Vehicle-mounted double-unmanned-aerial-vehicle automatic hangar

Abstract

The utility model relates to the technical field of unmanned aerial vehicle hangars, in particular to a vehicle-mounted double-unmanned aerial vehicle automatic hangar which comprises a carrier and a hangar body. A shell is arranged on the carrier; the hangar body comprises a rack and two sub hangars, the rack is installed in the shell, the two sub hangars are fixed to the rack, the two sub hangars are distributed in the preset direction, the preset direction is parallel to the horizontal direction, the two sub hangars are in communication connection, the rack is detachably connected to the carrier, and the sub hangars are used for parking unmanned aerial vehicles. The unmanned aerial vehicle enters and exits the shell through the take-off and According to the vehicle-mounted double-unmanned-aerial-vehicle automatic hangar provided by the invention, the deployment range and the adaptability of the unmanned aerial vehicles can be improved through the arranged carriers, and the deployment flexibility of the unmanned aerial vehicles and the operation quick response capability of the unmanned aerial vehicles are improved. Moreover, the flexibility, response speed and operation efficiency of the unmanned aerial vehicle are improved, and better technical support is provided for the industries such as emergency command, inspection, agriculture and forestry monitoring.

Description

Technical Field

[0001] The present application relates to the technical field of drone hangars, and in particular to a vehicle-mounted dual-drone automatic hangar. Background Art

[0002] A drone hangar is a facility specifically designed for the storage and management of drones. It is also known as a drone nest or drone warehouse. The primary function of a drone hangar is to provide services such as drone parking and management. Drone hangars play a crucial role in the drone industry, not only improving the efficiency and effectiveness of drone use but also providing a safe and secure environment for drones, ensuring their safe storage and operation.

[0003] Existing drone hangars typically accommodate a single drone. When drones are required to complete different missions, each drone completing these tasks consumes significant time, reducing operational efficiency. Furthermore, existing drone hangars are typically fixed in a specific location, limiting the drone's operational range and preventing widespread operations. When an emergency occurs, the drone hangar cannot quickly reach its designated location, preventing the drone from preparing for takeoff quickly and failing to provide rapid response capabilities. Utility Model Content

[0004] The purpose of this application is to provide a vehicle-mounted dual-UAV automatic hangar, which can improve the flexibility and rapid response capability of UAV deployment and improve operational efficiency.

[0005] To achieve the above objectives, the present application provides a vehicle-mounted dual-UAV automatic hangar, comprising a vehicle and a hangar body. The vehicle is provided with a housing with a take-off and landing door. The hangar body comprises a frame and two sub-hangars, the frame being mounted within the housing, the two sub-hangars being fixed to the frame, the two sub-hangars being arranged along a predetermined direction parallel to the horizontal direction, the two sub-hangars being communicatively connected, the frame being detachably connected to the vehicle, the sub-hangars being used to park UAVs, and the UAVs entering and exiting the housing through the take-off and landing doors.

[0006] In one embodiment, the hangar body further includes a vibration absorber, which is provided on the rack and the rack abuts against the carrier via the vibration absorber, and is used to absorb vibration transmitted from the rack to the carrier and from the carrier to the rack.

[0007] In one embodiment, the sub-hangar further includes a revolving plate and a locking pin. The revolving plate is rotatably mounted on the rack, and the two sub-hangars are mounted on corresponding revolving plates. The revolving plate rotates relative to the rack to drive the sub-hangar to rotate relative to the rack; the locking pin is detachably connected to the revolving plate and the rack to lock or unlock the revolving plate and the rack.

[0008] In one embodiment, the hangar body also includes a lifting frame, which is fixedly connected to the frame. The lifting frame includes a frame portion and a lifting portion, and the frame portion is fixedly connected to the hangar body; the lifting portion provides a lifting point for lifting the hangar body, and at least two lifting portions are arranged on the frame portion, and at least two of the lifting portions are evenly distributed on the frame portion around the first center of gravity. The first center of gravity is the common center of gravity after the frame portion and the hangar body are fixedly connected.

[0009] In one embodiment, the hangar body further includes a quick-install part, and the rack is detachably mounted on the carrier via the quick-install part.

