Unmanned aerial vehicle array square matrix net

By setting up connection components and interleaved connecting ropes on the drone to form a connecting rope net, the problem of insufficient drone carrying capacity is solved and the application range of drones is expanded.

CN120270555AInactive Publication Date: 2025-07-08阎东明
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202510627910.0
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-05-15
Publication Date
2025-07-08
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

The existing drone has limited capacity to carry, which limits its application range.

Method used

A drone array square array network is designed to form a connecting rope network by setting connection components on the drone and connecting crisscrossed connecting ropes through the connection components to form a connecting rope network, providing users with a wider equipment mounting platform.

Benefits of technology

It has expanded the application range of drones, allowing them to carry more, larger and heavier equipment, maintaining the flexibility of drones.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN120270555A_ABST
    Figure CN120270555A_ABST
Patent Text Reader

Abstract

The invention relates to the field of unmanned aerial vehicles, and particularly discloses an unmanned aerial vehicle array square matrix net. According to the unmanned aerial vehicle, the connecting assemblies are arranged on the unmanned aerial vehicle, the crisscrossed connecting ropes are connected through the connecting assemblies to form the connecting rope net, a wider equipment carrying platform is provided for a user, the user can carry various objects such as a placement barrel on the connecting rope net, and the unmanned aerial vehicle has the flexibility of the unmanned aerial vehicle and also can carry various objects on the placement barrel. And compared with an unmanned aerial vehicle, the unmanned aerial vehicle can carry more equipment with larger volume and heavier weight, and the application range of users can be effectively expanded.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The present invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle array square network. Background Art

[0002] An unmanned aerial vehicle is an unmanned aircraft remotely controlled by radio or autonomously programmed, with the characteristics of strong flexibility and adaptability to complex environments. With the development and progress of unmanned aerial vehicle technology, the application fields of unmanned aerial vehicles have gradually expanded. For example, unmanned aerial vehicles are used in many fields such as aerial photography, agriculture, logistics, and disaster relief during operation.

[0003] However, existing unmanned aerial vehicles basically operate individually, and the load capacity of a single unmanned aerial vehicle is limited. As a result, the unmanned aerial vehicle can only carry some small-sized and light-weight objects, restricting the application scope of the unmanned aerial vehicle. Therefore, it is necessary to improve the existing unmanned aerial vehicle, expand the application platform of the unmanned aerial vehicle, so that the unmanned aerial vehicle can carry and use more objects. Summary of the Invention

[0004] In order to overcome the deficiencies of the prior art, the purpose of the present invention is to provide an unmanned aerial vehicle array square network to solve the problem that the existing unmanned aerial vehicle has limited carrying capacity and restricts the use of the unmanned aerial vehicle.

[0005] To achieve the above purpose, the present invention provides the following technical solutions:

[0006] An unmanned aerial vehicle array square network, comprising:

[0007] Unmanned aerial vehicles, there are multiple of them, and each of the unmanned aerial vehicles is provided with a connection component at the bottom;

[0008] Connection ropes, there are multiple of them, and the multiple connection ropes are arranged vertically and horizontally in a criss-cross manner, and the connection ropes at the intersection are connected to the unmanned aerial vehicles through the connection components;

[0009] Placement cylinders, connected to the connection ropes.

[0010] Preferably, the connection component includes a threaded rod fixedly installed on the unmanned aerial vehicle, a threaded ring threadedly connected to the threaded rod, and an installation ring rotatably connected to the lower end of the threaded ring. A plurality of bent rods are equidistantly connected in an annular array at the lower end of the installation ring. A through hole is opened on the unmanned aerial vehicle. The bent rods pass through the through hole and extend below the unmanned aerial vehicle. The bent rods are bent outward, and a resisting rod is fixedly connected to the lower end of the bent rod. A plurality of clamping blocks are fixedly connected to the bottom of the unmanned aerial vehicle and are arranged equidistantly in an annular array. The connection rope is clamped between the clamping blocks. A sliding groove is opened on the clamping block, and the resisting rod is inserted into the sliding groove.

[0011] Preferably, the end of the resisting rod is provided with a ninety-degree sharp angle.

[0012] Preferably, a first groove is formed on one side of the end of the abutting rod, a magnet is fixedly connected inside the first groove, a second groove is formed on the other side of the end of the abutting rod, an iron block is slidably connected inside the second groove, a pulling groove is formed on the abutting rod, and a pull rod fixedly connected to the iron block is inserted inside the pulling groove.

