Unmanned aerial vehicle nest cabin assembly

Abstract

The utility model discloses an unmanned aerial vehicle nest cabin assembly which comprises a storage bin assembly, a cabin body, a cabin door, a cabin door opening structure and an unmanned aerial vehicle take-off and landing platform. The storage bin assembly is arranged in a container of the vehicle body and can be fixedly connected with the container of the vehicle body, and a first power source and a second power source are arranged in the storage bin assembly. The cabin body is arranged at the top of the storage box, and the cabin door opening structure is arranged in the cabin body, connected with the cabin door and used for driving the cabin door to be opened or closed; the unmanned aerial vehicle take-off and landing platform is arranged in the cabin body, is used for taking off and landing of the unmanned aerial vehicle and can extend out of the cabin body under the condition that the cabin door is opened, the unmanned aerial vehicle take-off and landing platform is provided with a charging interface, the charging interface is electrically connected with the first power source, and the unmanned aerial vehicle can be charged through the charging interface. According to the unmanned aerial vehicle nest cabin assembly, a wider take-off and landing space can be provided for the unmanned aerial vehicle, take-off and landing of the unmanned aerial vehicle are facilitated, and meanwhile energy is provided for the unmanned aerial vehicle.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle nest cabin assembly. Background Art

[0002] Unmanned aerial vehicles are widely used in industrial fields. With the continuous development and progress of their technologies and the intelligent upgrading of applications in various industrial fields, the practical application value of unmanned aerial vehicles has been continuously improved. Existing unmanned aerial vehicle mobile operation vehicles mainly include unmanned aerial vehicle inspection operation vehicles, unmanned aerial vehicle intelligent command operation vehicles, unmanned aerial vehicle fire trucks, etc.

[0003] During the process of an unmanned aerial vehicle mobile operation vehicle performing tasks, the mobile operation vehicle can transport the unmanned aerial vehicle to the destination according to the actual flight mission of the unmanned aerial vehicle, arrive in advance to provide a lifting platform for the unmanned aerial vehicle to land in a different place, and supply energy to the unmanned aerial vehicle.

[0004] However, the unmanned aerial vehicle of the unmanned aerial vehicle mobile body is generally placed in a nest cabin, and the nest cabin is generally placed at the tail of the mobile body. During the takeoff and landing processes, it is necessary to open the top cover of the nest cabin. This way of opening at the top will inevitably increase the requirement for the sealing performance of the top cover. At the same time, during the takeoff and landing processes, some operations need to be completed inside the vehicle body. Due to the limited space inside the vehicle body, this will inevitably have a certain impact on the takeoff and landing of the unmanned aerial vehicle. At the same time, it is also necessary to be able to supply energy to the unmanned aerial vehicle at any time to facilitate the unmanned aerial vehicle to perform relevant tasks. Summary of the Utility Model

[0005] Aiming at the deficiencies existing in the prior art, the technical problem to be solved by the utility model is to provide an unmanned aerial vehicle nest cabin assembly, which can provide a wider takeoff and landing space for the unmanned aerial vehicle, facilitate the takeoff and landing of the unmanned aerial vehicle, and can supply energy to the unmanned aerial vehicle.

[0006] To achieve the above object, the utility model is realized through the following technical solutions: An unmanned aerial vehicle nest cabin assembly, comprising:

[0007] A storage bin assembly, including a storage box, the storage box is arranged in the cargo box of the vehicle body and can be fixedly connected to the cargo box of the vehicle body, and a first power source and a second power source are arranged in the storage box;

[0008] A cabin body, placed on the top of the storage box and can be fixedly connected to the storage box, and a hatch is opened on the side wall of the cabin body;

[0009] A cabin door, arranged at the hatch for closing the hatch, and the bottom end of the cabin door is hinged to the cabin body through a rotating shaft;

[0010] A cabin door opening structure, the cabin door opening structure is arranged in the cabin body and is connected to the cabin door for driving the cabin door to open or close; and

[0011] The UAV takeoff and landing platform is arranged inside the cabin and is used for the takeoff and landing of the UAV. It can extend outside the cabin when the cabin door is opened. A charging interface is arranged on the UAV takeoff and landing platform, and the charging interface is electrically connected to the first power supply. The UAV can be charged through the charging interface.

