Automatic storage device for vehicle-mounted unmanned aerial vehicle

Abstract

The present application relates to a kind of automatic storage device of vehicle-mounted unmanned plane, comprising: take-off and landing platform, locking mechanism and lifting assembly, take-off and landing platform is erected in the shelter frame of transport vehicle, take-off and landing platform is connected with the lifting assembly of the inner wall of shelter frame by support frame, and guide positioning hole is provided on take-off and landing platform;Wherein, lifting assembly is used to drive support frame to move vertically along the inner wall of shelter frame so that take-off and landing platform enters or pushes out vehicle-mounted shelter, simultaneously drives locking mechanism to move vertically, so that lever assembly drives locking pin assembly to slide horizontally, from locking hole into locking sleeve to limit locking the foot structure of unmanned plane, or exit locking hole to release the fixed locking of unmanned plane.The device guarantees the stability of unmanned plane carrying, realizes the automatic storage locking and release locking of unmanned plane after landing in vehicle-mounted shelter.

Description

Technical Field

[0001] This invention relates to the field of vehicle-mounted drone technology, and more specifically to an automatic storage device for vehicle-mounted drones. Background Technology

[0002] Vehicle-mounted drone systems typically involve a vehicle carrying the drone and its associated systems. During operation, the drone needs to be manually moved out of the vehicle and taken off from the ground. Upon landing, the drone touches the ground and is manually moved into a designated container and secured. The method of securing the drone within the container varies, but nylon cable ties are commonly used. One end is fixed to the bottom of the container, and the other end is looped around any protruding part of the drone, such as the arm, and then tightened through the fasteners. Before takeoff, personnel enter the vehicle-mounted container, manually unfasten several nylon cable ties, and remove the drone from the container for takeoff. Upon landing, the drone touches the ground and is manually moved to its designated storage location within the container, where it is secured with cable ties. If the drone is not securely fixed or is not securely secured within the container, the shaking and bumps caused by the vehicle's movement can potentially cause fatal damage to the drone. This also reduces the drone's ease of use and hinders rapid, automated deployment and retrieval.

[0003] Therefore, there is a need to provide a vehicle-mounted drone automatic storage device to solve the above problems. Summary of the Invention

[0004] This invention provides a vehicle-mounted drone automatic storage device to solve the problems of poor ease of use of existing drones, which are not conducive to rapid and automatic deployment and rapid and automatic storage.

[0005] The present invention provides a vehicle-mounted drone automatic storage device with the following technical solution, comprising: The take-off and landing platform is horizontally erected within the cabin frame of the transport vehicle. It is connected to the lifting components installed on the inner wall of the cabin frame via a support frame, and is equipped with guide positioning holes for guiding the leg structure of the UAV. The locking mechanism includes: a locking sleeve, which is connected to the bottom of the support frame and corresponds one-to-one with the guide positioning holes; a locking pin assembly is horizontally slidably arranged on the support frame on the side of the locking sleeve facing the inside of the cabin frame; the locking end of the locking pin assembly matches the locking hole provided on the side of the locking sleeve; and a lever assembly is also provided on the inner wall of the cabin frame. The lifting assembly is used to drive the support frame to move vertically along the inner wall of the cabin frame, so that the take-off and landing platform can enter or exit the cabin. At the same time, it drives the locking mechanism to move vertically, so that the lever assembly moves the locking pin assembly to slide horizontally from the locking hole into or out of the locking sleeve, thereby limiting and locking or unlocking the UAV's foot structure.

[0006] Preferably, it also includes an on-board controller and a trigger switch. The trigger switch is installed inside the locking sleeve through a switch mounting hole at the bottom of the locking sleeve. The trigger switch and the lifting assembly are both electrically connected to the on-board controller. The on-board controller is used to control the lifting assembly to drive the take-off and landing platform and the locking mechanism to descend together when the UAV's foot structure enters the locking sleeve and triggers the trigger switch, until the locking pin assembly synchronously touches the lever assembly. The lever assembly moves the locking pin assembly to limit and lock the UAV's foot structure.

[0007] Preferably, the support structure includes: a support column, the bottom of which is connected to a nylon ball head via a vibration damping piston rod, and an annular locking groove is formed on the outer periphery of the vibration damping piston rod.

