Unmanned aerial vehicle dispatching command vehicle

Abstract

The utility model provides an unmanned aerial vehicle dispatching command vehicle which comprises a vehicle body, a carriage with an open rear end is arranged on a frame of the vehicle body, sliding strips are transversely and slidably connected to the bottom end in the carriage in the length direction of the carriage, and a device transverse plate matched with the sliding strips in length is transversely and fixedly connected between the top ends of the two sliding strips. The front portion of the lower surface of the device transverse plate is fixedly connected with a device frame. According to the unmanned aerial vehicle dispatching command vehicle provided by the utility model, the device transverse plate is arranged, and the device transverse plate capable of transversely sliding is arranged in the compartment in the dispatching vehicle, so that in actual use, the device transverse plate can be pulled out, the unmanned aerial vehicle is directly assembled on the device transverse plate, and then the unmanned aerial vehicle is directly controlled to take off on the device transverse plate; when landing, the unmanned aerial vehicle can directly land on the device, then a worker directly disassembles the unmanned aerial vehicle on the device transverse plate, fixes the disassembled parts and then controls the device transverse plate to be stored in the compartment, so that the unmanned aerial vehicle and the parts of the unmanned aerial vehicle do not need to be manually transferred, and the overall working efficiency is improved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) dispatching technology, and in particular to a UAV dispatching and command vehicle. Background Technology

[0002] Unmanned aerial vehicles (UAVs), also known as drones, are unmanned aircraft controlled by radio remote control equipment and their own program control devices. They are used in special missions such as disaster relief, agricultural and forestry protection, and power line inspection.

[0003] In some fields, there are high requirements for the performance of multi-rotor drones, such as endurance, payload, and stability. Therefore, multi-rotor drones that perform the above tasks are relatively large, making them inconvenient to schedule. During scheduling and transportation, the drones need to be disassembled, and the disassembled drone parts need to be transferred to the cargo compartment of the dispatch vehicle. The whole process is time-consuming and affects the efficiency of the operation.

[0004] Therefore, it is necessary to provide a new unmanned aerial vehicle (UAV) dispatch and command vehicle to solve the above-mentioned technical problems. Summary of the Invention

[0005] This utility model provides a drone dispatch and command vehicle, which solves the technical problem that when dispatching and transporting larger drones, the drones need to be disassembled, and the disassembled drone parts need to be transferred to the truck bed of the dispatch vehicle. The whole process is time-consuming and affects the efficiency of operation.

[0006] To solve the above-mentioned technical problems, the present invention provides a drone dispatch and command vehicle, which includes a vehicle body and a rear-opening compartment on the frame of the vehicle body.

[0007] The bottom of the interior of the carriage is laterally connected to a slide bar along its length. A device cross plate of the same length is laterally fixed between the top ends of the two slide bars. A device frame is fixedly connected to the front of the lower surface of the device cross plate. A rotating shaft is laterally rotatably connected to the bottom of the device frame. A servo motor is fixedly connected to the front of the lower surface of the device cross plate. Pulleys are fixedly connected to the output shaft of the servo motor and the outer surface of the rotating shaft. The two pulleys are connected by belt drive. A rack is fixedly connected to the bottom of the interior of the carriage along its length. A gear that meshes with the rack is fixedly connected to the outer surface of the rotating shaft.

[0008] Preferably, both sides of the device's horizontal plate are hinged to side plates, and multiple adjustment structures are provided between the two side plates and the device's horizontal plate. The multiple adjustment structures have the same structure. One of the adjustment structures includes a first fixing seat fixedly connected to the lower end of the inner surface of the side plate, and a second fixing seat fixedly connected to the outer side of the upper surface of the device's horizontal plate. A hydraulic rod is hinged between the first fixing seat and the second fixing seat.

[0009] Preferably, the bottom end of the device's horizontal plate and the outer surfaces of the two side plates are provided with multiple support leg structures. The multiple support leg structures are all identical. One of the support leg structures includes a first connecting seat fixedly connected to the bottom end of the device's horizontal plate. A support rod is hinged to the top end of the first connecting seat. A second connecting seat is fixedly connected to the front end of the upper surface of the support rod. A third connecting seat is fixedly connected to the top end of the device's horizontal plate. A cylinder is hinged between the second connecting seat and the third connecting seat.