[0012] Further, the cabin door opening structure includes:

[0013] A bottom plate fixed inside the cabin;

[0014] A rotary driving member arranged on the bottom plate and connected to the cabin door for driving the cabin door to rotate around the rotating shaft rotatably connected to the cabin body; and

[0015] An elastic auxiliary pulling member that can elastically expand and contract, and the auxiliary pulling member is connected between the cabin door and the bottom plate.

[0016] Further, the rotary driving member includes a rotary motor and a connecting rod assembly. The rotary motor is arranged on the bottom plate. One end of the connecting rod assembly is connected to the power output shaft of the rotary motor, and the other end is hinged to the inner wall of the cabin door. When the rotary motor is started, the cabin door can be driven to rotate around the rotating shaft through the connecting rod assembly.

[0017] Further, the elastic auxiliary pulling member includes a spring, and both ends of the spring are respectively connected between the cabin door and the bottom plate.

[0018] Further, the rotary driving member further includes an intermediate auxiliary support member. The auxiliary support member is fixed on the bottom plate. The power output shaft of the rotary motor can rotatably pass through the auxiliary support member and can be connected to the auxiliary support member through a bearing.

[0019] Further, the UAV takeoff and landing platform includes:

[0020] An installation platform installed on the bottom plate and fixedly connected to the top of the UAV storage bin assembly;

[0021] There are two centering platforms, and the two centering platforms are oppositely arranged inside the cabin. The charging interface is arranged on the centering platform;

[0022] A driving mechanism is arranged on the installation platform and connected to the two centering platforms for driving the two centering platforms to approach or separate from each other along the left and right sides of the vehicle body; and

[0023] A centering driving member is arranged on the centering platform and is used to drive the drone docked on the centering platform to move on the centering platform until the charging port of the drone is docked with the charging interface.

[0024] Further, the driving mechanism includes a first rotating power source, a first lead screw, and a first connecting block. The first rotating power source is arranged on the installation platform. The first lead screw is connected to the first rotating power source and extends along the left - right direction of the moving vehicle body, and can drive the first lead screw to rotate. The first connecting block is fixed on the centering platform and is threadedly connected to the first lead screw.

[0025] Further, the driving mechanism further includes a guiding structure. The guiding structure is connected between the centering platform and the installation platform and is used to guide the centering platform when it moves left and right.

[0026] Further, the guiding structure includes a sliding rod. A guiding groove extending along the left - right direction of the cabin is formed on the installation platform. The sliding rod is slidably inserted into the guiding groove, and the end of the sliding rod is fixed on the centering platform.

[0027] Further, the centering driving member includes a second rotating power source, a third rotating power source, two bidirectional lead screws, and four centering rods. The two bidirectional lead screws are rotatably arranged on the centering platform at a 90° intersection. The second rotating power source and the third rotating power source are respectively connected to the two bidirectional lead screws to respectively drive the two bidirectional lead screws to rotate. Threads with opposite helix directions are respectively arranged at both ends of the bidirectional lead screw. The four centering rods are respectively threadedly connected to the four ends of the two bidirectional lead screws and can slide along the surface of the centering platform.

[0028] The beneficial effects of the present utility model:

[0029] For the above - mentioned drone nest cabin assembly, during assembly, first, the first power source and the second power source are arranged in the storage box. Medium - sized and small drones can be stored in the storage box. Subsequently, the storage box is installed in the cargo box of the vehicle body. Then, the cabin is installed on the top of the storage box. Subsequently, the cabin door, the cabin door opening structure, and the drone take - off and landing platform are installed. Usually, when the drone needs to take off or land, first, the cabin door is opened through the cabin door opening structure, and then the drone take - off and landing platform extends out of the cabin. The drone can then take off or land. After completing take - off or landing, the drone take - off and landing platform retracts into the cabin again, and the cabin door can be closed. When in use, the vehicle body can be used to transport the drone to the destination to perform tasks. During the task execution process, the drone can be charged through the charging interface.