[0008] Preferably, the locking pin assembly includes: A horizontally positioned locking support, one end of which is connected to a support frame, and a slide rail is provided on its top; The slider is slidably connected to the top of the slide rail, and a locking pin is provided on it. The locking pin corresponds to the locking hole, and the locking end of the locking pin matches the locking groove. A limit seat is located at the end of the locking support opposite to the locking sleeve; And a reset component, which is mounted on the locking support, for resetting the slider; The locking support has a through groove for the lever assembly to pass through, the slider has a hole for the lever assembly to move the slider, and the limiting seat is used to restrict the movement of the slider so that the hole on the slider after reset matches the lever assembly.

[0009] Preferably, the reset component includes: A spring seat is located at the bottom of the locking support, and a mounting hole is provided at one end; The spring spindle is fitted into the mounting hole, and a connecting plate is provided at its end outside the mounting hole. The connecting plate is connected to the slider through a guide groove on the locking support. And a return spring, which is sleeved on the spring spindle, with one end connected to the mounting hole and the other end connected to the connecting plate.

[0010] Preferably, the lever assembly is connected to the inner wall of the container frame via a locking lever support. The lever assembly includes a base, which is disposed on the locking lever support. A locking lever is disposed on the top of the base. The locking lever is inclined in the direction away from the locking sleeve and matches the locking hole.

[0011] Preferably, the lifting assembly includes: The drive motor is located at the bottom of the modular housing frame; The lead screw guide rail slider assembly is vertically installed on the inner wall of the cabin frame. Its input end is connected to the output end of the drive motor through a synchronous belt transmission assembly, and its output end is connected to the support frame.

[0012] Preferably, the lead screw guide slider assembly includes: The lead screw is vertically and rotatably mounted on the inner wall of the container frame, and its lower end is connected to the output end of the drive motor through a synchronous belt drive assembly. The guide rails are set parallel to the lead screw on the inner walls of the container frame on both sides of the lead screw. The guide rail slider is mounted on the lead screw and slidably connected to the guide rail, and its side is connected to the support frame.

[0013] Preferably, it further includes a tensioning assembly for tensioning the synchronous belt of the synchronous belt drive assembly.

[0014] Preferably, the guide positioning hole is a conical hole, and the larger end of the conical hole faces upward.

[0015] The beneficial effects of this invention are: Since the vehicle-mounted container configured on the drone carrier, as a protective enclosure, often does not meet the requirements for equipment installation in terms of structural rigidity and dimensional accuracy, this invention configures a container frame for equipment installation within the vehicle-mounted container. The take-off and landing platform, locking mechanism, and lifting assembly are all mounted on the container frame. The lifting assembly controls the locking mechanism to lock the drone landing on the take-off and landing platform. Simultaneously, the drone is retracted into the container frame along with the lifting assembly, thus completing the drone's retraction and locking. In other words, this invention ensures the stability of the drone during transport, realizes automatic retraction, locking, and unlocking of the drone after landing in the vehicle-mounted container without manual intervention, and the overall mechanism is basically a mechanical mechanism, reducing the control logic of the entire system and improving the reliability of the entire system.

[0016] Secondly, the take-off and landing platform is equipped with guide positioning holes for guiding the drone's foot structure. When the drone automatically lands on the platform, it facilitates the entry of the drone's foot structure into the locking sleeve of the locking component, thus enabling the locking pin of the locking component to lock the drone's foot structure. This guides the drone, which has landed on the platform, to the correct locking position, preparing for subsequent automatic locking. Guided by the guide positioning holes, the drone's foot structure enters the retracted posture, and each foot structure enters the locking sleeve of the retracted locking mechanism. At this time, the trigger switch senses that the drone's foot structure has entered the correct locking position, and then controls the lifting component to drive the lifting platform and the locking mechanism to descend together. When the drone reaches the locking position inside the cabin, the locking mechanism simultaneously touches the lever component set on the inner wall of the cabin frame, driving the locking pin component to limit and lock the drone's foot structure. This causes the locking pin of the locking mechanism to extend and enter the locking groove of the drone's foot structure inside the locking sleeve, thereby locking the drone. Attached Figure Description

