Drawer type micro aircraft unit mother station capable of being carried by individual soldier

Abstract

The utility model discloses a drawer-type micro aircraft unit mother station capable of being carried by an individual soldier, which comprises a unit mother station cluster jacket, a plurality of unit mother station cabins are arranged on the outer side of the unit mother station cluster jacket, unit mother stations are clamped in the unit mother station cabins, an unmanned aerial vehicle cabin is arranged at the top of each unit mother station, and an unmanned aerial vehicle is arranged in each unmanned aerial vehicle cabin. An integrated antenna placement groove is formed in one side of the unit mother station, an integrated antenna is clamped in the integrated antenna placement groove, the miniature unmanned aerial vehicle mother station is improved in a miniaturized and integrated mode, the bearing burden of an individual soldier can be remarkably reduced, more unmanned aerial vehicles are loaded in a small space, and the unmanned aerial vehicle mother station is more convenient to carry. Therefore, large-capacity and multi-level battlefield information can be obtained with small investment for decision making.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the micro unmanned plane mother station technical field, concretely is a single soldier can bear the drawer type micro aircraft unit mother station. BACKGROUND

[0002] The essence of the micro unmanned plane mother station is a nest for storing unmanned planes, which protects the unmanned planes from mechanical damage and adverse environmental influences and can charge the unmanned planes.

[0003] The individual power limitation of the traditional micro unmanned plane results in a small distance for the combat personnel to control the unmanned plane. A relay base station is needed to amplify the signal of the unmanned plane, so that the combat personnel can control the unmanned plane remotely at a farther distance.

[0004] However, the traditional micro unmanned plane storage nest is large in size, and the number of the nests that a single soldier can carry is limited, which is not cost-effective for scenarios that require a large number of micro unmanned planes to work together. UTILITY MODEL CONTENTS

[0005] The utility model aims to provide a single soldier can bear the drawer type micro aircraft unit mother station to solve the problems raised in the above background.

[0006] The utility model adopts the following technical scheme:

[0007] A single soldier can bear the drawer type micro aircraft unit mother station, which comprises a unit mother station cluster outer cover, a plurality of unit mother station cabins are formed on the outer side of the unit mother station cluster outer cover, a unit mother station is clamped in the unit mother station cabin, a unmanned plane cabin is formed on the top of the unit mother station, a unmanned plane is arranged in the unmanned plane cabin, an integrated antenna placing groove is formed on one side of the unit mother station, and an integrated antenna is clamped in the integrated antenna placing groove.

[0008] Preferably, the unit mother station cluster outer cover adopts a circular structure, the unit mother station cabin adopts a fan-shaped structure, and the plurality of unit mother station cabins are arranged in a ring array, and the unit mother station adopts a fan-shaped structure.

[0009] Preferably, a unit mother station buckle is arranged on the side of the unit mother station away from the integrated antenna placing groove, a buckle clamping groove is formed in the unit mother station cabin in correspondence, a clamping block of the unit mother station buckle is clamped in the buckle clamping groove, and the clamping block is limited by a clamping edge.

[0010] Preferably, an integrated antenna clamping groove is arranged at the inner end of the integrated antenna placing groove, the integrated antenna is clamped in the integrated antenna clamping groove, and a USB socket is arranged at the outer end of the integrated antenna placing groove.

[0011] Preferably, the integrated antenna comprises a command control communication antenna, a UBS plug is arranged at the rear end of the command control communication antenna and rotates by 90 degrees, the rear end of the command control communication antenna is clamped in the integrated antenna clamping groove, and a control instruction communication antenna is arranged on the upper side of the command control communication antenna.

[0012] Therefore, the unmanned aerial vehicle mother station has the advantages that:

[0013] In the utility model, the unmanned aerial vehicle mother station is improved in small size and integration, the burden of a single soldier can be reduced obviously, more unmanned aerial vehicles can be loaded in a small space, and large capacity and multi-level battlefield information can be obtained with small investment for decision making. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 It is an overall structure schematic view of the utility model;

[0015] Figure 2 It is a unit mother station cluster outer sleeve structure schematic view of the utility model;

[0016] Figure 3 It is an integrated antenna storage structure schematic view of the utility model;

[0017] Figure 4 It is an integrated antenna split structure schematic view of the utility model;

[0018] Figure 5 It is an integrated antenna structure schematic view of the utility model; Figure 1

[0019] Figure 6 It is an integrated antenna structure schematic view of the utility model; Figure 2

[0020] Figure 7 It is an integrated antenna installation structure schematic view of the utility model;

[0021] Figure 8 It is a unit mother station buckle loosening state schematic view of the utility model;

[0022] Figure 9 It is a unit mother station buckle tightening state schematic view of the utility model under the action of external pressure;

[0023] Figure 10 It is a unit mother station cabin structure schematic view of the utility model;

[0024] Figure 11 It is a unit mother station buckle installation structure schematic view of the utility model;

[0025] Figure 12 ​​The use state schematic view of the utility model;

[0026] Figure 13 The control flow chart of the utility model;

[0027] In the drawing: 1, unit mother station; 2, unit mother station buckle; 3, unit mother station cabin; 4, unit mother station cluster outer cover; 5, unmanned aerial vehicle cabin; 6, integrated antenna installation groove; 7, integrated antenna; 8, unmanned aerial vehicle; 9, USB socket; 10, command control communication antenna; 11, control instruction communication antenna; 12, UBS plug; 13, card edge; 14, buckle card slot; 15, integrated antenna card slot. DETAILED DESCRIPTION

[0028] The specific embodiment of the utility model is explained in detail below.