[0010] Preferably, a cable drum is provided at the rear of the top of the interior of the carriage, and a cable block is fixedly connected to the rear end of the upper surface of the device's horizontal plate, with the outer end of the cable on the cable drum fixedly connected to the cable block.

[0011] Preferably, a first limiting block is fixedly connected laterally at the front end between the two sliding strips, and a second limiting block corresponding to the first limiting block is fixedly connected to the rear end of the lower surface of the carriage interior. Multiple straps are provided on the inner surfaces of the two side plates.

[0012] Preferably, the rear end of the carriage is provided with a carriage door.

[0013] Compared with related technologies, the drone dispatch and command vehicle provided by this utility model has the following beneficial effects: This utility model provides a drone dispatch and command vehicle. By setting a device horizontal plate, the vehicle compartment is equipped with a device horizontal plate that can slide laterally. In actual use, the device horizontal plate can be pulled outward, and then the drone can be directly assembled on it. After that, the drone can be directly controlled to take off on it and land directly on it. Then, the staff can directly disassemble the drone on the device horizontal plate and fix the disassembled parts. Then, the device horizontal plate is controlled to be retracted into the compartment. There is no need to manually transfer the drone and its parts, which improves the overall work efficiency. Attached Figure Description

[0014] Figure 1 A schematic diagram of a preferred embodiment of the unmanned aerial vehicle dispatch and command vehicle provided by this utility model;

[0015] Figure 2 for Figure 1 The diagram shows the overall external structure of the drone dispatch and command vehicle.

[0016] Figure 3 for Figure 1 The diagram shows the structural schematic of the adjustment mechanism in the drone dispatch and command vehicle.

[0017] The following are the labels in the diagram: 1. Vehicle body, 2. Carriage, 3. Sliding bar, 4. Device cross plate, 5. Rack, 6. Device frame, 7. Gear, 8. Servo motor, 9. Pulley, 10. First limit block, 11. Second limit block, 12. First connecting seat, 13. Support rod, 14. Second connecting seat, 15. Third connecting seat, 16. Cylinder, 17. Cable drum, 18. Cable, 19. Cable block, 20. Side plate, 21. Strap, 22. First fixing seat, 23. Second fixing seat, 24. Hydraulic rod, 25. Carriage door. Detailed Implementation

[0018] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0019] Please refer to the following: Figure 1 , Figure 2 ,and Figure 3 ,in, Figure 1 A schematic diagram of a preferred embodiment of the unmanned aerial vehicle dispatch and command vehicle provided by this utility model; Figure 2 for Figure 1 The diagram shows the overall external structure of the drone dispatch and command vehicle. Figure 3 for Figure 1 The diagram shows the structural schematic of the adjustment mechanism in the drone dispatch and command vehicle. The drone dispatch and command vehicle includes: a main body 1, and a rear-opening cargo compartment 2 mounted on the frame of the main body 1;

[0020] Inside the carriage 2, a sliding strip 3 is slidably connected to the bottom end along its length. A device cross plate 4, which is adapted to the length of the two sliding strips 3, is fixedly connected to the top of the two sliding strips 3. A device frame 6 is fixedly connected to the front of the lower surface of the device cross plate 4. A rotating shaft is rotatably connected to the bottom end of the device frame 6. A servo motor 8 is fixedly connected to the front of the lower surface of the device cross plate 4. Pulleys 9 are fixedly connected to the outer surface of the output shaft of the servo motor 8 and the rotating shaft. The two pulleys 9 are connected by belt drive. A rack 5 is fixedly connected to the bottom end along its length inside the carriage 2. A gear 7 that meshes with the rack 5 is fixedly connected to the outer surface of the rotating shaft.