[0017] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0018] Figure 1 This is a schematic diagram of the overall structure of an automatic storage device for a vehicle-mounted drone according to the present invention; Figure 2 This is a state diagram of the automatic drone storage device for vehicles according to the present invention, showing the start of drone storage. Figure 3 This is a schematic diagram showing the unlocked state of the locking mechanism and the foot structure of the drone in an embodiment of the present invention; Figure 4 This is a schematic diagram illustrating the locking process of the locking mechanism and the foot structure of the UAV in an embodiment of the present invention. Figure 5 This is a schematic diagram of the locking mechanism in an embodiment of the present invention; Figure 6 This is a schematic diagram showing the locked state of the locking mechanism and the foot structure of the UAV in an embodiment of the present invention; Figure 7 This is a cross-sectional view of the locking mechanism in an embodiment of the present invention; Figure 8 This is a schematic diagram of the locking sleeve in an embodiment of the present invention; Figure 9 This is a schematic diagram of the lever assembly in an embodiment of the present invention; Figure 10 This is a schematic diagram of the locking pin structure in an embodiment of the present invention.

[0019] In the diagram: 1. Unmanned Aerial Vehicle (UAV); 2. Transport Vehicle; 11. Support Leg Structure; 111. Locking Slot; 21. Container Frame; 22. Guide Rail; 23. Take-off and Landing Platform; 24. Locking Mechanism; 25. Tensioning Assembly; 26. Synchronous Belt Drive Assembly; 27. Lever Assembly; 28. Support Frame; 221. Guide Rail Slider; 241. Locking Sleeve; 242. Trigger Switch; 243. Locking Pin Assembly; 2411. Locking Hole; 2412. Switch Mounting Hole; 2431. Locking Pin; 2432. Slide Rail; 2433. Return Spring; 2434. Spring Spindle; 2435. Connecting Plate; 2436. Limit Seat; 2437. Lever Hole; 2438. Locking Support; 271. Locking Lever Support. Detailed Implementation

[0020] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0021] An embodiment of the vehicle-mounted drone automatic storage device of the present invention, such as... Figure 1 and Figure 2 As shown, it includes: a take-off and landing platform 23 and a locking mechanism 24. The take-off and landing platform 23 is horizontally erected within a container frame 21 in the cargo compartment of the transport vehicle 2. The take-off and landing platform 23 is connected to a lifting assembly installed on the inner wall of the container frame 21 via a support frame 28. The take-off and landing platform 23 is provided with guide positioning holes for guiding the leg structure 11 of the UAV 1. Figure 4 As shown, the locking mechanism 24 includes: a locking sleeve 241, which is connected to the bottom of the support frame 28, and the locking sleeve 241 corresponds one-to-one with the guide positioning holes. A locking pin assembly 243 is horizontally slidably disposed on the support frame 28 on the side of the locking sleeve 241 facing the inside of the cabin frame 21. Figure 8 As shown, the locking end of the locking pin assembly 243 matches the locking hole 2411 provided on the side of the locking sleeve 241, and also includes a lever assembly 27 provided on the inner wall of the cabin frame 21; wherein, the lifting assembly is used to drive the support frame 28 to move vertically along the inner wall of the cabin frame 21 so that the take-off and landing platform 23 enters the cabin, and at the same time drives the locking mechanism 24 to move vertically, so that the lever assembly 27 moves the locking pin assembly 243 to slide horizontally from the locking hole 2411 into the locking sleeve 241 to limit and lock the foot structure 11 of the UAV 1.

[0022] Specifically, it also includes the vehicle controller and trigger switch 242, such as Figure 3 and Figure 8 As shown, the trigger switch 242 is installed inside the locking sleeve 241 through the switch mounting hole 2412 at the bottom of the locking sleeve 241. The trigger switch 242 and the lifting assembly are both electrically connected to the vehicle controller. The vehicle controller is used to control the lifting assembly to drive the take-off and landing platform to descend together with the locking mechanism when the foot structure 11 of the UAV 1 enters the locking sleeve 241 and triggers the trigger switch 242. When the UAV 1 reaches the locking position inside the cabin frame 21, the dial hole 2437 of the locking mechanism 24 simultaneously touches the locking lever of the lever assembly 27 provided on the inner wall of the cabin frame 21. The locking lever drives the locking pin assembly 243 to limit and lock the foot structure 11 of the UAV.