[0030] By adopting the above-mentioned UAV nest cabin assembly, a wider take-off and landing space can be provided for the UAV. While facilitating the take-off and landing of the UAV, it can also provide energy for the UAV. BRIEF DESCRIPTION OF THE DRAWINGS

[0031] In order to more clearly illustrate the specific embodiments of the present invention, the drawings required for use in the specific embodiments will be briefly introduced below. In all the drawings, the components or parts do not necessarily draw according to the actual proportion.

[0032] Figure 1 FIG. Figure 1 is a schematic diagram of a UAV nest cabin assembly shown;

[0033] Figure 2 FIG. Figure 1 is a schematic diagram of the assembly of the cabin door opening structure and the UAV take-off and landing platform in a UAV nest cabin assembly shown;

[0034] Figure 3 FIG. Figure 1 is a three-dimensional schematic diagram of a storage bin assembly in a UAV nest cabin assembly shown;

[0035] Figure 4 FIG. Figure 1 is a bottom view of a storage bin assembly in a UAV nest cabin assembly shown;

[0036] Figure 5 FIG. Figure 1 is a schematic diagram of the cabin door opening structure in a UAV nest cabin assembly shown;

[0037] Figure 6 FIG. Figure 1 is a schematic diagram of the UAV take-off and landing platform in a UAV nest cabin assembly shown;

[0038] Reference numerals:

[0039] 200, storage bin assembly; 210, storage box; 220, partition; 230, battery drawer; 240, storage drawer; 250, first power supply; 260, second power supply; 270, top connector; 271, connecting straight plate; 272, hook; 280, bottom connector; 281, support frame; 282, L-shaped connecting plate;

[0040] 300, cabin body; 310, cabin door;

[0041] 400, cabin door opening structure; 410, bottom plate; 420, rotary drive member; 421, rotary motor; 422, connecting rod assembly; 423, intermediate auxiliary support member; 430, elastic auxiliary pulling member;

[0042] 500, UAV take-off and landing platform; 510, installation platform; 520, centering platform; 530, drive mechanism; 531, first rotary power source; 532, first lead screw; 533, guiding structure; 540, centering drive member; 541, second rotary power source; 542, third rotary power source; 543, bi-directional screw; 544, centering rod. Detailed implementation manners

[0043] The embodiments of the technical solution of the present utility model will be described in detail below with reference to the accompanying drawings. The following embodiments are only used to more clearly illustrate the technical solution of the present utility model, and thus are only examples and cannot be used to limit the protection scope of the present utility model.

[0044] Please refer to Figures 1 to 3 , the present utility model provides a UAV nest cabin assembly, including a vehicle body 100, a storage bin assembly 200, a cabin body 300, a cabin door opening structure 400 and a UAV take-off and landing platform 500.

[0045] Specifically, the storage bin assembly 200 includes a storage box 210. The storage box 210 is arranged in the cargo box of the vehicle body 100 and can be fixedly connected to the cargo box of the vehicle body 100. A first power source 250 and a second power source 260 are arranged in the storage box 210. The cabin body 300 is placed on the top of the storage box 210 and can be fixedly connected to the storage box 210. A cabin opening is provided on the side wall of the cabin body 300. A cabin door 310 is arranged at the cabin opening for closing the cabin opening. The bottom end of the cabin door 310 is hinged to the cabin body 300 through a rotating shaft. It should be noted that there can be one cabin opening or cabin openings can be provided on both the left and right sides, and the cabin door 310 is provided in a matching manner with the cabin opening. The cabin door opening structure 400 is arranged in the cabin body 300 and is connected to the cabin door 310 for driving the cabin door 310 to open or close. The UAV take-off and landing platform 500 is arranged in the cabin body 300 for the take-off, landing and docking of the UAV 1 and can extend out of the cabin body 310 when the cabin door 310 is opened. A charging interface is arranged on the UAV take-off and landing platform 500, and the charging interface is electrically connected to the first power source 250.