[0010] In one embodiment, the quick-install part includes a connecting rod and a mounting seat, the connecting rod is connected to the frame; the mounting seat is arranged on the carrier, the mounting seat has a matching hole, the connecting rod is installed at the matching hole of the mounting seat, and more than two mounting seats are arranged along the extension direction of the connecting rod to support the connecting rod.

[0011] In one embodiment, the quick-release component further includes a pin connector, which is disposed on the carrier, a fixing hole is provided on the pin connector, and a pin hole is provided on the connecting rod. The pin shaft passes through the pin hole of the connecting rod and the fixing hole of the pin connector to lock the connecting rod. The pin shaft is removed to unlock the connecting rod, and the connecting rod is made to slide axially in the matching hole to disengage the connecting rod from the mounting seat, and the frame is disconnected from the carrier.

[0012] In one embodiment, the sub-hangar further includes an annular parking rack, which is arranged on the rack, and the central through hole of the annular parking rack is used for parking drones.

[0013] In one embodiment, the hangar body further includes an angle sensor, which is disposed on the rack and is used to detect an inclination angle of the rack relative to a horizontal plane.

[0014] In one embodiment, the hangar body further includes a controller, the controller is electrically connected to the angle sensor, and the angle sensor sends the tilt angle to the controller.

[0015] In one embodiment, the hangar body further includes a communication module, the communication module is electrically connected to the controller, and the controller establishes a communication connection with external equipment through the communication module.

[0016] In one embodiment, the hangar body further includes a power supply, which is electrically connected to the controller and provides electrical energy to the hangar body. The power supply is electrically connected to a charging port and receives electrical energy through the charging port.

[0017] In one embodiment, the housing is provided with an inspection hatch for inspection and maintenance.

[0018] The vehicle-mounted dual-drone automatic hangar provided by this application can improve the deployment range and adaptability of drones through the provided vehicles. By transporting the automatic hangar and drones by vehicles, the problem of excessive energy consumption of drones can be solved, and the flexibility of drone deployment and the rapid response capability of drone operations can be improved. In addition, the design of one hangar and two drones provides more options for drone operation modes. You can choose each drone to perform different tasks separately, or you can choose two drones to perform a task at the same time, or you can choose two drones to perform a task in succession to ensure uninterrupted operation. This solution further improves the flexibility, response speed and operating efficiency of drones, and provides better technical support for industries such as emergency command, inspection, agriculture, and forestry monitoring.

[0019] Other features and advantages of the present application will be described in detail in the subsequent detailed description. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following is a brief introduction to the drawings required for use in the embodiments. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without creative work.

[0021] Figure 1 This is a structural schematic diagram from one perspective of one embodiment of a vehicle-mounted dual-UAV automatic hangar provided by this application;

[0022] Figure 2 This is a schematic structural diagram from two perspectives of one embodiment of a vehicle-mounted dual-UAV automatic hangar provided by this application;

[0023] Figure 3 for Figure 2 Cross-sectional view along the AA axis;

[0024] Figure 4This is a schematic diagram of the structure of a portion of the vehicle-mounted dual-UAV automatic hangar provided by the present application from three perspectives;

[0025] Figure 5 for Figure 4 A partial enlarged view of point B in the middle, with the obstructing plate hidden in the picture.

[0026] icon:

[0027] 100-Vehicle;

[0028] 200 - hangar body; 210 - frame; 220 - quick-release parts; 222 - connecting rod; 224 - mounting base; 226 - pinned base; 230 - shock absorber; 240 - sub-hangar; 242 - annular parking frame; 244 - drive plate;

[0029] 250 - controller; 252 - angle sensor; 254 - communication module; 256 - power supply; 270 - slewing plate; 275 - locking pin; 280 - housing; 282 - take-off and landing door; 284 - maintenance door; 290 - first spring fixing seat; 292 - second spring fixing seat;

[0030] 300-hoisting frame; 310-frame body; 320-hoisting part;

[0031] 400-UAV. DETAILED DESCRIPTION

[0032] To make the objectives, technical solutions, and advantages of the embodiments of the present application more clear, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the accompanying drawings of the embodiments of the present application. Obviously, the described embodiments are only some of the embodiments of the present application, not all of the embodiments. Generally, the components of the embodiments of the present application described and shown in the drawings herein can be arranged and designed in various different configurations.

