Folding wing unmanned aerial vehicle cluster launching device

Abstract

The invention relates to the technical field of unmanned aerial vehicles, and provides a folding wing unmanned aerial vehicle cluster launching device which comprises a storage bin and a group launching shell, a monitoring component is arranged on the surface of the storage bin, a plurality of electric sliding tables are fixedly connected to the inner bottom wall of the storage bin, and the electric sliding tables are used for being connected with the group launching shell. A plurality of moving parts matched with the electric sliding table are arranged at the bottom of the group-sending shell, two adjusting parts are arranged on the surface of the group-sending shell, and a pause frame is arranged on the surface of each adjusting part. And during recycling, air is injected into the storage opening through the air compressor, the storage plate slides in the limiting sliding groove through the limiting sliding block and stays at the top end of the storage opening, when the unmanned aerial vehicle is parked on the storage plate, the air compressor is stopped, the storage plate falls, and the unmanned aerial vehicle is recycled.

Description

Technical Field

[0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a folding-wing unmanned aerial vehicle cluster launching device. Background Art

[0002] With the continuous development of artificial intelligence technology, the combat style of drones has gradually evolved from "single-handed combat" to "cluster intelligence". Through close collaboration between individual units, drone clusters can conduct tactical deception, scan battlefield environments, implement multi-domain strikes, and so on.

[0003] Known Chinese public authorized patent: (publication number: CN209521880U) discloses a folding-wing UAV cluster launching device, which includes a plurality of gas storage modules connected together in a stacked arrangement, and a launching tube sealed and installed on the gas storage module on the same side in a one-to-one correspondence; the gas storage module includes a gas storage shell, a gas storage shell base installed at the rear end of the gas storage shell, a solenoid valve connected to the lower part of the gas storage shell base for controlling the connection of compressed air, and a compressed air interface connected to the back of the gas storage shell base; a core sleeve is coaxially installed in the inner cavity of the gas storage shell; an air duct for connecting the inner cavity of the core sleeve with the compressed air interface is opened in the gas storage shell base.

[0004] However, in the implementation of relevant technologies, it is found that the above-mentioned folding-wing UAV cluster launch device has the following problems: its UAV is launched once, and if the launched UAV needs to be recovered, two or even more sets of equipment are generally required to coordinate the launch and recovery tasks, which brings about problems such as high cost, poor maneuverability and concealment, and it is impossible to complete the launch and recovery of multiple UAVs within a limited time;

[0005] Therefore, a folding-wing UAV cluster launching device is proposed. Summary of the invention

[0006] The present invention proposes a folding-wing UAV cluster launching device, which solves the problem in the related technology that the human-machine single launch is required. If the launched UAV needs to be recovered, two or even more sets of equipment are generally required to coordinately complete the launching and recovery tasks, which brings about the problems of high cost, poor maneuverability and concealment, and the problem that multiple UAVs cannot be launched and recovered within a limited time.

[0007] The technical solution of the present invention is as follows: A folding-wing UAV cluster launch device comprises: a storage compartment and a cluster launch shell;

[0008] The surface of the storage bin is provided with a monitoring component, the bottom wall of the storage bin is fixedly connected with a plurality of electric slides, the electric slides are used to connect the hair group shell, the bottom of the hair group shell is provided with a plurality of groups of moving components cooperating with the electric slides, the surface of the hair group shell is provided with two groups of adjustment components, and the surface of the adjustment components is provided with a pause rack;

[0009] The inner wall of the suspension rack is provided with two sets of recovery parts, and the recovery parts include a receiving plate slidably connected to the inner wall of the suspension rack, an electric telescopic rod 1 fixedly connected to the bottom of the suspension rack, a connecting block fixedly connected to the output end of the electric telescopic rod 1, and a miniature radar fixedly connected to the surface of the receiving plate;

[0010] The surface of the hair-bearing shell is provided with a plurality of storage openings, the interiors of the storage openings are all provided with automatic recovery components, and the interior of the hair-bearing shell is provided with a chamber cooperating with the automatic recovery components.