[0046] During assembly, first place the first power supply 250 and the second power supply 260 inside the storage box 210. The medium and small-sized unmanned aerial vehicle 1 can be stored inside the storage box 210. Subsequently, install the storage box 210 inside the cargo box of the vehicle body 100. Then, install the cabin body 300 on top of the storage box 210. Subsequently, install the cabin door 310, the cabin door opening structure 400, and the unmanned aerial vehicle takeoff and landing platform 500. Usually, when the unmanned aerial vehicle 1 needs to take off or land, first open the cabin door 310 through the cabin door opening structure 400. Subsequently, the unmanned aerial vehicle takeoff and landing platform 500 extends outside the cabin body 300. The unmanned aerial vehicle 1 can either take off or land. After completing takeoff or landing, the unmanned aerial vehicle takeoff and landing platform 500 retracts back inside the cabin body 300 again, and then close the cabin door 310. When in use, the unmanned aerial vehicle 1 can be transported to the destination by the vehicle body 100 to perform tasks. During the task execution process, the unmanned aerial vehicle 1 can be charged through the charging interface.

[0047] Adopting the above-mentioned cabin body 300 can provide a wider takeoff and landing space for the unmanned aerial vehicle 1. While facilitating the takeoff and landing of the unmanned aerial vehicle 1, it can also provide energy for the unmanned aerial vehicle 1 at any time.

[0048] In this embodiment, a bottom connecting member 280 can be provided at the bottom of the storage box 210, and it is fixedly connected to the fixed skeleton of the cargo box of the vehicle body 100 through the bottom connecting member 280. A top connecting member 270 is provided at the top of the storage box 210, and it is connected to the cabin body 300 through the top connecting member 270. In addition, a partition 220 can also be provided inside the storage box 210. The partition 220 divides the inner cavity of the storage box 210 into a storage compartment and an installation compartment; the storage compartment is used to store the unmanned aerial vehicle 1. A hatch is provided on the side wall of the storage box 210 to communicate the storage compartment with the outside. The energy supply device is arranged in the installation compartment.

[0049] When in use, first fix the storage box 210 inside the cargo box of the vehicle body 100 through the bottom connecting member 280. Subsequently, place the first power supply 250 and the second power supply 260 inside the installation compartment. Then, the medium and small-sized unmanned aerial vehicle 1 can be stored in the storage compartment. Next, install the cabin body 300 on the top of the storage box 210 and fixedly connect them through the top connecting member 270.

[0050] During specific implementation, a cover plate that can cover the hatch can be provided on the storage box 210 to further improve safety.

[0051] Specifically, the top connecting member 270 includes two connecting straight plates 271 and two hooks 272. The two connecting straight plates 271 are located at both ends of the same side plate of the storage box 210. Connecting holes are provided on the connecting straight plates 271. The two hooks 272 are arranged at intervals on the side wall of the storage box 210 opposite to the connecting plate 271. The two hooks 272 can be hooked on the cabin body 300.

[0052] During installation, first hook the two hooks 272 to the corresponding positions of the cabin body 300, and then connect the connecting plate 271 to the threaded holes at the bottom of the cabin body 300 through connecting bolts. With this structure, the connection time can be reduced and the work efficiency can be improved.

[0053] The bottom connecting member 280 includes a support frame 281 and four L-shaped connecting plates 282. The support frame 281 is arranged on the bottom of the storage box 210, and the four support frames 281 are cross-connected to form a frame-shaped support frame 281. The support clamp can play a supporting role. The four L-shaped connecting plates 282 are arranged in pairs on the support frame 281. Installation holes are provided on the L-shaped connecting plates 282, and the L-shaped connecting plate 271 is bolted to the fixed skeleton of the cargo box of the vehicle body 100 through the installation holes. During assembly, only the four L-shaped connecting plates 271 need to be bolted to the fixed skeleton of the cargo box of the vehicle body 100.

[0054] As a preferred embodiment, a battery drawer 230 can also be arranged in the storage box 210. The battery drawer 230 is slidably arranged in the storage box 210 and can slide out from the side wall of the storage box 210. A plurality of first power sources 250 are arranged in the battery drawer 230. During use, the battery drawer 230 can be pulled out to replace the battery of the new first power source 250. Specifically, an exhaust fan can also be arranged on the battery drawer 230, and the exhaust fan is used to exhaust the air in the battery drawer 230 to dissipate heat from the first power source 250.

[0055] As a more preferred embodiment, a storage drawer 240 can also be arranged in the storage box 210. The storage drawer 240 is slidably arranged in the storage box 210 and can slide out from the side wall of the storage box 210, and is located below the battery drawer 230. During use, tools and other items can be placed in the tool storage drawer 240 for convenient use.

