Unmanned aerial vehicle storage and recovery cabin
By using the magnetic control of magnet plates and iron sheets in the drone storage and recovery cabin, the drone is automatically fixed and unlocked, solving the problems of complex operation and high labor intensity in the existing technology, improving operating efficiency and protecting the drone.
Patent Information
- Application Number
- CN202421170220.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-27
- Publication Date
- 2025-01-21
- Estimated Expiration
- 2034-05-27
AI Technical Summary
The existing drone storage recycling chamber lacks an automatic fixation mechanism, and operators need to manually fix and unlock the drone, increasing operational complexity and labor intensity.
A UAV storage and recovery cabin is designed, which uses a magnet plate to magnetically attract or separate from the iron pieces on the supporting feet. The hydraulic cylinder drives the magnet plate to move to realize automatic fixing and unlocking of the UAV.
The drone can be stably fixed and taken off without manual intervention, which improves the convenience and efficiency of operation, reduces labor intensity, and provides a buffering effect through the cooperation of springs and guide rods to protect the drone.
Smart Images

Figure CN222373140U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of unmanned aerial vehicles, and specifically relates to a storage and recovery cabin of an unmanned aerial vehicle. Background Art
[0002] A UAV, or unmanned aircraft, is an unmanned aircraft that is controlled by a radio remote control device and a self-contained program control device, or is operated completely or intermittently autonomously by an onboard computer. With the rapid development of UAV technology, UAVs are being used more and more widely in aerial photography, reconnaissance, environmental monitoring and other fields.
[0003] Existing drone storage and recovery cabins lack an automatic fixing mechanism when the drone is parked on the parking board. Operators need to manually use clamping or locking mechanisms to fix the drone, which undoubtedly increases the complexity and tediousness of the operation. Similarly, before the drone takes off, it also needs to be manually unlocked, further increasing the labor intensity. Utility Model Content
[0004] The purpose of this utility model is to provide a storage and recovery cabin for drones, which can control the magnetic attraction or separation between the magnet plate and the iron sheet on the support foot, so as to stably fix the drone body on the support plate, or facilitate the drone body to take off from the support plate, without manual intervention, thereby greatly improving the convenience and efficiency of operation.
[0005] The technical solutions adopted in this utility are as follows:
[0006] A drone storage and recovery cabin comprises a storage cabin body, wherein a first hydraulic cylinder is provided on the inner bottom wall of the storage cabin body, a movable plate is fixed to the output shaft of the first hydraulic cylinder, a plurality of guide holes are formed through the top of the movable plate, a first guide rod is installed with a damping slide inside the guide hole, a mounting box is fixed to the top ends of the plurality of first guide rods, a second hydraulic cylinder is fixed to the inner bottom wall of the mounting box, a magnet plate is fixed to the output shaft of the second hydraulic cylinder, a support plate is provided on the inner side of the mounting box and above the magnet plate, a drone body is provided above the support plate, two supporting feet are provided at the bottom of the drone body, and iron sheets that are magnetically attracted to the magnet plate are provided at the bottoms of the supporting feet.
[0007] Furthermore, sliding blocks are fixed on both sides of the movable plate, and a sliding groove slidably connected to the sliding blocks is provided on the inner side of the storage compartment.
[0008] Furthermore, a non-slip rubber pad is provided on the top of the support plate, and the thickness of the non-slip rubber pad and the support plate is two millimeters.
[0009] Furthermore, a spring is provided on the outer wall of the first guide rod and between the movable plate and the installation box.
[0010] Furthermore, telescopic guide rods are provided on the inner bottom wall of the installation box and on both sides of the second hydraulic cylinder, and the top ends of the telescopic guide rods are fixed to the bottom wall of the magnet plate.