[0011] Optionally, the monitoring component includes a base shell fixedly connected to the surface of the storage bin, a rotating seat rotatably connected to the surface of the base shell, a radar fixedly connected to the surface of the rotating seat, and a driving member arranged on the inner wall of the storage bin.

[0012] Optionally, the driving member includes a sliding groove 1 opened on the inner surface of the storage bin, a sliding base block slidably connected to the inner wall of the sliding groove 1, a rack fixedly connected to the surface of the sliding base block, a gear fixedly connected to the bottom center of the rotating seat, and an electric telescopic rod 2 fixedly connected to the inner surface of the storage bin;

[0013] The rack is meshed and connected with the gear, and the output end of the second electric telescopic rod is fixedly connected with the rack.

[0014] Optionally, the moving component includes a storage cavity provided at the bottom of the group hair shell, a second sliding groove provided on the inner wall of the storage cavity, a sliding bar slidably connected to the inner wall of the second sliding groove, a frame fixedly connected to one side of the sliding bar, a universal wheel rotatably connected to the inner wall of the frame, and a damper fixedly connected to the inner surface of the storage cavity;

[0015] One end of the damper is fixedly connected to the frame, a spring is provided at the center of the storage cavity, one end of the spring is connected to the inner wall of the storage cavity, and the other end of the spring is fixedly connected to one side of the frame.

[0016] Optionally, the adjustment component includes a slot opened on the side surface of the group hair shell, a sliding rod fixedly connected to the inner wall of the slot, a screw rod rotatably connected to the inner wall of the slot, a moving block threadedly connected to the surface of the screw rod, and a motor fixedly connected to the end surface of the group hair shell;

[0017] The output end of the motor is fixedly connected to one end of the screw rod, a sliding opening matching the sliding rod is provided on the surface of the moving block, the moving block is slidably connected to the sliding rod through the sliding opening, and the suspension frame is installed on one side of the moving block.

[0018] Optionally, the automatic recovery component includes a limiting slide groove opened on the inner wall of the storage port, a limiting slider slidably connected to the inner wall of the limiting slide groove, a storage plate fixedly connected to one side of the limiting slider, and an air compressor.

[0019] Optionally, an electrode is provided on the lower surface of the storage plate, and a wireless charging coil is provided inside the storage plate.

[0020] Optionally, an air inlet is provided on the surface of the chamber, and an air inlet fan is fixedly connected to the inner wall of the air inlet.

[0021] Optionally, a Velcro is fixedly connected to the inner wall of the storage bin, a dehumidification bag is fixedly connected to a sub-surface of the Velcro, and a rubber block is fixedly connected to one side of the bottom of the group hair shell.

[0022] Optionally, a mounting seat is provided at the bottom of the storage bin, and the mounting seat includes a base, a pedestal and a shock absorber;

[0023] A plurality of mounting openings are provided on the surface of the base, the base is fixedly connected to the bottom of the storage bin, and the shock absorber is arranged between the base and the bottom.

[0024] Optionally, a base frame is fixedly connected to the surface of the drone, a battery compartment is fixedly connected to the surface of the base frame, a heat dissipation port is opened on the end surface of the battery compartment, and a dustproof net is fixedly connected to the inner wall of the heat dissipation port;

[0025] The surface of the base frame is fixedly connected to a fixed frame, the surface of the fixed frame is rotatably connected to a rotating shaft 1, the surface of the rotating shaft 1 is fixedly connected to a rotating frame 1, the surface of the rotating frame 1 is rotatably connected to a rotating shaft 2, the surface of the rotating shaft 2 is fixedly connected to a rotating frame 2, the surface of the rotating frame 2 is fixedly connected to a camera, and the surface of the rotating frame 1 is fixedly connected to two groups of symmetrically arranged adjusting members;

[0026] The adjusting member comprises a motor fixedly connected to a surface of the rotating frame, a bearing fixedly connected to an outer surface of the rotating frame, a rotating shaft fixedly connected to an inner ring of the bearing, and an adjusting strip fixedly connected to an end surface of the rotating shaft, wherein a plurality of adjusting holes are provided on the surface of the adjusting strip;

[0027] The surface of the rotating frame 2 is rotatably connected to a pull rod 1 that matches the adjusting member, and the surface of the fixed frame is rotatably connected to a pull rod 2 that matches the adjusting member.