[0056] In this embodiment, the cabin door opening structure 400 includes a bottom plate 410, a rotary drive member 420, and an elastic auxiliary pulling member 430.

[0057] Specifically, the bottom plate 410 is fixed inside the cabin body 300. The rotary drive member 420 is arranged on the bottom plate 410 and is connected to the cabin door 310 of the cabin body 300 for driving the cabin door 310 to rotate around the rotating shaft rotatably connected to the cabin body 300. The elastic auxiliary pulling member 430 can elastically stretch and contract, and the elastic auxiliary pulling member 430 is connected between the cabin door 310 and the bottom plate 410.

[0058] During use, when it is necessary to open the hatch 310, only need to start the rotary drive member 420 to drive the hatch 310 to rotate outwards. On the contrary, when it is necessary to close the hatch 310, drive the hatch 310 to rotate in the reverse direction through the rotary drive member 420 until the hatch opening is covered. During the opening and closing processes, the elastic auxiliary pulling member 430 assists in pulling the hatch 310 to improve the stability of the hatch 310.

[0059] It should be noted that in specific implementation, when hatches 310 are provided on both the left and right sides of the cabin body 300, the rotary drive member 420 and the elastic auxiliary pulling member 430 need to be configured in a matching manner. In addition, multiple elastic auxiliary pulling members 430 between each hatch 310 and the bottom plate 410 can be provided at intervals.

[0060] In this embodiment, the rotary drive member 420 includes a rotary motor 421 and a connecting rod assembly 422. The rotary motor 421 is arranged on the bottom plate 410. One end of the connecting rod assembly 422 is connected to the power output shaft of the rotary motor 421, and the other end is hinged to the inner wall of the hatch 310. When the rotary motor 421 is started, the hatch 310 can be driven to rotate around the rotation axis through the connecting rod assembly 422. When the rotary motor 421 rotates clockwise or counterclockwise, the hatch 310 can be driven to rotate through the connecting rod assembly 422 to complete the opening or closing action.

[0061] The connecting rod assembly 422 can be a single L-shaped rod body, or can be formed by multiple struts being hinged to each other and fixed by bolts to form an L shape. In specific implementation, the connecting rod assembly 422 can be two groups, and the two groups of connecting rod assemblies 422 are arranged at intervals at the front and rear ends of the hatch 310. The two groups can improve the stability of the hatch 310.

[0062] In this embodiment, the elastic auxiliary pulling member 430 includes a spring, and the two ends of the spring are respectively connected between the hatch 310 and the bottom plate 410. When the hatch 310 rotates, the spring can play a role in assisting pulling to prevent the load of the rotary motor 421 from being too high.

[0063] In addition, in specific implementation, an intermediate auxiliary support member 423 can also be provided on the bottom plate 410. The power output shaft of the rotary motor 421 can rotatably pass through the intermediate auxiliary support member 423 and can be connected to the intermediate auxiliary support member 423 through a bearing.

[0064] The intermediate auxiliary support member 423 assists in supporting the power output shaft of the rotary motor 421 to prevent the power output shaft of the rotary motor 421 from being bent or deformed.

[0065] In this embodiment, the UAV takeoff and landing platform 500 includes an installation platform 510, a centering platform 520, a drive mechanism 530, and a centering drive member 540.

[0066] Specifically, the installation platform 510 is fixed inside the cabin body 300. The centering platform 520 is arranged inside the cabin body 300 and can extend out from the hatch opened on the side wall of the cabin body 300. A charging interface is provided on the centering platform 520. The driving mechanism 530 is arranged on the installation platform 510 and is connected to the centering platform 520 for driving the centering platform 520 to extend out from the hatch. The centering driving member 540 is arranged on the centering platform 520 and can extend outside the cabin body 300 when the cabin door 310 is opened. A charging interface is provided on the UAV takeoff and landing platform 500, and the charging interface is electrically connected to the first power supply 250.

[0067] During use, in the normal state, the centering platform 520 is located inside the cabin body 300. When the UAV 1 needs to take off or land, with the cabin door 310 of the cabin body 300 opened, the driving mechanism 530 drives the centering platform 520 to extend out from the hatch, and the UAV 1 can then take off or land from the centering platform 520. When it is necessary to charge the UAV 1, when the UAV 1 docks on the centering platform 520, the centering driving member 540 drives the UAV 1 to move on the centering platform 520 until the charging port of the UAV 1 is docked with the charging interface, and then the UAV 1 can be charged.