[0023] Specifically, such as Figure 4As shown, the support structure 11 includes: a support column, the bottom of which is connected to a nylon ball head via a vibration damping piston rod. An annular locking groove 111 is formed on the outer periphery of the vibration damping piston rod. It should be noted that the final locking of the drone 1 is achieved by inserting a locking pin into a locking sleeve in the locking mechanism, which then engages with the locking groove 111 of the support structure of the drone 1. The support structure 11 is as follows... Figure 2 As shown, the support column of the support structure 11 is installed on the bottom surface of the drone body. The bottom of the support column has an installation hole. The vibration damping piston rod is sleeved in the installation hole. A vibration damping spring is connected between the end of the vibration damping piston rod and the bottom surface of the installation hole at the bottom of the support column to achieve vibration damping of the drone 1.

[0024] Specifically, such as Figure 5 and Figure 7 As shown, the locking pin assembly 243 includes: a horizontally arranged locking support 2438, a slider, a limit seat 2436, and a reset assembly. One end of the locking support 2438 is connected to the support frame 28, and a slide rail 2432 is provided on the top of the locking support 2438; the slider is slidably connected to the top of the slide rail 2432, as shown. Figure 5 and 10 As shown, a horizontally positioned locking pin 2431 is fixed to the slider by screws. The locking pin 2431 corresponds to the locking hole 2411, and the locking end of the locking pin 2431 matches the locking groove 111. A limiting seat 2436 is disposed on the end of the locking support 2438 away from the locking sleeve 241. A reset assembly is disposed on the locking support 2438 for resetting the slider. The locking support 2438 has a through groove for the passage of the lever assembly 27, and the slider has a dial hole 2437 for the lever assembly 27 to move the slider. The limiting seat 2436 restricts the movement of the slider so that the dial hole 2437 on the reset slider matches the lever assembly 27. As shown... Figure 5 As shown, the reset assembly includes a spring seat, a spring spindle 2434, and a reset spring 2433. The spring seat is located at the bottom of the locking support 2438, and one end of the spring seat has a mounting hole. The spring spindle 2434 is fitted into the mounting hole. A connecting plate 2345 is provided at the end of the spring spindle 2434 outside the mounting hole. The connecting plate 2345 is connected to the slider through a guide groove on the locking support 2438. The reset spring 2433 is sleeved on the spring spindle 2434. One end of the reset spring 2433 is connected to the mounting hole, and the other end of the reset spring 2433 is connected to the connecting plate 2345.

[0025] Specifically, such as Figure 3 and Figure 9As shown, the lever assembly 27 is connected to the inner wall of the container frame 21 via a locking lever support 271. The lever assembly 27 includes a base, which is mounted on the locking lever support 271. A locking lever is mounted on the top of the base, and the locking lever is inclined away from the locking sleeve 241. The locking lever matches the locking hole 2437. Figure 9 As shown, in this embodiment, the lever assembly 27 is fixed by the mounting plates on both sides and the lever mounting cross plate, and then installed on the inner wall of the cabin frame 21 through the mounting back plate of the lifting assembly. The height of the lever assembly 27 on the lifting assembly in the vehicle cabin determines the storage position of the UAV 1 after entering the cabin. By using its inclined surface to act on the working surface of the dial hole 2437 on the slider of the locking mechanism 24, the slider of the locking mechanism 24 is adjusted to the left and right, so as to lock or unlock the locking pin 2431 to the locking groove 111 of the support structure 11.

[0026] Specifically, the lifting assembly includes a drive motor, a lead screw, and a lead screw guide rail slider assembly. The drive motor is located at the bottom of the cabin frame 21. The lead screw guide rail slider assembly is vertically mounted on the inner wall of the cabin frame 21. The input end of the lead screw guide rail slider assembly is connected to the output end of the drive motor via a synchronous belt transmission assembly 26, and the output end of the lead screw guide rail slider assembly is connected to the support frame 28. In this embodiment, the lead screw guide rail slider assembly includes a lead screw, a guide rail 22, and a guide rail slider 221. The lead screw is vertically and rotatably mounted on the inner wall of the cabin frame 21, and its lower end is connected to the output end of the drive motor via a synchronous belt transmission assembly 26. The guide rail 22 is parallel to the lead screw and is mounted on the inner wall of the cabin frame 21 on both sides of the lead screw. The guide rail slider 221 is mounted on the lead screw and slidably connected to the guide rail 22, and is connected to the support frame 28.

[0027] Specifically, it also includes: tensioning assembly 25, used to tension the synchronous belt of synchronous belt drive assembly 26.