[0028] The working principle and beneficial effects of the present invention are:

[0029] 1. The structure of the present application is reasonable. The air compressor is used to inject compressed gas into the storage port, so that the storage plate can instantly slide inside the limiting slide groove through the limiting slider, so that the UAV on the surface of the storage plate can be ejected. In addition, when recovering, the air compressor is used to inject gas into the storage port, so that the storage plate can slide inside the limiting slide groove through the limiting slider and stay at the top of the storage port. When the UAV lands on the storage plate, the air compressor is stopped to make the storage plate fall, so that the UAV can be recovered.

[0030] Second, the application is reasonably combined. The rack is slid on the inner wall of the sliding groove through the sliding base block through the electric telescopic rod 2. At the same time, the rack makes the rotating seat rotate inside the base shell through the gear, so as to adjust the direction of the radar, which is convenient for the radar to locate the position of the drone and also convenient for the drone to return. In addition, combined with the micro radar, when the drone is 0-10 meters away from the device, the micro radar on the surface of the receiving plate provides positioning for the drone, which is convenient for the drone to land on the receiving plate;

[0031] 3. The structure of this application is reasonable. The drone is also equipped with a wireless charging coil that cooperates with the wireless charging coil. After the drone is recovered, the wireless charging coil cooperates with the wireless charging coil of the drone to charge it.

[0032] 4. The present application has a reasonable structure. When the UAV is in operation, the motor in the adjustment member drives the adjustment bar to rotate via the rotating shaft, so that the pull rod one pulls the rotating frame two to rotate via the rotating shaft. In addition, the motor drives the adjustment bar to rotate via the rotating shaft, so that the pull rod two pulls the rotating frame one to rotate on the surface of the rotating shaft one, thereby achieving multi-angle adjustment of the camera. BRIEF DESCRIPTION OF THE DRAWINGS

[0033] The present invention is further described in detail below with reference to the accompanying drawings and specific embodiments.

[0034] Figure 1 The three-dimensional structure of the present invention is shown in FIG. Figure 1 ;

[0035] Figure 2 The three-dimensional structure of the present invention is shown in FIG. Figure 2 ;

[0036] Figure 3 It is a schematic cross-sectional structural diagram of the storage bin in the present invention;

[0037] Figure 4 It is a partial cross-sectional structural schematic diagram of the group hair shell in the present invention;

[0038] Figure 5 It is a schematic cross-sectional structure diagram of the group hair shell in the present invention;

[0039] Figure 6 for Figure 1 The enlarged structural diagram at A in the middle;

[0040] Figure 7 for Figure 2 The enlarged structural diagram at B in the middle;

[0041] Figure 8 The three-dimensional structure of the UAV in the present invention is shown in FIG. Figure 1 ;

[0042] Fig. 9 The three-dimensional structure of the UAV in the present invention is shown in FIG. Figure 2 ;

[0043] In the figure: 1. Storage compartment; 2. Base; 3. Group shell; 4. Radar; 5. Inlet fan; 6. Shock absorber; 7. Base; 8. Mounting port; 9. Universal wheel; 10. Electric telescopic rod 1; 11. Rubber block; 12. Rotating seat; 13. Base shell; 14. Motor; 15. Screw; 16. Slot; 17. Pause rack; 18. Receiving plate; 19. Mini radar; 20. Sliding slot 1; 21. Rack; 22. Electric telescopic rod 2; 23. Electric slide; 24. Velcro; 25. Dehumidification bag; 26. Storage cavity; 27. Sliding slot 2; 28. Sliding bar; 29. Damper; 30. Spring; 31. Frame; 32. Storage port; 33. Limiting slide; 34. Storage plate; 35. Air compressor; 36. Chamber; 37. Electrode; 38. Wireless charging coil; 39. Moving block; 40. Sliding rod; 41. Connecting block; 42. Drone; 43. Base; 44. Battery compartment; 45. Fixed frame; 46. Rotating axis 1; 47. Rotating frame 1; 48. Motor; 49. Rotating frame 2; 50. Bearing; 51. Adjustment bar; 52. Camera; 53. Rotating axis 2; 54. Pull rod 1; 55. Pull rod 2; 56. Dust net. DETAILED DESCRIPTION