[0068] In this embodiment, the driving mechanism 530 includes a first rotary power source 531, a first lead screw 532 and a first connecting block. The first rotary power source 531 is arranged on the installation platform 510. The first lead screw 532 is connected to the first rotary power source 531 and extends along the left - right direction of the cabin body 300. The first rotary power source 531 can drive the first lead screw 532 to rotate. The first connecting block is fixed on the centering platform 520 and is in threaded connection with the first lead screw 532.

[0069] During use, when the first rotary power source 531 is started, it can drive the first lead screw 532 to rotate. Through the first connecting block, the centering platform 520 can be driven to move left or right.

[0070] As a preferred embodiment, the driving mechanism 530 further includes a guiding structure 533. The guiding structure 533 is connected between the centering platform 520 and the installation platform 510 for guiding the left - right movement of the centering platform 520.

[0071] Specifically, the guiding structure 533 includes a slide bar. A guiding groove extending along the left - right direction of the cabin body 300 is formed on the installation platform 510. The slide bar can be slidably inserted into the guiding groove, and the end of the slide bar is fixed on the centering platform 520. The slide bar guides the centering platform 520 during its left - right movement, thereby improving the smoothness of the movement of the centering platform 520.

[0072] In this embodiment, the centering driving member 540 includes a second rotary power source 541, a third rotary power source 542, two bidirectional screws 543, and four centering rods 544. The two bidirectional screws 543 are rotatably arranged on the centering platform 520 at a 90° intersection. The second rotary power source 541 and the third rotary power source 542 are respectively connected to the two bidirectional screws 543 for respectively driving the two bidirectional screws 543 to rotate. Threads with opposite helix directions are respectively arranged at both ends of the bidirectional screw 543, and the four centering rods 544 are respectively threadedly connected to the four ends of the two bidirectional screws 543 and can slide along the surface of the centering platform 520.

[0073] When the UAV 1 needs to be centered, the second rotary power source 541 and the third rotary power source 542 can be started simultaneously to drive the two bidirectional screws 543 to rotate, thereby driving the four centering rods 544 to push the UAV 1 to move along the surface of the centering platform 520 until the charging port is docked with the charging interface.

[0074] Preferably, the centering driving member 540 further includes a guide rod and a slider. A guide rod is arranged between two relatively arranged centering rods 544 on the centering platform 520, and the centering rod 544 is slidably connected to the guide rod through the slider. Through the guide rod, the stability of the centering rod 544 can be improved.

[0075] When using the above UAV nest cabin assembly, the cabin door 310 can be automatically opened through the cabin door opening structure 400, facilitating the extension of the UAV takeoff and landing platform 500. The takeoff or landing of the UAV 1 is completed on the UAV takeoff and landing platform 500 outside the cabin body 300, thereby reducing the requirement for the sealing performance of the top of the cabin body 300. At the same time, the space for the takeoff or landing of the UAV 1 is greatly increased, facilitating the takeoff and landing of the UAV 1. In addition, the UAV 1 can be charged at any time, further facilitating the use.

[0076] When using the above UAV nest cabin assembly, the cabin door can be automatically opened through the cabin door opening structure, facilitating the extension of the UAV takeoff and landing platform. The UAV takeoff and landing platform can extend outside the UAV nest cabin, and the takeoff or landing of the UAV is completed outside the UAV nest cabin, thereby reducing the requirement for the sealing performance of the top of the UAV nest cabin. At the same time, the space for the takeoff or landing of the UAV is greatly increased, facilitating the takeoff and landing of the UAV. In addition, the UAV can be charged at any time, further facilitating the use.

[0077] The above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements on some or all of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the scope of the technical solutions of the various embodiments of the present invention, and they should all be covered within the scope of the claims and the description of the present invention.