[0028] Specifically, the guide positioning hole is a conical hole, with the larger end of the conical hole facing upwards.

[0029] It should be noted that, as Figure 8 As shown, the switch mounting hole 2412 at the bottom of the locking sleeve 241 is an M12 threaded hole for mounting the trigger switch 242; as Figure 10 As shown, the R7 arc of the locking pin 2431 matches the diameter of the locking ring groove at the front end of the vibration damping locking support.

[0030] Working principle like Figure 2 and Figure 3As shown, during the landing process from the UAV 1 to the landing platform 23, the nylon ball head of the support structure 11 at the bottom of the UAV 1 is guided by the guide positioning hole on the landing platform 23, passes through the support frame 28, and enters the locking sleeve 241 until the nylon ball head contacts the trigger switch 242 at the bottom of the locking sleeve 241. This causes the trigger switch 242 to transmit a trigger signal to the vehicle controller, which controls the drive motor of the lifting assembly to rotate in the forward direction. The drive motor drives the lead screw of the lead screw guide rail slider assembly to rotate through the synchronous belt transmission assembly 26. The guide rail slider 221 connected to the lead screw moves downward along the lead screw under the action of the guide rail 22. At the same time, the support frame 28 connected to the guide rail slider 221 moves downward until the landing platform 23 connected to the support frame 28 is stored in the container frame 21 of the transport vehicle 2. It should be noted that, as Figure 4 and Figure 6 As shown, during the downward movement of the support frame 28, the locking mechanism 24 at the bottom of the support frame 28 will continuously approach the lever assembly 27 until the locking lever of the lever assembly 27 passes through the through groove on the locking support 2438 of the locking pin assembly 243 and enters the dial hole 2437 on the slider of the locking pin assembly 243. Since the locking lever of the lever assembly 27 is inclined away from the locking sleeve 241, after the locking lever enters the dial hole 2437, it will push the slider towards the locking sleeve 241 until the locking pin on the slider is engaged. After passing through the locking hole 2411 on the locking sleeve 241, 2431 enters the locking groove 111 of the support structure 11 inside the locking sleeve 241. At the same time, the connecting plate 2345 of the reset assembly moves to the left along with the slider, compressing the reset spring 2433 in the spring seat to store energy, providing the reset energy required for the unlocking action when the UAV 1 is unlocked and takes off. At this time, the take-off and landing platform reaches the lower limit, and the vehicle controller controls the drive motor to shut down, thus locking the support structure 11 and completing the locking and storage of the UAV 1.

[0031] When the UAV 1 takes off, the on-board controller first controls the drive motor of the lifting assembly to rotate in the opposite direction. The drive motor drives the lead screw of the lead screw guide rail slider assembly to rotate through the synchronous belt transmission assembly 26. The guide rail slider 221 on the lead screw moves upward along the lead screw under the guidance of the guide rail 22. At the same time, the support frame 28 connected to the guide rail slider 221 moves upward until the take-off and landing platform 23 connected to the support frame 28 extends out from the container frame 21 of the transport vehicle 2. It should be noted that during the upward movement of the support frame 28, the locking mechanism 24 at the bottom of the support frame 28 will continuously move away from the lever. As the locking lever of the lever assembly 27 continuously disengages from the dial hole 2437, and due to its tilted orientation away from the locking sleeve 241, coupled with the action of the return spring 2433, the locking lever continuously disengages from the dial hole 2437, pushing the slider to move away from the locking sleeve 241 until the locking pin 2431 on the slider disengages from the locking hole 2411 on the locking sleeve 241. This unlocks the locking mechanism 24 from the foot structure 11 of the UAV 1, allowing the UAV 1 to take off from the landing platform 23. Due to the elastic force of the return spring 2433, the locking mechanism 24 reliably remains in the unlocked state, ensuring smooth storage and locking after the UAV lands again.

[0032] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. A vehicle-mounted automatic storage device for unmanned aerial vehicles, characterized in that, include: The take-off and landing platform is horizontally erected within the cabin frame of the transport vehicle. It is connected to the lifting components installed on the inner wall of the cabin frame via a support frame, and is equipped with guide positioning holes for guiding the leg structure of the UAV. The locking mechanism includes: a locking sleeve, which is connected to the bottom of the support frame and corresponds one-to-one with the guide positioning holes; a locking pin assembly is horizontally slidably arranged on the support frame on the side of the locking sleeve facing the inside of the cabin frame; the locking end of the locking pin assembly matches the locking hole provided on the side of the locking sleeve; and a lever assembly is also provided on the inner wall of the cabin frame. The lifting assembly is used to drive the support frame to move vertically along the inner wall of the cabin frame, so that the take-off and landing platform can enter or exit the cabin. At the same time, it drives the locking mechanism to move vertically, so that the lever assembly moves the locking pin assembly to slide horizontally from the locking hole into or out of the locking sleeve, thereby limiting and locking or unlocking the UAV's foot structure.