[0044] The following will be combined with the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0045] Embodiment 1

[0046] See also Figure 1 - Fig. 9 The present invention provides a folding-wing UAV cluster launch device, comprising: a storage compartment 1 and a cluster launch shell 3;

[0047] The surface of the storage bin 1 is provided with a monitoring component, and a plurality of electric slides 23 are fixedly connected to the bottom wall of the storage bin 1. The electric slides 23 are used to connect the hair group shell 3. The bottom of the hair group shell 3 is provided with a plurality of groups of moving components that cooperate with the electric slides 23. The surface of the hair group shell 3 is provided with two groups of adjustment components, and the surface of the adjustment components is provided with a pause frame 17;

[0048] The inner wall of the suspension frame 17 is provided with two sets of recovery parts, which include a receiving plate 18 slidably connected to the inner wall of the suspension frame 17, an electric telescopic rod 10 fixedly connected to the bottom of the suspension frame 17, a connecting block 41 fixedly connected to the output end of the electric telescopic rod 10, and a micro radar 19 fixedly connected to the surface of the receiving plate 18;

[0049] The surface of the hair-bearing shell 3 is provided with a plurality of storage openings 32 , each of which is provided with an automatic recovery component. The hair-bearing shell 3 is provided with a chamber 36 for cooperating with the automatic recovery component.

[0050] Further, the monitoring component includes a base shell 13 fixedly connected to the surface of the storage bin 1, a rotating seat 12 rotatably connected to the surface of the base shell 13, a radar 4 fixedly connected to the surface of the rotating seat 12, and a driving member arranged on the inner wall of the storage bin 1, the driving member includes a sliding groove 20 opened on the inner surface of the storage bin 1, a sliding base block slidably connected to the inner wall of the sliding groove 20, a rack 21 fixedly connected to the surface of the sliding base block, a gear fixedly connected to the bottom center of the rotating seat 12, and an electric telescopic rod 22 fixedly connected to the inner surface of the storage bin 1;

[0051] The rack 21 is meshed and connected with the gear, and the output end of the electric telescopic rod 22 is fixedly connected with the rack 21 .

[0052] Specifically, during use, the rack 21 slides on the inner wall of the sliding groove 20 through the sliding base block through the electric telescopic rod 22. At the same time, the rack 21 rotates the rotating seat 12 inside the base shell 13 through the gear, so as to adjust the direction of the radar 4.

[0053] Furthermore, the moving parts include a storage cavity 26 provided at the bottom of the group hair shell 3, a sliding groove 27 provided on the inner wall of the storage cavity 26, a sliding bar 28 slidably connected to the inner wall of the sliding groove 27, a frame 31 fixedly connected to one side of the sliding bar 28, a universal wheel 9 rotatably connected to the inner wall of the frame 31, and a damper 29 fixedly connected to the inner surface of the storage cavity 26;

[0054] One end of the damper 29 is fixedly connected to the frame 31 . A spring 30 is provided at the center of the storage chamber 26 . One end of the spring 30 is connected to the inner wall of the storage chamber 26 , and the other end of the spring 30 is fixedly connected to one side of the frame 31 .

[0055] Specifically, when the electric slide 23 moves the hair group shell 3 out of the storage bin 1, the spring 30 causes the frame 31 to slide inside the sliding groove 27 via the sliding bar 28, so that the universal wheel 9 inside the frame 31 contacts the ground or the surface of an object, thereby supporting and fixing the hair group shell 3. When shaking occurs, the shaking is slowed down by the spring 30 and the damper 29.

