control refers to at least one of the following: buttons, levers, joysticks, rocker switches, pedals, touch screen, gesture control sensors, pupil tracking scanners, microphone, and / or the like.

[061] As used in the present invention, the term charging device, unless the description in the present invention clearly indicates otherwise, refers to a device for replenishing the range of a self-propelled module or aircraft apparatus by recharging its battery and / or replenishing its fuel capacity.

[062] As used in the present invention, the term database, unless the description in the present invention clearly indicates otherwise, refers to any set of structured data that does not depend on a specific structure, database management software, computer hardware that stores the data, uses the data, or Petition 870250091550, dated 07 / 10 / 2025, page 42 / 180 28 / 154 Another way is to make the data available for use. The database may be present on the same hardware running the process that stores or uses the information stored in the database, or it may be present on separate hardware, for example, a dedicated server or a plurality of servers.

[063] In the context of the present invention, the term anchor point, unless the description in the present invention clearly indicates otherwise, refers to a region of the surface of the housing of the self-propelled module / aircraft device or other structural portion of the self-propelled module / aircraft device, in which region said self-propelled module / aircraft device couples, connects or interacts with another self-propelled module / aircraft device or any other structure anchorable to said self-propelled module / aircraft device.

[064] As used in the present invention, the term parking station, unless the description in the present invention clearly indicates otherwise, means a fixed or mobile structure adapted to accommodate unmanned aerial vehicles, store unmanned aerial vehicles and / or refuel (e.g., recharge) within the same range of self-propelled modules or aerial vehicles.

[065] As used in the present invention, the term control device refers to computing equipment that executes a computer program to enable the receipt of requests (e.g., from other computing devices) through a communication network, the execution or processing of such requests, and / or the transmission of such requests over a communication network (e.g., to other computing devices). The computing equipment executing a computer program may be, without limitation, a single physical computer. Petition 870250091550, dated 07 / 10 / 2025, page 43 / 180 29 / 154 or a single physical computer system. As used in the present invention, the use of the term control device does not mean that each computational task (e.g., instructions or commands received) or any other specific task will be received, executed, or cause performance by one and the same control device (i.e., one and the same software and / or hardware), meaning that any number of pieces of software or hardware may be involved in receiving / transmitting, executing, or causing the performance of any task or request, or the consequences of any task or request, where all such software and hardware may be implemented in the form of one or more control devices.

[066] As used in the present invention, the term server refers to computing equipment that executes a computer program to enable the receipt of requests (e.g., from other computing devices) through a communication network, the execution or processing of such requests, and / or the transmission of such requests through a communication network (e.g., to other computing devices). The computing equipment that executes a computer program may be, without limitation, a single physical computer or a single physical computer system.As used in the present invention, the use of the term server does not mean that each computational task (e.g., instructions or commands received) or any other specific task will be received, executed, or cause performance by one and the same server (i.e., one and the same software and / or hardware), meaning that any number of pieces of software or hardware may be involved in receiving / transmitting, executing, or causing the performance of any task or request, or the consequences of any task or request, where all such software and hardware may be implemented in the form of. Petition 870250091550, dated 07 / 10 / 2025, page 44 / 180 30 / 154 one or more servers. FIRST MODE OF THE SYSTEM FOR MOVING PAYLOAD

[067] Fig. 1 is a first embodiment of a 500-1 system for moving a payload according to the present invention, comprising two aircraft apparatus 100 configured to connect detachably to each other or to anchor detachably to each other to form a grouped aircraft apparatus.

[068] It should be noted that the 500-1 system may consist of two or more aircraft devices 100 configured to connect detachably to each other to form a grouped aircraft device, for example, three, four, five, six, seven, eight, nine, ten, eleven, twelve or more configured aircraft devices, each analogous to one of the embodiments of the aircraft device 100 described in the present invention.

[069] It should also be noted that, from the 100 aircraft devices that are part of the 500-1 system, one or more grouped aircraft devices may be formed or defined (for example, one, two, three, four, five, six, seven, eight, nine, ten or more grouped aircraft devices), wherein said grouped aircraft devices may each consist of two or more 100 aircraft devices and may have identical or different quantities of aircraft devices forming such grouped aircraft devices.

[070] Each of the 100 aircraft devices that are part of the 500-1 system shown in Fig. 1 can be used to move or transport a payload through the air, in particular people, animals or other living organisms, means of transport, equipment, medicines or any other type of merchandise. In particular, each of the 100 aircraft devices can be Petition 870250091550, dated 07 / 10 / 2025, page 45 / 180 31 / 154 implemented as any suitable unmanned aerial vehicle (UAV) known in the state of the art.

[071] Each of the aircraft apparatus 100 that is part of the 500-1 system shown in Fig. 1 comprises a structure or housing 110 of any suitable type which is provided with at least two air propulsion units 120, each of which is configured in the form of an air thruster and which are arranged or mounted on the housing 110 on the outside thereof and also comprises a control module (not shown) mounted inside the housing 110 and configured to control the operation of the aircraft apparatus 100, including the operation of the propulsion units 120 thereof.The control module in each of the aircraft 100 devices is also configured to present control commands for at least one of the air propulsion units 120 in order to operate it, or for both air propulsion units 120 in order to operate them, thus enabling movement through the air or flight of the aircraft 100 device, wherein the simultaneous operation of both propulsion units 120 increases the carrier capacity of the aircraft 100 device.

[072] In addition, at least one or each of the aircraft apparatus 100 may comprise at least one of the following wireless communication means: an SW band radio antenna, USW radio antenna, UHF radio antenna, an optical communication module, a half-duplex / simplex satellite communication module, a 2G / 3G / 4G / LTE / 5G cellular communication module, a wireless communication module, a wired communication module and the like, thus enabling said aircraft apparatus 100 to receive navigation commands and / or control commands from the system control device 500-1 and, consequently, enabling the system control device 500-1 to control the operation of said aircraft apparatus. Petition 870250091550, dated 07 / 10 / 2025, page 46 / 180 32 / 154 100.

[073] In turn, the control device of system 500-1 is configured to receive and process data (including system requests) from aircraft devices 100 and is also configured to generate control instructions / commands and / or generate navigation instructions / commands based on said received data and the results of its processing, in order to enable the presentation or direction of such generated control commands and / or navigation commands to at least one of the aircraft devices 100, including in response to a request from said aircraft device 100. In order to present navigation commands and / or control commands to at least one of the aircraft devices 100 that are part of system 500-1, the control device of system 500-1 is communicatively coupled, via a communication network (not shown) that is part of system 500-1, to said aircraft devices 100.

[074] The control module in each of the aircraft devices 100 is communicatively coupled to the wireless communication means above the aircraft device 100, thus enabling said control module to process navigation commands and / or control commands received, by said wireless communication means of the aircraft device, from the control device of system 500-1 and control the operation of said aircraft device 100, depending on said navigation commands and / or control commands. In particular, in response to navigation commands and / or control commands from the control device of system 500-1, the control module of aircraft device 100 can, for example, enable the performance of the following operations: (i) change the flight speed of aircraft device 100, (ii) change the flight direction of aircraft device Petition 870250091550, dated 07 / 10 / 2025, page 47 / 180 33 / 154 100, (iii) directing aircraft 100 from a parking station (not shown) or a current region of airspace to a target region of airspace in which it is contemplated to dock said aircraft 100 to at least one other aircraft, to at least one self-propelled module 300 described below and / or to at least one payload 200 described below; (iv) docking aircraft 100 to at least one other aircraft, to at least one self-propelled module 300 described below and / or to at least one payload 200 described below; (v) undocking aircraft 100 from at least one other aircraft, from at least one self-propelled module 300 described below and / or from at least one payload 200 described below;and (vi) directing the aircraft device 100 to one of the parking stations (not shown) for accommodation therein or therein in order to enable the storage of said aircraft device 100 at said parking station and / or in order to enable the range (charge) replenishment of the aircraft device 100. In some embodiments of the present invention, the control device (not shown) may also not be part of the system 500-1.;

[075] In some embodiments of the present invention, the communication protocols and / or technical means used for communication between the control device of system 500-1 and the aircraft devices 100 may be at least partially different from each other and / or may at least partially coincide with each other. Furthermore, one or more corresponding communication protocols and technical means of communication may be used simultaneously for communication.

[076] In some embodiments of the present invention, the control device of the 500-1 system can be configured to organize safety during flight or movement through the air of aircraft devices 100 or Petition 870250091550, dated 07 / 10 / 2025, page 48 / 180 34 / 154 aircraft devices in clusters formed from aircraft devices 100.

[077] The control device of the 500-1 system, providing control and / or navigation commands for the control module of at least one or each of the 100 aircraft devices that are part of the 500-1 system shown in Fig. 1, is a single server that can be configured in the form of, for example, a Dell™ PowerEdge™ server that can use the Ubuntu Server operating system or the Windows Server operating system. Furthermore, the control device of the 500-1 system may have or acquire access to at least one database (not shown) through the 500-1 system communication network or otherwise, or may comprise at least one local database stored in the storage device (not shown) or in the memory (not shown) of such control device.

[078] In some embodiments of the present invention, the control device of the 500-1 system may be any other suitable hardware, application software, system software, or any combination thereof.

[079] In other embodiments of the present invention, the functions of the 500-1 system control device can be shared among multiple computer devices or computing devices, for example, they can be implemented using multiple servers communicatively coupled to each other via the 500-1 system communication network.

[080] In other embodiments of the present invention, the functions of the control device of system 500-1 may be performed by a control module of another aircraft apparatus identical or distinct from aircraft apparatus 100, or by a group or combination of control modules of other Petition 870250091550, dated 07 / 10 / 2025, page 49 / 180 35 / 154 aircraft devices identical or distinct from aircraft device 100, by the control unit of the self-propelled module 300 described below or by any other suitable computing device configured to generate control commands and / or navigation commands and to present said generated commands to the control module of at least one or each of the aircraft devices 100 that are part of the 500-1 system.

[081] The communication network of the 500-1 system to which the 500-1 system control device and the 100 aircraft devices are at least communicatively coupled substantially enables the 500-1 system control device and the 100 aircraft devices to exchange system and / or operational data with each other, which data they use to implement the functions or functional capabilities described in the present invention. Such a communication network may be, for example, any suitable wireless communication link known in the art, such as a communication link based on wireless WiFi technology, a communication link based on 2G, 3G, 4G or 5G wireless technology, a communication link based on LTE technology and / or the like.

[082] In one embodiment of the present invention, the 500-1 system may comprise two or more configured wireless networks, each analogous to the communication network above the 500-1 system for performing communication between the control device of the 500-1 system, aircraft devices 100 and / or any other functional devices that may also be part of the 500-1 system and that are described in the present invention, in real-time or real-time mode.

[083] Housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 may have any suitable shape and overall dimensions characteristic of any Petition 870250091550, dated 07 / 10 / 2025, page 50 / 180 36 / 154 aircraft apparatus known in the state of the art and can be made of any suitable material known in the state of the art and normally used for the manufacture of aircraft apparatus housings, in particular of a composite material (e.g., composite sandwich panels), metal (e.g., interconnected metal channel beams), aluminum (e.g., interconnected aluminum carrier beams), plastic (e.g., a solid piece of plastic), titanium material (e.g., titanium sandwich panels), any other suitable material known in the state of the art, including the use of any suitable combination of the above materials (e.g., a sandwich panel or titanium panels with an aluminum honeycomb core) and / or the like.Thus, the type, shape, overall dimensions, and material of housing 110 in each of the aircraft devices that are part of the 500-1 system are not specifically limited in any way within the scope of the present invention. In particular, housing 110 in at least one or each of the aircraft devices 100 that are part of the 500-1 system may have a shape that is generally identical to the housing of a helicopter or drone; a person skilled in the art would appreciate, however, that housing 110 may have any other shape similar to any other aircraft or air transport vehicle, for example, for an airplane, shuttle, hang glider, paraglider, or any other analogous aircraft device known in the state of the art.

[084] In one embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 can be configured in the form of a regular or irregular three-dimensional geometric figure, for example, in the form of a cube, cuboid, ball or sphere, square pyramid, tetrahedron (triangular pyramid), hexagonal pyramid, triangular prism, hexahedron (octahedron), prism Petition 870250091550, dated 07 / 10 / 2025, page 51 / 180 37 / 154 pentagonal, hexagonal prism, dodecahedron, ellipsoid, 20-sided polyhedron (icosahedron), cone, cylinder, or any other known three-dimensional figure.

[085] In another embodiment of the present invention, at least one portion of the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may have a cross-sectional shape (longitudinal or transverse cut) of a triangle, square, circle, oval, rectangle, parallelogram, rhombus, trapezoid, quadrilateral, pentagon, hexagon, heptagon, octagon, enneagon, decagon, icosagon or any other known regular or irregular geometric figure.

[086] In yet another embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be a skeleton, structure or support frame to which panels may be attached or which may be at least partially enclosed by a casing.

[087] In other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be additionally provided with fins, wings and / or tail rotor etc. to improve the aerodynamic characteristics of the aircraft apparatus 100 and improve its carrier capacity by generating additional lift during flight.

[088] In some other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may also be provided with at least one aircraft engine (not shown) and, preferably, two aircraft engines, to enable the aircraft apparatus 100 to move through the air in case of emergency (for example, in case of failure or breakdown of the air propulsion units 120) or to increase the speed of movement. Petition 870250091550, dated 07 / 10 / 2025, page 52 / 18038 / 154 through the air of the aircraft apparatus 100 enabling the operation of aircraft engines in addition to or instead of the propulsion units 120 used to move the aircraft apparatus 100 through the air in a standard situation). It should be noted that each of these aircraft engines may be, for example, a propeller engine, jet engine, combined aircraft engine or any other suitable aircraft engine known in the state of the art. It should also be noted that in the case of using two aircraft engines in the aircraft apparatus 100, their designs and / or types may coincide or differ from each other.Each such aircraft engine with which housing 110 may be fitted may operate under the control of the aircraft control module 100, which may present control commands to the aircraft engine control actuator of aircraft 100, so as to enable starting, stopping or changing the operating mode of said aircraft engine (for example, changing the operating parameters of the aircraft engine of aircraft 100).

[089] In some other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may further be provided with at least one additional lift rotor (not shown) or rotor propulsion unit of any suitable type known in the prior art to enable the aircraft apparatus 100 to move through the air (including in an emergency, for example, in case of damage, failure and / or complete discharge of the aircraft apparatus 100) or to increase the speed of movement through the air of the aircraft apparatus 100 by enabling the operation of the lift rotor or rotor propulsion unit in addition to or instead of the propulsion units 120 used to move the aircraft apparatus 100 through the air in a standard situation. Furthermore, in this embodiment of the present invention, the Petition 870250091550, dated 07 / 10 / 2025, page 53 / 180 39 / 154 housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 may further comprise a power plant (not shown) which may be defined, for example, by one or two turboshaft engines and which may be operationally coupled to each of the elevator rotors of the aircraft apparatus 100, so as to enable the supply of power to operate them.Each of these power plants of aircraft apparatus 100, whose power plant is operationally coupled to the elevator rotors of aircraft apparatus 100, whose elevator rotors may also be supplied to housing 110 in order to transfer motive power to it, may operate under the control of the control module of aircraft apparatus 100, whose control module may present control commands to the control actuator of the power plant (not shown) of aircraft apparatus 100, in order to enable starting, stopping or changing the operating mode of said power plant (for example, changing the operating parameters of the power plant of aircraft apparatus 100) to change the state of these elevator rotors of aircraft apparatus 100.

[090] In other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may further be provided with a landing gear (not shown) which may be an extendable support system or at least a rigidly attached support which may be provided to the housing 110 and which may be necessary at least for takeoff of the aircraft apparatus 100, landing of the aircraft apparatus 100 and / or accommodation of the aircraft apparatus at one of the parking stations to replenish its range. In particular, the landing gear of the aircraft apparatus 100 may be of the skid type, wheel type, track type, float type or any other type known in the state of the art. The type, shape, overall dimensions and material of the Petition 870250091550, dated 07 / 10 / 2025, page 54 / 180 40 / 154 The landing gear of aircraft apparatus 100 is not specifically limited in any way within the scope of the present invention. It should be noted that in this embodiment of the present invention, the landing gear of aircraft apparatus 100 can at least provide (i) static load support of its own weight while aircraft apparatus 100 is in a stationary state; and (ii) shock absorption of dynamic loads arising during the landing of aircraft apparatus 100 (including emergency landing) on ​​the surface of the ground, water or other physical object at least partially present in airspace, land space, water space and / or underwater space, depending on a particular embodiment of the present invention.

[091] In some other embodiments of the present invention, the housing 110 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may also not be provided with any type of landing gear. In one of the variations of such an embodiment of the present invention, the bottom of the housing 110 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may be provided with an impact-absorbing pad (not shown) made of an elastic material (e.g., rubber), which impact-absorbing pad may be attached to said bottom on the outside thereof or with any other suitable support known in the art and used in the art for known aircraft devices (in particular, for drones or other unmanned aerial vehicles).

[092] Furthermore, as shown in Fig. 1, the housing 110 in each of the aircraft devices 100 that are part of the 500-1 system is provided with two docking modules 130, each configured for Petition 870250091550, dated 07 / 10 / 2025, page 55 / 180 41 / 154 enable the detachable connection of housing 110 to the housing of another aircraft device corresponding to or different from aircraft device 100 while anchoring said aircraft devices to each other, wherein the anchoring modules 130 are mounted at opposite ends, on the outside of said housing 110. In some embodiments of the present invention, the housing 110 of at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may be provided with one or more anchoring modules 130, in particular with one, two, three, four, five, six, seven, eight, nine, ten or more anchoring modules 130. In other embodiments of the present invention, at least one of the anchoring modules 130 provided to the housing 110 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may be mounted inside said housing. Accommodation 110.In other embodiments of the present invention, at least one first anchoring module of the anchoring modules 130 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be mounted within said housing 110 and at least one second anchoring module of said anchoring modules 130 may be mounted within said housing 110.

[093] It should be noted that the anchoring modules 130 supplied to housing 110 in at least one or each of the aircraft devices 100 that are part of the 500-1 system shown in Fig. 1 allow for the detachable connection to said housing 110 of one or more additional housings 110 relating to other aircraft devices of the 500-1 system, wherein said additional housings 110 can be detachably connected to said housing 110 from one or both sides. Petition 870250091550, dated 07 / 10 / 2025, page 56 / 180 42 / 154 distinct, and to provide detachable connection of each of these additional housings 110, one or more pairs of anchoring modules 130 may be used (i.e., an anchoring module 130 on the side of the additional housing 110 to be connected and an anchoring module 130 on the side of the housing 110 to which said additional housing 110 is being detachably connected).

[094] Furthermore, at least one or each of the anchoring modules 130 in at least one or each of the aircraft devices 100 that are part of the 500-1 system may be configured to enable detachable connection of housing 110 to housing 310 of the self-propelled module 300 described below and / or to housing 210 of the supported load 200 described below. Thus, at least one of the anchoring modules 130 provided to housing 110 in each of the aircraft devices 100 that are part of the 500-1 system may enter into detachable interaction with at least one of the identical anchoring modules that may be provided to the housing of another aircraft device so as to provide detachable connection of the housings of the same to each other and thus provide detachable anchoring of said two aircraft devices to each other to form a grouped aircraft device.

[095] In one embodiment of the present invention, the anchoring module 130 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 can be configured to interact with at least one of the gripping or connecting elements (for example, with a cam, hook, clamp, eyelet, clamp, latch, electromechanical gripper, magnetic gripper and the like) that can be provided to the housing of another aircraft device corresponding to or distinct from aircraft device 100 in order to provide detachable connection of the housings thereof. Petition 870250091550, dated 07 / 10 / 2025, page 57 / 180 43 / 154 aircraft devices to each other for detachable anchoring of said two aircraft devices to each other, the anchoring of which results in a grouped aircraft device.

[096] Non-limiting examples of anchoring modules 130 for providing detachable gripping or connection of aircraft device housings 110 to each other are the following gripping or connecting elements, which must be provided to the anchoring modules 130 interacting with each other at the corresponding anchoring points of the aircraft device housings 110: various suitable mechanical means of connection or gripping (supports, grips, fasteners, mounting slots, cams, hooks, latches and the like), electromechanical means under the control of the aircraft device control module 100 (for example, electromechanical anchoring means for anchoring by a combination element to be anchored, electromechanical gripping means for gripping a combination element to be gripped or the like), electromagnetic means under the control of the aircraft device control module 100, magnetic means,Vacuum grippers under the control of the aircraft apparatus control module 100 and / or similar. It should be noted that if the anchoring module 130 in one of the aircraft apparatus 100 to be anchored together is provided with any gripping or connecting element of the mechanical connecting or gripping means, electromechanical means, electromagnetic means, magnetic means and vacuum grippers mentioned above, then the anchoring module 130 in the other of the said aircraft apparatus 100 to be anchored together must be provided with combination gripping or connecting means of a suitable type enabling the formation of a detachable connection between said anchoring modules 130.

[097] In one embodiment of the present invention, the module of Petition 870250091550, dated 07 / 10 / 2025, page 58 / 180 44 / 154 anchorage 130 in at least one or each of the aircraft devices 100 that are part of the 500-1 system shown in Fig. 1 may be a rigid gripping or connecting structure that may be configured to interact in a detachable manner with the anchoring modules 130 of one or more other aircraft devices 100 and which may be (i) attached to the housing 110 of the aircraft device on the outside thereof or (ii) partially embedded or integrated into the body of the housing 110 of the aircraft device so as to provide access to it from the outside of said housing 110.