[0011] The technical effects achieved by this utility model are:
[0012] The practical drone storage and recovery cabin is provided with a magnet plate, which is driven to move by a second hydraulic cylinder, thereby controlling the magnetic attraction or separation between the magnet plate and the iron sheet on the supporting foot, thereby stably fixing the drone body on the supporting board, or facilitating the drone body to take off from the supporting board, without the need for manual intervention, greatly improving the convenience and efficiency of operation, and reducing labor intensity. The provided spring, first guide rod and guide hole enable the installation box to have a buffering and shock-absorbing effect, thereby buffering the drone body at the moment when the supporting foot on the drone body contacts the supporting board, avoiding hard collision and damage between the drone body and the supporting board, and is relatively complete. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model in a front view;
[0014] Figure 2 It is a side view cutaway structural schematic diagram of the present utility model.
[0015] In the accompanying drawings, the components represented by the reference numerals are listed as follows:
[0016] 1. Storage cabin; 2. First hydraulic cylinder; 3. Moving plate; 4. First guide rod; 5. Mounting box; 6. Spring; 7. Second hydraulic cylinder; 8. Magnet plate; 9. Support plate; 10. UAV body; 11. Support foot; 12. Iron sheet; 13. Telescopic guide rod; 14. Cabin door. DETAILED DESCRIPTION
[0017] In order to make the purpose and advantages of the present invention more clearly understood, the present invention is specifically described below in conjunction with the embodiments. It should be understood that the following text is only used to describe one or several specific implementations of the present invention, and does not strictly limit the scope of protection specifically requested by the present invention.
[0018] like Figure 1-2As shown, the UAV storage and recovery cabin includes a storage cabin body 1, and the inner bottom wall of the storage cabin body 1 is provided with a first hydraulic cylinder 2, and the output shaft of the first hydraulic cylinder 2 is fixed with a movable plate 3, which is convenient for pushing the UAV body 10 out of the storage cabin body 1 or storing it in the storage cabin body 1, which is more practical. A plurality of guide holes are opened through the top of the movable plate 3, and the first guide rod 4 is installed with a damping sliding inside the guide hole, so that the movement of the installation box 5 is more stable, and the tops of the plurality of first guide rods 4 are fixed with an installation box 5, and the inner bottom wall of the installation box 5 is fixed with a second hydraulic cylinder 7, and the output shaft of the second hydraulic cylinder 7 is fixed with a magnet plate 8, and a support plate 9 is provided on the inner side of the installation box 5 and above the magnet plate 8, and the support plate 9 is made of iron plate and has good magnetic conductivity. A UAV body 10 is arranged above the support plate 9, and two supporting feet 11 are arranged at the bottom of the UAV body 10, and the bottom of the supporting feet 11 An iron sheet 12 is provided which is magnetically attracted to the magnet plate 8, and has a simple structure and is easy to operate. Through the cooperation of the magnet plate 8 and the iron sheet 12, the drone body 10 can be stably fixed on the support plate 9, without the need for a complicated locking mechanism. The iron sheet 12 only needs to be simply fitted with the magnet plate 8 to ensure that the drone body 10 is firmly and stably fixed on the support plate 9, which greatly improves the convenience and efficiency of operation, and can also store the drone body 10 in the storage cabin 1 for protection; a spring 6 is provided on the outer wall of the first guide rod 4 and between the movable plate 3 and the mounting box 5, and the provided spring 6 cooperates with the first guide rod 4 and the guide hole to make the support plate 9 have a buffering effect, so that the moment the supporting foot 11 on the drone body 10 contacts the support plate 9, the drone body 10 can be buffered, thereby reducing the impact force of the drone body 10 and protecting the drone body 10 from damage;
[0019] like Figure 2 As shown, sliders are fixed on both sides of the movable plate 3, and a slide groove slidably connected to the slider is provided on the inner side of the storage cabin 1, so that the movement of the movable plate 3 is relatively stable, and the movement of the movable plate 3 can be limited so that the top of the support plate 9 is just kept on the same plane as the top wall of the hatch 14;
[0020] like Figure 2 As shown, a non-slip rubber pad is provided on the top of the support plate 9. The thickness of the non-slip rubber pad and the support plate 9 is two millimeters, which increases the friction between the support plate 9 and the support foot 11, thereby increasing the stability of the drone body 10 parked on the support plate 9;
[0021] like Figure 2 As shown, telescopic guide rods 13 are provided on the inner bottom wall of the mounting box 5 and on both sides of the second hydraulic cylinder 7, and the top of the telescopic guide rods 13 is fixed to the bottom wall of the magnet plate 8, so that the up and down movement of the magnet plate 8 is relatively stable and relatively perfect;
[0022] like Figure 1-2As shown, two opposing doors 14 are slidably installed on the top of the storage cabin 1, which is relatively complete and convenient for protecting the UAV in the storage cabin 1.