[0013] Preferably, an arc-shaped clamping groove is formed on the iron block, and a limiting rod fixedly connected to the inner wall of the second groove is inserted inside the clamping groove.

[0014] Preferably, a receiving groove is formed on the iron block, a spring is arranged inside the receiving groove, one end of the spring is connected to the inner wall of the second groove, and the other end is connected to the iron block.

[0015] Preferably, the abutting rod is made of a metal rigid material.

[0016] Preferably, the material of the connecting rope includes metal and synthetic fiber.

[0017] Compared with the prior art, the beneficial effects of the present invention are as follows:

[0018] By arranging a connecting component on the unmanned aerial vehicle and connecting criss-crossing connecting ropes through the connecting component to form a connecting rope net, the present invention provides a wider equipment carrying platform for the user. The user can carry various items such as placing cylinders on the connecting rope net, which not only has the flexibility of the unmanned aerial vehicle but also can carry more equipment with larger volume and heavier mass than the unmanned aerial vehicle, effectively expanding the application range of the user. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 is a schematic diagram of the overall structure of the present invention Figure 1 ;

[0020] Figure 2 is a schematic diagram of the overall structure of the present invention Figure 2 ;

[0021] Figure 3 is a schematic diagram of the structure of the unmanned aerial vehicle of the present invention;

[0022] Figure 4 is a schematic diagram of the sectional structure of the connecting component of the present invention;

[0023] Figure 5 is a schematic diagram of the structure of the bent rod of the present invention Figure 1 ;

[0024] Figure 6 is a schematic diagram of the structure of the bent rod of the present invention Figure 2 ;

[0025] Figure 7Schematic cross-sectional structure diagram of the abutting rod of the present invention;

[0026] In the figure: 1, unmanned aerial vehicle; 2, connecting component; 21, threaded rod; 22, threaded ring; 23, mounting ring; 24, bent rod; 25, abutting rod; 26, clamping block; 27, chute; 28, magnet; 29, iron block; 30, clamping groove; 31, limiting rod; 32, spring; 33, pulling groove; 34, pulling rod; 3, connecting rope; 4, placing cylinder. Specific implementation mode

[0027] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0028] Embodiment 1:

[0029] Please refer to Figure 1 - Figure 7 As shown, a drone array square network includes:

[0030] A plurality of unmanned aerial vehicles 1 are provided, and a connecting component 2 is provided at the bottom of each unmanned aerial vehicle 1;

[0031] A plurality of connecting ropes 3 are provided, and the plurality of connecting ropes 3 are arranged vertically and horizontally in a crisscross manner, and the connecting ropes 3 at the intersections are connected to the unmanned aerial vehicle 1 through the connecting component 2;

[0032] A placing cylinder 4 is connected to the connecting rope 3.

[0033] As can be seen from the above, by providing the connecting component 2 on the unmanned aerial vehicle 1 and connecting the vertically and horizontally crisscrossing connecting ropes 3 through the connecting component 2 to form a connecting rope network, a wider equipment carrying platform is provided for the user. The user can carry various items such as placing cylinders on the connecting rope network, which not only has the flexibility of the unmanned aerial vehicle 1, but also can carry more equipment with larger volume and heavier mass than the unmanned aerial vehicle 1, and can effectively expand the application range of the user.

[0034] Please refer to Figure 3 - Figure 4As shown in the figure, the connecting component 2 includes a threaded rod 21 fixedly installed on the drone 1, a threaded ring 22 threadedly connected to the threaded rod 21, and a mounting ring 23 rotatably connected to the lower end of the threaded ring 22. A plurality of bent rods 24 are evenly connected to the lower end of the mounting ring 23 at equal intervals in a circular array. A through hole is formed in the drone 1, and the bent rods 24 pass through the through hole and extend below the drone 1. The bent rods 24 are bent outward, and a resisting rod 25 is fixedly connected to the lower end of the bent rod 24. A plurality of clamping blocks 26 are fixedly connected to the bottom of the drone 1 and are arranged at equal intervals in a circular array. The connecting rope 3 is clamped between the clamping blocks 26. A sliding groove 27 is formed in the clamping block 26, and the resisting rod 25 is inserted into the sliding groove 27.