[098] In another embodiment of the present invention, the docking module 130 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may be a mobile gripping or connecting structure that may be under the control of the control module of said aircraft device 100 and that may be configured to interact in a detachable manner with the docking modules 130 of one or more other aircraft devices 100, wherein said mobile structure may be attached to the housing 110 of the aircraft device on the outside thereof and may be configured to deploy, unfold or expand at least partially under the control of the control module of said aircraft device 100 so as to enable the return thereof to the initial state under the control of the control module of said aircraft device 100.Alternatively, the mobile attachment or connection structure, in the form of which the anchoring module 130 can be implemented, can be fully mounted or attached to the housing 110 of the aircraft device (i.e., in the internal space of the housing 110 of the aircraft device) and can be configured to extend at least partially from said housing 110 and / or deploy beyond the limits of said housing 110 under the control of the aircraft device control module 100 so as to enable its return to the initial state under. Petition 870250091550, dated 07 / 10 / 2025, page 59 / 180 45 / 154 control of the aircraft device control module 100. In yet another alternative, the mobile gripping or connection structure, in the form of which the anchoring module 130 can be implemented, can be partially embedded or integrated into the body of the housing 110 of the aircraft device and can be configured to deploy, unfold, expand or extend at least partially under the control of the aircraft device control module 100 so as to enable its return to the initial state under the control of the aircraft device control module 100. In yet another embodiment of the present invention, the anchoring module 130 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 can be a fixed gripping or connection structure that can be attached to the housing 110 of the aircraft device from the outside thereof,fastened inside housing 110 or partially embedded / integrated into the body of housing 110, wherein access to the free anchoring modules 130 for detachable interaction with the same from the anchoring modules 130 of other aircraft devices 100, in order to provide detachable connection of the housings 110 of such aircraft devices 100 to be anchored to each other, may be provided under the control of the control module of the aircraft device 100, whose housing 110 is provided with said free anchoring modules 130, by means, for example, of the opening of a barrier structure or cover structure that prevents the possibility of access to at least one of the free anchoring modules 130 from the outside of housing 110 and which may be, for example, (i) a hatch, door or flaps provided in the body of housing 110 or (ii) a hatch,door or flaps provided in a separate protective housing enclosing or containing said at least one free anchorage module 130 or (iii) a combination of the foregoing (i.e., a combination of (i) and (ii)). In another embodiment of, Petition 870250091550, dated 07 / 10 / 2025, p. 60 / 180 46 / 154 present invention, the possibility of actuation of the anchoring module 130 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig.1. In order to enable deployment, expansion, unfolding or extension thereof, it may be provided under the control of the aircraft control module 100 by means of, for example, opening a barrier structure or cover structure that prevents the possibility of movement of the anchor module 130 away from the housing 110 and which may be, for example, (i) a hatch, door or flaps provided in the body of the housing 110 or (ii) a hatch, door or flaps provided in a separate protective housing surrounding or enclosing the anchor module 130 or (iii) an element or plate attached to the housing 110 and preventing the possibility of carrying out an operation of deployment, expansion, unfolding or extension of the anchor module 130 or (iv) a combination of the foregoing (i.e., a combination of (i), (ii) and (iii)).In some other embodiment of the present invention, the anchoring module 130 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may be a fixed gripping or connecting structure that may be rigidly attached to the housing 110 of the aircraft device on the outside thereof or partially embedded / integrated into the body of the housing 110 and which may be closed by a barrier structure or covering structure (for example, an outer cover, coating or protective housing) preventing access to said fixed structure on the outside of the housing 110 for interaction with the same of the anchoring modules 130 of one or more other aircraft devices 100 and being under the control of the control module of the aircraft device 100 that is provided with said fixed gripping or connecting structure, wherein access to such anchoring module 130 may be provided by means of, by. Petition 870250091550, dated 07 / 10 / 2025, page 61 / 180 47 / 154 example, of the opening, outward opening, wide opening, displacement, sliding or removal of said barrier structure or cover structure under the control of said aircraft control module 100 in order to enable its subsequent return to its original position under the control of the aircraft control module 100 (as such need arises).

[099] Thus, thanks to the presence of the anchoring module 130, the aircraft devices 100 can be detachably connected (i.e., connected with the possibility of being detached) to the housing 110 of at least one of the aircraft devices 100 that are part of the 500-1 system shown in Fig. 1 in a quantity required to provide sufficient lift to move a payload through the air.

[100] In one embodiment of the present invention, at least one of the anchoring modules 130 provided to the housing 110 in one of the aircraft apparatus 100 that are part of the 500-1 system can be placed in detachable interaction with one or more anchoring modules 130 provided to the housing 110 in another aircraft apparatus of said aircraft apparatus 100, in particular with one anchoring module 130, two anchoring modules 130, three anchoring modules 130, four anchoring modules 130, five anchoring modules 130 and more anchoring modules 130 in said other aircraft apparatus 100.Thus, in this embodiment of the present invention, a case is possible in which, in order to detachably anchor two aircraft devices 100 to each other, it may be necessary to bring only one anchoring module 130 supplied to the housing 110 in the first aircraft device 100 to the detachable interaction with only one anchoring module 130 supplied to the housing 110 in the second aircraft device 100. Furthermore, in this embodiment of the present invention, Petition 870250091550, dated 07 / 10 / 2025, page 62 / 180 48 / 154 Another case is possible where, in order to detachably anchor two aircraft devices 100 to each other, it may be necessary to bring only one anchoring module 130 supplied to the housing 110 in the first aircraft device 100 to the detachable interaction with two, three, four, five or more anchoring modules 130 supplied to the housing 110 in the second aircraft device 100. Furthermore, in this embodiment of the present invention, yet another case is possible where, in order to detachably anchor two aircraft devices 100 to each other, it may be necessary to bring two anchoring modules 130 supplied to the housing 110 in the first aircraft device 100 to the detachable interaction with two, three, four, five or more anchoring modules 130 supplied to the housing 110 in the second aircraft device 100.

[101] In another embodiment of the present invention, the anchoring modules 130 that can be supplied to the housing 110 in any of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 can be supplied on one and the same external side of said housing 110 or at least partially on distinct external sides of said housing 110.

[102] In yet another embodiment of the present invention, at least one or each of the anchoring modules 130 that may be supplied to the housing 110 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 may anchor an aircraft device 100, at least two aircraft devices 100, an aircraft device in a group, at least two aircraft devices in a group or any possible combination thereof.

[103] In some embodiments of the present invention, the aircraft apparatus in a cluster formed as a result of the detachable connection Petition 870250091550, dated 07 / 10 / 2025, p. 63 / 180 49 / 154 between the anchoring modules 130 related to the two or more aircraft devices 100 to be anchored to each other is a grouping or mountable structure having any shape and geometric dimensions suitable for the free movement of such structure through the air, so as to enable the movement through the air of a payload that can be disposed or mounted in at least a portion of the housings 110 related to the aircraft devices 100 that are part of said aircraft device in grouping and suitable for enabling the anchoring of at least one (another) additional aircraft device in grouping and / or at least one additional aircraft device 100 to said aircraft device in grouping by placing the anchoring modules 130 of the same in detachable interaction.

[104] It should be noted that the grouped aircraft apparatus shown in Fig. 1 and formed as a result of the detachable connection of the housings 110 of two aircraft apparatus 100 can respond as an integral whole to control commands and / or control instructions received from the system control device 500-1, i.e., the operation of the aircraft apparatus 100 as part of such a grouped aircraft apparatus can be synchronized (for example, using the system control device 5001 or the control module of one of the aircraft apparatus 100 forming such a grouped aircraft apparatus).Furthermore, the 100 aircraft devices that form such a clustered aircraft device may be electrically connected to each other to form a single power supply circuit and a clustered power source (for example, the clustered power source may be formed from batteries of 100 aircraft devices anchored to each other) supplying power or powering all said 100 aircraft devices substantially simultaneously, thus making it possible to consider the range of not each of these devices. Petition 870250091550, dated 07 / 10 / 2025, page 64 / 180 50 / 154 of aircraft 100 individually, but rather the range of an aircraft unit in a group as a whole. It should also be noted that the mutual docking process of aircraft units 100 can occur directly in the air, where said docking process can be initiated or launched in response to control commands presented by the control device of system 500-1 to the aircraft units 100 to be docked together to form an aircraft unit in a group.

[105] The number of aircraft 100 devices anchored together to form a grouped aircraft device may be two or more units, wherein, in some embodiments of the present invention, the number of aircraft 100 devices anchored together may be multiple units, multiple tens of units or even multiple hundreds of units. To provide a required payload capacity, multiple aircraft 100 devices with the same payload capacity or different payload capacities may be used; however, the total payload capacity provided by these aircraft 100 devices must correspond to said required payload capacity, wherein the aircraft 100 devices to be anchored together may coincide as well as differ in terms of design, for example, in terms of overall dimensions and / or power and / or flight characteristics and / or type of propulsion unit.

[106] In addition, housing 110 in each of the two aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 is further provided with a straight guide 140 which is configured to mount or suspend a payload thereon, including the payload 200 described below, and to move said mounted or suspended payload straight along said guide 140. It should be noted that the shape, length (spatial extent) or other geometric dimensions, as well as the sectional shape and the Petition 870250091550, dated 07 / 10 / 2025, p. 65 / 180 51 / 154 The manufacturing material of the guides 140 in any of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 are not specifically limited in any way, wherein the shape and / or geometric dimensions (e.g., the length or spatial extent of the guide 140) of the guides 140 relating to distinct aircraft apparatus 100 that are part of the 500-1 system may coincide with each other or may differ from each other.

[107] According to one embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 may be provided with one or more guides 140 (for example, two, three, four, five, six, seven, eight, nine, ten and more guides 140), each of which may be configured to mount or suspend a payload thereon, including the payload 200 described below, and to move said mounted or suspended payload along said guide 140. In one variation of this embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 may be provided with two or more guides 140, wherein at least some or all of said guides 140 may be arranged parallel to each other, perpendicular to each other and / or at a predetermined angle to each other.In yet another variation of this embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system may be provided with two or more guides 140, at least some or all of which may be connected to each other to define the path of movement of a payload in relation to said housing 110 of the aircraft apparatus. In another variation of this embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system may be provided with two or more guides 140, wherein at least one of said guides... Petition 870250091550, dated 07 / 10 / 2025, p. 66 / 180 52 / 154 guides 140 can be used to mount or suspend a first payload in order to enable the movement of the first payload along said guide 140, and at least one other of said guides 140 can be used to mount or suspend a second payload in order to enable the movement of the second payload along said guide 140.

[108] According to yet another embodiment of the present invention, all guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 can be mounted or attached to the outside of said housing 110. According to another embodiment of the present invention, all guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 can be mounted or attached inside said housing 110 or in the internal space of said housing 110.According to another embodiment of the present invention, a portion of the guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 may be partially mounted or attached to the outside of said housing 110 and the other portion of said guides 140 may be partially mounted or attached inside said housing 110 or in the internal space of said housing 110.

[109] According to some embodiments of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 may be at least partially configured as foldable or flexible, thus allowing to at least partially compensate for the loads exerted on said guide 140 by the payload mounted or suspended on that guide 140 and moved along said guide 140 to position Petition 870250091550, dated 07 / 10 / 2025, page 67 / 180 53 / 154 the same at a suitable point in relation to the aircraft's housing 110.

[110] According to some other embodiments of the present invention, at least one or each of the guides 140 that can be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig.1 can be configured as straight or curved, thus allowing the definition not only of a straight path (straight trajectory) of movement of a payload along said guide 140 in relation to said housing 110 of the aircraft apparatus, but also to define a curved path (curved trajectory) of movement of a payload along said guide 140 in relation to said housing 110 of the aircraft apparatus, and also to define a combined path (combined trajectory) of movement of a payload along said guide 140 in relation to said housing 110 of the aircraft apparatus whose path has at least one straight section of the path and at least one curved section of the path.

[111] According to some other embodiments of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 may be configured in a T shape, Z shape, X shape, Y shape, inverted U shape, E shape, U shape, N shape, L shape, F shape, O shape, H shape, V shape, inverted L shape, C shape or W shape. It should be noted that in this embodiment of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system Petition 870250091550, dated 07 / 10 / 2025, p. 68 / 180 54 / 154 shown in Fig. 1 may also have any other shape corresponding to any known symbol, any known letter, any known geometric shape, any known numeral, or similar.

[112] According to some other embodiments of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be configured to enable the movement of a payload along at least one of the three coordinate axes (in particular, along any one of the three coordinate axes, along any two of the three coordinate axes or along all three coordinate axes) or may be configured to move relative to said aircraft apparatus housing 110 so as to enable the movement of a payload mounted or suspended in the guide 140, relative to said aircraft apparatus housing 110.

[113] According to other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be provided with two or more parallel guides 140 configured to mount or suspend a payload, including the payload 200 described below, and to move substantially in a straight line along the same mounted or suspended payload.

[114] The guides 140 in the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 are configured to connect detachably to each other in order to enable the formation of a straight grouping guide 145. As shown in Fig. 1, the grouping guide in a grouping aircraft apparatus comprises connecting detachably to each other two guides 140, each of which is mounted or fastened to Petition 870250091550, dated 07 / 10 / 2025, p. 69 / 180 55 / 154 outer side of housing 110 of the corresponding one of the two aircraft devices 100. Thus, the grouping guide 145 can be formed as a result of anchoring two or more aircraft devices 110 together to form a grouping aircraft device. In other words, the grouping guide 145 is substantially a guide for a grouping aircraft device and allows a payload, including the payload 200 described below, to be moved between the housings 110 of the aircraft devices 100 forming said grouping aircraft device, in particular to a vacant point in at least one of said housings 110.

[115] In one embodiment of the present invention, the grouping guide 145 can be formed from two or more distinct guides 140, each of which relates to one of the aircraft devices 100 anchored in a detachable manner, in particular it can be formed from two, three, four, five, six, seven, eight, nine, ten or more of these distinct guides 140, wherein the shape, length (spatial extension) or other geometric dimensions, manufacturing material of the grouping guide 145 and / or the like are not specifically limited in any way. It should be noted that the grouping guide 145 formed as a result of the detachable connection of distinct guides 140 can have a rectilinear shape or a curvilinear shape.

[116] According to other embodiments of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may comprise two or more portions, at least one of which is configured as movable, wherein said housing 110 of the aircraft apparatus may further comprise an actuation device under the control of the control module of said aircraft apparatus 100 and operationally coupled to said at least Petition 870250091550, dated 07 / 10 / 2025, p. 70 / 180 56 / 154 a movable portion of guide 140 in order to enable the movement of said at least one movable portion of guide 140 in relation to the remaining portions of guide 140 to change the shape of said guide 140.

[117] It should also be noted that the control device of the 500-1 system or the control module of one of the 100 aircraft devices anchored together used to form a grouping aircraft device may further enable the undocking of at least one of said 100 aircraft devices anchored together, so as to enable the formation of a grouping guide from the guides of the remaining 100 aircraft devices anchored together (in particular, so as to alter the total spatial extent of the guide towards reduction and / or alter the shape of the grouping guide) and / or enable the anchoring of yet another 100 additional aircraft device to one of said 100 aircraft devices anchored together, so as to enable the formation of a grouping guide from the guides of said 100 aircraft devices anchored together (in particular, so as to alter the total spatial extent of the guide to increase and / or alter the shape of the grouping guide).Furthermore, the process of docking yet another additional aircraft 100 unit to one of the aforementioned aircraft 100 units already docked together, in order to enable the formation of a grouping guide for the guides of the aforementioned aircraft 100 units docked together, can also be controlled by the control module of the aforementioned additional aircraft 100 unit to be docked.

[118] In one embodiment of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 may be mounted on a rotating device (not shown) mounted in said housing 110 of the aircraft apparatus. Petition 870250091550, dated 07 / 10 / 2025, p. 71 / 180 57 / 154 in order to enable the rotation of said guide 140 by a predetermined rotation angle, thus allowing the path or trajectory of movement of a payload along said guide 140 to be changed and / or allowing said guide 140 mounted on the rotating device to be connected to at least one other guide that is part of said guides 140 supplied to said housing 110.

[119] In another embodiment of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be rotatably mounted in said housing 110 of the aircraft apparatus, wherein said housing 110 of the aircraft apparatus may further comprise an actuation device (not shown) being under the control of the control module of said aircraft apparatus 100 and operationally coupled to said guide 140 or configured to interact with said guide 140 so as to enable rotation thereof by a predetermined angle of rotation, also allowing the path or trajectory of movement of a payload along said guide 140 to be altered and / or enabling the connection of said rotating guide 140 to at least one other guide that is part of said guides 140 provided to said housing 110.

[120] In yet another embodiment of the present invention, at least one or each of the guides 140 that may be provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be configured telescopic, wherein said housing 110 of the aircraft apparatus may further comprise an actuation device (not shown) being under the control of the control module of said aircraft apparatus 100 and operationally coupled to said guide 140 or configured to interact with said guide 140 in such a way Petition 870250091550, dated 07 / 10 / 2025, p. 72 / 180 58 / 154 to enable at least its partial extension. It should be noted that in this embodiment of the present invention, the aircraft control module 100 can also be configured to enable at least the partial or total retraction of the guide 140 that was previously totally or partially extended under the control of said aircraft control module 100 so as to provide the return of said guide 140 to a partially retracted state or a fully retracted state.It should also be noted that in this embodiment of the present invention, in order to extend or retract guide 140, the aircraft apparatus control module 100 can be further configured to present control commands to the actuating device (not shown) operationally coupled to said guide 140 to actuate them in an operating mode enabling at least partial extension of guide 140, at least partially or completely extended, or at least partial or total retraction of guide 140, at least partially or completely extended, respectively.

[121] In another embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 can be configured to tilt or rotate at a predetermined angle relative to at least one of the guides 140 from which said housing 110 of the aircraft apparatus can be provided.

[122] In some other embodiment of the present invention, the housing 110 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 can be configured to alter its shape and / or dimensions. In one of the variations of this embodiment of the present invention, the housing 110 in at least one or each of the aircraft devices 100 that are part of the system 500-1 shown in Fig. 1 can be a detachable mesh (not shown). Petition 870250091550, dated 07 / 10 / 2025, p. 73 / 180 59 / 154 configured to involve aircraft apparatus 100 while being deployed, wherein aircraft apparatus 100 may further comprise an actuation device (not shown) being under the control of the control module of aircraft apparatus 100 which control module, in turn, may receive control commands from the control device of system 5001 and operationally coupled to said loop of aircraft apparatus 100 in order to enable the deployment or deployment thereof in response to the control commands of the control device of system 500-1.It should be noted that in this variation of the embodiment of the present invention, the mesh of the aircraft apparatus 100 can be present in two states: a folded or disassembled state which corresponds to the initial state of the mesh of the aircraft apparatus 100 and in which the mesh of the aircraft apparatus 100 can be present during the movement of the aircraft apparatus 100 through the air, and an unfolded state in which the mesh of the aircraft apparatus 100 can be present while anchoring the aircraft apparatus 100 to at least one other aircraft apparatus to form a grouped aircraft apparatus, wherein the mesh of the aircraft apparatus 100 in the disassembled state has its minimum size and the mesh of the aircraft apparatus 100 in the unfolded state has its maximum size. In another variation of this embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig.1 may be formed from distinct functional portions (not shown) and may further comprise an actuation device (not shown) operationally coupled to said functional portions so as to enable the expansion or deployment of said functional portions to alter the shape and / or dimensions of said housing 110 of the aircraft apparatus. In yet another variation of this embodiment of the present invention, housing 110 in. Petition 870250091550, dated 07 / 10 / 2025, p. 74 / 180 60 / 154 at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be formed from distinct controllable functional portions (not shown) and the control module of the aircraft apparatus 100 may be further communicatively coupled to said controllable functional portions, so as to enable displacement (alteration of spatial locations) of said functional portions relative to each other in response to control commands from said control module, which commands may be generated by the control module of the aircraft apparatus 100 in response to corresponding control commands from the control device of the system 500-1 to alter the shape and / or dimensions of said housing 110 of the aircraft apparatus. In another variation of this embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig.1 can be formed from distinct controllable functional portions (not shown), wherein the aircraft apparatus control module 100 can be communicatively coupled to said controllable functional portions, so as to enable the expansion or deployment of said functional portions in response to the control commands of said control module, which commands can be generated by the aircraft apparatus control module 100 in response to the corresponding control commands of the system control device 500-1 to alter the shape and / or dimensions of said aircraft apparatus housing 110.

[123] In some other embodiment of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may further be provided with one or more controllable working members (not shown) configured to interact with a payload when actuated so as to enable the Petition 870250091550, dated 07 / 10 / 2025, page 75 / 180 61 / 154 mounting or suspending said payload on at least one of the guides 140 of said housing 110 and enabling the movement of said payload along said at least one guide 140 while the said working members are actuated and may further comprise an actuating device (not shown) being under the control of the control module of said aircraft apparatus 100 and operationally coupled to said controllable working members so as to enable the actuation of at least one of them in response to the control commands of the control module of the aircraft apparatus 100.

[124] In other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be provided with two distinct guides and a movable connecting guide, each of which is configured to mount or suspend a payload thereon and to move said mounted or suspended payload along thereon and may further comprise an actuating device (not shown) being under the control of the control module of said aircraft apparatus 100 and operationally coupled to said movable connecting guide so as to enable it to move to connect said guides to each other.

[125] In other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may further be provided with a payload movement module (not shown) being under the control of the control module of said aircraft apparatus 100 and configured to interact with a payload mounted or suspended in at least one of the guides 140 provided to said housing 110 of the aircraft apparatus so as to enable the movement of said payload along said at least Petition 870250091550, dated 07 / 10 / 2025, page 76 / 180 62 / 154 a guide 140. In one variation of this embodiment of the present invention, the payload movement module (not shown) may be a robotic manipulator or gripper configured to grasp and move a payload along at least one of the guides 140 provided to the housing 110 of the aircraft apparatus. In another variation of this embodiment of the present invention, the payload movement module (not shown) may be an impeller configured to momentarily exert force on a payload during the actuation of said impeller to move said payload along at least one of the guides provided to the housing 110 of the aircraft apparatus, wherein said housing 110 of the aircraft apparatus may further comprise an actuation device (not shown) being under the control of the control module of said aircraft apparatus 100 and operationally coupled to said impeller so as to actuate them.In yet another variation of this embodiment of the present invention, the payload movement module (not shown) can be movably mounted on at least one additional guide (not shown) distinct from guides 140 to move a payload along at least one guide 140. In another variation of this embodiment of the present invention, the payload movement module (not shown) can further be configured to dismount a payload from at least one guide 140 provided to the housing 110 of the aircraft apparatus.

[126] In some other embodiments of the present invention, the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may further be provided with one or more weight sensors (not shown), each of which is configured to measure the weight of a payload at one of the points of said housing 110 of the aircraft apparatus for payload accommodation and which are configured to present their readings to the control module of said aircraft apparatus. Petition 870250091550, dated 07 / 10 / 2025, page 77 / 180 63 / 154 aircraft apparatus 100, wherein the control module of the aircraft apparatus 100 may enable the presentation of control instructions to the payload movement module which may be further provided to said housing 110 of the aircraft apparatus to move a payload along at least one guide 140 in accordance with said weight sensor readings.

[127] In some other embodiments of the present invention, at least one of the guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be further configured to disassemble a payload mounted on said at least one guide 140, thus allowing said payload to be removed from said at least one guide 140 as the need arises, for example, in the event of damage to at least a portion of said at least one guide 140 or when it is necessary to reassemble or resuspend said payload on another guide 140. In one of the variations of this embodiment of the present invention, at least one of the guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig.1 may have one or more payload disassembly points, also allowing the removal of said payload from said at least one guide 140 as the need arises, for example, in the event of damage to at least a portion of said at least one guide 140 or when it is necessary to reassemble or resuspend said payload on another guide 140.

[128] In various embodiments of the present invention, at least one of the anchoring modules 130 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the 500-1 system shown in Fig. 1 can be mounted in a movable manner in at least one of the guides 140 provided to said housing 110 of the aircraft apparatus, Petition 870250091550, dated 07 / 10 / 2025, p. 78 / 180 64 / 154 thus allowing the use of the anchoring modules 130 not only to enable the mutual anchoring of the housings 110 of the aircraft apparatus, but also for the mobile attachment of a payload to said guide 140, thus in turn expanding the variety of payloads that can be mounted or suspended on said guide 140 so as to move along it in relation to the housing 110 of the aircraft apparatus.