[0056] Furthermore, the adjusting component includes a slot 16 provided on the side surface of the hair group housing 3, a sliding rod 40 fixedly connected to the inner wall of the slot 16, a screw rod 15 rotatably connected to the inner wall of the slot 16, a moving block 39 threadedly connected to the surface of the screw rod 15, and a motor 14 fixedly connected to the end surface of the hair group housing 3;

[0057] The output end of the motor 14 is fixedly connected to one end of the screw rod 15 , and a sliding opening for matching the sliding rod 40 is provided on the surface of the moving block 39 . The moving block 39 is slidably connected to the sliding rod 40 through the sliding opening, and the pause frame 17 is installed on one side of the moving block 39 .

[0058] Specifically, when launching the UAV 42, the UAV 42 at the suspension rack 17 is temporarily suspended. After the launch of the UAVs 42 at other positions is completed, the motor 14 drives the screw rod 15 to rotate, so that the suspension rack 17 is displaced through the moving block 39. After the suspension rack 17 is displaced, the UAV 42 under the original suspension rack 17 is launched.

[0059] Furthermore, the automatic recovery component includes a limiting slide groove 33 opened on the inner wall of the storage port 32, a limiting slider slidably connected to the inner wall of the limiting slide groove 33, a storage plate 34 and an air compressor 35 fixedly connected to one side of the limiting slider, an electrode 37 is provided on the lower surface of the storage plate 34, a wireless charging coil 38 is provided inside the storage plate 34, an air inlet is opened on the surface of the chamber 36, an air inlet fan 5 is fixedly connected to the inner wall of the air inlet, and the drone 42 is also provided with a wireless charging coil that cooperates with the wireless charging coil 38.

[0060] Specifically, the air compressor 35 injects compressed gas into the storage port 32, causing the storage plate 34 to instantly slide inside the limiting slide groove 35 through the limiting slider, thereby ejecting the UAV 42 on the surface of the storage plate 34. When the UAV 42 needs to be recovered, the air compressor 35 injects gas into the storage port 32, causing the storage plate 34 to slide inside the limiting slide groove 35 through the limiting slider, and stay at the top of the storage port 32. When the UAV 42 lands on the storage plate 34, the air compressor 35 is stopped to cause the storage plate 34 to fall. After the UAV 42 is recovered, it is charged through the wireless charging coil 38.

[0061] Furthermore, a Velcro 24 is fixedly connected to the inner wall of the storage bin 1 , a dehumidification bag 25 is fixedly connected to a sub-surface of the Velcro 24 , and a rubber block 11 is fixedly connected to one side of the bottom of the group hair shell 3 .

[0062] Specifically, the dehumidification bag 25 is fixed by the Velcro 24 , and the dehumidification bag 25 absorbs the humid gas inside the storage bin 1 .

[0063] The working process of the present application is as follows: when the electric slide 23 moves the hair group shell 3 out of the storage bin 1, the spring 30 makes the frame 31 slide inside the sliding groove 27 through the sliding bar 28, so that the universal wheel 9 inside the frame 31 contacts the ground or the surface of an object, so as to support and fix the hair group shell 3;

[0064] When launching the drone 42, the air compressor 35 injects compressed gas into the storage port 32, so that the storage plate 34 slides in the limiting slide groove 35 through the limiting slider instantly, so that the drone 42 on the surface of the storage plate 34 is ejected. When launching the drone 42, the drone 42 under the suspension rack 17 is temporarily suspended. When the drone 42 at other positions is launched, the motor 14 drives the screw rod 15 to rotate, so that the suspension rack 17 is displaced through the moving block 39. After the suspension rack 17 is displaced, the drone 42 under the original suspension rack 17 is launched.