[0029] The "range" disclosed by the utility model is limited in the form of lower limit and upper limit, and the given range is limited by selecting a lower limit and an upper limit. The selected lower limit and upper limit define the boundaries of the specific range. The range defined in this way can include or not include end values, and can be arbitrarily combined, that is, any lower limit can be combined with any upper limit to form a range. For example, if a range of 10-50 is listed for a specific parameter, it is understood that the ranges of 10-40 and 20-50 are also expected. In addition, if the minimum range values 1 and 2 are listed, and if the maximum range values 3, 4 and 5 are listed, the following ranges can all be expected: 1-3, 1-4, 1-5, 2-3, 2-4 and 2-5. In this application, unless otherwise stated, the range of values "a-b" represents a shorthand representation of any real number combination between a and b, where a and b are real numbers. For example, the value range "0-5" means that all real numbers between "0-5" have been listed in this document, and "0-5" is only a shorthand representation of these value combinations.

[0030] Unless otherwise specified, all embodiments and optional embodiments of the present application can be combined with each other to form new technical solutions.

[0031] Unless otherwise specified, all technical features and optional technical features of the present application can be combined with each other to form new technical solutions.

[0032] If there is no special description, all steps of the present application can be carried out in sequence, or randomly, preferably in sequence. For example, the method comprises steps (a) and (b), which means that the method can comprise steps (a) and (b) in sequence, or steps (b) and (a) in sequence. For example, the method also comprises step (c), which means that step (c) can be added to the method in any order, for example, the method can comprise steps (a), (b) and (c), or steps (a), (c) and (b), or steps (c), (a) and (b), etc.

[0033] If there is no special description, the "includes" and "contains" mentioned in the present application mean open or closed. For example, "includes" and "contains" can mean that other components not listed can also be included or contained, or only the listed components can be included or contained.

[0034] If there is no special description, the reaction is carried out under normal temperature and pressure conditions.

[0035] If there is no special description, all parts or percentages are weight parts or weight percentages.

[0036] In the present application, all the substances used are known substances, which can be purchased or synthesized by known methods.

[0037] In the present application, all the devices or equipment used are conventional devices or equipment known in the field, which can be purchased.

[0038] In order to make the purpose, technical scheme and advantages of the present application more clear, the present application will be further described in detail below with reference to the drawings and examples. It should be understood that the specific examples described herein are only used to explain the present application and do not limit the present application.

[0039] Embodiment:

[0040] A single soldier can carry a drawer type micro air vehicle unit mother station, as shown in Figures 1-12 The unit mother station cluster cover 4 is provided with a plurality of unit mother station cabins 3 on the outside, and the unit mother station 1 is clamped in the unit mother station cabin 3. The unit mother station 1 is provided with a UAV cabin 5 on the top, and the UAV 8 is arranged in the UAV cabin 5. The unit mother station 1 is provided with an integrated antenna placement groove 6 on one side, and the integrated antenna 7 is clamped in the integrated antenna placement groove 6.

[0041] In one possible embodiment, the unit mother station cluster cover 4 adopts a circular structure, the unit mother station cabin 3 adopts a fan-shaped structure, and the plurality of unit mother station cabins 3 adopt a ring array distribution, and the unit mother station 1 adopts a fan-shaped structure.

[0042] In a possible implementation, the unit mother station 1 is provided with a unit mother station buckle 2 on one side away from the integrated antenna installation slot 6, and the unit mother station cabin 3 is correspondingly provided with a buckle clamping groove 14, the clamping block of the unit mother station buckle 2 is clamped in the buckle clamping groove 14, and is limited by the clamping edge 13.

[0043] In a possible implementation, the integrated antenna installation slot 6 is provided with an integrated antenna clamping groove 15 at the inner end, the integrated antenna 7 is clamped at the rear end in the integrated antenna clamping groove 15, and the integrated antenna installation slot 6 is provided with a USB socket 9 at the outer end.

[0044] In a possible implementation, the integrated antenna 7 includes a command and control communication antenna 10, the command and control communication antenna 10 is rotatably provided with a UBS plug 12 at the rear end, the rotation angle of the UBS plug 12 is 90°, the command and control communication antenna 10 is clamped at the rear end in the integrated antenna clamping groove 15, and the command and control communication antenna 10 is provided with a control instruction communication antenna 11 on the upper side.

[0045] In a possible implementation, the micro unmanned aerial vehicle mother station is a fan-shaped metal container like a drawer, the container is an electromechanical device, the electronic system core of which includes two transceiving antennas and a circuit board. For specific architecture and three-dimensional structure, please refer to the drawing description below.