2. The vehicle-mounted unmanned aerial vehicle (UAV) automatic storage device according to claim 1, characterized in that, It also includes an on-board controller and a trigger switch. The trigger switch is installed inside the locking sleeve through a switch mounting hole at the bottom of the locking sleeve. The trigger switch and the lifting assembly are both electrically connected to the on-board controller. The on-board controller is used to control the lifting assembly to drive the take-off and landing platform and the locking mechanism to descend together when the drone's foot structure enters the locking sleeve and triggers the trigger switch, until the locking pin assembly touches the lever assembly. The lever assembly moves the locking pin assembly to limit and lock the drone's foot structure.

3. The vehicle-mounted unmanned aerial vehicle (UAV) automatic storage device according to claim 1, characterized in that, The support structure includes: a support column, the bottom of which is connected to a nylon ball head via a vibration damping piston rod, and an annular locking groove is provided on the outer periphery of the vibration damping piston rod.

4. The vehicle-mounted unmanned aerial vehicle automatic storage device according to claim 3, characterized in that, The locking pin assembly includes: A horizontally positioned locking support, one end of which is connected to a support frame, and a slide rail is provided on its top; The slider is slidably connected to the top of the slide rail, and a locking pin is provided on it. The locking pin corresponds to the locking hole, and the locking end of the locking pin matches the locking groove. A limit seat is located at the end of the locking support opposite to the locking sleeve; And a reset component, which is mounted on the locking support, for resetting the slider; The locking support has a through groove for the lever assembly to pass through, the slider has a hole for the lever assembly to move the slider, and the limiting seat is used to restrict the movement of the slider so that the hole on the slider after reset matches the lever assembly.

5. The vehicle-mounted unmanned aerial vehicle (UAV) automatic storage device according to claim 4, characterized in that, The reset component includes: A spring seat is located at the bottom of the locking support, and a mounting hole is provided at one end; The spring spindle is fitted into the mounting hole, and a connecting plate is provided at its end outside the mounting hole. The connecting plate is connected to the slider through a guide groove on the locking support. And a return spring, which is sleeved on the spring spindle, with one end connected to the mounting hole and the other end connected to the connecting plate.

6. The vehicle-mounted unmanned aerial vehicle (UAV) automatic storage device according to claim 1, characterized in that, The lever assembly is connected to the inner wall of the container frame via a locking lever support. The lever assembly includes a base, which is mounted on the locking lever support. A locking lever is mounted on the top of the base and is inclined away from the locking sleeve. The locking lever matches the locking hole.

7. The vehicle-mounted unmanned aerial vehicle automatic storage device according to claim 1, characterized in that, The lifting assembly includes: The drive motor is located at the bottom of the modular housing frame; The lead screw guide rail slider assembly is vertically installed on the inner wall of the cabin frame. Its input end is connected to the output end of the drive motor through a synchronous belt transmission assembly, and its output end is connected to the support frame.

8. The vehicle-mounted unmanned aerial vehicle automatic storage device according to claim 7, characterized in that, The lead screw guide slider assembly includes: The lead screw is vertically and rotatably mounted on the inner wall of the container frame, and its lower end is connected to the output end of the drive motor through a synchronous belt drive assembly. The guide rails are set parallel to the lead screw on the inner walls of the container frame on both sides of the lead screw. The guide rail slider is mounted on the lead screw and slidably connected to the guide rail, and its side is connected to the support frame.

9. The vehicle-mounted unmanned aerial vehicle automatic storage device according to claim 7, characterized in that, Also includes: The tensioning assembly is used to tension the synchronous belt of the synchronous belt drive assembly.

10. The vehicle-mounted unmanned aerial vehicle (UAV) automatic storage device according to claim 1, characterized in that, The guide positioning hole is a tapered hole, with the larger end of the tapered hole facing upwards.

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