[0065] When the drone 42 needs to be recovered, the rack 21 is slid on the inner wall of the sliding groove 20 through the sliding base block by the electric telescopic rod 22. At the same time, the rack 21 rotates the rotating seat 12 inside the base shell 13 through the gear, so as to adjust the direction of the radar 4, so that the radar 4 can locate the position of the drone 42, and it is also convenient for the drone 42 to return. When the drone 42 is 0-10 meters away from the device, the micro radar 19 on the surface of the receiving plate 18 provides positioning for the drone 42, so that the drone 42 can land on the receiving plate 18, and then the motor 14 drives the screw rod 15 to rotate, so that the drone 42 can be recovered by the electric telescopic rod 22. 9 makes the suspension frame 17 move to the top of each storage opening 32, and then the receiving plate 18 is pulled out through the electric telescopic rod 10 through the connecting block 41, so that the drone 42 on the surface of the receiving plate 18 falls into the storage opening 32 through the suspension frame 17. At the same time, the air compressor 35 is used to inject gas into the storage opening 32, so that the storage plate 34 slides in the limiting slide groove 35 through the limiting slider and stays at the top of the storage opening 32. When the drone 42 stops on the storage plate 34, the air compressor 35 is stopped to make the storage plate 34 fall. After the drone 42 is recovered, it is charged through the wireless charging coil 38.

[0066] Embodiment 2

[0067] Based on Example 1, this embodiment includes: a mounting base is provided at the bottom of the storage bin 1, the mounting base includes a base 2, a base 7 and a shock absorber 6, a plurality of mounting openings 8 are provided on the surface of the base 2, the base 7 is fixedly connected to the bottom of the storage bin 1, and the shock absorber 6 is arranged between the base 7 and the base 2.

[0068] The base 2 is installed and fixed by passing bolts through the installation opening 8. When shaking occurs, the shock absorber 6 installed on the base 2 is used to reduce vibration to prevent the storage bin 1 from shaking too much.

[0069] Embodiment 3

[0070] Based on the first and second embodiments, in this embodiment, the following is included: a base frame 43 is fixedly connected to the surface of the drone 42, a battery compartment 44 is fixedly connected to the surface of the base frame 43, a heat dissipation port is opened on the end surface of the battery compartment 44, and a dustproof net 56 is fixedly connected to the inner wall of the heat dissipation port;

[0071] The surface of the base frame 43 is fixedly connected to a fixing frame 45, the surface of the fixing frame 45 is rotatably connected to a rotating shaft 1 46, the surface of the rotating shaft 1 46 is fixedly connected to a rotating frame 1 47, the surface of the rotating frame 1 47 is rotatably connected to a rotating shaft 2 53, the surface of the rotating shaft 2 53 is fixedly connected to a rotating frame 2 49, the surface of the rotating frame 2 49 is fixedly connected to a camera 52, and the surface of the rotating frame 1 47 is fixedly connected to two groups of symmetrically arranged adjusting members;

[0072] The adjusting member includes a motor 48 fixedly connected to the surface of the rotating frame 47, a bearing 50 fixedly connected to the outer surface of the rotating frame 47, a rotating shaft fixedly connected to the inner ring of the bearing 50, and an adjusting strip 51 fixedly connected to the end surface of the rotating shaft, and a plurality of adjusting holes are opened on the surface of the adjusting strip 51;

[0073] A pull rod 1 54 that matches the adjusting member is rotatably connected to the surface of the second rotating frame 49 , and a pull rod 2 55 that matches the adjusting member is rotatably connected to the surface of the fixed frame 45 .

[0074] When the drone 42 is in operation, the motor in the adjustment member drives the adjustment bar 51 to rotate via the rotating shaft, so that the pull rod 1 54 pulls the rotating frame 2 49 to rotate via the rotating shaft 2 53. In addition, the motor drives the adjustment bar 51 to rotate via the rotating shaft, so that the pull rod 2 55 pulls the rotating frame 1 47 to rotate on the surface of the rotating shaft 1 46, thereby achieving multi-angle adjustment of the camera 52. At the same time, the heat dissipation port facilitates air flow to enter the battery compartment 44, thereby achieving the effect of cooling it.

[0075] The advantages of this application are:

[0076] 1. The structure of the present application is reasonable. The air compressor 35 is used to inject compressed gas into the storage port 32, so that the storage plate 34 can instantly slide inside the limiting slide groove 35 through the limiting slider, so that the UAV 42 on the surface of the storage plate 34 can be ejected. In addition, when recovering, the air compressor 35 is used to inject gas into the storage port 32, so that the storage plate 34 can slide inside the limiting slide groove 35 through the limiting slider and stay at the top of the storage port 32. When the UAV 42 lands on the storage plate 34, the air compressor 35 is stopped to make the storage plate 34 fall, so that the UAV 42 can be recovered.

