Unmanned aerial vehicle landing protection device

Abstract

The utility model discloses an unmanned aerial vehicle landing protection device, relates to the technical field of unmanned aerial vehicle protection, and provides the following scheme that the unmanned aerial vehicle landing protection device comprises a rack and a buffer mechanism arranged at the bottom of the rack, the buffer mechanism comprises a working assembly and a buffer assembly, the working assembly comprises a connecting plate, the connecting plate is arranged at the bottom of the rack, and the buffer assembly is arranged at the bottom of the rack. By arranging a positioning cone, when the unmanned aerial vehicle lands, the positioning cone can make contact with the ground firstly, the bottom of the positioning cone is inserted into the ground, a certain stabilizing effect is achieved, and the unmanned aerial vehicle is prevented from bouncing and rolling; the supporting length can be controlled by rotating a threaded column, at the moment, the impact force of landing can make a sliding column contract into a groove of a contraction column, the buffering supporting effect is achieved through a first spring, meanwhile, the telescopic column contracts, the elastic supporting effect is achieved through a second spring, lateral buffering is achieved, the impact strength is reduced, and unmanned aerial vehicle equipment is protected.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle protection, in particular to a landing protection device for an unmanned aerial vehicle. Background Art

[0002] A drone is an unmanned aircraft that usually consists of a flight control system and an autonomous navigation system, and can perform flight missions through remote control or preset navigation plans.

[0003] For example, the Chinese utility model patent (CN 220430574 U) discloses a device for protecting a drone from a fall, which includes a fuselage and legs, with legs distributed at the bottom of the fuselage. The device is characterized in that: a support plate is provided below the fuselage, and slide grooves are symmetrically provided on the support plate. A clamping assembly is slidably provided in each slide groove, and each clamping assembly can clamp the legs. A corrugated plate is provided at the bottom of the support plate, a shock absorbing plate is provided at the bottom of the corrugated plate, and a shock absorber is provided between the support plate and the shock absorbing plate. The utility model provides a corrugated plate and a shock absorbing plate at the bottom of the support plate to buffer the impact generated by the collision between the drone and the bottom surface when the drone falls. At the same time, a shock absorber is provided between the support plate and the shock absorbing plate to absorb the impact force between the drone and the bottom surface, thereby reducing the bouncing frequency of the corrugated plate, thereby achieving a protective effect when the drone lands.

[0004] However, in the above patent, the cushioning and shock-absorbing effect is only achieved through the shock-absorbing plate and the protrusions. However, when the drone malfunctions and falls, the impact force is too large, and the corrugated plate not only fails to achieve the cushioning effect, but also increases the height of the bounce, causing further damage to the drone. This patent cannot stabilize the drone in time, the drone will roll over, and the length of the buffer structure cannot be controlled. In addition, the structure is large in size and will block the drone from installing other equipment for operation. The utility model can achieve a good cushioning effect, can solve the problem of drone falling, and quickly complete the disassembly and assembly work. For this reason, a drone landing protection device is needed. Utility Model Content

[0005] The purpose of the utility model is to provide a UAV landing protection device, which solves the problem of buffering and shock-absorbing effects through shock-absorbing plates and protrusions in the prior art. However, when the UAV malfunctions and falls, the impact force is too large, and the corrugated plate not only fails to play a buffering effect, but also increases the height of the bounce, causing further damage to the UAV. This patent cannot stabilize the UAV in time, the UAV will roll over, and the length of the buffer structure cannot be controlled. In addition, the structure is large in size and will block the installation of other equipment on the UAV for operation.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a UAV landing protection device, comprising a frame and a buffer mechanism arranged at the bottom of the frame, wherein the buffer mechanism comprises a working component and a buffer component;

[0007] The working assembly includes a connection plate, the bottom of the frame is provided with a connection plate, the bottom of the connection plate is fixedly connected with a threaded column, and the outer wall of the threaded column is spirally connected with a fixed disk;

[0008] The buffer assembly includes a sliding column, the bottom of the fixed plate is fixedly connected to the sliding column, the outer wall of the sliding column is slidably connected to the contraction column, the outer wall of the contraction column is provided with a first spring, the bottom of the fixed plate is rotatably connected to the telescopic column, the outer wall of the telescopic column is provided with a second spring, and the bottom end of the contraction column is fixedly connected to a positioning cone.

[0009] Preferably, a pressing block is provided at the bottom of the frame, a locking block is fixedly connected to the top of the pressing block, a third spring is fixedly connected to one side of the locking block, a connecting column is slidably connected to the outer wall of the locking block, a fourth spring is fixedly connected to one side of the pressing block, a supporting column is fixedly connected to the bottom of the frame, a bracket is fixedly connected to the bottom end of the supporting column, a connecting rod is fixedly connected to the outer wall of the frame, a blade is provided at one end of the connecting rod, and a camera is fixedly connected to the top of the frame.