[129] In several other embodiments of the present invention, at least one of the guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be further provided with a gripping mechanism (not shown) configured to grip a payload to enable it to be mounted or suspended on said at least one guide and configured to move along said at least one guide to enable said gripped payload to move along said at least one guide. In one variation of this embodiment of the present invention, the gripping mechanism (not shown) may be configured to rotate so as to enable rotation of said gripped payload relative to said at least one guide.

[130] In several other embodiments of the present invention, at least one of the guides 140 provided to the housing 110 in at least one or each of the aircraft apparatus 100 that are part of the system 500-1 shown in Fig. 1 may be configured as movable, wherein said housing 110 of the aircraft apparatus may further comprise a guide movement module (not shown) being under the control of the control module of said aircraft apparatus 100 and configured to interact operationally with said movable guide 140 so as to enable it to move together with a payload mounted or suspended on said movable guide. In one variation of this embodiment of the present invention, the movable guide 140 may further be configured Petition 870250091550, dated 07 / 10 / 2025, p. 79 / 180 65 / 154 to mount or suspend a payload on it in order to enable the movement of said payload along said movable guide 140 during the movement of said guide 140.

[131] According to one embodiment of the present invention, the housing 110 of at least one or each of the aircraft devices 100 anchored together forming a grouped aircraft device shown in Fig. 1 may further be provided with a payload movement module (not shown) being under the control of the control module of said aircraft device 100 and configured to interact with a payload mounted or suspended in at least one of the guides 140 provided to said housing 110 of the aircraft device, so as to enable the movement of said payload along said at least one guide 140, wherein said control module may further be configured to present control commands to said payload movement module, so as to enable the movement of said payload of the aircraft device 100 to be unanchored from at least one of the remaining anchored aircraft devices 100.Thus, in this embodiment of the present invention, the payload movement module (not shown) being under the control of the control module (not shown) related to one of the aircraft devices 100 anchored together to form a clustered aircraft device substantially allows reloading or unloading, at least partially, a payload from the housing 110 of the aircraft device to be unanchored from said clustered aircraft device to at least one of the housings 110 of other aircraft devices that are part of said clustered aircraft device, while said clustered aircraft device is present in the airspace (i.e., in the air). It should be noted that in this embodiment of the present invention, the module of... Petition 870250091550, dated 07 / 10 / 2025, page 80 / 180 66 / 154 payload movement, which may be further provided to the housing 110 of the aircraft apparatus, may be, for example, a robotic arm, a robotic manipulator, a robotic gripper, a controllable electromechanical gripper, a controllable electromagnetic gripper or other controllable technical means configured to grasp a payload so as to enable its movement along at least one guide 140 or to exert continuous or periodic force on a payload so as to enable its movement along at least one guide 140. It should be noted that in this embodiment of the present invention, the payload movement module that may be further provided to the housing 110 of the aircraft apparatus may also be configured to move under the control of the aircraft apparatus control module 100 in relation to said housing 110 to enable the movement of a payload along at least one guide 140.In particular, in this embodiment of the present invention, the payload movement module of the aircraft apparatus 100 can be mounted from the outside or inside of the housing 110 related to said aircraft apparatus 100, so as to move along a distinct guide, which may also be provided to said housing 110 of the aircraft apparatus, can be mounted so as to move along said at least one guide 140 (i.e., on the same guide 140 on which the payload to be moved is mounted or suspended), can be mounted on a wheeled base so as to move relative to said housing 110 of the aircraft apparatus, can be configured in the form of a telescopic gripper for grasping a payload configured to fold and unfold, during which said telescopic gripper pulls or pushes, respectively, said payload so as to enable the movement of said payload along at least one guide 140 or similar.It should also be noted that in this embodiment of the present invention, the mobility of... Petition 870250091550, dated 07 / 10 / 2025, page 81 / 180 67 / 154 payload movement module of aircraft apparatus 100 may be provided by a drive module or drive that may be further provided to the housing 110 of the aircraft apparatus and which may be operationally coupled to said payload movement module in order to enable the transmission of movement to said payload movement module while the actuation of said drive is under the control of the control module related to one of the aircraft apparatus 100 anchored together forming a grouped aircraft apparatus.

[132] According to another embodiment of the present invention, the housing 110 of at least one or each of the aircraft devices 100 anchored together forming a grouped aircraft device shown in Fig.1 may also be provided with a payload movement module (not shown) being under the control of the control module of said aircraft apparatus 100 and configured to interact with a payload mounted or suspended in at least one of the guides 140 provided to said housing 100 of the aircraft apparatus, so as to enable the movement of said payload along said at least one guide 140, wherein said control module may further be configured to present control commands to said payload movement module so as to enable the receipt of said payload from at least one of the remaining docked aircraft apparatus 100 and to enable the movement of said received payload in the aircraft apparatus to be undocked.Thus, in this embodiment of the present invention, the payload movement module (not shown) being under the control of the control module (not shown) related to one of the aircraft devices 100 anchored together to form a grouped aircraft device allows substantially at least partially reloading a payload. Petition 870250091550, dated 07 / 10 / 2025, page 82 / 180 68 / 154 in housing 110 of the aircraft apparatus to be undocked from said grouped aircraft apparatus, from housing 110 of any other aircraft apparatus 100 that is part of said grouped aircraft apparatus or from housings 110 of any other aircraft apparatus that are part of said grouped aircraft apparatus while said grouped aircraft apparatus is present in the airspace (i.e., in the air).It should be noted that in this embodiment of the present invention, the payload movement module, which may also be provided to the housing 110 of the aircraft apparatus, may be, for example, a robotic arm, a robotic manipulator, a robotic gripper, a controllable electromechanical gripper, a controllable electromagnetic gripper or other controllable technical means configured to grasp a payload so as to enable its movement along at least one guide 140 or to exert continuous or periodic force on a payload so as to enable its movement along at least one guide 140.It should be noted that in this embodiment of the present invention, the payload movement module, which may be further provided to the housing 110 of the aircraft apparatus, may also be configured to move under the control of the aircraft apparatus control module 100 in relation to said housing 110 to enable the movement of a payload along at least one guide 140. In particular, in this embodiment of the present invention, the payload movement module of the aircraft apparatus 100 may be mounted from the outside or inside of the housing 110 related to said aircraft apparatus 100, so as to move along a distinct guide, which may further be provided to said housing 110 of the aircraft apparatus, may be mounted so as to move along said at least one guide 140 (i.e., on the same guide 140 on which the payload to be moved is mounted or). Petition 870250091550, dated 07 / 10 / 2025, p. 83 / 180 69 / 154 suspended), can be mounted on a wheeled base so as to move relative to said housing 110 of the aircraft apparatus, can be configured in the form of a telescopic gripper to grasp a payload configured to fold and unfold, during which said telescopic gripper pulls or pushes, respectively, said payload so as to enable the movement of said payload along at least one guide 140 or similar.It should also be noted that in this embodiment of the present invention, the mobility of the payload movement module of the aircraft apparatus 100 may be provided by a drive module or drive (not shown) which may be further provided to the housing 110 of the aircraft apparatus and which may be operationally coupled to said payload movement module so as to enable the transmission of motion to said payload movement module while the actuation of said drive is under the control of the control module related to one of the aircraft apparatus 100 anchored together forming a grouped aircraft apparatus.

[133] According to another embodiment of the present invention, the control module in one of the aircraft devices 100 forming a grouped aircraft device may further enable the direction of the aircraft device 100 to be undocked to a parking station (not shown) equipped with one or more charging devices (not shown) each electrically connected to at least one of the power sources of the parking station and enabling each connection to the same of at least one aircraft device for at least partial charging or at least partial refueling of the range of said aircraft device 100 to be undocked so that said aircraft device 100 transitions to a range state Petition 870250091550, dated 07 / 10 / 2025, page 84 / 180 70 / 154 at least partially refueled or fully refueled, thus allowing it to be re-docked with at least one of the aircraft devices 100 docked together forming a grouped aircraft device. It should be noted that each of the power sources of the parking station in this embodiment of the present invention may be one or more batteries, a generator based on an internal combustion engine, a generator based on a hydrogen engine, a solar panel, and any other suitable power source known in the art. It should also be noted that at least one or each of the charging devices (not shown) of the parking station in this embodiment of the present invention may be a wireless charging device, a wired charging device, or a charging dock.Alternatively, at least one or each of the charging devices at the parking station may be configured, for example, as a device to supply electrical power, a device to supply liquid or gaseous fuel, and / or similar devices.As yet another alternative, at least one or each of the parking station's charging devices may be hydraulically connected to a pump (not shown) connected by a hydraulic line to a reservoir or container (not shown) containing fuel in such a way as to enable the intake of fuel from said container, so as to enable the supply of said volume of fuel ingested to the fuel tank of aircraft 100 whose fuel tank is hydraulically connected to the fuel-powered engine of aircraft 100, thus enabling refueling of the range of aircraft 100 (in particular, due to at least partial refueling of the fuel volume in the fuel tank of aircraft 100).

[134] In one of the variations of this embodiment of the present invention, the Petition 870250091550, dated 07 / 10 / 2025, p. 85 / 180 71 / 154 The control module in one of the aircraft units 100 forming a grouped aircraft unit can further enable the docking of an aircraft unit with a refueled range to one of the aircraft units docked together 100 forming a grouped aircraft unit. In another variation of this embodiment of the present invention, the control module in one of the aircraft units 100 forming a grouped aircraft unit can also be configured to provide control commands to the payload movement module (not shown) related to the aircraft unit to be docked so as to enable the movement of a payload from said aircraft unit to be docked to at least one of the aircraft units 100 docked together forming a grouped aircraft unit.

[135] According to another embodiment of the present invention, at least two of the aircraft devices 100 to be anchored together may further be provided, each with an additional guide (not shown), wherein the control module in one of said aircraft devices 100 may further enable movement of the payload movement module (not shown) along an additional grouping guide (not shown) formed from said additional guides of the aircraft devices 100 by anchoring said aircraft devices 100 together.

[136] It should also be noted that at least one or each of the control units of the grouped aircraft apparatus shown in Fig. 1 and formed from aircraft apparatus 100 of Fig. 1 anchored together or the control device of system 500-1 for moving a payload whose system may comprise said grouped aircraft apparatus, may also be configured to enable the undocking of at least a portion or all of the aircraft apparatus 100 of Fig. 1 forming the Petition 870250091550, dated 07 / 10 / 2025, page 86 / 180 72 / 154 said aircraft apparatus in cluster. In addition, at least one or each of the control units of the aircraft apparatus in cluster shown in Fig. 1 and formed from aircraft apparatus 100 of Fig. 1 anchored together or the control device of system 500-1 for moving a payload whose system may comprise said aircraft apparatus in cluster, may be further configured to enable the detachable anchoring, to said aircraft apparatus in cluster, of one or more additional aircraft apparatus 100 shown in Fig. 1, one or more aircraft apparatus in cluster above formed, each from aircraft apparatus 100 anchored together of Fig. 1, one or more self-propelled modules described below, one or more self-propelled modules in cluster 300 described below, one or more payloads 200 described below and / or one or more payloads in cluster described below.It should also be noted that the process of detachably anchoring an aircraft cluster formed from 100 aircraft clusters anchored together as shown in Fig. 1, which are part of the 500-1 system, to one or more additional 100 aircraft clusters as shown in Fig. 1, one or more additional aircraft clusters formed, each, from 100 aircraft clusters anchored together as shown in Fig. 1.1, one or more self-propelled modules described below, one or more self-propelled modules in a group of 300 described below, one or more payloads 200 described below and / or one or more payloads in a group described below, can be achieved by placing at least one or each of the anchoring modules 130 supplied to the housings 110 of the aircraft devices forming said aircraft device in a group in detachable interaction with at least one of the auxiliary anchoring modules that may be supplied to the housings of said one or more additional aircraft devices 100. Petition 870250091550, dated 07 / 10 / 2025, p. 87 / 180 73 / 154 of Fig. 1, one or more additional grouped aircraft devices, one or more self-propelled modules, one or more self-propelled modules in group 300, one or more payloads 200 described below and / or one or more payloads in group described below, respectively. SECOND MODE OF THE SYSTEM FOR MOVING PAYLOAD

[137] Fig. 2 is a second embodiment of a 500-2 system for moving a payload according to the present invention, comprising two aircraft apparatus 100 configured to connect detachably to each other or to anchor detachably to each other to form a grouped aircraft apparatus.

[138] It should be noted that system 500-2 is substantially a variant or variation of system 500-1 shown in Fig. 1; therefore, similar functional components that are part of system 500-1 and system 500-2 and similar constituent elements that are part of said similar functional components are referenced in Fig. 1 and Fig. 2 and in the text of this document using the same reference numbers. It should also be noted that, where applicable, the above embodiments of system 500-1 also apply to or are related to system 500-2 shown in Fig. 2 and, consequently, particular embodiments of the present invention, alternative embodiments of the present invention and / or variations described above in relation to system 500-1 should be interpreted as embodiments of system 500-2.

[139] Analogously to the 500-1 system described above, the 500-2 system may consist of two or more aircraft units 100 configured to connect detachably to each other to form a grouped aircraft unit, for example, three, four, five, six, seven, eight, nine, ten, eleven, twelve or more configured aircraft units, each configured to Petition 870250091550, dated 07 / 10 / 2025, page 88 / 180 74 / 154 in a manner analogous to one of the embodiments described in the present invention of aircraft apparatus 100, wherein the aircraft apparatus 100 in the 500-2 system may define or form one or more grouped aircraft apparatuses (for example, one, two, three, four, five, six, seven, eight, nine, ten or more grouped aircraft apparatuses), each of which is composed of two or more aircraft apparatus 100 and which have the same or different quantity of aircraft apparatus 100 as part thereof.

[140] In addition, analogously to system 500-1 above, each of the aircraft apparatus 100, which are part of system 500-2, comprises a housing 110 provided with two air propulsion units 120 enabling the movement of said aircraft apparatus 100 through the air, a guide 140 attached to the housing 110 on the outside thereof and configured to mount or suspend a payload therein (including the payload 200 described below) and to move said mounted or suspended payload along the same guide, and a control module configured to control the operation of said aircraft apparatus 100 (including to control the operation of the propulsion units 120 thereof) and configured to receive control commands and / or navigation commands from the control device that is part of system 500-2 so as to enable the docking of said aircraft apparatus 100 to at least one other aircraft apparatus identical or distinct from aircraft apparatus 100.However, in contrast to system 500-1 shown in Fig. 1, in system 500-2 shown in Fig. 2, the anchoring modules 130 are rigidly attached to opposite ends of said guide 140, thus allowing one or more other guides 140 supplied to the housing 110 of one or more other aircraft devices 100, which are part of system 500-2, to be detachably connected or anchored to said guide 140, thereby providing detachable anchoring of the aircraft devices. Petition 870250091550, dated 07 / 10 / 2025, p. 89 / 180 75 / 154 100 among themselves, wherein the detachable anchoring of the guides 140 related to the housings 110 of the aircraft devices 100 among themselves is carried out by placing the anchoring modules 130 of the guides of said aircraft devices in detachable interaction with each other. Analogously to system 500-1, in system 500-2, after the anchoring of the aircraft devices 100 to each other, the anchoring of the guides 140 of these aircraft devices 100 is carried out to form a grouping guide 145 shown in Fig. 2. Thus, at least one of the guides provided to the housing 110 in at least one or each of the aircraft devices 100, which are part of system 500-2, is configured to connect or anchor in a detachable manner to one or more other guides of the housing of at least one other aircraft device 100 to form a grouping guide when anchoring such aircraft devices 100 to each other.

[141] In one embodiment of the present invention, the housing 110 of at least one or each of the aircraft apparatus 100, which are part of the system 500-2, may be provided with one or more air propulsion units enabling the movement of said aircraft apparatus 100 through the air and one or more guides 140, at least one or each of which may be configured to mount or suspend therein a payload (including the payload 200 described below) so as to enable the movement of said payload along said guide 140 and may be configured to connect or anchor in a detachable manner to one or more guides 140 which may be related to the housing 110 of at least one other aircraft apparatus 100 which is also part of the system 500-2.

[142] In another embodiment of the present invention, the housing 110 of at least one or each of the aircraft devices 100, which are part of the 500-2 system, may be provided with one or more anchoring modules 130 provided in the guide 140 of said housing 110 at points or regions thereof. Petition 870250091550, dated 07 / 10 / 2025, p. 90 / 180 76 / 154 guide 140 that allow connecting or anchoring in a detachable manner said guide to one or more guides 140 of the housing 110 of another aircraft apparatus 100 by bringing the anchoring modules 130 of said aircraft apparatus 100 to be anchored to each other into detachable interaction with each other to form a grouping guide 145 of said distinct guides 140 anchored to each other and that enable the free movement of a payload along said grouping guide 145.

[143] Furthermore, the control module (not shown) related to one of the aircraft devices 100, which are part of the 500-2 system shown in Fig. 2, and anchored together to form a grouping aircraft device also allows the undocking of at least one of the anchored aircraft devices 100, so as to enable the formation of a grouping guide from the guides 140 of the remaining anchored aircraft devices and / or enables the anchoring of yet another aircraft device 100 to one of the said anchored aircraft devices so as to enable the formation of a grouping guide from the guides of said anchored aircraft devices.

[144] It should also be noted that at least one or each of the control units of the clustered aircraft apparatus shown in Fig. 2 and formed from aircraft apparatus 100 of Fig. 2 anchored together or the control device of system 500-2 for moving a payload whose system may comprise said clustered aircraft apparatus, may be further configured to enable the undocking of at least a portion or all of the aircraft apparatus 100 of Fig. 2 forming said clustered aircraft apparatus. In addition, at least one or each of the control units of the clustered aircraft apparatus shown in Fig. 2 and formed from aircraft apparatus Petition 870250091550, dated 07 / 10 / 2025, page 91 / 180 77 / 154 100 of Fig. 2 anchored together or the control device of system 500-2 for moving a payload, the system of which may comprise said grouped aircraft, may also be configured to enable detachable docking to such grouped aircraft of one or more additional aircraft 100 shown in Fig. 2, one or more grouped aircraft formed, each, from interconnected aircraft 100 of Fig. 2, one or more self-propelled modules described below, one or more grouped self-propelled modules 300 described below, one or more payloads 200 described below and / or one or more grouped payloads described below. It should also be noted that the process of detachably docking a grouped aircraft formed from interconnected aircraft 100 of Fig.2, which are part of the 500-2 system, to one or more additional aircraft devices 100 of Fig. 2, one or more additional grouped aircraft devices formed, each, from aircraft devices 100 anchored together of Fig. 2, one or more self-propelled modules described below, one or more grouped self-propelled modules 300 described below, one or more payloads 200 described below and / or one or more grouped payloads described below, can be achieved by placing at least one or each of the supplied anchoring modules 130 to the guides 140 of the aircraft devices forming said grouped aircraft device in detachable interaction with at least one of the auxiliary anchoring modules that may be supplied to the housings of said one or more additional aircraft devices 100 of Fig.2, one or more additional aircraft devices in groupings, one or more self-propelled modules, one or more self-propelled modules in groupings of 300, one or more payloads described below and / or one or. Petition 870250091550, dated 07 / 10 / 2025, p. 92 / 180 78 / 154 plus payloads in groupings described below, respectively. THIRD MODE OF THE SYSTEM FOR MOVING PAYLOAD

[145] The third embodiment of the system for moving a payload is a variation of system 500-2 described above with reference to Fig. 2; therefore, similar functional components that are part of the third embodiment of the system for moving a payload and similar constituent elements that are part of said similar functional components are referenced in the text of this document using the same reference numbers used in relation to system 500-2 above. It should also be noted that, where applicable, the above embodiments of system 500-2 also apply to or are related to the third embodiment of the system for moving a payload; and, therefore, particular embodiments of the present invention, alternative embodiments of the present invention and / or variations thereof described above in relation to system 500-2 should be interpreted as embodiments of the third embodiment of the system for moving a payload.

[146] Analogously to the 500-2 system, the third embodiment of the system for moving a payload may comprise two or more aircraft devices 100 configured to connect detachably to each other or to anchor detachably to each other to form a grouped aircraft device.

[147] Furthermore, analogously to the 500-2 system above, in the third embodiment of the system for moving a payload, each of the aircraft apparatus 100 comprises a housing 110 provided with two air propulsion units 120 enabling the movement of said aircraft apparatus 100 through the air, a guide 140 attached to the housing 110 on the outside thereof and configured to mount or suspend a payload therein and to move said mounted or suspended payload along therein and a Petition 870250091550, dated 07 / 10 / 2025, page 93 / 180 79 / 154 control module configured to control the operation of said aircraft apparatus 100 (including to control the operation of the propulsion units 120 thereof) and configured to receive control commands and / or navigation commands from the control device that is part of the third embodiment of the system to move a payload in order to enable the docking of said aircraft apparatus 100 to at least one other aircraft apparatus identical or distinct from aircraft apparatus 100.

[148] Furthermore, analogously to system 500-2 above, in the third embodiment of the system for moving a payload, the anchoring modules 130 are rigidly attached to opposite ends of said guide 140, thus allowing one or more other guides 140 provided to the housing 110 of one or more other aircraft devices 100 that are part of the third embodiment of the system for moving a payload to be connected or anchored in a detachable manner to said guide 140, which are part of the third embodiment of the system for moving a payload, thus providing aircraft devices 100 anchored in a detachable manner to each other, wherein the detachable anchoring of the guides 140 related to the housings 110 of the aircraft devices 100 to each other is carried out by placing the anchoring modules 130 of the guides of said aircraft devices in detachable interaction with each other.

[149] Furthermore, analogously to system 500-2 above, in the third embodiment of the system for moving a payload, after the anchoring of the aircraft devices 100 to each other, the guides 140 of these aircraft devices 100 are anchored to form a grouping guide 145. Thus, at least one of the guides provided to the housing 110 in at least one or each of the aircraft devices 100, which are part of the third embodiment of the system for moving a payload, is configured to connect or anchor in a detachable manner to one or more other guides of the housing 110. Petition 870250091550, dated 07 / 10 / 2025, page 94 / 180 80 / 154 of at least one other aircraft device 100 to form a grouping guide 145 when anchoring such aircraft devices 100 to each other.

[150] In contrast to system 500-2 above, in the third embodiment of the system for moving a payload, at least one or each of one or more guides 140 provided to the housing 110 of at least one or each of the aircraft apparatus 100, which are part of the third embodiment of the system for moving a payload, is at least partially or completely configured to move relative to said housing 110 of the aircraft apparatus, thus allowing further movement of a payload mounted or suspended on said movable guide relative to said housing 110 during the movement of said guide 140, wherein, simultaneously, said payload can be moved immediately along said guide, thus not only increasing the speed of movement of said payload relative to the housing 110 of the aircraft apparatus, but also increasing the smoothness of the movement of said payload in general,thereby reducing the vibration stress on the payload.

[151] In particular, the movement of a payload along the guide 140 in the third embodiment of the system for moving a payload can be provided by means of the use of a payload moving module or a gripping mechanism for moving a payload that was described above in relation to the 500-1 system, wherein such a payload moving module or such a gripping mechanism for moving a payload can be mounted on the housing 110 of the aircraft apparatus or on the guide 140 itself.