[0021] When the servo motor 8 is running, its output shaft rotates, and the pulley 9 on the surface of the output shaft drives another pulley 9 that is connected to it to rotate. The rotating shaft that is fixed to it will rotate synchronously, and the gear 7 on the surface of the rotating shaft will also rotate synchronously. Then, under the action of the rack 5, the device cross plate 4 will move along the length of the carriage 2, and it can extend outward from the rear end of the carriage 2. The drone can be disassembled and assembled on it. After disassembly, the drone can be sent into the interior of the carriage 2 through this structure again, without the need for manual transfer operations, thus improving the overall efficiency of the operation.

[0022] Both sides of the device's horizontal plate 4 are hinged with side plates 20. Multiple adjustment structures are provided between the two side plates 20 and the device's horizontal plate 4. The structures of the multiple adjustment structures are all the same. One of the adjustment structures includes a first fixing seat 22 fixedly connected to the lower end of the inner surface of the side plate 20, and a second fixing seat 23 fixedly connected to the outer side of the upper surface of the device's horizontal plate 4. A hydraulic rod 24 is hinged between the first fixing seat 22 and the second fixing seat 23.

[0023] The two side plates 20 can be flipped under the action of the adjustment structure. After the hydraulic rod 24 of the adjustment structure is extended, the two side plates 20 can be flipped to a horizontal state. At this time, the two side plates 20 and the device cross plate 4 can be spliced ​​together to form a larger plate, making it more convenient for the staff to disassemble the drone. After the hydraulic rod 24 is completely shortened, the two side plates 20 can be flipped to a state perpendicular to the device cross plate 4, at which time it can be stored inside the carriage 2.

[0024] Multiple support leg structures are provided at the bottom end of the device horizontal plate 4 and on the outer surfaces of the two side plates 20. The structures of the multiple support leg structures are all the same. One of the support leg structures includes a first connecting seat 12 fixedly connected to the bottom end of the device horizontal plate 4. A support rod 13 is hinged to the top end of the first connecting seat 12. A second connecting seat 14 is fixedly connected to the front end of the upper surface of the support rod 13. A third connecting seat 15 is fixedly connected to the top end of the device horizontal plate 4. A cylinder 16 is hinged between the second connecting seat 14 and the third connecting seat 15.

[0025] The support leg structure can support the device horizontal plate 4 when it is extended. When the structure is in use, the cylinder 16 extends, which can then drive the support rod 13 to rotate downward until it reaches a vertical position, and then support the device horizontal plate 4 through it.

[0026] A cable drum 17 is installed at the rear of the top of the interior of the carriage 2. A cable block 19 is fixedly connected to the rear end of the upper surface of the device cross plate 4. The outer end of the cable 18 on the cable drum 17 is fixedly connected to the cable block 19.

[0027] The cable 19 on the cable drum 17 can support the device horizontal plate 4, further improving the stability of the device horizontal plate 4.

[0028] A first limiting block 10 is fixedly connected laterally at the front end between the two sliding strips 3, and a second limiting block 11 corresponding to the first limiting block 10 is fixedly connected to the rear end of the lower surface inside the carriage 2. Multiple straps 21 are provided on the inner surface of both side panels 20.

[0029] The strap 21 can fix the disassembled drone parts, and the first limiting block 10 and the second limiting block 11 can limit the device cross plate 4 to prevent it from sliding directly out of the carriage 2.

[0030] The rear end of carriage 2 is equipped with carriage door 25.

[0031] The carriage door 25 can close the carriage 2, protecting the drone and its components.

[0032] The working principle of the unmanned aerial vehicle dispatch and command vehicle provided by this utility model is as follows:

[0033] When the servo motor 8 is running, its output shaft rotates, and the pulley 9 on the surface of the output shaft drives another pulley 9 that is connected to it to rotate. The rotating shaft that is fixed to it will rotate synchronously, and the gear 7 on the surface of the rotating shaft will also rotate synchronously. Then, under the action of the rack 5, the device cross plate 4 will move along the length of the carriage 2, and it can extend outward from the rear end of the carriage 2. The drone can be disassembled and assembled on it. After disassembly, the drone can be sent into the interior of the carriage 2 through this structure again, without the need for manual transfer operations, thus improving the overall efficiency of the operation.