[0046] In a possible implementation, the two transceiving antennas of the mother station, one of which is used for communication with the operators outside the station or other command and control platforms; the other is mainly used for communication with the unmanned aerial vehicles performing tasks away from the station. The main function of the circuit board is to perform time synchronization of multiple unmanned aerial vehicles; exchange data between the command and control platform, the unit mother station and the micro aerial vehicles outside the station; monitor the humidity and temperature outside the station in real time to determine whether the current environment is most suitable for the unmanned aerial vehicles to perform tasks; charge the returning aerial vehicles.

[0047] In a possible implementation, the angle of the unit mother station is 120°, 90°, 60°, 45° or other angles, a certain number of micro unmanned aerial vehicles are stored in each fan-shaped container, and when more unmanned aerial vehicles are needed for combat tasks, the fan-shaped containers can be spliced together to form a circular combined mother station for carrying or launching.

[0048] The specifications of the host cabin of the unmanned aerial vehicles stored in each fan-shaped mother station can be replaced to place different numbers and different models of micro unmanned aerial vehicles.

[0049] In a possible implementation, the antenna of the mother station is in the form of a pluggable USB interface, and the two transceiving antennas are integrated together and connected to the interface of the recess on one side of the unit mother station through a USB plug to be connected with the internal circuit board. This form can replace the antenna of different frequency bands as needed, preventing interference between different mother stations and the communication channel with the outside world. When the antenna is not in use, the USB plug can be pulled out and folded to be stored in the recess.

[0050] Working principle, refer to Figures 1-12 When in use, after the soldier carries the circular mother station cluster cover containing 8 fan-shaped unit mother stations to the designated combat location, the circular mother station cluster cover is placed at the designated position. Since the buckle 2 of the fan-shaped unit mother station 1 is clamped by the clamping edge 13 of the fan-shaped unit mother station cluster cover 4, the edge of the buckle 2 needs to be pinched by hand to make it disengage from the blocking of the clamping edge 13, so that the fan-shaped unit mother station 1 can be separated from the cluster cover unit mother station cabin 3, then the integrated antenna 7 is taken out from the integrated antenna clamping slot 15 of the integrated antenna installation slot 6 on the side of the unit mother station, the USB plug 12 of the integrated antenna 7 is rotated to be perpendicular to the integrated antenna 7 itself, the USB plug 12 is inserted into the USB plug 9 of the antenna installation slot, so as to complete the setting of the quasi-working state of the fan-shaped unit mother station 1.

[0051] The control of the micro unmanned plane by the station external command control platform is shown in the specific control flow chart as Figure 13 The two antenna command control communication antennas 10 on the integrated antenna 7 are connected together through the internal circuit together with the micro unmanned plane control instruction communication antenna 11.

[0052] The above is only a preferred embodiment of the present application, and is not used to limit the present application, and any modification, equivalent replacement and improvement made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A man-portable drawer micro aerial vehicle unit mother station, characterized by: Including unit mother station cluster outer sleeve (4), the unit mother station cluster outer sleeve (4) outside is provided with a plurality of unit mother station cabin (3), the unit mother station cabin (3) is provided with unit mother station (1), the unit mother station (1) top is provided with unmanned aerial vehicle cabin (5), the unmanned aerial vehicle cabin (5) is provided with unmanned aerial vehicle (8), the unit mother station (1) one side is provided with integrated antenna setting groove (6), the integrated antenna setting groove (6) is provided with integrated antenna (7).

2. A single soldier backpackable drawer micro aerial vehicle unit mother station according to claim 1, characterized in that: The unit mother station cluster outer sleeve (4) adopts a circular structure, the unit mother station cabin (3) adopts a fan-shaped structure, and a plurality of unit mother station cabins (3) adopt an annular array distribution, and the unit mother station (1) adopts a fan-shaped structure.

3. A single soldier backpackable drawer micro aerial vehicle unit mother station as in claim 1, wherein: The unit mother station (1) is provided with a unit mother station buckle (2) away from the integrated antenna setting groove (6) on one side, the unit mother station cabin (3) is provided with a buckle slot (14) corresponding, the clamping block of the unit mother station buckle (2) is clamped in the buckle slot (14), and is limited by the clamping edge (13).

4. A single soldier backpackable drawer micro aerial vehicle unit mother station as in claim 1, wherein: The integrated antenna setting groove (6) is provided with an integrated antenna slot (15) at the inner end, the integrated antenna (7) is clamped at the rear in the integrated antenna slot (15), and the integrated antenna setting groove (6) is provided with a USB socket (9) at the outer end.

5. A single soldier backpackable drawer micro aerial vehicle unit mother station as in claim 4, wherein: The integrated antenna (7) includes a command control communication antenna (10), the command control communication antenna (10) is provided with a UBS plug (12) at the rear end, the UBS plug (12) rotates at an angle of 90°, the command control communication antenna (10) is clamped at the rear in the integrated antenna slot (15), and the command control communication antenna (10) is provided with a control instruction communication antenna (11) on the upper side.

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