[0033] In the description of this application, it should be noted that the terms "inner" and "outer" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, or the orientations or positional relationships in which the product of this application is typically placed when in use. These terms are intended solely to facilitate the description of this application and simplify the description, and are not intended to indicate or imply that the device or element referred to must have a specific orientation, be constructed, or operate in a specific orientation. Therefore, they should not be construed as limitations on this application. Furthermore, the terms "first" and "second" and the like are used solely for distinction and should not be construed as indicating or implying relative importance.

[0034] It should also be noted that, in the description of this application, unless otherwise expressly specified or limited, the terms "disposed" and "connected" should be understood broadly. For example, they can refer to fixed connections, detachable connections, or integral connections; they can refer to direct connections, indirect connections through an intermediate medium, or internal connections between two components. Those skilled in the art will understand the specific meanings of the above terms in this application based on the specific circumstances.

[0035] The embodiment of the present application provides a vehicle-mounted dual-UAV automatic hangar, such as Figure 1 As shown, the vehicle-mounted dual-UAV automatic hangar includes a vehicle 100 and a hangar body 200. By way of example, the vehicle 100 includes but is not limited to: a vehicle, a ship, or an aircraft. The provision of the vehicle 100 expands the deployment range and adaptability of the UAV 400.

[0036] The vehicle 100 is provided with a housing 280, and the housing 280 is provided with a take-off and landing door 282 for the drone 400 to enter and exit the housing 280. Exemplarily, the take-off and landing door 282 is sealed, but in another embodiment, the take-off and landing door 282 is hollowed out.

[0037] The hangar body 200 includes a frame 210, which is detachably connected to the vehicle 100 and located within the housing 280. This allows the hangar body 200 to be detachably mounted on the vehicle 100 via the frame 210, and movement of the vehicle 100 can drive movement of the hangar body 200. The detachable connection between the frame 210 and the vehicle 100 facilitates installation and removal of the hangar body 200, increasing flexibility.

[0038] Two sub-hangars 240 for parking the drone 400 are arranged in sequence along a preset direction on the rack 210. The sub-hangar 240 is set on the rack 210. For example, the preset direction is roughly parallel to the horizontal direction, and the preset direction may have an angle α with the forward direction of the vehicle 100, where 0°≤α≤180°.

[0039] The two sub-hangars 240 are communicatively connected, and the sub-hangar 240 is used to park the UAV 400 , which enters and exits the housing 280 through the take-off and landing door 282 .

[0040] The dual-unit design provides more options for the UAV 400's operational modes. Each UAV 400 can independently perform different tasks, two UAVs 400 can simultaneously perform a single task, or two UAVs 400 can perform a task in sequence to ensure uninterrupted operation. This solution further enhances the UAV 400's flexibility, responsiveness, and operational efficiency, providing enhanced technical support for industries such as emergency command, inspection, agriculture, and forestry monitoring.

[0041] like Figure 4 As shown, in one embodiment, the hangar body 200 further includes a shock absorber 230, which is disposed on the rack 210 and the rack 210 abuts against the carrier 100 through the shock absorber 230. The shock absorber 230 is used to absorb vibrations transmitted from the rack 210 to the carrier 100 and to absorb vibrations transmitted from the carrier 100 to the rack 210.

[0042] For example, Figure 4 As shown, the shock absorber 230 includes a coil spring, the axis of which is parallel to the horizontal direction, and the coil spring is disposed between the carrier 100 and the frame 210 .

[0043] For example, Figure 4 As shown, a first spring retainer 290 is provided on the frame 210, and a second spring retainer 292 is provided on the carrier 100. The first spring retainer 290 and the second spring retainer 292 are arranged opposite each other, and the coil spring is fixedly arranged between the first spring retainer 290 and the second spring retainer 292. In another embodiment, this embodiment differs from the above embodiment in that the axis of the coil spring is arranged in the vertical direction or the axis forms an angle with the vertical direction.

[0044] However, in another embodiment, the shock absorber is one of the following: a butterfly spring, an annular spring, a leaf spring, a steel plate spring, a rubber spring or an air spring, etc.

[0045] The vibration damper 230 effectively isolates and absorbs vibrations between the frame 210 and the carrier 100. Whether transmitted from the frame 210 to the carrier 100 or vice versa, the vibration damper 230 effectively absorbs the vibrations, thereby reducing the impact of vibrations on the overall stability of the mechanical structure. Vibration isolation and absorption improve the overall stability of the mechanical structure. This is particularly important for mechanical structures requiring high-precision operation, as reducing vibrations helps improve operational accuracy and reliability.