[0035] As can be seen from the above, after the connecting rope 3 is clamped between the clamping blocks 26, the threaded ring 22 can be rotated. The threaded ring 22 will slide on the threaded rod 21. At this time, the threaded ring 22 will drive the mounting ring 23 and the bent rod 24 to move upward. The upward moving bent rod 24 moves inside the through hole. Due to the small size of the through hole, under the blocking action of the through hole, the bent rod 24 gradually rotates and straightens. At this time, the resisting rod 25 at the end of the bent rod 24 will rotate and insert into the sliding groove 27. Finally, the ends of the plurality of resisting rods 25 will abut against each other to block the lower outlet of the clamping block 26. At this time, the connecting rope 3 will be stably clamped in the clamping block 26 to keep the connecting rope 3 stable. At the same time, the user can continue to rotate the threaded ring 22 to make the resisting rod 25 keep rising, and finally make the connecting rope 3 be clamped between the drone and the resisting rod 25, further improving the stability of the connecting rope 3.

[0036] Please refer to Figure 5 - Figure 6 As shown in the figure, to facilitate the tight abutment of the ends of the plurality of resisting rods 25 against each other, the ends of the resisting rods 25 are provided with a ninety-degree sharp angle, and the ends of the plurality of resisting rods 25 can be closely attached together.

[0037] A first groove is formed on one side of the end of the resisting rod 25, and a magnet 28 is fixedly connected inside the first groove. A second groove is formed on the other side of the end of the resisting rod 25, and an iron block 29 is slidably connected inside the second groove. A pulling groove 33 is formed on the resisting rod 25, and a pull rod 34 fixedly connected to the iron block 29 is inserted into the pulling groove 33.

[0038] After the ends of the two abutting rods 25 come into contact, the iron block 29 rotates under the attraction of the magnet 28 on the adjacent abutting rod 25. At this time, the iron block 29 on one abutting rod 25 will rotate and insert into the first groove of the other abutting rod 25, and attract together with the magnet 28 in the first groove. At this time, the iron block 29 straddles the two abutting rods 25, which can improve the vertical bearing capacity of the two abutting rods 25, so that the abutting rods 25 can better bear the weight of the connecting rope 3. When the user needs to release the attraction between the magnet 28 and the iron block 29, the iron block 29 can be driven by the pull rod 34 to slide away from the magnet 28. When the iron block 29 slides out of the first groove, the abutting rods 25 are no longer restricted by the iron block 29, and the user can separate the abutting rods 25 and put down the connecting rope 3.

[0039] An arc-shaped slot 30 is formed in the iron block 29, and a limiting rod 31 inserted into the slot 30 is fixedly connected to the inner wall of the second groove. The cooperation between the limiting rod 31 and the slot 30 restricts the movement of the iron block 29, which is convenient for the iron block 29 to rotate and insert into the first groove of the corresponding abutting rod 25 according to the preset moving direction.

[0040] Embodiment 2:

[0041] Please refer to Figure 1 - Figure 7 As shown in the figure, an unmanned aerial vehicle array square net includes:

[0042] A plurality of unmanned aerial vehicles 1, and a connecting component 2 is arranged at the bottom of each unmanned aerial vehicle 1;

[0043] A plurality of connecting ropes 3 are arranged, and the plurality of connecting ropes 3 are arranged vertically and horizontally in a criss-cross manner, and the connecting ropes 3 at the intersections are connected to the unmanned aerial vehicle 1 through the connecting component 2;

[0044] A placing cylinder 4 is connected to the connecting rope 3.

[0045] As can be seen from the above, by arranging the connecting component 2 on the unmanned aerial vehicle 1 and connecting the vertically and horizontally criss-cross connecting ropes 3 through the connecting component 2 to form a connecting rope net, a wider equipment carrying platform is provided for the user. The user can carry a variety of items such as placing cylinders on the connecting rope net, which not only has the flexibility of the unmanned aerial vehicle 1, but also can carry more, larger and heavier equipment than the unmanned aerial vehicle 1, and can effectively expand the application range of the user.

[0046] Please refer to Figure 3 - Figure 4As shown in the figure, the connection component 2 includes a threaded rod 21 fixedly installed on the drone 1, a threaded ring 22 threadedly connected to the threaded rod 21, and a mounting ring 23 rotatably connected to the lower end of the threaded ring 22. A plurality of bent rods 24 are equidistantly connected in an annular array at the lower end of the mounting ring 23. A through hole is formed in the drone 1, and the bent rods 24 pass through the through hole and extend below the drone 1. The bent rods 24 are bent outward, and a resisting rod 25 is fixedly connected to the lower end of the bent rod 24. A plurality of clamping blocks 26 are fixedly connected to the bottom of the drone 1 and are equidistantly arranged in an annular array. The connecting rope 3 is clamped between the clamping blocks 26. A sliding groove 27 is formed in the clamping block 26, and the resisting rod 25 is inserted into the sliding groove 27.