[0034] Compared with related technologies, the unmanned aerial vehicle dispatch and command vehicle provided by this utility model has the following beneficial effects:

[0035] This utility model provides a drone dispatch and command vehicle. By setting up a device horizontal plate 4, the vehicle compartment 2 is equipped with a horizontally sliding device horizontal plate 4. In actual use, the device horizontal plate 4 can be pulled outward, and then the drone can be directly assembled on it. After that, the drone can be directly controlled to take off on it and land directly on it. Then, the staff can directly disassemble the drone on the device horizontal plate 4 and fix the disassembled parts. Then, the device horizontal plate 4 is controlled to be put back into the compartment 2, eliminating the need for manual transfer of drones and their parts, thus improving the overall work efficiency.

[0036] The above description is merely an embodiment of this utility model and does not limit the patent scope of this utility model. Any equivalent structural or procedural transformations made based on the content of this utility model specification and drawings, or direct or indirect applications in other related technical fields, are similarly included within the patent protection scope of this utility model.

Claims

1. A drone dispatch command vehicle, characterized in that, Includes a vehicle body (1), and a rear-opening compartment (2) is provided on the frame of the vehicle body (1). The bottom of the carriage (2) is slidably connected to a slide bar (3) along its length. A device cross plate (4) of the same length is fixedly connected between the top ends of the two slide bars (3). A device frame (6) is fixedly connected to the front of the lower surface of the device cross plate (4). A rotating shaft is rotatably connected to the bottom of the device frame (6). A servo motor (8) is fixedly connected to the front of the lower surface of the device cross plate (4). A pulley (9) is fixedly connected to the output shaft of the servo motor (8) and the outer surface of the rotating shaft. The two pulleys (9) are connected by belt drive. A rack (5) is fixedly connected to the bottom of the carriage (2) along its length. A gear (7) that meshes with the rack (5) is fixedly connected to the outer surface of the rotating shaft.

2. The unmanned aerial vehicle dispatch vehicle of claim 1, wherein, Both sides of the device's horizontal plate (4) are hinged with side plates (20). Multiple adjustment structures are provided between the two side plates (20) and the device's horizontal plate (4). The structures of the multiple adjustment structures are all the same. One of the adjustment structures includes a first fixing seat (22) fixedly connected to the lower end of the inner surface of the side plate (20). A second fixing seat (23) is fixedly connected to the outer side of the upper surface of the device's horizontal plate (4). A hydraulic rod (24) is hinged between the first fixing seat (22) and the second fixing seat (23).

3. The UAV command vehicle of claim 2, wherein, Multiple support leg structures are provided at the bottom end of the device horizontal plate (4) and on the outer surfaces of the two side plates (20). The structures of the multiple support leg structures are all the same. One of the support leg structures includes a first connecting seat (12) fixedly connected to the bottom end of the device horizontal plate (4). A support rod (13) is hinged to the top end of the first connecting seat (12). A second connecting seat (14) is fixedly connected to the front end of the upper surface of the support rod (13). A third connecting seat (15) is fixedly connected to the top end of the device horizontal plate (4). A cylinder (16) is hinged between the second connecting seat (14) and the third connecting seat (15).

4. The UAV command vehicle of claim 1, wherein, A cable drum (17) is provided at the rear of the top of the interior of the carriage (2). A cable block (19) is fixedly connected to the rear end of the upper surface of the device cross plate (4). The outer end of the cable (18) on the cable drum (17) is fixedly connected to the cable block (19).

5. The UAV command vehicle of claim 2, wherein, A first limiting block (10) is fixedly connected laterally at the front end between the two slide bars (3), and a second limiting block (11) corresponding to the first limiting block (10) is fixedly connected to the rear end of the lower surface inside the carriage (2). Multiple straps (21) are provided on the inner surfaces of the two side plates (20).

6. The unmanned aerial vehicle dispatch and command vehicle according to claim 1, characterized in that, The rear end of the carriage (2) is provided with a carriage door (25).

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