Claims

1. An unmanned aerial vehicle (UAV) nest cabin assembly, characterized in that, Comprising: A storage bin assembly, including a storage box, the storage box is arranged in the cargo box of the vehicle body and can be fixedly connected to the cargo box of the vehicle body, and a first power source and a second power source are arranged in the storage box; A cabin body, placed on the top of the storage box and can be fixedly connected to the storage box, and a cabin opening is formed on the side wall of the cabin body; A cabin door, arranged at the cabin opening for closing the cabin opening, and the bottom end of the cabin door is hinged to the cabin body through a rotating shaft; A cabin door opening structure, the cabin door opening structure is arranged in the cabin body and is connected to the cabin door for driving the cabin door to open or close; and A drone take-off and landing platform, the drone take-off and landing platform is arranged in the cabin body for the take-off and landing of the drone, and can extend out of the cabin body when the cabin door is opened, and a charging interface is arranged on the drone take-off and landing platform, the charging interface is electrically connected to the first power source, and the drone can be charged through the charging interface.

2. The drone nest cabin assembly according to claim 1, characterized in that, The cabin door opening structure includes: A bottom plate, the bottom plate is fixed in the cabin body; A rotary driving member, the rotary driving member is arranged on the bottom plate and is connected to the cabin door for driving the cabin door to rotate around the rotating shaft rotatably connected to the cabin body; and An elastic auxiliary pulling member, the elastic auxiliary pulling member can elastically stretch and contract, and the auxiliary pulling member is connected between the cabin door and the bottom plate.

3. The drone nest cabin assembly according to claim 2, wherein The rotary driving member includes a rotary motor and a connecting rod assembly, the rotary motor is arranged on the bottom plate, one end of the connecting rod assembly is connected to the power output shaft of the rotary motor, and the other end is hinged to the inner wall of the cabin door. When the rotary motor is started, the cabin door can be driven to rotate around the rotating shaft through the connecting rod assembly.

4. The drone nest cabin assembly according to claim 2, wherein, The elastic auxiliary pulling member includes a spring, and both ends of the spring are respectively connected between the cabin door and the bottom plate.

5. The drone nest cabin assembly according to claim 3, characterized in that, The rotary driving member further includes an intermediate auxiliary support member, the auxiliary support member is fixed on the bottom plate, and the power output shaft of the rotary motor can rotatably pass through the auxiliary support member and can be connected to the auxiliary support member through a bearing.

6. The drone nest cabin assembly according to claim 2, wherein, The drone take-off and landing platform includes: An installation platform, installed on the bottom plate and fixedly connected to the top of the drone storage bin assembly; Two centering platforms, the two centering platforms are oppositely arranged in the cabin body, and the charging interface is arranged on the centering platform; A driving mechanism, arranged on the installation platform and connected to the two centering platforms for driving the two centering platforms to approach or separate from each other along the left and right sides of the vehicle body; and A centering driving member, arranged on the centering platform for driving the drone parked on the centering platform to move on the centering platform until the charging port of the drone is docked with the charging interface.

7. The drone nest compartment assembly according to claim 6, characterized in that, The driving mechanism includes a first rotary power source, a first lead screw and a first connecting block, the first rotary power source is arranged on the installation platform, the first lead screw is connected to the first rotary power source and extends along the left and right directions of the cabin body and can drive the first lead screw to rotate, and the first connecting block is fixed on the centering platform and is in threaded connection with the first lead screw.

8. The drone nest cabin assembly according to claim 6, wherein, The driving mechanism further includes a guiding structure, which is connected between the centering platform and the mounting platform and is used for guiding the centering platform when it moves left and right.

9. The drone nest cabin assembly according to claim 8, characterized in that, The guiding structure includes a sliding rod. A guiding groove extending left and right along the cabin is formed on the mounting platform. The sliding rod is slidably inserted into the guiding groove, and the end of the sliding rod is fixed on the centering platform.

10. The drone nest cabin assembly according to claim 6, characterized in that, The centering driving member includes a second rotary power source, a third rotary power source, two bidirectional screws, and four centering rods. The two bidirectional screws are rotatably arranged on the centering platform at a 90° intersection. The second rotary power source and the third rotary power source are respectively connected to the two bidirectional screws for respectively driving the two bidirectional screws to rotate. Threads with opposite helix directions are respectively arranged at both ends of the bidirectional screw. The four centering rods are respectively threadedly connected to the four ends of the two bidirectional screws and can slide along the surface of the centering platform.

Images