[0047] As can be seen from the above, after the connecting rope 3 is clamped between the clamping blocks 26, the threaded ring 22 can be rotated. The threaded ring 22 will slide on the threaded rod 21. At this time, the threaded ring 22 will drive the mounting ring 23 and the bent rod 24 to move upward. The upward-moving bent rod 24 moves inside the through hole. Due to the small size of the through hole, under the blocking effect of the through hole, the bent rod 24 gradually rotates and straightens. At this time, the resisting rod 25 at the end of the bent rod 24 will rotate and insert into the sliding groove 27. Finally, the ends of the plurality of resisting rods 25 will abut against each other to block the lower outlet of the clamping block 26. At this time, the connecting rope 3 will be stably clamped in the clamping block 26 to keep the connecting rope 3 stable. At the same time, the user can continue to rotate the threaded ring 22 to make the resisting rod 25 keep rising, and finally make the connecting rope 3 be clamped between the drone and the resisting rod 25, further improving the stability of the connecting rope 3.

[0048] Please refer to Figure 5 - Figure 6 As shown in the figure, to facilitate the tight abutment of the ends of the plurality of resisting rods 25, the ends of the resisting rods 25 are provided with a ninety-degree sharp angle, and the ends of the plurality of resisting rods 25 can be closely attached together.

[0049] A first groove is formed on one side of the end of the resisting rod 25, and a magnet 28 is fixedly connected inside the first groove. A second groove is formed on the other side of the end of the resisting rod 25, and an iron block 29 is slidably connected inside the second groove. A pulling groove 33 is formed on the resisting rod 25, and a pull rod 34 fixedly connected to the iron block 29 is inserted into the pulling groove 33.

[0050] After the ends of the two abutting rods 25 come into contact, the iron block 29 rotates under the attraction of the magnet 28 on the adjacent abutting rod 25. At this time, the iron block 29 on one abutting rod 25 rotates and inserts into the first groove of the other abutting rod 25, and is attracted together with the magnet 28 in the first groove. At this time, the iron block 29 straddles the two abutting rods 25, which can improve the vertical bearing capacity of the two abutting rods 25, so that the abutting rods 25 can better bear the weight of the connecting rope 3. When the user needs to release the attraction between the magnet 28 and the iron block 29, the iron block 29 can be driven by the pull rod 34 to slide away from the magnet 28. When the iron block 29 slides out of the first groove, the abutting rods 25 are no longer restricted by the iron block 29, and the user can separate the abutting rods 25 and put down the connecting rope 3.

[0051] An arc-shaped card slot 30 is formed in the iron block 29, and a limiting rod 31 inserted into the inside of the card slot 30 is fixedly connected to the inner wall of the second groove. The cooperation between the limiting rod 31 and the card slot 30 restricts the movement of the iron block 29, which is convenient for the iron block 29 to rotate and insert into the first groove of the corresponding abutting rod 25 according to the preset moving direction.

[0052] Please refer to Figure 7 As shown, a receiving groove is formed in the iron block 29, and a spring 32 is arranged inside the receiving groove. One end of the spring 32 is connected to the inner wall of the second groove, and the other end is connected to the iron block 29. The spring 32 is provided with a pre-tightening force and is in a tensioned state, providing a pulling force for the iron block 29, so that the iron block 29 stays stably inside the second groove without external force.

[0053] To enhance the anti-deformation ability of the abutting rod 25, the abutting rod 25 is made of a metal rigid material.

[0054] The material of the connecting rope 3 includes metal and synthetic fiber, and other materials can also be used. The material needs to have flexibility and strength, be able to deform and not break.

[0055] The standard parts used in the present invention can all be purchased from the market. The special-shaped parts can be customized according to the description in the specification and the drawings. The specific connection methods of each part all adopt conventional means such as bolts, rivets, and welding in the existing technology. The machines, parts, and equipment all adopt conventional models in the existing technology. Coupled with the circuit connection adopting the conventional connection method in the existing technology, it will not be elaborated here. The content not described in detail in this specification belongs to the prior art well-known to those skilled in the art.