[0046] like Figures 3 to 5 As shown, in one embodiment, sub-hangar 240 includes a ring-shaped docking rack 242 and a drive plate 244 .

[0047] The annular parking frame 242 is provided on the frame 210 , and the central through hole of the annular parking frame 242 is used for parking the UAV 400 .

[0048] like Figure 4 As shown, a plurality of driving plates 244 are slidably mounted on the annular docking frame 242 . For example, the plurality of driving plates 244 are distributed around the axial circumference of the annular docking frame 242 .

[0049] As multiple drive plates 244 synchronously approach the central through-hole of the annular docking frame 242, they push the drone 400 to move, thereby bringing the drone 400 closer to and securing it in the central through-hole of the annular docking frame 242. Once the drone 400 is secured to the annular docking frame 242, maintenance can be performed on the drone 400. In this exemplary embodiment, three drive plates 244 are provided. In other embodiments, four, five, or six drive plates 244 may be provided.

[0050] By sliding and synchronously moving the drive plate 244, the drone 400 can be automatically pushed into the central through-hole of the annular docking frame 242 and secured. This automated design not only improves the efficiency of parking the drone 400, but also reduces the tedious manual operation, making the entire system more intelligent.

[0051] In one embodiment, a connection terminal for electrically connecting to the drone 400 is provided on one end of the driving plate 244 near the center of the annular docking frame 242. For example, multiple driving plates 244 are provided, with the connection terminals on some driving plates 244 serving as power supply terminals and the connection terminals on other driving plates 244 serving as communication terminals.

[0052] like Figures 4 and 5 As shown, in one embodiment, the sub-hangar 240 further includes a swing plate 270 and a locking pin 275 .

[0053] Figure 5 for Figure 4 The local enlarged view of point B in the middle, and Figure 5 Hidden in the middle Figure 4 The plate structure of the middle shielding rotating plate 270. Figure 5 As shown, the rotating plate 270 is rotatably mounted on the frame 210, and the annular docking frame 242 is mounted on the rotating plate 270. The rotation of the rotating plate 270 relative to the frame 210 drives the annular docking frame 242 to rotate relative to the frame 210. The rotation of the rotating plate 270 allows for convenient adjustment of the angle of the annular docking frame 242, the drone 400, and other components mounted thereon.

[0054] Locking pin 275 detachably connects swivel plate 270 and frame 210, locking the swivel plate 270 to the frame 210. When maintenance is required on drone 400 or related components, simply remove locking pin 275 from swivel plate 270 and frame 210. This allows for easy rotation of swivel plate 270, positioning annular docking frame 242 and the equipment mounted thereon in a convenient position. This design significantly improves the convenience and efficiency of maintenance.

[0055] When the drone 400 is in use, the locking pin 275 is connected to the rotating plate 270 and the frame 210 so that the rotating plate 270 and the frame 210 are relatively locked, ensuring that the drone 400 can be parked and taken off normally.

[0056] The design of the swing plate 270 ensures greater flexibility while maintaining overall stability. Whether taking off, docking, or performing maintenance on the UAV 400, the angle of the swing plate 270 can be adjusted to meet varying needs. This flexibility not only enhances the adaptability of the hangar body 200 but also allows for greater operational flexibility and versatility.

[0057] like Figure 3 As shown, in one embodiment, the hangar body 200 further includes a lifting frame 300, which is fixedly connected to the rack 210. After the hangar body 200 is disconnected from the carrier 100, the lifting equipment lifts the rack 210 and the hangar body 200 as a whole by connecting the lifting frame 300.

[0058] The hanging frame 300 includes a frame body 310 and a hanging portion 320 .

[0059] The frame portion 310 is fixedly connected to the hangar body 200. For example, the frame portion 310 is fixedly connected to the frame 210 by welding, bolt connection, riveting, clamping or integral molding.

[0060] The hoisting sections 320 provide lifting points for the hangar body 200. At least two hoisting sections 320 are provided on the frame 310, evenly distributed around the first center of gravity of the frame 310. The first center of gravity is the common center of gravity of the frame 310 and the hangar body 200 after they are fixedly connected. This layout ensures more uniform force on the hangar body 200 during the lifting process, avoids structural distortion or damage caused by single-point lifting, and enhances the stability of the overall structure.