[0077] Second, the application is reasonably combined. The rack 21 slides on the inner wall of the sliding groove 20 through the sliding base block through the electric telescopic rod 22. At the same time, the rack 21 rotates the rotating seat 12 inside the base shell 13 through the gear, so as to adjust the direction of the radar 4, which is convenient for the radar 4 to locate the position of the drone 42, and also convenient for the drone 42 to return. In addition, combined with the micro radar 19, when the drone 42 is 0 meters to 10 meters away from the device, the micro radar 19 on the surface of the receiving plate 18 provides positioning for the drone 42, so that the drone 42 can land on the receiving plate 18;

[0078] 3. The structure of the present application is reasonable. The drone 42 is also provided with a wireless charging coil that cooperates with the wireless charging coil 38. After the drone 42 is recovered, the wireless charging coil 38 cooperates with the wireless charging coil of the drone 42 to charge it.

[0079] 4. The present application has a reasonable structure. When the drone 42 is in operation, the motor in the adjustment member drives the adjustment bar 51 to rotate via the rotating shaft, so that the pull rod 1 54 pulls the rotating frame 2 49 to rotate via the rotating shaft 2 53. In addition, the motor drives the adjustment bar 51 to rotate via the rotating shaft, so that the pull rod 2 55 pulls the rotating frame 1 47 to rotate on the surface of the rotating shaft 1 46, thereby achieving multi-angle adjustment of the camera 52.

[0080] The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A folding-wing UAV cluster launching device, characterized in that: include: A storage bin (1), a group-sending shell (3) and a drone (42); The surface of the storage bin (1) is provided with a monitoring component, the inner bottom wall of the storage bin (1) is fixedly connected with a plurality of electric slides (23), the electric slides (23) are used to connect the hair group shell (3), the bottom of the hair group shell (3) is provided with a plurality of groups of moving components cooperating with the electric slides (23), the surface of the hair group shell (3) is provided with two groups of adjusting components, and the surface of the adjusting components is provided with a pause frame (17); The inner wall of the suspension frame (17) is provided with two sets of recovery parts, and the recovery parts include a receiving plate (18) slidably connected to the inner wall of the suspension frame (17), an electric telescopic rod (10) fixedly connected to the bottom of the suspension frame (17), a connecting block (41) fixedly connected to the output end of the electric telescopic rod (10), and a micro radar (19) fixedly connected to the surface of the receiving plate (18); The surface of the hair-bearing shell (3) is provided with a plurality of storage openings (32), the interiors of the storage openings (32) are provided with automatic recovery components, and the interior of the hair-bearing shell (3) is provided with a chamber (36) cooperating with the automatic recovery components.

2. A folding-wing UAV cluster launch device according to claim 1, characterized in that: The monitoring component comprises a base shell (13) fixedly connected to the surface of the storage bin (1), a rotating seat (12) rotatably connected to the surface of the base shell (13), a radar (4) fixedly connected to the surface of the rotating seat (12), and a driving member arranged on the inner wall of the storage bin (1).

3. A folding-wing UAV cluster launch device according to claim 2, characterized in that: The driving member comprises a sliding groove (20) provided on the inner surface of the storage bin (1), a sliding base block slidably connected to the inner wall of the sliding groove (20), a rack (21) fixedly connected to the surface of the sliding base block, a gear fixedly connected to the bottom center of the rotating seat (12), and an electric telescopic rod (22) fixedly connected to the inner surface of the storage bin (1); The rack (21) is meshedly connected with the gear, and the output end of the second electric telescopic rod (22) is fixedly connected with the rack (21).

4. The folding-wing UAV cluster launch device according to claim 1, characterized in that: The moving component comprises a storage chamber (26) provided at the bottom of the group hair shell (3), a second sliding groove (27) provided on the inner wall of the storage chamber (26), a sliding bar (28) slidably connected to the inner wall of the second sliding groove (27), a frame (31) fixedly connected to one side of the sliding bar (28), a universal wheel (9) rotatably connected to the inner wall of the frame (31), and a damper (29) fixedly connected to the inner surface of the storage chamber (26); One end of the damper (29) is fixedly connected to the frame (31); a spring (30) is provided at the center of the storage chamber (26); one end of the spring (30) is connected to the inner wall of the storage chamber (26); and the other end of the spring (30) is fixedly connected to one side of the frame (31).