[0056] In the description of the present invention, the terms "first" and "second" are used for descriptive purposes only and cannot be construed as indicating or implying relative importance or implicitly specifying the quantity of the indicated technical features. Thus, features defined with "first" and "second" may explicitly or implicitly include one or more of such features. The meaning of "a plurality" is two or more unless specifically defined otherwise.

[0057] In the present invention, unless otherwise clearly defined and limited, the terms "mounted", "connected", "coupled", "fixed", etc. shall be construed broadly. For example, it may be a fixed connection, a detachable connection, or integrated; it may be a mechanical connection or an electrical connection; it may be directly connected or indirectly connected through an intermediate medium, and it may be the communication inside two elements or the interaction relationship between two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0058] In the present invention, unless otherwise clearly defined and limited, the first feature being "on" or "under" the second feature may be that the first and second features are in direct contact, or the first and second features are in indirect contact through an intermediate medium. Moreover, the first feature being "above", "over" and "on top of" the second feature may be that the first feature is directly above or obliquely above the second feature, or merely indicates that the first feature has a higher horizontal height than the second feature. The first feature being "under", "below" and "beneath" the second feature may be that the first feature is directly below or obliquely below the second feature, or merely indicates that the first feature has a lower horizontal height than the second feature.

[0059] In the description of this specification, the descriptions with reference to the terms "one embodiment", "some embodiments", "example", "specific example" or "some examples", etc. mean that the specific features, structures, materials or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the above terms do not have to be directed to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments or examples in a suitable manner. In addition, without contradiction, those skilled in the art may combine and combine the different embodiments or examples described in this specification and the features of different embodiments or examples.

[0060] In the drawings of the disclosed embodiments of the present invention, only the structures related to the disclosed embodiments are involved, and other structures may refer to the general design. Without conflict, the same embodiment and different embodiments of the present invention may be combined with each other.

Claims

1. An unmanned aerial vehicle array square network, characterized in that Including: A plurality of drones (1), each of which is provided with a connection component (2) at the bottom; A plurality of connecting ropes (3), which are arranged vertically and horizontally in a criss-cross manner, and the connecting ropes (3) at the intersection are connected to the drones (1) through the connection components (2); A placement cylinder (4) connected to the connecting rope (3).

2. The drone array square network according to claim 1, characterized in that: The connection component (2) includes a threaded rod (21) fixedly installed on the drone (1), a threaded ring (22) threadedly connected to the threaded rod (21), and a mounting ring (23) rotatably connected to the lower end of the threaded ring (22). A plurality of bent rods (24) are equidistantly connected in a circular array at the lower end of the mounting ring (23). A perforation is formed on the drone (1). The bent rods (24) pass through the perforation and extend below the drone (1). The bent rods (24) are bent outward, and a resisting rod (25) is fixedly connected to the lower end of the bent rod (24). A plurality of clamping blocks (26) arranged equidistantly in a circular array are fixedly connected to the bottom of the drone (1). The connecting rope (3) is clamped between the clamping blocks (26). A sliding groove (27) is formed on the clamping block (26). The resisting rod (25) is inserted into the sliding groove (27).

3. The drone array square network according to claim 2, characterized in that: The end of the resisting rod (25) is provided with a ninety-degree sharp angle.

4. The drone array square network according to claim 3, characterized in that: A first groove is formed on one side of the end of the resisting rod (25), and a magnet (28) is fixedly connected inside the first groove. A second groove is formed on the other side of the end of the resisting rod (25), and an iron block (29) is slidably connected inside the second groove. A pulling groove (33) is formed on the resisting rod (25), and a pulling rod (34) fixedly connected to the iron block (29) is inserted into the pulling groove (33).

5. The drone array square network according to claim 4, characterized in that: An arc-shaped clamping groove (30) is formed on the iron block (29), and a limiting rod (31) fixedly connected to the inner wall of the second groove is inserted into the clamping groove (30).

6. The drone array square network according to claim 4, wherein: A receiving groove is formed on the iron block (29), and a spring (32) is arranged inside the receiving groove. One end of the spring (32) is connected to the inner wall of the second groove, and the other end is connected to the iron block (29).

7. The drone array square network according to claim 2, characterized in that: The resisting rod (25) is made of a metal rigid material.

8. The drone array square network according to claim 1, wherein: The material of the connecting rope (3) includes metal and synthetic fiber.