[0061] For example, Figure 3 As shown, four hanging parts 320 are provided. In another embodiment, two hanging parts 320 are provided. Of course, in other embodiments, other numbers of hanging parts 320 can also be provided, such as five, six, etc.

[0062] The introduction of the lifting frame 300 allows the hangar body 200 to be easily lifted as a whole by lifting equipment after the hangar body 200 is disconnected from the carrier 100. This design greatly simplifies the movement and transportation process of the hangar body 200 and facilitates the maintenance of the hangar body 200.

[0063] like Figure 4As shown, in one embodiment, the hangar body 200 further includes a quick-installation component 220, through which the rack 210 can be detachably mounted on the carrier 100. The rack 210 can be quickly mounted on the carrier 100 using the quick-installation component 220 and locked using a pin. The rack 210 can also be quickly unlocked by removing the pin, making the connection and disconnection of the rack 210 to the carrier 100 very simple and quick.

[0064] like Figure 4 As shown, the quick-install component 220 includes a connecting rod 222 and a mounting seat 224 .

[0065] like Figure 4 As shown, the connecting rod 222 is connected to the frame 210. A mounting base 224 is provided on the carrier 100. The mounting base 224 has a matching hole. The connecting rod 222 is mounted at the matching hole of the mounting base 224. Two or more mounting bases 224 are provided along the extension direction of the connecting rod 222 to support the connecting rod 222 and indirectly support the frame 210.

[0066] For example, Figure 4 As shown, two mounting bases 224 are provided. Of course, in other embodiments, three, four or five mounting bases 224 can also be provided.

[0067] The mounting seat 224 is provided with two or more matching holes to support the connecting rod 222 , which increases the stability and support of the frame 210 on the carrier 100 and ensures the stability and reliability of the mechanical structure during operation.

[0068] like Figure 4 As shown, in another embodiment, the quick-install component 220 further includes a pin connector 226. The pin connector 226 is disposed on the carrier 100, and the connecting rod 222 is detachably connected to the pin connector 226 via a pin shaft to lock the connecting rod 222. Removing the pin shaft unlocks the connecting rod 222, allowing the connecting rod 222 to slide axially within the mating hole, thereby disengaging the connecting rod 222 from the mounting seat 224. This disconnects the rack 210 from the carrier 100, thereby disconnecting the hangar body 200 from the carrier 100. The hangar body 200 can then be removed from the carrier 100 for maintenance or replacement of another hangar body 200 on the carrier 100.

[0069] However, in another embodiment, the technical solution in which the quick-install part 220 in the above embodiment includes a connecting rod 222, a mounting seat 224 and a pin-connecting seat 226 can also be replaced by the following technical solution: the quick-install part 220 includes a connecting seat, which is fixedly connected to the frame 210, and a threaded hole is provided on the connecting seat. The connecting seat is fixedly mounted on the carrier 100 by bolts. By removing the bolts, the connecting seat can be disconnected from the carrier 100, and the hangar body 200 can be disconnected from the carrier 100.

[0070] The introduction of quick-install components 220 enables rapid installation and removal between the hangar body 200 and the carrier 100, simplifying the maintenance process for the mechanical structure. When maintenance or replacement of the rack 210 or carrier 100 is required, the rack 210 can be easily removed and reinstalled without requiring complex operations or disassembly of other components. This rapid installation and removal significantly improves work efficiency. For example, in situations where frequent replacement of the rack 210 or carrier 100 is required, this arrangement can significantly reduce the time and labor costs required for replacement.

[0071] like Figure 4 As shown, in one embodiment, the hangar body 200 further includes an angle sensor 252, which is disposed on the annular mooring frame 242. The angle sensor 252 is used to detect the inclination angle of the annular mooring frame 242 relative to the horizontal plane to confirm whether it affects the take-off and landing of the drone 400, thereby ensuring the safe use of the drone 400.

[0072] like Figure 3 As shown, in one embodiment, the hangar body 200 further includes a controller 250 .

[0073] The controller 250 is electrically connected to the angle sensor 252, and the angle sensor 252 converts the detection result into an electrical signal and sends it to the controller 250. The controller 250 is, for example, a central processing unit (CPU), a programmable logic controller (PLC), or an electronic device with logic control function.