5. The folding-wing UAV cluster launch device according to claim 1, characterized in that: The adjusting component comprises a slot (16) formed on the side surface of the hair group housing (3), a sliding rod (40) fixedly connected to the inner wall of the slot (16), a screw rod (15) rotatably connected to the inner wall of the slot (16), a moving block (39) threadedly connected to the surface of the screw rod (15), and a motor (14) fixedly connected to the end surface of the hair group housing (3); The output end of the motor (14) is fixedly connected to one end of the screw rod (15); a sliding opening for matching the sliding rod (40) is provided on the surface of the moving block (39); the moving block (39) is slidably connected to the sliding rod (40) through the sliding opening; and the suspension frame (17) is mounted on one side of the moving block (39).

6. The folding-wing UAV cluster launch device according to claim 1, characterized in that: The automatic recovery component comprises a limiting slide groove (33) provided on the inner wall of the storage opening (32), a limiting slider slidably connected to the inner wall of the limiting slide groove (33), a storage plate (34) fixedly connected to one side of the limiting slider, and an air compressor (35).

7. The folding-wing UAV cluster launch device according to claim 6, characterized in that: An electrode (37) is provided on the lower surface of the storage plate (34), and a wireless charging coil (38) is provided inside the storage plate (34).

8. The folding-wing UAV cluster launch device according to claim 1, characterized in that: An air inlet is provided on the surface of the chamber (36), and an air inlet fan (5) is fixedly connected to the inner wall of the air inlet.

9. The folding-wing UAV cluster launch device according to claim 1, characterized in that: The inner wall of the storage bin (1) is fixedly connected with a Velcro (24), a sub-surface of the Velcro (24) is fixedly connected with a dehumidification bag (25), and one side of the bottom of the group hair shell (3) is fixedly connected with a rubber block (11); A mounting seat is provided at the bottom of the storage bin (1), and the mounting seat comprises a base (2), a pedestal (7) and a shock absorber (6); The surface of the base (2) is provided with a plurality of mounting openings (8); the base (7) is fixedly connected to the bottom of the storage bin (1); and the shock absorber (6) is arranged between the base (7) and the base (2).

10. The folding-wing UAV cluster launch device according to claim 1, characterized in that: The surface of the drone (42) is fixedly connected to a base frame (43), the surface of the base frame (43) is fixedly connected to a battery compartment (44), an end surface of the battery compartment (44) is provided with a heat dissipation port, and an inner wall of the heat dissipation port is fixedly connected to a dustproof net (56); The surface of the base frame (43) is fixedly connected to a fixed frame (45), the surface of the fixed frame (45) is rotatably connected to a rotating shaft 1 (46), the surface of the rotating shaft 1 (46) is fixedly connected to a rotating frame 1 (47), the surface of the rotating frame 1 (47) is rotatably connected to a rotating shaft 2 (53), the surface of the rotating shaft 2 (53) is fixedly connected to a rotating frame 2 (49), the surface of the rotating frame 2 (49) is fixedly connected to a camera (52), and the surface of the rotating frame 1 (47) is fixedly connected to two groups of symmetrically arranged adjustment members; The adjusting member comprises a motor (48) fixedly connected to the surface of a rotating frame (47), a bearing (50) fixedly connected to the outer surface of the rotating frame (47), a rotating shaft fixedly connected to the inner ring of the bearing (50), and an adjusting strip (51) fixedly connected to the end surface of the rotating shaft, wherein a plurality of adjusting holes are formed on the surface of the adjusting strip (51); The surface of the second rotating frame (49) is rotatably connected to a pull rod (54) that matches the adjusting member, and the surface of the fixed frame (45) is rotatably connected to a pull rod (55) that matches the adjusting member.

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