[152] Furthermore, the movement of the guide 140 in relation to the housing 110 of the aircraft apparatus can be provided in the third embodiment of the system for moving a payload by means of the use of a guide movement module that can be mounted in the housing 110 of the apparatus. Petition 870250091550, dated 07 / 10 / 2025, page 95 / 180 81 / 154 aircraft and which can operationally interact with said guide 140 in order to enable its movement relative to said housing. In one embodiment of the present invention, said guide 140 can be mounted or attached directly to the guide movement module which, in turn, can be mounted in the housing 110 of the aircraft apparatus, in a movable manner relative to said housing 110, so that the movement of the guide movement module relative to the housing 110 of the aircraft apparatus also leads to the movement of the guide mounted on said guide movement module, relative to said housing 110. In another embodiment of the present invention, said guide 140 can be configured telescopically so that at least the partial or complete folding / unfolding of said guide 140 leads to the movement of a payload mounted or suspended in said guide 140 relative to the housing 110 of the aircraft apparatus.

[153] It should be noted that the guide motion module can be implemented analogously to the payload motion module or gripping mechanism for moving a payload that was described above in relation to system 500-1, therefore, the embodiments of the payload motion module or gripping mechanism for moving a payload described in the present invention can be considered possible exemplary embodiments of the guide motion module.

[154] It should also be noted that the guide movement module and the payload movement module can be configured as a single functional or drive device implementing the above functions of the guide movement module and the payload movement module, that is, enabling the movement of a payload along one or more guides 140 provided to the housing 110 of the aircraft apparatus and, simultaneously, enabling the movement of said guides 140 in relation to the Petition 870250091550, dated 07 / 10 / 2025, p. 96 / 180 82 / 154 referred to as accommodation 110.

[155] In one embodiment of the present invention, the housing 110 of at least one or each of the aircraft apparatus 100, which are part of the third embodiment of the system for moving a payload, may be provided with one or more air propulsion units enabling the movement of said aircraft apparatus 100 through the air and one or more guides 140, at least one or each of which may be configured to mount or suspend a payload thereon (including the payload 200 described below) so as to enable the movement of said payload along said guide 140 and may be configured to connect or anchor in a detachable manner to one or more guides 140 which may be related to the housing 110 of at least one other aircraft apparatus 100 which is also part of the third embodiment of the system for moving a payload.

[156] In another embodiment of the present invention, the housing 110 of at least one or each of the aircraft devices 100, which are part of the third embodiment of the system for moving a payload, may be provided with one or more anchoring modules 130 provided in the guide 140 of said housing 110 at points or regions of said guide 140 that allow said guide to be detachably connected or anchored to one or more guides 140 of the housing 110 of another aircraft device 100 by bringing the anchoring modules 130 of said aircraft devices 100 to be anchored to each other into detachable interaction with each other to form a grouping guide 145 of said distinct guides 140 anchored to each other and that enable the free movement of a payload along said grouping guide 145.

[157] In addition, the control module (not shown) related to one of the 100 aircraft devices, which are part of the third mode of Petition 870250091550, dated 07 / 10 / 2025, p. 97 / 180 83 / 154 system for moving a payload shown in Fig. 2, and anchored together to form a grouping aircraft device further allows the un-anchoring of at least one of the aircraft devices 100 anchored together, so as to enable the formation of a grouping guide 145 from the guides 140 of the remaining aircraft devices anchored together and / or enables the anchoring of yet another aircraft device 100 to one of the said aircraft devices 100 anchored together so as to enable the formation of a grouping guide 145 from the guides of said aircraft devices anchored together.

[158] Furthermore, the control module (not shown) related to one of the aircraft devices 100, which are part of the third embodiment of the system for moving a payload and are anchored together to form a grouping aircraft device equipped with the grouping guide 145 above, also allows the movement of a payload (including the payload 200 described below) along said grouping guide 145 and, simultaneously to the same, allows the movement of at least a portion of said grouping guide 145 in relation to at least one of the housings 110 of the aircraft devices 100 anchored together.

[159] It should also be noted that at least one or each of the control units of the aircraft cluster formed from the 100 docked aircraft clusters that are part of the third embodiment of the system for moving a payload, or the control device of the third embodiment of the system for moving a payload, the system of which may comprise said aircraft cluster, may be further configured to enable the undocking of at least some or all of the 100 aircraft clusters forming said aircraft cluster. In addition, at least one or each of the Petition 870250091550, dated 07 / 10 / 2025, page 98 / 180 84 / 154 aircraft control units in a cluster formed from 100 interconnected aircraft units that are part of the third embodiment of the system for moving a payload, or the control device of the third embodiment of the system for moving a payload, which system may comprise said aircraft cluster may be further configured to enable the detachable docking, to said aircraft cluster, of one or more additional 100 aircraft units related to the third embodiment of the system for moving a payload, one or more aircraft clusters formed, each, from 100 interconnected aircraft units related to the third embodiment of the system for moving a payload, one or more self-propelled modules described below, one or more self-propelled modules in a cluster described below,one or more payloads in clusters of 200 described below and / or one or more payloads in clusters described below. It should also be noted that the process of detachably anchoring an aircraft unit in a cluster formed from 100 aircraft units anchored together in relation to the third mode of the system for moving a payload to one or more additional 100 aircraft units related to the third mode of the system for moving a payload, one or more additional aircraft units in clusters formed, each, from 100 aircraft units anchored together in relation to the third mode of the system for moving a payload, one or more self-propelled modules described below, one or more self-propelled modules in clusters of 300 described below, one or more payloads in clusters of 200 described below and / or one or more payloads in clusters described below,This can be accomplished by placing at least one or each of the 130 anchoring modules supplied for 140 aircraft device guides. Petition 870250091550, dated 07 / 10 / 2025, p. 99 / 180 85 / 154 forming the said aircraft apparatus in a detachable interacting group with at least one of the auxiliary anchoring modules that may be provided to the housings of said one or more additional aircraft apparatus 100 related to the third mode of the system for moving a payload, one or more additional aircraft apparatus in a group related to the third mode of the system for moving a payload, one or more self-propelled modules, one or more self-propelled modules in a group 300, one or more payloads 200 described below and / or one or more payloads in a group described below, respectively. FOURTH MODE OF THE SYSTEM FOR MOVING PAYLOAD

[160] The fourth embodiment of the system for moving a payload is a variation of system 500-1 described above with reference to Fig. 1; therefore, similar functional components that are part of the fourth embodiment of the system for moving a payload and similar constituent elements that are part of said similar functional components are referenced in the text of this document using the same reference numbers used in relation to system 500-1 above. It should also be noted that, where applicable, the above embodiments of system 500-1 also apply to or are related to the fourth embodiment of the system for moving a payload; and, therefore, particular embodiments of the present invention, alternative embodiments of the present invention and / or variations thereof described above in relation to system 500-1 should be interpreted as embodiments of the third embodiment of the system for moving a payload.

[161] Analogously to the 500-1 system, the fourth embodiment of the system for moving a payload may comprise two or more aircraft devices 100 configured to connect detachably to each other or to anchor detachably to each other to form a device of Petition 870250091550, dated 07 / 10 / 2025, pages 100 / 180 86 / 154 aircraft in grouping.

[162] Furthermore, analogously to system 500-1 above, in the fourth embodiment of the system for moving a payload, each of the aircraft apparatus 100 comprises a housing 110 provided with two air propulsion units 120 enabling the movement of said aircraft apparatus 100 through the air,a guide 140 attached to housing 110 on the outside thereof and configured to mount or suspend a payload therein and to move said mounted or suspended payload along the same guide, and a control module configured to control the operation of said aircraft apparatus 100 (including controlling the operation of its propulsion units 120) and configured to receive control commands and / or navigation commands from the control device that is part of the fourth embodiment of the system for moving a payload in order to enable the docking of said aircraft apparatus 100 to at least one other aircraft apparatus identical or distinct from aircraft apparatus 100.

[163] Furthermore, analogously to system 500-1 above, in the fourth embodiment of the system for moving a payload, the anchoring modules 130 are mounted from the outside of the housing 110, thus allowing one or more other anchoring modules 130 supplied to the housing 110 of one or more other aircraft devices 100 that are part of the fourth embodiment of the system for moving a payload to be connected or anchored in a detachable manner, thus providing detachable anchoring of the aircraft devices 100 to each other. Thus, in the fourth embodiment of the system for moving a payload, the detachable anchoring of the housings 110 of the aircraft devices to each other is achieved by placing the anchoring modules 130 of these housings 110 in detachable interaction with each other. Petition 870250091550, dated 07 / 10 / 2025, pp. 101 / 180 87 / 154

[164] Furthermore, analogously to system 500-1 above, in the fourth embodiment of the system for moving a payload, when anchoring the aircraft devices 100 to each other, detachable anchoring (i.e., a top connection) or detachable connection of the guides 140 provided to the housings 110 to be anchored to each other of the aircraft devices is performed to form a grouping guide 145. Thus, at least one of the guides provided to the housing 110 in at least one or each of the aircraft devices 100, which are part of the fourth embodiment of the system for moving a payload, is configured to connect or anchor in a detachable manner to one or more other guides of the housing 110 of at least one other aircraft device 100 to form a grouping guide 145 when anchoring such aircraft devices to each other.

[165] In contrast to system 500-1 above, in the fourth embodiment of the system for moving a payload, at least one or each of one or more guides 140 provided to the housing 110 of at least one or each of the aircraft apparatus 100, which are part of the fourth embodiment of the system for moving a payload, is at least partially or completely configured to move relative to said housing 110 of the aircraft apparatus, thus allowing further movement of a payload mounted or suspended on said movable guide relative to said housing 110 during the movement of said guide 140, wherein, simultaneously, said payload can be moved immediately along said guide 140, thus not only increasing the speed of movement of said payload relative to the housing 110 of the aircraft apparatus, but also increasing the smoothness of the movement of said payload in general,thereby reducing the vibration stress on the payload.

[166] In particular, the movement of a payload along the guide Petition 870250091550, dated 07 / 10 / 2025, page 102 / 180 88 / 154 140 in the fourth embodiment of the system for moving a payload can be provided by means of the use of a payload moving module or a gripping mechanism for moving a payload that was described above in relation to system 500-1, wherein such a payload moving module or such a gripping mechanism for moving a payload can be mounted in the housing 110 of the aircraft apparatus or in the guide 140 itself.

[167] Furthermore, the movement of guide 140 relative to housing 110 of the aircraft apparatus can be provided in the fourth embodiment of the system for moving a payload by means of the use of a guide movement module that can be mounted in housing 110 of the aircraft apparatus and that can operationally interact with said guide 140 so as to enable movement of the same relative to said housing 110. In one embodiment of the present invention, such guide 140 can be mounted or attached directly to the guide movement module which, in turn, can be mounted in housing 110 of the aircraft apparatus, in a movable manner relative to said housing 110, so that the movement of the guide movement module relative to housing 110 of the aircraft also leads to the movement of the guide 140 mounted in said guide movement module, relative to said housing 110.In another embodiment of the present invention, such guide 140 may be configured telescopically such that at least the partial or complete folding / unfolding of said guide 140 leads to the movement of a payload mounted or suspended on said guide 140 in relation to the housing 110 of the aircraft apparatus.

[168] It should be noted that the guide motion module can be implemented analogously to the payload motion module or gripping mechanism for moving a payload that was described above in relation to the 500-1 system, therefore, the embodiments of the motion module Petition 870250091550, dated 07 / 10 / 2025, p. 103 / 180 89 / 154 of payload or gripping mechanism for moving a payload described in the present invention may be considered possible exemplary embodiments of the guide motion module.

[169] It should also be noted that the guide movement module and the payload movement module can be configured as a single functional or drive device implementing the above functions of the guide movement module and the payload movement module, namely enabling the movement of a payload along one or more guides 140 provided to the housing 110 of the aircraft apparatus and, simultaneously to the same, enabling the movement of said guides 140 in relation to said housing 110.

[170] In one embodiment of the present invention, the housing 110 of at least one or each of the aircraft apparatus 100, which are part of the fourth embodiment of the system for moving a payload, may be provided with one or more air propulsion units enabling the movement of said aircraft apparatus 100 through the air and one or more guides 140, at least one or each of which may be configured to mount or suspend a payload thereon (including the payload 200 described below) so as to enable the movement of said payload along said guide 140 and may be configured to connect or anchor in a detachable manner to one or more guides 140 which may be related to the housing 110 of at least one other aircraft apparatus 100 which is also part of the fourth embodiment of the system for moving a payload.

[171] In another embodiment of the present invention, the housing 110 of at least one or each of the aircraft devices 100 that are part of the fourth embodiment of the system for moving a payload may be provided with one or more anchoring modules 130 provided in the housing 110 of Petition 870250091550, dated 07 / 10 / 2025, page 104 / 180 90 / 154 aircraft apparatus at points or regions of the body of said housing 110 allowing said housing 110 to be detachably connected or anchored to one or more housings 110 of other aircraft apparatus 100 by placing the anchoring modules 130 of said housing 110 in detachable interaction with each other and to detachably connect or anchor at least one of the guides 140 provided to said housing 110 to one or more guides 140 of the housing 110 of one or more other aircraft apparatus 100 to form a grouping guide 145 of said distinct guides 140 anchored to each other and to enable the free movement of a payload along said grouping guide 145.

[172] Furthermore, the control module (not shown) related to one of the aircraft devices 100, which are part of the fourth embodiment of the system for moving a payload shown in Fig. 2, and anchored together to form a grouping aircraft device also allows the undocking of at least one of the aircraft devices 100 anchored together, so as to enable the formation of a grouping guide 145 from the guides 140 of the remaining anchored aircraft devices and / or enables the anchoring of yet another aircraft device 100 to one of said anchored aircraft devices so as to enable the formation of a grouping guide 145 from the guides of said anchored aircraft devices.

[173] In addition, the control module (not shown) related to one of the aircraft devices 100, which are part of the fourth system mode for moving a payload and are anchored together to form a grouping aircraft device equipped with the grouping guide 145 above, also allows the movement of a payload (including the payload 200 described below) along said grouping guide 145 and, Petition 870250091550, dated 07 / 10 / 2025, pp. 105 / 180 91 / 154 simultaneously allows the movement of at least a portion of said grouping guide 145 in relation to at least one of the housings 110 of the aircraft devices 100 anchored together.

[174] It should also be noted that at least one or each of the control units of the aircraft cluster formed from the 100 docked aircraft clusters that are part of the fourth mode of the system for moving a payload, or the control device of the fourth mode of the system for moving a payload, which may comprise said aircraft cluster, may be further configured to enable the undocking of at least some or all of the 100 aircraft clusters forming said aircraft cluster. Furthermore,at least one or each of the control units of the aircraft cluster formed from the 100 aircraft clusters anchored together that are part of the fourth embodiment of the system for moving a payload, or the control device of the fourth embodiment of the system for moving a payload, which system may comprise said aircraft cluster may be further configured to enable the detachable anchoring, to said aircraft cluster, of one or more additional 100 aircraft clusters that are part of the fourth embodiment of the system for moving a payload, one or more of the above-formed aircraft clusters, each of the 100 aircraft clusters anchored together that are part of the fourth embodiment of the system for moving a payload, one or more self-propelled modules described below, one or more self-propelled modules in clusters described below,one or more payloads in a grouping of 200 described below and / or one or more payloads in a grouping described below. It should also be noted that the process of anchoring in a detachable manner, Petition 870250091550, dated 07 / 10 / 2025, pp. 106 / 180 92 / 154 an aircraft cluster formed from 100 aircraft clusters anchored together that are part of the fourth embodiment of the system for moving a payload to one or more additional 100 aircraft clusters related to the fourth embodiment of the system for moving a payload, one or more additional aircraft clusters formed, each, from 100 aircraft clusters anchored together related to the fourth embodiment of the system for moving a payload, one or more self-propelled modules described below, one or more self-propelled modules in clusters 300 described below, one or more payloads in clusters 200 described below and / or one or more payloads in clusters described below,This can be achieved by placing at least one or each of the supplied anchoring modules 130 into the housings 110 of the aircraft devices, forming said aircraft device in a detachable interaction with at least one of the auxiliary anchoring modules that may be supplied to the housings of said aircraft devices, one or more additional aircraft devices 100 related to the fourth system modality for moving a payload, one or more additional aircraft devices in a group related to the fourth system modality for moving a payload, one or more self-propelled modules, one or more self-propelled modules in a group 300, one or more payloads 200 described below and / or one or more payloads in a group described below, respectively.

[175] In particular, in view of the above description of the embodiments of aircraft devices 100 and embodiments of grouped aircraft devices formed from aircraft devices 100 anchored together, one of the variations of the systems for moving a payload according to the present invention may comprise one or more aircraft devices 100 according to the second embodiment above of the 500-2 system for moving a Petition 870250091550, dated 07 / 10 / 2025, page 107 / 180 93 / 154 payload, at least one of which aircraft devices may be detachably anchored to one or more additional aircraft devices according to the second embodiment above of system 500-2 for moving a payload or one or more aircraft devices in a grouping according to the second embodiment above of system 500-2 for moving a payload by detachably connecting the guides 140 thereof to each other so as to enable the movement of a payload (including the payload 200 described below or the grouping payload described below) along the grouping guide 145 formed from the guides 140 of said aircraft devices anchored to each other, or may comprise one or more aircraft devices in a grouping according to the second embodiment above of system 500-2 for moving a payload,at least one of which aircraft devices can be detachably anchored to one or more additional aircraft devices 100 according to the second embodiment above of system 500-2 for moving a payload or to one or more grouped aircraft devices according to the second embodiment above of system 500-2 for moving a payload by detachably connecting the guides 140 thereof to each other so as to enable the movement of a payload (including the payload 200 described below or the grouped payload described below) along the grouping guide 145 formed from the guides 140 of said aircraft devices anchored together.

[176] Furthermore, considering the above description of the embodiments of aircraft devices 100 and embodiments of grouped aircraft devices formed from aircraft devices 100 anchored to each other, yet another variation of the system for moving a payload according to the present invention may comprise one or more aircraft devices 100 according to the third embodiment above of the system for moving a payload. Petition 870250091550, dated 07 / 10 / 2025, pp. 108 / 180 94 / 154 useful, at least one of which aircraft devices can be detachably anchored to one or more additional aircraft devices 100 according to the third embodiment above of the system for moving a payload or one or more aircraft devices in a grouping according to the third embodiment above of the system for moving a payload by detachably connecting the guides 140 thereof to each other, so as to enable the simultaneous movement of a payload (including the payload 200 described below or the payload in a grouping described below) along the grouping guide 145 formed from the guides 140 of said aircraft devices anchored together and movement of at least a portion of said grouping guide 145 in relation to one or more housings 110 of said aircraft devices anchored together,or it may comprise one or more aircraft devices grouped together according to the third embodiment above of the system for moving a payload, at least one of which aircraft devices may be detachably anchored to one or more additional aircraft devices according to the third embodiment above of the system for moving a payload or to one or more aircraft devices grouped together according to the third embodiment above of the system for moving a payload by detachably connecting the guides of the same to each other,in order to enable the simultaneous movement of a payload (including the payload 200 described below or the grouped payload described below) along the grouping guide 145 formed from the guides 140 of said aircraft devices anchored to each other and the movement of at least a portion of said grouping guide 145 in relation to one or more housings 110 of said aircraft devices anchored to each other.

[177] Furthermore, considering the above description of the modalities Petition 870250091550, dated 07 / 10 / 2025, pp. 109 / 180 95 / 154 of the aircraft devices 100 and groupings of aircraft devices formed from aircraft devices 100 anchored together, yet another variation of the system for moving a payload according to the present invention may comprise one or more aircraft devices 100 according to the first embodiment of the system 500-1 for moving a payload, at least one of which aircraft devices may be detachably anchored to one or more additional aircraft devices according to the first embodiment of the system 500-1 for moving a payload or one or more groupings of aircraft devices according to the first embodiment of the system 500-1 for moving a payload by detachably connecting the anchoring modules 130 thereof together,in order to enable the movement of a payload (including payload 200 described below or the group payload described below) along group guide 145 formed from guides 140 of said aircraft devices anchored together, or it may comprise one or more aircraft devices grouped together according to the first embodiment of system 500-1 for moving a payload,at least one of whose aircraft devices can be detachably anchored to one or more additional aircraft devices 100 according to the first embodiment of system 500-1 for moving a payload or to one or more grouped aircraft devices according to the first embodiment of system 500-1 for moving a payload by detachably connecting the anchoring modules 130 thereof to each other so as to enable the movement of a payload (including the payload 200 described below or the grouped payload described below) along the grouping guide 145 formed from the guides 140 of said aircraft devices anchored together.

[178] Furthermore, considering the above description of the modalities Petition 870250091550, dated 07 / 10 / 2025, pp. 110 / 180 96 / 154 of the aircraft devices 100 and embodiments of the grouped aircraft devices formed from aircraft devices 100 anchored to each other, some other variation of the system for moving a payload according to the present invention may comprise one or more aircraft devices 100 according to the fourth embodiment of the system for moving a payload, at least one of which aircraft devices may be detachably anchored to one or more additional aircraft devices according to the fourth embodiment of the system for moving a payload or one or more grouped aircraft devices according to the fourth embodiment of the system for moving a payload by detachably connecting the anchoring modules 130 thereof to each other,in order to enable the simultaneous movement of a payload (including the payload 200 described below or the grouped payload described below) along the grouping guide 145 formed from the guides 140 of said aircraft devices anchored to each other and movement of at least a portion of said grouping guide 145 in relation to one or more housings 110 of said aircraft devices anchored to each other, or may comprise one or more aircraft devices grouped according to the fourth embodiment of the system for moving a payload, at least one of which aircraft devices may be detachably anchored to one or more additional aircraft devices 100 according to the fourth embodiment of the system for moving a payload or to one or more aircraft devices grouped according to the fourth embodiment of the system for moving a payload by detachably connecting the anchoring modules 130 thereof to each other,in order to enable the simultaneous movement of a payload (including the payload 200 described below or the grouped payload described below) along the grouping guide 145 formed from the guides, Petition 870250091550, dated 07 / 10 / 2025, p. 111 / 180 97 / 154 140 of said aircraft devices moored together and movement of at least a portion of said grouping guide 145 in relation to one or more housings 110 of said aircraft devices moored together.

[179] Furthermore, in some other embodiment of the present invention, at least one or each of one or more anchoring modules 130, which may be provided to the housing 110 in the aircraft apparatus 100 in accordance with any of the embodiments described in the present invention, known in the prior art or which would be appreciated by a person skilled in the art, may be arranged on one side of the housing 110 of the aircraft apparatus, distinct from the remaining anchoring modules of said anchoring modules 130.In one variation of this embodiment of the present invention, one or more anchoring modules 130, which may be provided to the housing 110 in the aircraft apparatus 100 according to any of the embodiments thereof described in the present invention, known in the prior art or appreciated by a person skilled in the art, may be arranged on one and the same side of the housing 110 of the aircraft apparatus or on different sides of the housing 110 of the aircraft apparatus.