[0074] In one embodiment, the hangar body 200 further includes a communication module 254 .

[0075] The communication module 254 is electrically connected to the controller 250, and the controller 250 establishes a communication connection with external devices through the communication module 254. Exemplarily, the external devices include, but are not limited to, drone 400, computers, mobile phones, tablets, or other smart platforms. For example, the controller 250 can send the detection results of the angle sensor 252 to the drone 400 via the communication module 254. After receiving the signal, the drone 400 determines whether it can take off and land on the circular docking station 242. Alternatively, the controller 250 determines whether the drone 400 can take off and land on the circular docking station 242 after receiving the detection results of the angle sensor 252, and then sends a signal indicating whether the drone 400 can take off and land to the drone 400 via the communication module 254.

[0076] For example, the communication module 254 includes a positioning unit and an image transmission unit. The positioning unit is used to exchange position information with external devices, and the image transmission unit is used to exchange image information with external devices. Figure 1 and Figure 2 As shown, the communication module 254 is disposed on the housing 280 .

[0077] The positioning unit and the image transmission unit are respectively connected to external devices for communication.

[0078] In one embodiment, the image transmission unit includes an antenna signal transmitter for communicating with external devices. The antenna signal transmitter is mounted on the housing 280 and has a ceramic outer shell to prevent rainwater from entering the antenna signal transmitter. However, in another embodiment, the antenna signal transmitter can be handheld or mounted on the vehicle 100.

[0079] In one embodiment, the housing 280 has a mounting opening, and a mounting shell is provided at the mounting opening of the housing 280. The mounting shell has an opening through which the positioning unit is installed into the mounting shell. The mounting shell is provided with an end cap at the opening, which can seal the opening to prevent rainwater from entering the mounting shell and damaging the communication module 254. Of course, in other embodiments, the positioning unit can also be handheld or mounted on the vehicle 100. The antenna used by the positioning unit is an RTK antenna.

[0080] like Figure 3 As shown, in one embodiment, the hangar body 200 further includes a power supply 256. The power supply 256 provides electrical energy to the hangar body 200. The hangar body 200 supplies power to the drone 400 via the connection terminals. The power supply 256 can also power electrical components such as the controller 250 and the angle sensor 252. For example, the controller 250 is electrically connected to the power supply 256.

[0081] The power supply 256 is electrically connected to the charging port, and the power supply 256 receives power through the charging port. For example, the power supply 256 receives power from the power grid and the vehicle 100 through the charging port.

[0082] For example, the power supply 256 can store electrical energy, regulate voltage, and the like.

[0083] like Figure 1 and Figure 2 As shown, in one embodiment, the housing 280 is further provided with an inspection hatch 284 .

[0084] It should be noted that, unless there is any conflict, the features in the embodiments of this application can be combined with each other.

[0085] The above description is merely a preferred embodiment of the present application and is not intended to limit the present application. Various modifications and variations are possible for those skilled in the art. Any modifications, equivalent substitutions, or improvements made within the spirit and principles of the present application shall be included within the scope of protection of the present application.

Claims

1. A vehicle-mounted dual-UAV automatic hangar, characterized in that: include: A vehicle (100), wherein a housing (280) is provided on the vehicle (100), and a take-off and landing door (282) is provided on the housing (280); A hangar body (200) is provided, wherein the hangar body (200) comprises a rack (210) and two sub-hangars (240), wherein the rack (210) is installed in the shell (280), and the two sub-hangars (240) are fixed on the rack (210), and the two sub-hangars (240) are distributed along a preset direction, wherein the preset direction is parallel to the horizontal direction, and the two sub-hangars (240) are communicatively connected to each other, and the rack (210) is detachably connected to the vehicle (100), and the sub-hangars (240) are used for parking a drone (400), and the drone (400) enters and exits the shell (280) through the take-off and landing door (282).

2. The vehicle-mounted dual-UAV automatic hangar according to claim 1 is characterized in that: The hangar body (200) further includes: A vibration damper (230) is provided on the frame (210), and the frame (210) abuts against the carrier (100) via the vibration damper (230), and the vibration damper (230) is used to absorb vibration transmitted from the frame (210) to the carrier (100) and to absorb vibration transmitted from the carrier (100) to the frame (210).