[0023] The working principle of the utility model is as follows: when recovering the UAV, the second hydraulic cylinder 7 is started to drive the magnet plate 8 to move upward, so that the magnet plate 8 contacts the support plate 9. When the support foot 11 on the UAV body 10 contacts the support plate 9, the magnet plate 8 and the iron sheet 12 are attracted away by the magnetic force, and the support foot 11 is stably sucked on the support plate 9. At the same time, the spring 6 is arranged to cooperate with the first guide rod 4 and the guide rod, so that the installation box 5 has a buffering effect, thereby buffering the UAV body 10 parked on the support plate 9, avoiding the support foot 11 on the UAV body 10 from being damaged when it contacts the support plate 9, and effectively protecting the UAV body 10.
[0024] The above is only a preferred embodiment of the present invention. It should be noted that, for ordinary technicians in the field, several improvements and modifications can be made without departing from the principle of the present invention, and these improvements and modifications should also be regarded as the protection scope of the present invention. The structures, devices and operating methods not specifically described and explained in the present invention shall be implemented according to the conventional means in the field unless otherwise specified and limited.
Claims
1. UAV storage and recovery cabin, characterized by: The invention comprises a storage cabin (1), wherein a first hydraulic cylinder (2) is arranged on the inner bottom wall of the storage cabin (1), a movable plate (3) is fixed to the output shaft of the first hydraulic cylinder (2), a plurality of guide holes are formed through the top of the movable plate (3), a first guide rod (4) is installed in a damping sliding manner inside the guide hole, a mounting box (5) is fixed to the top of the plurality of first guide rods (4), a second hydraulic cylinder (7) is fixed to the inner bottom wall of the mounting box (5), a magnet plate (8) is fixed to the output shaft of the second hydraulic cylinder (7), a support plate (9) is arranged on the inner side of the mounting box (5) and above the magnet plate (8), a drone body (10) is arranged above the support plate (9), two support feet (11) are arranged at the bottom of the drone body (10), and an iron sheet (12) which is magnetically attracted to the magnet plate (8) is arranged at the bottom of the support feet (11).
2. The drone storage and recovery cabin according to claim 1, characterized in that: Slide blocks are fixed on both sides of the movable plate (3), and a sliding groove slidably connected to the slide blocks is provided on the inner side of the storage compartment (1).
3. The drone storage and recovery cabin according to claim 1, characterized in that: The top of the support plate (9) is provided with an anti-skid rubber pad, and the thickness of the anti-skid rubber pad and the support plate (9) is two millimeters.
4. The drone storage and recovery cabin according to claim 1, characterized in that: A spring (6) is provided on the outer wall of the first guide rod (4) and is located between the moving plate (3) and the installation box (5).
5. The drone storage and recovery cabin according to claim 1, characterized in that: Telescopic guide rods (13) are arranged on the inner bottom wall of the installation box (5) and on both sides of the second hydraulic cylinder (7), and the top ends of the telescopic guide rods (13) are fixed to the bottom wall of the magnet plate (8).
6. The drone storage and recovery cabin according to claim 1, characterized in that: Two opposing doors (14) are slidably mounted on the top of the storage compartment (1).