[180] Furthermore, in some other embodiment of the present invention, at least one or each of one or more guides 140, which may be provided to the housing 110 in the aircraft apparatus according to any of the embodiments thereof described in the present invention, known in the prior art or which would be appreciated by a person skilled in the art, may be disposed on one side of the housing 110 of the aircraft apparatus, distinct from the remaining guides of said guides 140 of the aircraft apparatus. In one of the variations of this embodiment of the present invention, one or more guides Petition 870250091550, dated 07 / 10 / 2025, p. 112 / 180 98 / 154 140, which may be provided to housing 110 in aircraft apparatus 100 in accordance with any of the embodiments thereof described in the present invention, known in the prior art or appreciated by a person skilled in the art, may be arranged on one and the same side of housing 110 of aircraft apparatus or on different sides of housing 110 of aircraft apparatus. SELF-PROPELLED MODULES

[181] Figs. 3.1, 3.2 and 3.3 show illustrative self-propelled modules 300-1, 300-2, 300-3, 300-4, each of which can be configured to detachably dock to at least one of the aircraft apparatus 100 above and / or to detachably dock to at least one of the payloads 200 described below, wherein at least a portion or each of said self-propelled modules 300-1, 300-2, 300-3, 300-4 can be initially accommodated, stored or parked at at least one of the parking stations (not shown) configured to load such self-propelled modules or to replenish the range of such self-propelled modules.

[182] It should be noted that the self-propelled modules 300-1, 300-2, 300-3, 300-4 shown in Figs. 3.1, 3.2 and 3.3 are of different types characterized by different movement capabilities of such self-propelled modules in space. It should also be noted that while the self-propelled modules 3001, 300-2, 300-3, 300-4 shown in Figs. 3.1, 3.2 and 3.3 are shown only as illustrative examples, a person skilled in the art would readily appreciate that such self-propelled modules may also have other types known in the state of the art, whereby the dimensions, manufacturing material, housing shape and the like of such self-propelled modules are not specifically limited in any way. Petition 870250091550, dated 07 / 10 / 2025, pp. 113 / 180 99 / 154

[183] ​​Fig. 3.1 shows a self-propelled module 300-1 comprising a housing 310 provided with a main docking module 330 and two unmanned aerial vehicles 320, each of which is provided with an air thruster 325 and each of which is detachably docked or connected to said housing 310 using a corresponding two auxiliary docking modules 350, wherein the main docking module 330 and the auxiliary docking modules 350 can be configured analogously to the docking module 130 above according to any embodiment thereof described in the present invention. It should be noted that the unmanned aerial vehicles 320, with their air thrusters 325, detachably connected to the housing 310 of the self-propelled module, function substantially as air propulsion units for the self-propelled module 300-1, enabling the self-propelled module 300-1 to move in the air or fly.It should also be noted that each unmanned aerial vehicle 320 with the air thruster 325 of the same in the self-propelled module 300-1 is substantially an independent unmanned aerial vehicle provided with its own control module configured to control the operation of that unmanned aerial vehicle 320 and configured to receive navigation commands and / or control commands from at least the control unit of the self-propelled module 300-1 and / or from the control device described in the present invention of the system to enable the implementation of the process of controlling the operation of that unmanned aerial vehicle 320 based on said navigation commands and / or control commands received and provided with anchoring means or an anchoring module analogous to one of the anchoring modules described in the present invention to enable detachable anchoring to an auxiliary anchoring module 350 related to the housing 310 of the self-propelled module and, by. Petition 870250091550, dated 07 / 10 / 2025, pp. 114 / 180 100 / 154 consequently, enable the detachable docking of such unmanned aerial vehicle 320 to the housing 310 of the self-propelled module.

[184] It should also be noted that the main anchoring module 330 provided to housing 310 in the self-propelled module 300-1 can be placed in detachable interaction with at least one of the guides 140, which can be provided to housing 110 of at least one of the aircraft devices 100 in the first, second, third and fourth embodiments above of the system to move a payload and / or can be placed in interaction with at least one of the guides 240, which can be provided to housing 210 of at least one of the payloads 200 described below, thus enabling the self-propelled module 300-1 to be mounted or suspended on said at least one guide and enabling the self-propelled module 300-1 to move along said guide.

[185] Furthermore, housing 310 in the self-propelled module 300-1 shown in Fig. 3.1 is provided with a wheeled propulsion unit 340 in the form of a wheeled base enabling movement of the self-propelled module 300-1 over the ground surface (over the earth) or over the surface of a stationary or moving physical object that may be at least partially present in airspace, ground space, space above water and / or underwater space. Thus, the wheeled propulsion unit 340 in the self-propelled module 300-1 shown in Fig. 3.1 is substantially an additional means of movement provided to housing 310 of the self-propelled module in addition to the unmanned aerial vehicles 320 with the air thrusters 325 thereof, detachably connected to said housing 310.

[186] In one embodiment of the present invention, the housing 310 in the self-propelled module 300-1 shown in Fig. 3.1 may be provided with one or more air propulsion units (for example, one, two, three, Petition 870250091550, dated 07 / 10 / 2025, pp. 115 / 180 101 / 154 four, five, six, seven, nine, ten or more air propulsion units) enabling the self-propelled module 300-1 to move through air and be attached in a non-detachable manner to said housing 310.

[187] In another embodiment of the present invention, the housing 310 in the self-propelled module 300-1 shown in Fig. 3.1 may be provided with one or more unmanned aerial vehicles 320 with air thrusters 325 thereof (for example, with one, two, three, four, five, six, seven, nine, ten or more of these unmanned aerial vehicles) attached in a non-detachable manner to said housing 310 using auxiliary anchoring modules 350. In one of the variations of this embodiment of the present invention, at least one of the unmanned aerial vehicles 320, which may be detachably anchored to the housing 310 of the self-propelled module, may be provided with one or more air thrusters 325 (for example, with one, two, three, four, five, six, seven, eight, nine, ten or more of these air thrusters 325) enabling the self-propelled module 300-1 move in the air or fly.

[188] In another embodiment of the present invention, the housing 310 in the self-propelled module 300-1 shown in Fig. 3.1 may be provided with one or more unmanned aerial vehicles 320 with air thrusters 325 thereof, detachably attached to the housing 310 of the self-propelled module, and may be fitted with one or more additional air propulsion units non-detachably attached to the housing 310 of the self-propelled module.

[189] In addition, the self-propelled module 300-1 comprises a control unit (not shown) mounted inside the housing 310 and configured to control the operation of the self-propelled module 300-1, including controlling in general the operation of the unmanned aerial vehicles 320 and particularly the operation of the air thrusters 325 thereof. Petition 870250091550, dated 07 / 10 / 2025, pp. 116 / 180 102 / 154

[190] The control unit of the self-propelled module 300-1 is configured to present control commands to at least one or each of the unmanned aerial vehicles 320 in order to enable the actuation of the air thruster 325 of said unmanned aerial vehicle 320, thus enabling the self-propelled module 300-1 to move through the air or fly due to the thrust generated by said actuated air thruster 325, wherein the actuation of the air thrusters 325 of both unmanned aerial vehicles 320 performing the function of air propulsion units of the self-propelled module 300-1 in a manner that provides substantially simultaneous or parallel operation thereof increases the carrying capacity of said self-propelled module 300-1.

[191] Furthermore, the control unit of the self-propelled module 3001 is configured to present control commands to at least one or each of the unmanned aerial vehicles 320, in order to enable the undocking of the same from the housing 310 as a result of the removal of said unmanned aerial vehicle 320 from interaction with the corresponding auxiliary docking module 350.

[192] The control unit of the self-propelled module 300-1 is also configured to present control commands to at least one of the unmanned aerial vehicles 320 present in the airspace or accommodated in parking stations (not shown) in order to enable the direction of said at least one unmanned aerial vehicle 320 to said self-propelled module 300-1 for detachable docking of said unmanned aerial vehicle 320 directed to the housing 310 of the self-propelled module when placing said unmanned aerial vehicle 320 in interaction with one of the free auxiliary docking modules 350.

[193] In addition, the control unit of the self-propelled module 300- Petition 870250091550, dated 07 / 10 / 2025, pp. 117 / 180 103 / 154 is configured to provide control commands to an additional means of movement of the self-propelled module 300-1 in the form of a wheeled propulsion unit 340 to drive it in order to enable the self-propelled module 300-1 to move over the ground surface (over the earth) or over the surface of a stationary or moving physical object that may be at least partially present in airspace, ground space, space above water and / or underwater space.

[194] It should be noted that, in order to enable the use of the self-propelled module 300-1 as part of one of the systems for moving a payload described in the present invention, the control unit of the self-propelled module 300-1 is further configured to communicate via a communication network with the control module of at least one of the aircraft devices 100 and / or with the payload control module 200 (if the latter is present in the payload housing 200).Furthermore, the control unit of the self-propelled module 300-1 can also be configured to receive and process navigation commands and / or control commands from a control device that may be part of any of the systems for moving a payload described in the present invention and to control the operation of the self-propelled module 300-1, including the performance of the functions above assigned to the control unit of the self-propelled module 300-1, depending on said navigation commands and / or control commands.

[195] Furthermore, the main anchoring module 330 provided to housing 310 in the self-propelled module 300-1 can be placed in detachable interaction with at least one of the guides 140 with which the housing 110 of at least one of the aircraft devices 100 forming the aircraft device in the above grouping can be fitted, thus enabling the self-propelled module 300-1 to be mounted or suspended on said at least Petition 870250091550, dated 07 / 10 / 2025, pp. 118 / 180 104 / 154 a guide 140 and enabling the self-propelled module 300-1 to move along a grouping guide comprising said at least one guide 140 and relating to said grouping aircraft apparatus and / or may be placed in interaction with at least one of the guides 240 that may be provided to the housing 210 of at least one of the payloads 200 described below forming the grouping payload described below, thus enabling the self-propelled module 300-1 to be mounted or suspended on said at least one guide 240 and enabling the self-propelled module 300-1 to move along a grouping guide comprising said at least one guide 240 and relating to said grouping payload.

[196] In one of the alternative embodiments of the present invention, housing 310 in the self-propelled module 300-1 may be provided instead of the main anchoring module 330 shown in Fig. 3.1, with a 360° guide characteristic of the self-propelled module 300-2 described below, wherein such 360° guide may be placed in detachable interaction with at least one of the anchoring modules 130 that may be provided to the housing 110 of at least one of the aircraft devices 100 in the first and fourth embodiments above of the system to move a payload and / or may be placed in detachable interaction with at least one of the anchoring modules 230, which may be provided to the housing 210 of at least one of the payloads 200 described below, thus enabling, in such an alternative embodiment of the present invention, anchoring the self-propelled module 300-1 to said at least one aircraft device 100 or said at least one payload 200 and enabling said at least one aircraft device 100 or said at least one payload 200 to move along said 360° guide provided to the housing 310 in the module Self-propelled 300-1.Furthermore, thanks to the 360° guide, which can be supplied to housing 310 in the self-propelled module 300-1. Petition 870250091550, dated 07 / 10 / 2025, pp. 119 / 180 105 / 154 In accordance with this alternative embodiment of the present invention, the self-propelled module 300-1 can be detachably anchored to at least one of the aircraft devices 100 above, forming a grouped aircraft device, in particular by bringing the guide 360 ​​into detachable interaction with at least one of the anchoring modules 130, which can be provided to the housing 110 of said at least one aircraft device 100 and / or can be detachably anchored to at least one of the payloads 200 described below, forming a grouped payload, in particular by bringing the guide 360 ​​into detachable interaction with at least one of the anchoring modules 230, which can be provided to the housing 210 of said at least one payload 200.

[197] Fig. 3.2 shows a self-propelled module 300-2 comprising a housing 310 provided with a single guide 360 ​​and two unmanned aerial vehicles 320, each of which is provided with an air thruster 325 and each of which is detachably anchored or connected to said housing 310 by means of a corresponding to one of two anchoring modules 350, wherein the auxiliary anchoring modules 350 can be configured analogously to the anchoring module 130 above according to any of the embodiments thereof described in the present invention and the guide 360 ​​can be configured analogously to the guide 140 above according to any of the embodiments thereof described in the present invention.It should be noted that the unmanned aerial vehicles 320 with the air thrusters 325 thereof, detachably connected to the housing 310 of the self-propelled module, substantially perform the function of air propulsion units for the self-propelled module 300-2, enabling the self-propelled module 300-2 to move in the air or fly. It should also be noted that each unmanned aerial vehicle 320 with the air propellant... Petition 870250091550, dated 07 / 10 / 2025, pp. 120 / 180 106 / 154 325 of the same in the self-propelled module 300-2 is substantially an independent unmanned aerial vehicle provided with its own control module configured to control the operation of that unmanned aerial vehicle 320 and configured to receive navigation commands and / or control commands from at least the control unit of the self-propelled module 300-2 and / or from the control device described in the present invention of the system to enable the implementation of the process of controlling the operation of that unmanned aerial vehicle 320 based on said navigation commands and / or control commands received and provided with anchoring means or an anchoring module analogous to one of the anchoring modules described in the present invention to enable detachable anchoring to an auxiliary anchoring module 350 related to the housing 310 of the self-propelled module and, consequently,to enable the detachable docking of such unmanned aerial vehicle 320 to the housing 310 of the self-propelled module.,

[198] It should also be noted that the 360 ​​guide provided to housing 310 in the self-propelled module 300-2 can be placed in detachable interaction with at least one of the anchoring modules 130, which can be provided to housing 110 of at least one of the aircraft devices 100 in the first and fourth embodiments above of the system to move a payload and / or can be placed in detachable interaction with at least one of the anchoring modules 230, which can be provided to housing 210 of at least one of the payloads 200 described below, thus enabling the anchoring of the self-propelled module 300-2 to said at least one aircraft device 100 or said at least one payload 200 and enabling said at least one aircraft device 100 or said at least one payload 200 to move along said 360 guide provided to housing 310 in Petition 870250091550, dated 07 / 10 / 2025, pp. 121 / 180 107 / 154 self-propelled module 300-2. Furthermore, thanks to the guide 360 ​​provided to housing 310 in the self-propelled module 300-2, the self-propelled module 3002 can be detachably anchored to at least one of the aircraft devices 100 above, forming a grouped aircraft device, in particular by bringing the guide 360 ​​into detachable interaction with at least one of the anchoring modules 130, which can be provided to housing 110 of said at least one aircraft device 100, and / or can be detachably anchored to at least one of the payloads 200 described below, forming a grouped payload, in particular by bringing the guide 360 ​​into detachable interaction with at least one of the anchoring modules 230, which can be provided to housing 210 of said at least one payload 200.

[199] Furthermore, analogously to the self-propelled module 300-1 shown in Fig. 3.1, the housing 310 in the self-propelled module 300-2 shown in Fig. 3.2 is provided with a wheeled propulsion unit 340 in the form of a wheeled base enabling the movement of the self-propelled module 300-2 over the ground surface (over the earth) or over the surface of a stationary or moving physical object that may be at least partially present in airspace, ground space, space above water and / or underwater space. Thus, the wheeled propulsion unit 340 in the self-propelled module 300-2 shown in Fig. 3.2 is substantially an additional means of movement provided to the housing 310 of the self-propelled module in addition to the unmanned aerial vehicles 320 with the air thrusters 325 thereof, detachably connected to said housing 310.

[200] In one embodiment of the present invention, the housing 310 in the self-propelled module 300-2 shown in Fig. 3.2 can be provided with one or more air propulsion units (for example, one, two, three, Petition 870250091550, dated 07 / 10 / 2025, pp. 122 / 180 108 / 154 four, five, six, seven, nine, ten or more air propulsion units) enabling the self-propelled module 300-2 to move through the air and be attached in a non-detachable manner to said housing 310.

[201] In another embodiment of the present invention, the housing 310 in the self-propelled module 300-2 shown in Fig. 3.2 may be provided with one or more unmanned aerial vehicles 320 with air thrusters 325 thereof (for example, with one, two, three, four, five, six, seven, nine, ten or more of these unmanned aerial vehicles) attached in a non-detachable manner to said housing 310 using auxiliary anchoring modules 350. In one of the variations of this embodiment of the present invention, at least one of the unmanned aerial vehicles 320, which may be detachably anchored to the housing 310 of the self-propelled module, may be provided with one or more air thrusters 325 (for example, with one, two, three, four, five, six, seven, eight, nine, ten or more of these air thrusters 325) enabling the self-propelled module 300-2 move in the air or fly.

[202] In another embodiment of the present invention, the housing 310 in the self-propelled module 300-2 shown in Fig. 3.2 may be provided with one or more unmanned aerial vehicles 320 with air thrusters 325 thereof, detachably attached to the housing 310 of the self-propelled module, and may be fitted with one or more additional air propulsion units non-detachably attached to the housing 310 of the self-propelled module.

[203] In addition, the self-propelled module 300-2 comprises a control unit (not shown) mounted inside the housing 310 and configured to control the operation of the self-propelled module 300-2, including generally controlling the operation of unmanned aerial vehicles 320 and particularly the operation of their air thrusters 325. Petition 870250091550, dated 07 / 10 / 2025, pp. 123 / 180 109 / 154

[204] The control unit of the self-propelled module 300-2 is configured to present control commands to at least one or each of the unmanned aerial vehicles 320 in order to enable the actuation of the air thruster 325 of said unmanned aerial vehicle 320, thus enabling the self-propelled module 300-2 to move through the air or fly due to the thrust generated by said actuated air thruster 325, wherein the actuation of the air thrusters 325 of both unmanned aerial vehicles 320 performing the function of air propulsion units of the self-propelled module 300-2 in a manner that provides a substantially simultaneous or parallel operation thereof increases the carrying capacity of said self-propelled module 300-2.

[205] In addition, the control unit of the self-propelled module 3002 is configured to present control commands to at least one or each of the unmanned aerial vehicles 320, in order to enable the undocking of the same from the housing 310 as a result of the removal of said unmanned aerial vehicle 320 from interaction with the corresponding auxiliary docking module 350.

[206] The control unit of the self-propelled module 300-2 is also configured to present control commands to at least one of the unmanned aerial vehicles 320 present in the airspace or accommodated in parking stations (not shown) in order to enable the direction of said at least one unmanned aerial vehicle 320 to said self-propelled module 300-2 for detachable docking of said unmanned aerial vehicle 320 directed to the housing 310 of the self-propelled module when placing said unmanned aerial vehicle 320 in interaction with one of the free auxiliary docking modules 350.

[207] In addition, the control unit of the self-propelled module 300- Petition 870250091550, dated 07 / 10 / 2025, pp. 124 / 180 110 / 154 is configured to provide control commands to an additional means of movement of the self-propelled module 300-2 in the form of a wheeled propulsion unit 340 to drive it in order to enable the self-propelled module 300-2 to move over the ground surface (over the earth) or over the surface of a stationary or moving physical object that may be at least partially present in airspace, ground space, space above water and / or underwater space.

[208] It should be noted that, in order to enable the use of the self-propelled module 300-2 as part of one of the systems for moving a payload described in the present invention, the control unit of the self-propelled module 300-2 is further configured to communicate via a communication network with the control module of at least one of the aircraft devices 100 and / or with the payload control module 200 (if such a module is present in the payload housing 200).Furthermore, the control unit of the 300-2 self-propelled module can also be configured to receive and process navigation commands and / or control commands from a control device that may be part of any of the systems for moving a payload described in the present invention and to control the operation of the 300-2 self-propelled module, including the performance of the functions above assigned to the control unit of the 300-2 self-propelled module, depending on said navigation commands and / or control commands.

[209] Furthermore, the 360 ​​guide provided to housing 310 in the self-propelled module 300-2 can be brought into detachable interaction with at least one of the anchoring modules 130 of which the housing 110 of at least one of the aircraft devices 100 forming the above grouped aircraft device can be fitted, thus enabling said grouped aircraft device 100 to be mounted or suspended on said guide. Petition 870250091550, dated 07 / 10 / 2025, pp. 125 / 180 111 / 154 360 and enabling the movement of said aircraft apparatus in grouping along said 360 guide, and / or may be placed in interaction with at least one of the anchoring modules 230 of which the housing 210 of at least one of the payloads 200 forming the grouping payload described below may be fitted, thus enabling said grouping payload to be mounted or suspended on said 360 guide and enabling said grouping payload to move along said 360 guide.

[210] In one of the alternative embodiments of the present invention, housing 310 in the self-propelled module 300-2 may be provided instead of guide 360 ​​shown in Fig. 3.2, with the main anchoring module 330 characteristic of the self-propelled module above 300-1, wherein such main anchoring module 330 may be placed in detachable interaction with at least one of the guides 140 which the housing 110 of at least one of the aircraft devices 100 in the first, second, third and fourth embodiments above of the system for moving a payload may be fitted with and / or may be placed in detachable interaction with at least one of the guides 240, which may be provided to the housing 210 of at least one of the payloads 200 described below, thus enabling, in such an alternative embodiment of the present invention, that the self-propelled module 300-2 be anchored to said at least one aircraft device 100 or to said at least one payload 200 and enabling said self-propelled module 300-2 to move along said at least one guide.Furthermore, thanks to the main anchoring module 330, which can be supplied to the housing 310 in the self-propelled module 300-2 according to this alternative embodiment of the present invention, the self-propelled module 300-2 can be detachably anchored to at least one of the aircraft devices 100 above forming a unit. Petition 870250091550, dated 07 / 10 / 2025, pp. 126 / 180 112 / 154 aircraft apparatus in grouping, in particular by placing the anchoring module 330 in detachable interaction with at least one of the guides 140, which may be provided to the housing 110 of said at least one aircraft apparatus 100, and / or may be detachably anchored to at least one of the payloads 200 described below forming a grouping payload, in particular by placing the guide 330 in detachable interaction with at least one of the guides 240, which may be provided to the housing 210 of said at least one payload 200.

[211] Fig. 3.3 shows a self-propelled module 300-3 comprising a housing 310 provided with a main docking module 330 and two unmanned aerial vehicles 320, each of which is provided with an air thruster 325 and each of which is detachably docked or connected to said housing 310 by means of the corresponding one of the two auxiliary docking modules 350 and comprising a control unit (not shown) disposed in said housing 310. Thus, one skilled in the art would readily appreciate that the self-propelled module 300-3 is generally configured analogously to the self-propelled module 300-1 shown above in Fig. 3.1; therefore, the description of housing 310, main docking module 330, unmanned aerial vehicles 320, air thrusters 325 for unmanned aerial vehicles and auxiliary docking modules 350, whose description is given above in relation to the self-propelled module 300-1, including descriptions of particular and alternative embodiments of the above functional components of the self-propelled module 300-1s, should be interpreted as also referring to the self-propelled module 300-3. Furthermore, the above functional capabilities of the control unit of the self-propelled module 300-1 are also equally applicable to the control unit of the self-propelled module 300-3. Petition 870250091550, dated 07 / 10 / 2025, pp. 127 / 180 113 / 154

[212] However, in contrast to the self-propelled module 300-1, in the self-propelled module 300-3, the housing is provided with a caterpillar propulsion unit 342 in the form of a caterpillar track that performs the function of an additional means of movement enabling the movement of the self-propelled module 300-3 over the ground surface (over the earth) with poorly passable road conditions. In other words, in the self-propelled module 300-3, the caterpillar propulsion unit 342 provided to the housing 310 of the self-propelled module complements the unmanned aerial vehicles 320 with the air thrusters 325 of the same, connected in a detachable manner to said housing 310.In turn, the control unit of the self-propelled module 300-3 is configured to present control commands to the additional means of movement of the self-propelled module 300-3 in the form of a tracked propulsion unit 342 to actuate it in order to enable the self-propelled module 300-3 to move over a poorly traversable ground surface (over the ground).