3. The vehicle-mounted dual-UAV automatic hangar according to claim 1 is characterized in that: The sub-hangar (240) further comprises: A rotating plate (270), wherein the rotating plate (270) is rotatably mounted on the frame (210), and the two sub-hangars (240) are mounted on corresponding rotating plates (270), and the rotating plate (270) rotates relative to the frame (210) to drive the sub-hangars (240) to rotate relative to the frame (210); A locking pin (275) is provided, wherein the locking pin (275) is detachably connected to the rotating plate (270) and the frame (210), so as to lock or unlock the rotating plate (270) and the frame (210).

4. The vehicle-mounted dual-UAV automatic hangar according to claim 1 is characterized in that: The hangar body (200) further includes: A hanging frame (300), the hanging frame (300) is fixedly connected to the frame (210), and the hanging frame (300) comprises: A frame portion (310), wherein the frame portion (310) is fixedly connected to the hangar body (200); A hoisting portion (320), wherein the hoisting portion (320) provides a hoisting point for hoisting the hangar body (200), and at least two hoisting portions (320) are provided on the frame portion (310), and at least two hoisting portions (320) are evenly distributed around a first center of gravity on the frame portion (310), wherein the first center of gravity is the common center of gravity of the frame portion (310) and the hangar body (200) after being fixedly connected.

5. The vehicle-mounted dual-UAV automatic hangar according to claim 1 is characterized in that: The hangar body (200) further includes: A quick-install part (220), through which the frame (210) is detachably mounted on the carrier (100).

6. The vehicle-mounted dual-UAV automatic hangar according to claim 5 is characterized in that: The quick-install part (220) includes: a connecting rod (222), the connecting rod (222) being connected to the frame (210); A mounting seat (224) is provided on the carrier (100), the mounting seat (224) having a matching hole, the connecting rod (222) being installed at the matching hole of the mounting seat (224), and more than two mounting seats (224) are provided along the extending direction of the connecting rod (222) to support the connecting rod (222).

7. The vehicle-mounted dual-UAV automatic hangar according to claim 6 is characterized in that: The quick-install part (220) further includes: A pin connection seat (226), the pin connection seat (226) is arranged on the carrier (100), a fixing hole is provided on the pin connection seat (226), and a pin hole is provided on the connecting rod (222), a pin shaft passes through the pin hole of the connecting rod (222) and the fixing hole of the pin connection seat (226) to lock the connecting rod (222), and the pin shaft is removed to unlock the connecting rod (222), so that the connecting rod (222) slides axially in the matching hole, so that the connecting rod (222) is disengaged from the mounting seat (224), and the frame (210) is disconnected from the carrier (100).

8. The vehicle-mounted dual-UAV automatic hangar according to claim 1 is characterized in that: The sub-hangar (240) further comprises: An annular mooring frame (242) is provided on the frame (210), and a central through hole of the annular mooring frame (242) is used for mooring a drone (400).

9. The vehicle-mounted dual-UAV automatic hangar according to claim 1 is characterized in that: The hangar body (200) further includes: An angle sensor (252) is provided on the frame (210), and the angle sensor (252) is used to detect an inclination angle of the frame (210) relative to a horizontal plane.

10. The vehicle-mounted dual-UAV automatic hangar according to claim 9 is characterized in that: The hangar body (200) further includes: A controller (250) is electrically connected to the angle sensor (252), and the angle sensor (252) sends the tilt angle to the controller (250).

11. The vehicle-mounted dual-UAV automatic hangar according to claim 10, characterized in that: The hangar body (200) further includes: A communication module (254) is electrically connected to the controller (250), and the controller (250) establishes a communication connection with an external device through the communication module (254).

12. The vehicle-mounted dual-UAV automatic hangar according to claim 10, characterized in that: The hangar body (200) further includes: A power supply (256), the power supply (256) is electrically connected to the controller (250), the power supply (256) provides electrical energy to the hangar body (200), the power supply (256) is electrically connected to a charging port, and the power supply (256) receives electrical energy through the charging port.

13. The vehicle-mounted dual-UAV automatic hangar according to any one of claims 1 to 12, characterized in that: The housing (280) is provided with an inspection hatch (284) for inspection and maintenance.

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