[213] Furthermore, analogously to the self-propelled module 300-1, the main anchoring module 330 provided to the housing 310 in the self-propelled module 300-3 can be placed in detachable interaction with at least one of the guides 140, which can be provided to the housing 110 of at least one of the aircraft devices 100 in the first, second, third and fourth embodiments above of the system to move a payload and / or can be placed in interaction with at least one of the guides 240, which can be provided to the housing 210 of at least one of the payloads 200 described below, thus enabling the self-propelled module 300-3 to be mounted or suspended on said at least one guide and enabling the self-propelled module 300-3 to move along said at least one guide.

[214] In addition, the main anchoring module 330 supplied to Petition 870250091550, dated 07 / 10 / 2025, pp. 128 / 180 Housing 310 in self-propelled module 300-3 may be placed in detachable interaction with at least one of the guides 140, which may be provided to housing 110 of at least one of the aircraft devices 100 forming the above-mentioned grouping aircraft device, thus enabling the self-propelled module 300-3 to be mounted or suspended on said at least one guide 140 and enabling the self-propelled module 300-3 to move along a grouping guide comprising said at least one guide 140 and related to said grouping aircraft device and / or may be placed in interaction with at least one of the guides 240, which may be provided to housing 210 of at least one of the payloads 200 described below forming the grouping payload described below.thus enabling the self-propelled module 300-3 to be mounted or suspended on said at least one guide 240 and enabling the self-propelled module 300-3 to move along a grouping guide comprising said at least one guide 240 and related to said grouping payload.

[215] In one of the alternative embodiments of the present invention, the housing 310 in the self-propelled module 300-3 may be provided, instead of the main anchoring module 330, with a guide 360, wherein such guide may be placed in detachable interaction with at least one of the anchoring modules 130 that may be provided to the housing 110 of at least one of the aircraft devices 100 in the first and fourth embodiments above of the system for moving a payload and / or may be placed in detachable interaction with at least one of the anchoring modules 230, which may be provided to the housing 210 of at least one of the payloads 200 described below, thus enabling, in such an alternative embodiment of the present invention, anchoring the self-propelled module 300-3 to said at least one aircraft device 100 or said at least one payload 200 and enabling that the Petition 870250091550, dated 07 / 10 / 2025, pp. 129 / 180 115 / 154 referred to as at least one aircraft apparatus 100 or referred to as at least one payload 200 moves along referred to as guide 360 ​​provided to housing 310 in self-propelled module 300-3.Furthermore, thanks to the 360 ​​guide, which can be provided to the housing 310 in the self-propelled module 300-3 according to this alternative embodiment of the present invention, the self-propelled module 300-3 can be detachably anchored to at least one of the aircraft devices 100 above, forming a grouping aircraft device, in particular by placing the 360 ​​guide in detachable interaction with at least one of the anchoring modules 130, which can be provided to the housing 110 of said at least one aircraft device 100, and / or can be detachably anchored to at least one of the payloads 200 described below, forming a grouping payload, in particular by placing the 360 ​​guide in detachable interaction with at least one of the anchoring modules 230, which can be provided to the housing 210 of said at least one payload 200.

[216] Fig. 3.3 also shows a self-propelled module 300-4 comprising a housing 310 provided with a main docking module 330 and two unmanned aerial vehicles 320, each of which is provided with an air thruster 325 and each of which is detachably docked or connected to said housing 310 by means of the corresponding one of the two auxiliary docking modules 350 and comprising a control unit (not shown) disposed in said housing 310. Thus, one skilled in the art would readily appreciate that the self-propelled module 300-3 is generally configured analogously to the self-propelled module 300-1 shown above in Fig. 3.1; therefore, the description of the housing 310, main docking module 330, unmanned aerial vehicles 320, air thrusters 325 of unmanned aerial vehicles Petition 870250091550, dated 07 / 10 / 2025, pages 130 / 180 The description of the 116 / 154 manned and auxiliary docking modules 350, given above in relation to the self-propelled module 300-1, including descriptions of particular and alternative embodiments of the functional components above of the self-propelled module 300-1s, should be interpreted as also referring to the self-propelled module 300-4. Furthermore, the functional capabilities described above of the control unit of the self-propelled module 300-1 are equally applicable to the control unit of the self-propelled module 300-4.

[217] However, in contrast to the self-propelled module 300-1, in the self-propelled module 300-3, the housing is provided with a snowmobile propulsion unit 344 in the form of skates performing the function of an additional means of movement enabling the movement of the self-propelled module 300-3 over a snowy or icy surface (over land). In other words, in the self-propelled module 300-4, the snowmobile propulsion unit 344 provided to the housing 310 of the self-propelled module complements the unmanned aerial vehicles 320 with the air thrusters 325 of the same, connected in a detachable manner to said housing 310.In turn, the control unit of the self-propelled module 300-4 is configured to present control commands to one or each of the unmanned aerial vehicles 320 to actuate them into an operational mode enabling the self-propelled module 300-4 to move over snowy and / or icy ground using an additional means of movement in the form of the snowmobile propulsion unit 344.

[218] Furthermore, analogously to the self-propelled module 300-1, the main docking module 330 provided to housing 310 in the self-propelled module 300-4 can be placed in detachable interaction with at least one of the guides 140, which can be provided to housing 110 of at least one of the aircraft devices 100 in the first, second, third and Petition 870250091550, dated 07 / 10 / 2025, pp. 131 / 180 117 / 154 fourth above system modalities for moving a payload and / or can be placed in interaction with at least one of the guides 240, which can be provided to the housing 210 of at least one of the payloads 200 described below, thus enabling the self-propelled module 300-4 to be mounted or suspended on said at least one guide and enabling the self-propelled module 300-4 to move along said at least one guide.

[219] Furthermore, the main anchoring module 330 provided to housing 310 in the self-propelled module 300-4 may be placed in detachable interaction with at least one of the guides 140, which may be provided to housing 110 of at least one of the aircraft devices 100 forming the above-grouped aircraft device, thus enabling the self-propelled module 300-4 to be mounted or suspended on said at least one guide 140 and enabling the self-propelled module 300-4 to move along a grouping guide comprising said at least one guide 140 and related to said grouped aircraft device and / or may be placed in interaction with at least one of the guides 240, which may be provided to housing 210 of at least one of the payloads 200 described below forming the grouping payload described below,thus enabling the self-propelled module 300-4 to be mounted or suspended on said at least one guide 240 and enabling the self-propelled module 300-3 to move along a grouping guide comprising said at least one guide 240 and related to said grouping payload.

[220] In one of the alternative embodiments of the present invention, the housing 310 in the self-propelled module 300-4 may be provided, instead of the main anchoring module 330, with a guide 360, wherein such guide may be placed in detachable interaction with at least one of the anchoring modules 130 that may be provided to the housing 110 of at least one Petition 870250091550, dated 07 / 10 / 2025, pp. 132 / 180 118 / 154 of the aircraft apparatus 100 in the first and fourth embodiments above the system for moving a payload and / or may be placed in detachable interaction with at least one of the anchoring modules 230, which may be provided to the housing 210 of at least one of the payloads 200 described below, thus enabling, in such an alternative embodiment of the present invention, anchoring the self-propelled module 300-4 to said at least one aircraft apparatus 100 or said at least one payload 200 and enabling said at least one aircraft apparatus 100 or said at least one payload 200 to move along said guide 360 ​​provided to the housing 310 in the self-propelled module 300-4.Furthermore, thanks to the 360 ​​guide, which can be provided to the housing 310 in the self-propelled module 300-4 according to this alternative embodiment of the present invention, the self-propelled module 300-4 can be detachably anchored to at least one of the aircraft devices 100 above, forming a grouping aircraft device, in particular by placing the 360 ​​guide in detachable interaction with at least one of the anchoring modules 130, which can be provided to the housing 110 of said at least one aircraft device 100, and / or can be detachably anchored to at least one of the payloads 200 described below, forming a grouping payload, in particular by placing the 360 ​​guide in detachable interaction with at least one of the anchoring modules 230, which can be provided to the housing 210 of said at least one payload 200.

[221] Furthermore, as shown in Fig. 3.3, at least one or each of the control units of the self-propelled modules 300-3, 300-4, whose control units are configured to communicate with each other via a communication network, may further enable detachable docking or detachable connection of these self-propelled modules 300-3, 300-4. Petition 870250091550, dated 07 / 10 / 2025, pp. 133 / 180 119 / 154 among themselves to form a self-propelled module in grouping 300, wherein the anchoring of the self-propelled modules 300-3, 300-4 among themselves can be carried out by placing a free auxiliary anchoring module 350 related to the self-propelled module 300-3 in detachable interaction with a free auxiliary anchoring module 350 related to the self-propelled module 300-4.To enable the auxiliary docking modules 350 related to the self-propelled modules 300-3, 300-4 to interact detachably with each other, the control unit of at least one or each of the self-propelled modules 300-3, 300-4 is configured to generate control commands enabling the undocking, one by one, of an unmanned aerial vehicle from the housing 310 of each of the self-propelled modules 300-3, 300-4 to be docked together, thus enabling, in turn, the release, one by one, of the auxiliary docking modules 350 in each of the self-propelled modules 300-3, 300-4, which may be involved in or used for detachable docking or detachable connection of said self-propelled modules 300-3, 300-4 to each other.It should be noted that the unmanned aerial vehicles 320, each of which is undocked from the housing 310 of the corresponding self-propelled modules 300-3, 300-4, may be directed to at least one parking station for refueling or parking and / or may be directed to other self-propelled modules that require unmanned aerial vehicles 320 for movement through the air, in order to enable detachable docking to release auxiliary docking modules from said other self-propelled modules. Furthermore, the control unit of at least one or each of the self-propelled modules 300-3, 300-4 may also be configured to generate control commands enabling detachable docking of one or more unmanned aerial vehicles 320 to the housing 310. Petition 870250091550, dated 07 / 10 / 2025, pp. 134 / 180 120 / 154 of at least one or each of the self-propelled modules 300-3, 300-4, provided that there are free auxiliary docking modules 350 with which said unmanned aerial vehicles 320 enter into detachable interaction in said housing 310. Furthermore, the control unit of at least one or each of the self-propelled modules 300-3, 300-4 may also be configured to generate control commands enabling the undocking of the self-propelled modules 300-3, 300-4 forming a grouping self-propelled module 300 to form two distinct self-propelled modules 300-3, 300-4, each of which is provided with at least one free auxiliary docking module 350 released as a result of the completion of said undocking process of the self-propelled modules 300-3, 300-4.

[222] In an alternative embodiment of the present invention, at least one or each of the control units of the self-propelled modules 300-3, 300-4 may enable the performance of the above process of undocking the unmanned aerial vehicles 320 from the housings 310 of the self-propelled modules 300-3, 300-4, followed by enabling the performance of the above process of detachably docking or detachably connecting the housings 310 of the self-propelled modules 300-3, 300-4 to each other in response to the control commands of the control device being part of the same system to move a payload to which the system of said self-propelled modules 300-3, 300-4 relate.Furthermore, in this alternative embodiment of the present invention, such control device may also enable the docking of one or more unmanned aerial vehicles 320 to the housing 310 of at least one or each of the self-propelled modules 3003, 300-4, provided that there are free auxiliary docking modules 350 which the said housing 310 must be fitted with and / or enable the undocking of the self-propelled modules 300-3, 300-4 forming a self-propelled module. Petition 870250091550, dated 07 / 10 / 2025, pp. 135 / 180 121 / 154 of grouping 300 to form two distinct self-propelled modules 300-3, 300-4, each of which has at least one free auxiliary anchoring module 350 released as a result of the completion of said un-anchoring process of the self-propelled modules 300-3, 300-4.

[223] In one embodiment of the present invention, the self-propelled cluster module 300 may be formed from two or more of the above self-propelled modules (two, three, four, five, six, seven, eight, nine, ten or more self-propelled modules), each of which may be of the type described in the present invention or may be of any other type known in the prior art, wherein such self-propelled cluster module may comprise identical self-propelled modules (for example, only self-propelled modules 300-1, self-propelled modules 300-2, self-propelled modules 300-3 or self-propelled modules 300-4), as well as self-propelled modules that are at least partially or completely different in any combination of the types described herein and known in the prior art.Thus, the sizes, types, manufacturing materials and / or the like of the self-propelled modules being part of any 300-group self-propelled module are not specifically limited in any way. Furthermore, the 300-group self-propelled module formed from a pair, group or combination of identical or different self-propelled modules may have any size (including spatial extent) and / or any shape suitable for undocking at least a portion or all of the self-propelled modules forming such 300-group self-propelled module and for detachable docking, to such 300-group self-propelled module, of one or more additional self-propelled modules, one or more additional self-propelled modules, one or more aircraft devices 100, one or more group aircraft devices, one or more payloads 200 and / or a. Petition 870250091550, dated 07 / 10 / 2025, pp. 136 / 180 122 / 154 or more group payloads

[224] It should also be noted that at least one or each of the control units of the 300 group self-propelled module or the control device of the system for moving a payload whose system comprises said 300 group self-propelled module may be further configured to enable the undocking of at least a portion or all of the self-propelled modules forming said 300 group self-propelled module.Furthermore, at least one or each of the control units of the 300 group self-propelled module or the control device of the system for moving a payload whose system comprises said 300 group self-propelled module may also be configured to enable detachable docking, such as the 300 group self-propelled module, of one or more additional self-propelled modules, one or more additional group self-propelled modules, one or more group 100 or higher aircraft devices, one or more group 200 payloads described below and / or one or more group payloads described below.It should also be noted that, depending on the specific type of self-propelled modules that are part of the 300 group self-propelled module, the process of detaching said 300 group self-propelled module to one or more additional self-propelled modules, one or more additional group self-propelled modules, one or more aircraft devices 100 above, one or more aircraft devices in group above, one or more payloads 200 described below and / or one or more of the group payloads described below can be carried out in two possible ways: 1) by placing at least one or each of the supplied main anchoring modules 330 into the housings 310 of the self-propelled modules forming said module. Petition 870250091550, dated 07 / 10 / 2025, pp. 137 / 180 123 / 154 self-propelled group 300 in detachable interaction with at least one of the guides, which may be provided to the housings of said one or more additional self-propelled modules, one or more additional self-propelled group modules, one or more aircraft devices 100 above, one or more aircraft devices in group above, one or more payloads 200 described below and / or one or more group payloads described below, respectively;2) by placing at least one or each of the 360 ​​guides provided to the housings 310 of the self-propelled modules forming said grouping self-propelled module 300 in detachable interaction with at least one of the main anchoring modules, which may be provided to the housings of said one or more additional self-propelled modules, one or more additional grouping self-propelled modules, one or more aircraft devices 100 above, one or more grouping aircraft devices above, one or more payloads 200 described below and / or one or more grouping payloads described below, respectively;

[225] Thus, in view of the description given above in relation to self-propelled modules and self-propelled modules in clusters, in the present invention there may be an embodiment of the system for moving a payload comprising (i) one or more aircraft 100s above or at least one aircraft 100s in clusters above formed from two or more aircraft 100s; and (ii) one or more self-propelled modules above, at least one or each of which is anchored to at least one of the aircraft 100s or at least one of the aircraft 100s forming said at least one aircraft 100s in clusters, respectively, by placing at least one of the guides of said self-propelled module in interaction with the anchoring module of Petition 870250091550, dated 07 / 10 / 2025, pp. 138 / 180 124 / 154 referred to as at least one aircraft device in order to enable the movement of said aircraft device and the aircraft devices anchored to it along said at least one guide of the self-propelled module or by placing at least one of the anchoring modules of said self-propelled module in interaction with the guide of said at least one aircraft device in order to enable the movement of the self-propelled module along said guide of the aircraft device.

[226] In some embodiments of the present invention, the housing 310 of one of the supplied self-propelled modules, each with one or more main anchoring modules 330 and forming a grouping self-propelled module 300, may be further provided with a self-propelled module motion unit (not shown) being under the control of the control unit of said self-propelled module and configured to move the self-propelled module along a guide related to the aircraft apparatus 100 or to the payload 200 or along a grouping guide related to the above-grouped aircraft apparatus or to the grouping payload described below. It should be noted that in this embodiment of the present invention, the motion module of the self-propelled module may generally be configured analogously to the above-grouped payload motion module or guide motion module.

[227] In other embodiments of the present invention, the control unit of one of the self-propelled modules, each equipped with one or more main anchoring modules 330 and forming a grouping self-propelled module 300, may be further configured to receive a movement pattern from the self-propelled module of the system control device to move a payload whose system comprises said grouping self-propelled module 300 in order to enable said self-propelled module Petition 870250091550, dated 07 / 10 / 2025, pp. 139 / 180 125 / 154 moves along a guide related to aircraft apparatus 100 or payload 200 or along a grouping guide related to the above grouping aircraft apparatus or grouping payload described below by means of the self-propelled module's motion module (not shown) in accordance with said motion pattern, wherein the self-propelled module's motion pattern may be pre-generated based on data relating to said guide or said grouping guide and said data may be updated in real-time mode or in real-time according to changes in the system's structure or architecture to move a payload whose system will be based on aircraft apparatus 100 above, payload 200, grouping aircraft apparatus or grouping payload.

[228] In other embodiments of the present invention, instead of at least one or each of the unmanned aerial vehicles 320, which may be provided to the housing 310 of any of the self-propelled modules above, the aircraft apparatus 100 above may be used, the housing 110 of which may be provided with docking modules 130 for detachable docking of the aircraft apparatus 100 to the housing 310 of the self-propelled module, wherein, to enable the movement of said self-propelled module through the air, at least one of said docking modules 130 of the aircraft apparatus must enter into detachable interaction with one or more auxiliary docking modules 350 provided to the housing 310 of said self-propelled module so that the aircraft apparatus 100 docked to said self-propelled module may perform the function of an air propulsion unit instead of the unmanned aerial vehicle 320 or unmanned aerial vehicles. 320.

[229] In alternative embodiments of the present invention, an additional means of movement, which may be provided to housing 310 in one or more self-propelled modules, may be configured, for example, by Petition 870250091550, dated 07 / 10 / 2025, pp. 140 / 180 126 / 154 less in the form of one of the following propulsion units comprising: a sail, marine propeller, Voith Schneider propeller, paddle propeller, water jet propulsion unit, paddle wheel, paddle-type propulsion unit, finned propulsion unit, fishtail propulsion unit, chassis with one or more wheels, pneumatic tire roller propulsion unit, rotary cutting propulsion unit, caterpillar propulsion unit, half-track propulsion unit, ski-track propulsion unit, screw-type propulsion unit, walking-type propulsion unit, electromagnetic propulsion unit, jet propulsion unit, oscillating wing propulsion unit, walking wheel propulsion unit, square wheel propulsion unit, vibration propulsion unit, amoebic type propulsion unit, sectional wheel propulsion unit and inertial propulsion unit.Furthermore, in other alternative embodiments of the present invention, the housing 310 in one or more self-propelled modules may be provided with two or more identical or different additional means of motion configured in the form of a propulsion unit of the above group of propulsion units of various types, for example, it may be provided with two identical paddle-type propulsion units or it may be provided with a combination of a paddle-type air propeller and a paddle-type propulsion unit.

[230] Furthermore, in some embodiment of the present invention, at least one or each of one or more auxiliary anchoring modules 350 that may be provided to the housing 310 in the self-propelled module according to any of the embodiments described in the present invention, known in the prior art or appreciated by a person skilled in the art, may be arranged on one side of the housing 310 of the self-propelled module, distinct from the remaining auxiliary anchoring modules of said modules. Petition 870250091550, dated 07 / 10 / 2025, pp. 141 / 180 127 / 154 auxiliary anchoring modules 350. In one of the variations of this embodiment of the present invention, one or more auxiliary anchoring modules 350 that can be provided to the housing 310 in the self-propelled module according to any of its embodiments described in the present invention, known in the state of the art or appreciated by a person skilled in the art, can be arranged on one and the same side of the housing 310 of the self-propelled module or on different sides of the housing 310 of the self-propelled module.

[231] Furthermore, in some other embodiment of the present invention, at least one or each of one or more main anchoring modules 330 that may be provided to the housing 310 in the self-propelled module according to any of the embodiments described in the present invention, known in the prior art or appreciated by a person skilled in the art, may be arranged on one side of the housing 310 of the self-propelled module, distinct from the remaining main anchoring modules of said main anchoring modules 330.In one variation of this embodiment of the present invention, one or more main anchoring modules 330, which may be provided to the housing 310 in the self-propelled module according to any of its embodiments described in the present invention, known in the prior art or appreciated by a person skilled in the art, may be arranged on one and the same side of the housing 310 of the self-propelled module or on different sides of the housing 310 of the self-propelled module.

[232] Furthermore, in some other embodiment of the present invention, at least one or each of one or more guides 360, which may be provided to the housing 310 in the self-propelled module according to any of the embodiments described in the present invention, known in the state of Petition 870250091550, dated 07 / 10 / 2025, pp. 142 / 180 128 / 154 technical or appreciated by a person skilled in the art may be arranged on one side of the housing 310 of the self-propelled module, distinct from the other guides 360 of the self-propelled module. In one of the variations of this embodiment of the present invention, one or more guides 360, which may be provided to the housing 310 in the self-propelled module according to any of its embodiments described in the present invention, known in the prior art or appreciated by a person skilled in the art, may be arranged on one and the same side of the housing 310 of the self-propelled module or on different sides of the housing 310 of the self-propelled module. PAYLOAD

[233] Figs. 4-6 show an illustrative embodiment of a payload 200 in the form of a passenger cabin comprising an accommodation 210 in the form of a fuselage configured to accommodate within it persons (e.g., one or more passengers and / or a pilot), various living beings and / or various goods of any kind. It should be noted that the payload 200 can be used to deliver, move or transport persons, various living beings and / or goods of various kinds (solid, gaseous, liquid, fluid, bulk, viscous, radioactive, chemical goods and / or the like) through the air, over land (terrestrial), over water and / or underwater, thus enabling the payload to be referred to as a means of transport, transport module or transport module.

[234] In one embodiment of the present invention, a pilot's seat may be provided in the internal space of housing 210 in the payload 200, which may accommodate a pilot (not shown) capable of operating a means of transport, which will be based on one or more payloads 200 anchored together, using the instrument panel and control elements, which may also be arranged in said housing 210. Furthermore, Petition 870250091550, dated 07 / 10 / 2025, pages 143 / 180 129 / 154 in this embodiment of the present invention, in the internal space of accommodation 210 in the payload 200, in addition to a pilot, at least one passenger, at least one item of passenger baggage and / or at least one item of merchandise may also be accommodated, wherein said pilot, passengers, merchandise items and passenger baggage items may be accommodated at corresponding points in the common internal space or may each be accommodated in its distinct zone defined at least partially by one or more partitions, or in a distinct compartment defined at least partially by one or more partitions.

[235] In another embodiment of the present invention, the pilot's seat may be arranged in the pilot's cabin provided in the internal space of the payload compartment 210 and separated by a partition from the rest of the internal space of the compartment 210 which, in turn, may be divided by another partition into a passenger compartment in which one or more passenger seats may be installed to accommodate passengers therein, and into a baggage compartment or cargo compartment in which cargo (in particular, one or more items of cargo) and / or passenger baggage (in particular, one or more items of passenger baggage) may be accommodated, wherein said items of cargo, passenger baggage items and / or passenger seats may be arranged or attached to the underside, floor, walls of the compartment 210.In one variation of this embodiment of the present invention, the passenger compartment, instead of or in addition to passenger seats, may provide the following: (i) rails installed on the side walls, floor and / or ceiling of the accommodation 210 to accommodate passengers in any position in the accommodation 210, for example, seated or standing on the floor of the accommodation 210; (ii) sofas, beds or benches attached to the floor, walls and / or ceiling of the accommodation 210 to accommodate passengers. Petition 870250091550, dated 07 / 10 / 2025, pp. 144 / 180 130 / 154 same passengers in a seated, standing and / or lying position; (iii) specialized areas to accommodate persons with disabilities in a seated, standing and / or lying position; (iv) specialized areas for wheelchairs used by persons with disabilities; (v) specialized areas to accommodate cribs used by children and (if necessary) specialized areas for accompanying persons; and / or (vi) specialized areas to accommodate stretchers for transporting patients used by bedridden patients. It should be noted that the number of passengers in the passenger accommodation may be from one person to several dozen or even hundreds of people without making any limitation, wherein the said number of passengers is substantially limited only by the area of ​​the passenger compartment within the internal space of the accommodation 210.In another variation of this embodiment of the present invention, the cargo compartment of accommodation 210 may be enabled not only to accommodate cargo and / or passenger baggage on the floor of the fuselage 102 but also to attach the same to the cargo compartment of accommodation 210 using conventional fastening means known in the prior art, wherein the cargo compartment of accommodation 210 may also be provided with shelves, hangers, crates and other means of transport attached to the floor, ceiling and / or side walls of accommodation 210 and allowing additional items of cargo and / or items of passenger baggage to be accommodated in the cargo compartment of accommodation 210.In another variation of this embodiment of the present invention, areas for passenger baggage, including shelves, hangers, boxes and other means of transport for accommodating passenger baggage items, may only be provided in the passenger compartment of accommodation 210, in addition to the above variants of means for accommodating passengers in said passenger compartment. A person skilled in the art would readily appreciate that merchandise items and / or items. Petition 870250091550, dated 07 / 10 / 2025, pages 145 / 180 131 / 154 passenger baggage can be at least partially secured or fixed also on the outside of the payload compartment 210 using suitable fastening means known in the state of the art (for example, using a dedicated closed-type attachment used in airplanes, cars, motorcycles, helicopters, bicycles and the like). It should be noted that the cockpit, passenger compartment and cargo compartment above in the payload compartment 210 can generally be configured analogously to the corresponding compartments of airplanes, helicopters, buses, cars, ships, motorboats and the like.

[236] In yet another embodiment of the present invention, the pilot's seat may be arranged in the pilot's cabin in the internal space of the payload compartment 210, which the pilot's cabin is separated from by means of a partition from the remaining portion of the internal space of the compartment 210, in which portion, in turn, at the bottom, ceiling and / or floor of the compartment 210, there may be passengers accommodated or restrained (for example, in passenger seats), merchandise items and passenger baggage items.Furthermore, it is possible to have an embodiment of the present invention in which the interior space of accommodation 210 can accommodate only a pilot and passengers; it is possible to have an embodiment of the present invention in which the interior space of accommodation 210 can accommodate only a pilot and cargo; it is possible to have an embodiment of the present invention in which the interior space of accommodation 210 can accommodate only passengers and cargo; it is possible to have an embodiment of the present invention in which the interior space of accommodation 210 can accommodate only passengers; it is possible to have an embodiment of the present invention in which the interior space of accommodation 210 can accommodate only a pilot in the pilot's seat; and it is possible to have an embodiment of the present invention in which the interior space of accommodation 210 can accommodate... Petition 870250091550, dated 07 / 10 / 2025, pp. 146 / 180 132 / 154 merchandise only.

[237] It should be noted that the control elements that can be installed in the internal space of housing 210, whose internal space is defined by the walls of housing 210 from the inside of the same, in the payload shown in Figs. 3-6 allow substantially controlling the payload 200 in semi-automatic mode (i.e., a combination of manual control by a pilot and automatic control using autopilot) and enable manual input, by the pilot present in the pilot's seat and monitoring of the instrument readings on the instrument panel, of at least one control command.The control elements of housing 210 must be communicatively coupled to the control unit described below (not shown) being part of payload 200, so as to enable each of said pilot control commands to be presented to said payload control unit 200, wherein some of said pilot control commands may substantially replace the corresponding control commands of the payload control unit 200 generated by the payload control unit 200 while controlling the means of transport which is based on one or more payloads anchored to each other 200 in automatic mode (i.e., in autopilot mode).In one embodiment of the present invention, the participation of a pilot in the process of controlling the means of transport based on one or more payloads 200 anchored to each other may not be foreseen and, therefore, the instrument panel above, control elements and pilot's seat may not be present in the internal space of the payload housing 210 and the control of the means of transport based on one or more payloads 200 anchored to each other may be carried out substantially entirely in automatic mode (i.e., in autopilot mode) using the control module described below of the payload 210 which module, in turn, may. Petition 870250091550, dated 07 / 10 / 2025, pages 147 / 180 133 / 154 receive control commands from the system control device to move a payload, the system of which may comprise said payload 200. In another embodiment of the present invention, the above control elements and / or the above instrument panel in the payload housing 210 may be comprised in the payload control module 200 described below, thus enabling the control module to simultaneously enable manual control of the means of transport based on one or more payloads 200 anchored to each other by means of a pilot and automatic control of such means of transport in autopilot mode.

[238] Additionally, as shown in Figs. 4 to 6, the housing 210 of a payload is provided with an anchoring module 230, which is attached to the housing 210 from the outside thereof and which is configured to interact with at least one guide, which may be configured in the form of a guide 140 of an aircraft apparatus, a grouping guide 145 of an aircraft apparatus in grouping, a guide 360 ​​of a self-propelled module or a grouping guide of a self-propelled module in grouping 300 so as to enable the housing 210 of the payload to move along said at least one guide.Thus, the payload 200 can be mounted or suspended, by means of the anchoring module 230, on a guide and can also move in one direction or another along said guide, so as to occupy a suitable spatial position in relation to the housing of a functional object, which is equipped with said guide (that is, for example, in relation to the housing 110 of an aircraft apparatus, the housing 110 of at least one of the aircraft apparatuses 100 forming a grouped aircraft apparatus, the housing 310 of a propelled module or the housing 310 of at least one of the self-propelled modules forming a grouped self-propelled module 300). Petition 870250091550, dated 07 / 10 / 2025, pp. 148 / 180 134 / 154

[239] In one embodiment of the present invention, the payload housing 210 may be provided with one or more anchoring modules 230 (for example, one, two, three, four, five, six, seven, eight, nine, ten or more anchoring modules 230), at least one of which may be configured to interact with at least one guide 140 of an aircraft apparatus, at least one guide 140 of at least one of the aircraft apparatus 100 forming a grouping aircraft apparatus, at least one guide 360 ​​of a self-propelled module or at least one guide 360 ​​of at least one of the self-propelled modules forming a grouping self-propelled module 300 so as to enable the payload housing 210 to move along said at least one guide.

[240] It should be noted that at least one or each of the 230 docking modules on the 200 payload can generally be configured analogously to the 130 docking module above an aircraft apparatus, the 330 docking module above a self-propelled module or the 350 auxiliary docking module above a self-propelled module.

[241] Additionally, as shown in Figs. 4-6, the payload housing 210 is provided with a guide 240, which is configured to interact with at least one anchoring module that can be configured in the form of an anchoring module 130 of an aircraft apparatus, an anchoring module 130 of one of the aircraft apparatuses forming an aircraft apparatus in cluster, an anchoring module 330 of a self-propelled module or an anchoring module 330 of one of the self-propelled modules forming a self-propelled cluster module 300 so as to enable the movement of a functional object, which is provided with said anchoring module (i.e., the aircraft apparatus 100, aircraft apparatus in cluster, self-propelled module or self-propelled module Petition 870250091550, dated 07 / 10 / 2025, pages 149 / 180 135 / 154 of grouping 300) along the aforementioned guide 240, thus enabling the aircraft apparatus 100, aircraft apparatus in grouping, self-propelled module or self-propelled module of grouping 300, respectively, to assume a suitable spatial position in relation to the payload housing 210.

[242] In another embodiment of the present invention, the payload housing 210 may be provided with one or more guides 240 (for example, one, two, three, four, five, six, seven, eight, nine, ten or more guides 240), at least one of which may be configured to interact with at least one anchoring module 130 of an aircraft apparatus, at least one anchoring module 130 of one of the aircraft apparatuses 100 forming a grouped aircraft apparatus, at least one anchoring module 330 of a self-propelled module, at least one anchoring module 330 of one of the self-propelled modules forming a grouped self-propelled module 300 so as to enable the movement of a functional object that is equipped with said anchoring module (i.e., the aircraft apparatus 100, grouped aircraft apparatus, self-propelled module or grouped self-propelled module 300) along said at least one guide. 240, thus enabling the aircraft device 100,aircraft apparatus in cluster, self-propelled module or self-propelled cluster module 300, respectively, to assume a suitable spatial position relative to the payload housing 210.

[243] It should be noted that at least one or each of the 240 guides on the 200 payload can generally be configured analogously to guide 140 above an aircraft apparatus or guide 360 ​​above a self-propelled module.

[244] In yet another embodiment of the present invention, the housing Petition 870250091550, dated 07 / 10 / 2025, pp. 150 / 180 136 / 154 210 of a payload can be supplied with at least one anchoring module 230 or at least one guide 240.

[245] In some embodiment of the present invention, at least one or each of one or more anchoring modules 230, which may be provided to the housing 210 in the payload 200, may be arranged on one side of the housing 210 of a payload, distinct from the remaining anchoring modules of said anchoring modules 230. In one variation of this embodiment of the present invention, one or more anchoring modules 230, which may be provided to the housing 210 in the payload 200, may be arranged on one and the same side of the housing 210 of a payload or on different sides of the housing 210 of a payload.

[246] In some other embodiment of the present invention, at least one or each of one or more guides 240, which may be provided to the housing 210 in the payload 200, may be arranged on one side of the housing 210 of a payload, distinct from the remaining guides of said guides 240.

[247] In another embodiment of the present invention, at least two of the guides 240, which may be provided to the housing 210 in the payload 200, may be arranged on one side of the housing 210 of a payload, distinct from the remaining guides of said guides 240.

[248] In some other embodiment of the present invention, at least one or each of the guides 240, which may be provided to the housing 210 in the payload 200, may be arranged on a side of the housing 210 of the payload different from the sides of the housing 210 of the payload in which the anchoring modules 230 are arranged.

[249] In other embodiments of the present invention, at least one or each of the guides 240, which may be provided to the housing 210 in Petition 870250091550, dated 07 / 10 / 2025, pp. 151 / 180 137 / 154 payload 200, can be configured in a straight or curved manner. In other embodiments of the present invention, at least one or each of the guides 240, which can be provided to the housing 210 in the payload 200, can be configured in the form of a regular or irregular geometric figure.

[250] It should be noted that the self-propelled module 200 may also comprise a control unit (not shown) mounted in the internal space of the housing 210 in order to control the anchoring and / or unanchoring operation, to / from the housing 210 of a payload, of one or more aircraft devices 100, one or more aircraft devices in a group, one or more self-propelled modules, one or more group self-propelled modules 300, one or more additional payloads 200 and / or one or more group payloads formed from two or more payloads 200 anchored together, wherein to anchor to the housing 210 of a payload of at least one of the aforementioned functional objects one or more anchoring modules 230 and / or one or more guides 240 may be used.

[251] It should also be noted that the detachable anchoring of two or more payloads 200 to each other to form a grouping payload may be carried out under the control of at least one or each of the control units of said payloads 200 configured to mutually exchange data via a communication network and / or under the control of the system control device to move a payload whose system may comprise said payloads 200 to be anchored to each other, wherein, to implement said mutual anchoring process, detachable anchoring modules 230 may be used entering into detachable interaction with each other during the anchoring of payloads 200 to be anchored to each other and / or detachable guides 240 may be used entering into detachable interaction with each other (for example, by means of auxiliary anchoring modules, which may be provided to these guides 240) Petition 870250091550, dated 07 / 10 / 2025, pp. 152 / 180 138 / 154 during the anchoring of the payloads 200 to be anchored to each other and / or guides 240 entering into detachable interaction with the anchoring modules 230 during the anchoring of the payloads 200 to be anchored to each other. In addition, at least one or each of the control units of the payloads 200 anchored to each other to form a grouping payload may also be configured to generate control commands that allow the unanchoring of said payloads 200 to form distinct payloads 200, each of which is provided with at least one free anchoring module 230 and / or at least one free guide 240.

[252] In one embodiment of the present invention, the group payload may be formed from two or more payloads 200 above (for example, two, three, four, five, six, seven, eight, nine, ten or more payloads), each of which may be of the type described in the present invention or may be of any other type known in the prior art or appreciated by a person skilled in the art, wherein such group payload may comprise payloads 200 of an identical type (for example, only passenger cabins) as well as payloads 200 that are at least partially or completely different in any combinations of the types described in the present invention and known in the prior art (for example, a passenger cabin and a bag with bulk cargo).Thus, the sizes, types, manufacturing materials and / or the like of the payloads 2002 being part of any self-propelled bundle module 300 are not specifically limited in any way. Furthermore, the bundle payload formed from a pair, group or combination of identical or different payloads 200 may have any size (including spatial extent or overall dimensions) and / or any shape suitable for uncoupling at least some or all of the payloads 200 forming such payload. Petition 870250091550, dated 07 / 10 / 2025, pages 153 / 180 139 / 154 grouping and for detachable anchoring, for such grouping payload, one or more additional payloads 200, one or more additional grouping payloads, one or more self-propelled modules, one or more grouping self-propelled modules 300, one or more aircraft devices 100 and / or one or more aircraft devices in grouping.

[253] It should also be noted that at least one or each of the payload control units of the 300 grouping or the system control device for moving a payload whose system comprises said 300 grouping payload may be further configured to enable the unhooking of at least a portion or all of the 200 payloads forming said payload.Furthermore, at least one or each of the cluster payload control units or the system control device for moving a payload whose system comprises said cluster payload may also be configured to enable detachable coupling, for such cluster payload, one or more additional 200 payloads, one or more additional cluster payloads, one or more 100 aircraft devices, one or more cluster self-propelled modules, each of which is formed from one or more 100 aircraft devices, one or more self-propelled modules and / or one or more 300 cluster self-propelled modules.It should also be noted that, depending on a particular type of payload 200 being part of the group payload, the detachable coupling process of said group payload to one or more additional payloads 200, one or more additional group payloads, one or more self-propelled modules, one or more self-propelled modules of group 300, one or more aircraft 100 and / or one or more aircraft of the above group can be carried out in two possible ways: 1) by placing at least one or. Petition 870250091550, dated 07 / 10 / 2025, pp. 154 / 180 140 / 154 each of the anchoring modules 230 supplied to the payload housings 210 forming the said group payload in detachable interaction with at least one of the guides, which may be supplied to the housings of said one or more additional payloads 200, one or more additional group payloads, one or more self-propelled modules, one or more group self-propelled modules 300, one or more aircraft devices 100 and / or one or more group aircraft devices, respectively;and / or 2) by placing at least one or each of the guides 240 supplied to the housings 210 of the payloads forming said group payload in detachable interaction with at least one of the anchoring modules that may be supplied to the housings of said one or more additional payloads 200, one or more additional group payloads, one or more self-propelled modules, one or more self-propelled group modules 300, one or more aircraft devices 100 and / or one or more aircraft devices in grouping, respectively;

[254] Thus, in view of the description given above with respect to payloads and group payloads, in the present invention there may be an embodiment of the system for moving a payload comprising (i) one or more aircraft devices 100 above or one or more grouped aircraft devices above, each of which comprises two or more aircraft devices anchored together 100; and (ii-1) one or more payloads 200, at least one of which is anchored to at least one of said aircraft devices 100 by placing at least one of the guides 240 of said at least one payload 200 in interaction with at least one anchoring module 130 of said at least one aircraft device 100 so as to enable the movement of said at least one aircraft device 100 along the Petition 870250091550, dated 07 / 10 / 2025, pp. 155 / 180 141 / 154 referred to by at least one guide 240 of the payload or by placing at least one of the anchoring modules 230 of said payload 200 in interaction with at least one guide 140 of said at least one aircraft apparatus 100, so as to enable the movement of said at least one payload 200 along said at least one guide 140 of the aircraft apparatus, or (ii-2) one or more payloads 200,at least one of which is anchored to at least one of said aircraft devices in group 100 by placing at least one of the guides 240 of said at least one payload 200 in interaction with at least one anchoring module 130 of said at least one aircraft device in group so as to enable the movement of said at least one aircraft device in group along said at least one guide 240 of the payload or by placing at least one of the anchoring modules 230 of said payload 200 in interaction with at least one guide 140 of said at least one aircraft device in group so as to enable the movement of said at least one payload 200 along said at least one guide 140 of said aircraft device in group.

[255] Furthermore, in view of the description given above with respect to payloads and group payloads, in the present invention there may be yet another embodiment of the system for moving a payload, comprising (i) one or more payloads 200; and (ii) one or more self-propelled modules above, at least one of which is detachably anchored to at least one of said payloads 200 by placing at least one of the guides 360 of said self-propelled module in interaction with the anchoring module 230 of said at least one payload 200 so as to enable the movement of said payload 200 along said at least one guide 360 ​​of the self-propelled module or by placing at least one Petition 870250091550, dated 07 / 10 / 2025, pp. 156 / 180 142 / 154 of the anchoring modules 330 of said self-propelled module interacting with the guide 240 of said at least one payload 200, in order to enable the movement of said at least one self-propelled module along said at least one guide 240 of the payload.

[256] According to a variation of this embodiment of the present invention, such a system for moving a payload may further comprise one or more additional self-propelled modules that may be detachably anchored to at least one of the payloads 200, such that the guides 360 of at least a portion of said anchored self-propelled modules form a grouping guide for moving said at least one payload 200 along the same.

[257] According to another variation of this embodiment of the present invention, such a system for moving a payload may further comprise one or more additional self-propelled modules, each of which may be anchored to at least one of the self-propelled modules that are already part of said system.

[258] In particular, Fig. 4 shows the process of anchoring the payload 200 above to the self-propelled wheeled module 300-1 above by placing the payload guide 240 in detachable interaction with the anchoring module 330 of the self-propelled module and to the aircraft apparatus 100 above by placing the aircraft apparatus guide 140 in detachable interaction with the anchoring module 230 of the payload, so that it results in a means of transport configured to move over the ground surface (over the earth) while using the self-propelled wheeled module 300-1 and configured to move in airspace or fly while using the aircraft apparatus 100 anchored to the payload 200.

[259] In addition, Fig. 5 shows the payload anchoring process. Petition 870250091550, dated 07 / 10 / 2025, pages 157 / 180 143 / 154 200 anchored to the self-propelled wheeled module 300-1 above and to the aircraft apparatus 100 above as per Fig. 4, to the grouped aircraft apparatus above formed from two detachably anchored aircraft apparatus 100 and provided with a grouping guide 145 formed from two connected guides 140, by placing the anchoring module 130 of the aircraft apparatus for detachable interaction with one of the free anchoring modules 130 of the grouped aircraft apparatus so as to provide the connection of the guide 140 of the aircraft apparatus to the grouping guide 145 of the grouped aircraft apparatus, so that it results in a means of transport configured to move over the ground surface (over the earth) while using the self-propelled wheeled module 300-1 and configured to move in airspace or fly while using the expanded grouped aircraft apparatus. As shown in Fig.5, the resulting transport means is formed from the payload 200 mounted on the self-propelled module 300-1 and detachably anchored to the aircraft apparatus in an expanded grouping provided with an expanded grouping guide formed from three connected guides 140 and formed from three aircraft apparatus 100 anchored to each other, wherein the anchoring module 230 with which the payload housing 200 is provided is placed in detachable interaction with one of the three guides 140 forming the said expanded grouping guide. Furthermore, as shown in Fig.5, thanks to the fact that the anchoring module 230, by means of which the payload 200 is mounted or suspended on the expanded grouping guide of the means of transport, is placed in detachable interaction with one of the three guides 140 forming said expanded grouping guide, the payload 200 can be moved in relation to the aircraft apparatus in expanded grouping by moving the anchoring module 230 along said guide. Petition 870250091550, dated 07 / 10 / 2025, pp. 158 / 180 144 / 154 expanded grouping guide, in order to provide the occupation, by the payload 200 together with the self-propelled module 300-1, of the desired position in relation to said aircraft apparatus in expanded grouping to improve the flight characteristics of the means of transport.

[260] Furthermore, Fig. 6 shows the process of undocking one of the aircraft devices 100 forming the expanded grouping aircraft device in the transport means of Fig. 5 by removing the anchoring module 130 related to said aircraft device 100 to be undocked and the anchoring module 130 related to the aircraft device 100 to which said aircraft device to be undocked as part of said expanded grouping aircraft device was immediately detachably anchored from the interaction with each other. Fig.Figure 6 also shows the process of undocking the self-propelled wheeled module 300-1 from the payload 200 by removing the anchoring module 330 from the self-propelled module through interaction with the payload guide 240, as a result of which the payload 200 is anchored only to the grouping aircraft equipped with the grouping guide 145 formed from two connected guides 140 and formed from two aircraft 100 anchored to each other. Furthermore, Fig.Figure 6 shows the process of anchoring another aircraft device 100 to a grouping aircraft device to which the payload 200 is detachably anchored and which is formed from two aircraft devices 100 anchored together by placing the anchoring module 130 of the aircraft device 100 to be anchored in detachable interaction with one of the free anchoring modules 130 of the grouping aircraft device so as to provide the connection of the guide 140 of the aircraft device to be anchored to the grouping guide 145 of the grouping aircraft device. Petition 870250091550, dated 07 / 10 / 2025, pages 159 / 180 145 / 154 also shows the process of anchoring the 300 self-propelled grouping module formed from two 300-3 self-propelled modules, 3004 above anchored together by placing one of the 330 anchoring modules of such 300 self-propelled grouping module onto the 240 guide of a payload in order to provide the obtaining of an altered means of transport configured to move in airspace. In particular, the resulting modified transport means shown in Fig. 6 is formed from a payload 200 detachably anchored to an aircraft apparatus in a grouping provided with a grouping guide 145 formed from two connected guides 140 and formed from two aircraft apparatus 100 anchored to each other, wherein the anchoring module 230 from which the payload housing 200 is provided is placed in detachable interaction with one of the two guides 140 forming said grouping guide 145.

[261] Fig. 7.1 is an illustrative example of the system comprising an aircraft apparatus in grouping with a grouping guide 145 and two payloads 200 configured to move along the grouping guide 145.

[262] The grouping aircraft apparatus is formed by a plurality of aircraft apparatus 100 with guides 140 that are connected together to form a branching grouping guide 145.

[263] On grouping guide 145, two payloads 200 are mounted, in a movable manner along the same. The first payload 200-1 is a fuselage to accommodate cargo and passengers, to which a self-propelled module 300-1 is also attached. Aircraft devices 320 are attached to the self-propelled module 300-1.

[264] The second payload 200-2 is a container, for example, a crate for transporting products and equipment. Petition 870250091550, dated 07 / 10 / 2025, pp. 160 / 180 146 / 154

[265] Fig. 7.2 schematically shows a non-limiting illustrative example of a method for moving payloads 200 (200-1 and 200-2) along a branching guide 145. Furthermore, Fig. 7.2 shows that at least one or each of the payloads 200 (200-1, 200-2), after being moved along the branching grouping guide 145 to a predetermined position, can be unanchored along with a predetermined portion of said grouping guide 145 so as to provide alteration of the movement patterns of the remaining payloads of said payloads 200 mounted or suspended on said branching grouping guide 145. Said unanchored portion of the grouping guide 145 consists of one or more guides 140 of one or more aircraft apparatus 100 connected to each other.

[266] After the undocking of the last payload 200 (200-2), the grouping guide 145 may continue flight as part of an aircraft apparatus in a grouping of a plurality of aircraft apparatus 100 with corresponding guides 140 or may be partially or completely separated with allocation to distinct aircraft apparatus 100 with corresponding distinct guides 140. Subsequently, said aircraft apparatus may form one or more new grouping guides 145 to move one or more payloads 200. METHODS OF HANDLING PAYLOAD

[267] Fig. 8 is a flow diagram showing the main operations of a method 600 of moving a payload, wherein the method 600 of moving a payload shown in Fig. 8 can be performed using system 500-1 to move a payload which system can be implemented according to any of the relevant embodiments of the present invention described in the present invention. Petition 870250091550, dated 07 / 10 / 2025, pp. 161 / 180 147 / 154

[268] In particular, method 600 of moving a payload shown in Fig. 8 comprises the following two main operations or two main steps 610 and 620, wherein step 610 comprises anchoring at least one of one or more aircraft devices 100 being part of the first embodiment above of the system to move a payload or one or more aircraft devices in clusters formed, each, by two or more aircraft devices 100 anchored together being part of the first embodiment above of the system to move a payload to one or more additional aircraft devices being part of the first embodiment above of the system to move a payload or to one or more additional aircraft devices in clusters formed, each,by two or more aircraft devices 100 anchored together being part of the first embodiment above of the system for moving a payload by connecting the anchoring modules 130 of said aircraft devices 100 to be anchored together to form a grouping guide 145 from the guides 140 of said aircraft devices 100 to be anchored together, and step 620 comprises moving the payload (including payload 200) along said grouping guide 145 formed in at least one of said aircraft devices 100 anchored together.

[269] One embodiment is possible in which, prior to the anchoring stage, the rotation of the aircraft device housing 100 is performed relative to the guide 140. The rotation angle may be, for example, 1°-30° in the vertical plane and / or 90° or 45° or 180° or another angle from 1° to 180° in the horizontal plane. The rotation of the aircraft device housing 100 enables the facilitation of anchoring the guide 140 to the grouping guide 145 and / or optimizes the arrangement of the air propulsion units to exclude the crossing of airflows and / or collision of the aircraft device components 100 during the Petition 870250091550, dated 07 / 10 / 2025, pp. 162 / 180 148 / 154 anchoring.

[270] After docking, the aircraft housing 100 can be returned to its original position relative to guide 140 by rotating it backward by the corresponding angle, or it can be rotated relative to the guides by a different angle, for example, 10° in the vertical plane and / or 30° or 25° or 120° or another angle from 1° to 180° in the horizontal plane. The value of the rotation angle can be defined taking into account the configuration of the grouped aircraft and the optimized arrangement of the air propulsion units, airflow distribution and optimized flight characteristics of the grouped aircraft. Alternatively, the aircraft housing 100 can remain in the same position relative to the guide that was adjusted before docking.

[271] Fig. 9 is a flow diagram showing the main operations of the 650 method of moving a payload, wherein the 650 method of moving a payload shown in Fig.9 comprises the following main operation or main step 660 of anchoring one or more payloads 200 each to at least one of one or more aircraft devices 100 being part of the first embodiment above of the system for moving a payload or to one or more aircraft devices in groups formed, each, by two or more aircraft devices 100 anchored to each other being part of the first embodiment above of the system for moving a payload by placing at least one of the guides 240 of said payload 200 in interaction with the anchoring module 130 of said at least one aircraft device 100 in order to enable the movement of said aircraft device 100 and aircraft devices 100 anchored to it along said at least one guide 240 of the payload or by placing at least one of the anchoring modules 230 of said payload in interaction with the guide 140 of said payload. Petition 870250091550, dated 07 / 10 / 2025, pp. 163 / 180 149 / 154 at least one aircraft device in order to enable the movement of payload 200 along said guide 140 of the aircraft device.

[272] Fig. 10 is a flow diagram showing the main operations of method 700 for moving a payload, wherein method 700 for moving a payload shown in Fig. 10 comprises the following main operation or main step 710 of anchoring one or more self-propelled modules above each to at least one of one or more aircraft 100s being part of system 500-1 or the first embodiment above of the system to move a payload to one or more aircraft 100s in groupings formed, each,by two or more aircraft units 100 anchored to each other, being part of the first embodiment above of the system for moving a payload by placing at least one of the 360° guides of said payload 200 in interaction with the anchoring module 130 of said at least one aircraft unit 100 so as to enable the movement of said aircraft unit 100 and aircraft units 100 anchored to it along said at least one 360° guide of said self-propelled module or by placing at least one of the 330° anchoring modules of said self-propelled module in interaction with the guide 140 of said at least one aircraft unit 100 so as to enable the movement of the self-propelled module along said guide 140 of the aircraft unit.

[273] Fig. 11 is a flow diagram showing the main operations of a method 750 of moving a payload, wherein the method 750 of moving a payload shown in Fig. 11 comprises the following main operation or main step 760 of anchoring one or more self-propelled modules above, each to at least one of one or more payloads 200 by placing at least one of the guides 360 of said self-propelled module in interaction with the anchoring module 230 of said self-propelled module. Petition 870250091550, dated 07 / 10 / 2025, pp. 164 / 180 150 / 154 less a payload 200 in order to enable the movement of said payload 200 along said at least one guide 360 ​​of the self-propelled module or by placing at least one of the anchoring modules 330 of said self-propelled module in interaction with the guide 240 of said at least one payload 200 in order to enable the movement of the self-propelled module along said guide 240 of the payload.

[274] One embodiment is possible in which, prior to the docking stage, the self-propelled module housing 300 is rotated relative to the guide 360. The rotation angle may be, for example, 1°-30° in the vertical plane and / or 90° or 45° or 180° or another angle from 1° to 180° in the horizontal plane. Rotation of the self-propelled module housing 300 facilitates docking of the guide 360 ​​to the payload 200 and / or optimizes the arrangement of the air propulsion units to exclude airflow crossing with that of the aircraft 100 and / or collision of the self-propelled module 300 components with the payload 200 during docking.

[275] After docking, the housing for the self-propelled module 300 can be returned to its original position relative to the 360 ​​guide by rotating it backward by the corresponding angle, or it can be rotated relative to the guides by a different angle, for example, 10° in the vertical plane and / or 30° or 25° or 120° or another angle from 1° to 180° in the horizontal plane. The value of the rotation angle can be defined taking into account the system configuration and the optimized arrangement of the air propulsion units, the distribution of airflows from the self-propelled module and the aircraft equipment, and the optimized flight characteristics of the system or its distinct components. Alternatively, the housing for the self-propelled module 300 can remain in the same position relative to the 360 ​​guide as it was adjusted before docking. Petition 870250091550, dated 07 / 10 / 2025, pp. 165 / 180 151 / 154

[276] Fig. 12 is a flow diagram showing the main operations of a method 800 of moving a payload, wherein the method 800 of moving a payload shown in Fig. 12 comprises two main operations or two main steps 810, 820.Step 810 of method 800 comprises anchoring at least one of one or more aircraft devices 100 being part of system 500-2 or the second embodiment of the system above to move a payload or one or more aircraft devices in clusters formed, each, by two or more aircraft devices 100 anchored together being part of the second embodiment of the system to move a payload to one or more additional aircraft devices 100 being part of the second embodiment of the system to move a payload or to one or more aircraft devices in additional clusters formed, each, by two or more additional aircraft devices 100 anchored together being part of the second embodiment of the system to move a payload by detachably connecting the guides 140 of said aircraft devices 100 to be anchored together to form a cluster guide 145 from the guides 140 of said aircraft devices 100 to be anchored together.Step 820 of method 800 is a step of moving the payload (inter alia, it could be payload 200 as well) along the grouping guide 145 formed for at least one of the aircraft devices 100 anchored to each other.

[277] One embodiment is possible in which, before the movement (movement stage) of the payload 200, the payload is rotated relative to the grouping guide 145. The rotation angle can be, for example, 1°-30° in the vertical plane and / or 90° or 45° or 180° or another angle from 1° to 180° in the horizontal plane. The rotation of the payload 200 facilitates the movement of the payload 200 and / or optimizes the arrangement of the payload 200 relative to the guide. Petition 870250091550, dated 07 / 10 / 2025, pages 166 / 180 152 / 154 grouping 145 and to the accommodations of the aircraft devices 100 and can also promote passenger comfort while they are present in the payload 200 or optimized flight characteristics of the system, for example, reduced aerodynamic drag.

[278] After the movement of payload 200, it can be returned to its original position relative to the grouping guide 145 by rotating it backwards by the corresponding angle, or it can be further rotated relative to the grouping guide 145 by a different angle, for example, 10° in the vertical plane and / or 30° or 25° or 120° or another angle from 1° to 180° in the horizontal plane. The value of the rotation angle can be defined taking into account the system configuration and optimized arrangement of payload 200 relative to the air propulsion unit or optimized flight characteristics of the system, for example, reduced aerodynamic drag and / or optimized flight characteristics of the system or distinct components thereof. Alternatively, payload 200 can remain in the same position relative to the grouping guide 145 as defined before the start of the movement along the grouping guide 145.Furthermore, during movement along the grouping guide 145, the payload 200 may perform one or more rotations relative to the grouping guide 145, wherein the angle of each subsequent rotation may coincide with or differ from the previous one.

[279] Fig. 13 is a flow diagram showing the main operations of a method 850 for moving a payload, wherein the method 850 for moving a payload shown in Fig. 13 comprises two main operations or two main steps 860, 870. Step 860 of method 850 comprises anchoring at least one of one or more aircraft devices 100 being part of the third embodiment of the above system to move a payload or one or more aircraft devices in a grouping. Petition 870250091550, dated 07 / 10 / 2025, pages 167 / 180 153 / 154 each formed by two or more aircraft devices 100 anchored together being part of the third embodiment above of the system for moving a payload to one or more additional aircraft devices 100 being part of the third embodiment above of the system for moving a payload or to one or more additional grouping aircraft devices each formed by two or more additional aircraft devices 100 anchored together being part of the third embodiment above of the system for moving a payload by detachably connecting the guides 140 of said aircraft devices 100 to be anchored together to form a grouping guide 145 from the guides 140 of said aircraft devices 100 to be anchored together.Step 870 of method 850 comprises simultaneously moving at least a portion of the grouping guide 145 formed in relation to one or more housings of the aircraft apparatus 100 anchored together and moving the payload (including payload 200) along said grouping guide 145 formed in at least one of said aircraft apparatus 100 anchored together.

[280] Fig. 14 is a flow diagram showing the main operations of a method 900 of moving a payload, wherein the method 900 of moving a payload shown in Fig. 14 comprises two main operations or two main steps 910, 920. Step 910 of method 900 comprises anchoring at least one of one or more aircraft devices 100 being part of the fourth embodiment of the above system to move a payload or one or more aircraft devices in clusters formed, each, by two or more aircraft devices 100 anchored together being part of the fourth embodiment of the system to move a payload to one or more additional aircraft devices being part of the fourth embodiment of the above system to move a payload or to one or more Petition 870250091550, dated 07 / 10 / 2025, pages 168 / 180 154 / 154 additional aircraft units in clusters, each formed by two or more additional aircraft units 100 anchored together, being part of the fourth embodiment above of the system for moving a payload by detachably connecting the anchoring modules 130 of said aircraft units 100 to be anchored together to form a cluster guide 145 from the guides 140 of said aircraft units 100 to be anchored together. Step 920 of method 900 comprises simultaneously moving at least a portion of the cluster guide 145 formed in relation to one or more housings 210 of the aircraft units 100 anchored together and moving the payload (including payload 200) along said cluster guide 145 formed in at least one of said aircraft units 100 anchored together.

[281] The illustrative embodiments provided of the present invention, examples and description serve only to facilitate understanding of the principles of the claimed invention and are not limiting. Other possible embodiments of the present invention or modifications or improvements to the above embodiments of the present invention will be suggested to a person skilled in the art after reading the above description. The scope of the present invention is limited only by the appended claims.

Claims

1. System for moving a payload, the system characterized in that it comprises: two or more aircraft units, each having a housing provided with one or more air propulsion units designed to enable the aircraft unit to be moved in an airspace and each being provided with one or more guides, wherein each of the aircraft unit guides is designed to have a payload mounted or suspended in a movable manner on it, wherein at least one of the aircraft unit guides is further designed to be detachably connected or anchored to one or more guides of the other aircraft unit by means of one or more anchoring modules, to form a grouping guide,and wherein the system further comprises a control module configured to enable said aircraft devices to be detachably connected or anchored to each other by means of the anchored guides to form a grouped aircraft device, and wherein the system further comprises a payload movement module controlled by the control module and designed to engage with the mounted or suspended payload so as to enable the payload to be moved controllably along the grouping guide formed to a required position relative to at least one of the anchored aircraft devices.

2. System, according to claim 1, characterized in that at least some of the aircraft apparatus guides are arranged parallel to each other, perpendicular to each other and / or at a predetermined angle to each other. Petition 870250091550, dated 07 / 10 / 2025, pp. 170 / 180 2 / 10 3. System according to claim 1, characterized in that at least one of the aircraft apparatus guides is mounted on a rotating device mounted in the aircraft housing so as to enable said at least one guide to rotate by a predetermined angle of rotation.

4. System according to claim 1, characterized in that at least one of said aircraft apparatus guides is rotatably mounted in the aircraft apparatus housing, and the aircraft apparatus housing further comprises an actuation device controlled by the control module and operationally coupled to said at least one guide or configured to interact with said at least one guide so as to enable its rotation by a predetermined angle of rotation.

5. System according to claim 1, characterized in that at least one of said aircraft apparatus guides is configured telescopically, and the aircraft apparatus housing further comprises an actuation device controlled by the control module and operationally coupled to said at least one guide or configured to interact with said at least one guide so as to enable at least its partial extension.

6. System according to claim 5, characterized in that the control module is additionally configured to present control commands to the drive device in order to enable at least partial retraction of said extended guide.

7. System according to claim 1, characterized in that the housing is configured to tilt or rotate by a predetermined angle relative to at least one of said guides.

8. System, according to claim 1, characterized by the fact that the housing is configured to change its shape and / or dimensions.

9. System according to claim 1, characterized in that at least one of said guides is at least partially configured as foldable or flexible.

10. System according to claim 1, characterized in that at least one of said guides is configured in a straight or curved line.

11. System according to claim 1, characterized in that at least one of said guides is configured in the shape of a T, Z, X, Y, inverted U, E, U, N, L, F, O, H, V, inverted L, C or W.

12. System, according to claim 1, characterized in that at least one of said guides is configured to enable the movement of the payload along at least one of the three coordinate axes or configured to move relative to the aircraft housing so as to enable the movement of the payload mounted or suspended on said at least one guide relative to the aircraft housing.

13. System, according to claim 1, characterized in that the housing is additionally provided with one or more controllable work members configured to interact with the payload when actuated so as to enable the mounting or suspension of said payload on at least one of said guides and to enable its movement along said at least one guide during the actuation of said work members and further comprises an actuation device controlled by the control module and operationally coupled to said controllable work members so as to enable the actuation of at least one of them in response to the control commands of the control module.

14. System according to claim 1, characterized in that said aircraft apparatus guides comprise two or more parallel guides designed to cause the payload to be mounted or suspended on them and designed to move said payload substantially rectilinearly along them.

15. System, according to claim 1, characterized in that at least one of said guides comprises two or more portions, and in that at least one of the portions is configured as movable, and in that the housing further comprises a drive device controlled by the control module and operationally coupled to said at least one movable portion of the guide so as to enable its movement relative to the remaining portions of the guide to change the shape of said at least one guide.

16. System according to claim 1, characterized in that said aircraft apparatus guides comprise two distinct guides and a movable connecting guide, each of which is configured to mount or suspend the payload thereon and to move said mounted payload along it, and wherein the aircraft apparatus housing further comprises an actuation device controlled by the control module and operationally coupled to said movable connecting guide so as to enable it to move to connect said guides to each other.

17. System, according to claim 1, characterized in that the payload movement module is a robotic manipulator or gripper configured to grasp and move the payload along the formed grouping guide. Petition 870250091550, dated 10 / 07 / 2025, pp. 173 / 180 5 / 10 18. System according to claim 1, characterized in that the payload movement module is a thruster configured to momentarily exert force on the payload during the actuation of said thruster to move the payload along the assembly guide, and wherein the aircraft housing further comprises a drive device controlled by the control module and operationally coupled to said thruster so as to actuate it.

19. System according to claim 1, characterized in that the aircraft apparatus housing is additionally provided with one or more weight sensors, wherein each of the weight sensors is configured to measure the weight of the payload at one of the points of the payload support structure for payload accommodation, and wherein the weight sensors are configured to provide their readings to the control module, and wherein the control module enables control instructions to be provided to the payload movement module to move the payload along the grouping guide, depending on said weight sensor readings.

20. System according to claim 1, characterized in that the payload movement module is movably mounted on at least one additional guide to move the payload.

21. System according to claim 1, characterized in that the payload movement module is additionally configured to disassemble the payload from the guide.

22. System according to claim 1, characterized in that at least one of said guides is additionally configured to disassemble the payload mounted or suspended on said at least one guide.

23. System, according to claim 14, characterized by the fact that at least one guide has one or more payload disassembly points.

24. System according to claim 1, characterized in that at least one of said anchoring modules is mounted in a movable manner on at least one of said guides.

25. System according to claim 1, characterized in that at least one of said guides is additionally provided with a gripping mechanism designed to grip the payload so as to enable the payload to be mounted or suspended on said at least one guide and designed to move along said at least one guide so as to enable the gripped payload to be moved along said at least one guide.

26. System according to claim 25, characterized in that said gripping mechanism is designed to be rotated to enable rotation of said gripped payload relative to said at least one guide.

27. System according to claim 1, characterized in that at least one of said guides is movable, and wherein the aircraft apparatus housing further comprises a guide movement module controlled by the control module and designed to interact operationally with said at least one movable guide so as to enable the movable guide and the payload mounted or suspended on said at least one movable guide to be moved together.

28. System, according to claim 1, characterized in that the control module is additionally configured to present control commands to the payload movement module so as to enable the movement of the payload from the aircraft unit to be undocked to at least one of the remaining aircraft units docked to each other during the presence of the aircraft units in the airspace.

29. System, according to claim 1, characterized in that the control module is further configured to present control commands to the payload movement module in order to enable the receipt of the payload from at least one of the remaining docked aircraft units and to enable the movement of said received payload in the aircraft unit to be undocked during the presence of the aircraft units in the airspace.

30. System according to claim 28, characterized in that the control module additionally enables the direction of an aircraft to be undocked to a parking station for refueling within its range.

31. System according to claim 30, characterized in that the control module additionally enables the docking of the aircraft unit with the refueled range to one of the docked aircraft units.

32. System according to claim 31, characterized in that the control module is additionally configured to provide control commands to the payload movement module of the aircraft unit to be docked so as to enable the movement of the payload from the aircraft unit to be docked to at least one of the docked aircraft units.

33. System, according to claim 28 or 29, characterized in that at least two of the aircraft devices to be docked together are each additionally provided with an additional guide and the control module additionally enables the movement of the payload movement module along an additional grouping guide formed from said additional guides when docking said aircraft devices together.

34. System according to claim 1, characterized in that the anchoring modules are provided at adjacent ends of the anchored guides.

35. System according to claim 34, characterized in that each of the anchored guides is additionally provided with an additional anchoring module at an opposite end thereof, the additional anchoring module being designed to be anchored to a guide of an additional aircraft apparatus.

36. System according to claim 34, characterized in that at least some of the anchored guides of the aircraft apparatus are positioned perpendicular to each other or positioned at an angle to each other, and the anchoring modules provided at the ends of the anchored guides are designed to be connected or anchored in a detachable manner to the anchored guides of two or more other aircraft apparatus so as to define a payload movement pattern.

37. System according to claim 1, characterized in that at least one of the anchored guides is designed to be used for mounting or suspending a first payload on it and to enable the first payload to be moved along at least one guide, and at least one other guide of the anchored guides is designed to be used for mounting or suspending a second payload on it and to enable the second payload to be moved along at least one other guide.

38. System, according to claim 1, characterized in that the aircraft device housing is additionally provided with one or more docking modules, and each of the docking modules is designed to enable one aircraft device housing to be detachably connected to a housing of another aircraft device.

39. Method for moving a payload, the method characterized in that it comprises: detachably anchoring in an airspace, under the control of a control module, at least one of the guide rails of a first aircraft unit to at least one of the guide rails of a second aircraft unit to form a grouping guide rail composed of the anchored guide rails and to form a grouping aircraft unit composed of the first and second aircraft units anchored to each other by the anchored guide rails; and providing the engagement of a payload movement module controlled by the control module with a payload mounted or suspended on at least one guide rail of the grouping guide rail formed, so as to move the payload along the grouping guide rail to a required position on the grouping guide rail relative to at least one of the anchored aircraft units.

40. Method according to claim 39, characterized in that it further comprises rotating the payload relative to the grouping guide before the payload moves in the grouping guide.

41. Method, according to claim 39, characterized in that it further comprises detachably anchoring in an airspace, under the control of a control module, a guide of an additional aircraft apparatus to an anchoring module provided at one of the opposite free ends of the grouping guide formed so as to form an extended grouping guide and an extended grouping aircraft apparatus composed of the previously formed grouping aircraft apparatus and the additional aircraft apparatus, and moving, under the control of the control module, the payload along the extended grouping guide of the extended grouping aircraft apparatus.

42. Method according to claim 39, characterized in that it further comprises anchoring the aircraft fixture housings by means of the anchoring modules provided in the corresponding anchored aircraft fixture housings.

Images