[0010] Preferably, the fixed disk and the sliding column are in a fixed connection relationship, and the fixed disk and the sliding column are provided with a thread groove that matches the thread column.

[0011] Preferably, the shrinkage column is provided with a sliding groove matched with the sliding column, and the sliding column and the shrinkage column form a buffer structure through a first spring.

[0012] Preferably, three groups of positioning cones are provided, and the positions of the three groups of positioning cones are symmetrically distributed about the center of the frame, and the positioning cones have a conical appearance.

[0013] Preferably, the connecting column is provided with a sliding groove which matches the pressing block, and the pressing block forms a sliding structure with the connecting column via a fourth spring.

[0014] Preferably, the frame is provided with a sliding groove matched with the engaging block, and the engaging block forms a snap-fit ​​structure with the frame via a pressing block and a third spring.

[0015] Compared with the prior art, the beneficial effects of the utility model are:

[0016] 1. By setting the positioning cone, when the drone lands, the positioning cone will first contact the ground, so that the bottom of the positioning cone is inserted into the ground, which has a certain stabilizing effect and prevents the drone from bouncing and rolling. The length of the support can be controlled by rotating the threaded column. At this time, the impact force of landing will cause the sliding column to shrink into the groove of the contraction column, and the first spring will play a buffering support effect. At the same time, the telescopic column shrinks and relies on the second spring to play an elastic support effect, which can buffer the side, reduce the impact force, and protect the drone equipment.

[0017] 2. By setting the snap-fit ​​block, the user inserts the connecting column into the groove at the bottom of the frame, and the snap-fit ​​block retracts into the groove of the connecting column. When the position is reached, the snap-fit ​​block pops out from the groove of the connecting column by the elastic force of the third spring and is inserted into the slot of the frame to complete the fixation. Then, the snap-fit ​​block is retracted back into the groove of the connecting column by pressing the pressing block, and the connecting column can be quickly installed and disassembled, which is convenient for its inspection and maintenance. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 This is a first-perspective structural diagram of a UAV landing protection device proposed by the utility model;

[0019] Figure 2 This is a second perspective structural schematic diagram of a UAV landing protection device proposed by the utility model;

[0020] Figure 3 This is a schematic diagram of a buffer structure of a UAV landing protection device proposed by the utility model;

[0021] Figure 4 The utility model is a schematic diagram of a buckle structure of a UAV landing protection device.

[0022] In the figure: 1. frame; 2. connecting plate; 3. threaded column; 4. fixed plate; 5. sliding column; 6. retractable column; 7. first spring; 8. telescopic column; 9. second spring; 10. positioning cone; 11. pressing block; 12. engaging block; 13. third spring; 14. connecting column; 15. fourth spring; 16. supporting column; 17. bracket; 18. connecting rod; 19. blade; 20. camera. DETAILED DESCRIPTION

[0023] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0024] Example 1

[0025] like Figure 1-4 As shown, a UAV landing protection device shown in the figure includes a frame 1 and a buffer mechanism arranged at the bottom of the frame 1, and the buffer mechanism includes a working component and a buffer component;

[0026] The working assembly includes a connecting plate 2, the bottom of the frame 1 is provided with the connecting plate 2, the bottom of the connecting plate 2 is fixedly connected with a threaded column 3, and the outer wall of the threaded column 3 is spirally connected with a fixing plate 4;

[0027] The buffer assembly includes a sliding column 5, the bottom of the fixed plate 4 is fixedly connected to the sliding column 5, the outer wall of the sliding column 5 is slidably connected to the contraction column 6, the outer wall of the contraction column 6 is provided with a first spring 7, the bottom of the fixed plate 4 is rotatably connected to the telescopic column 8, the outer wall of the telescopic column 8 is provided with a second spring 9, and the bottom end of the contraction column 6 is fixedly connected to a positioning cone 10.

[0028] Among them, Figure 3 As shown, the fixed plate 4 and the sliding column 5 are fixedly connected, and the fixed plate 4 and the sliding column 5 are provided with thread grooves that match the threaded column 3, which is beneficial for the rotation of the threaded column 3, adjusting the distance between the connecting plate 2 and the fixed plate 4, and controlling the length of the support.

[0029] Among them, Figure 3 As shown, the retractable column 6 is provided with a sliding groove that matches the sliding column 5. The sliding column 5 forms a buffer structure with the retractable column 6 through the first spring 7, which is conducive to retracting the sliding column 5 into the groove of the retractable column 6, providing a buffer distance and reducing the impact force of the drone.

[0030] Among them, Figure 2 As shown, three groups of positioning cones 10 are provided, and the positions of the three groups of positioning cones 10 are symmetrically distributed about the center of the frame 1. The positioning cones 10 have a conical appearance, which is conducive to the positioning cones 10 being inserted into the ground when the drone falls, and can play a certain stabilizing effect, preventing the drone from falling and rolling multiple times.

[0031] Example 2

[0032] like Figure 1 , Figure 2 and Figure 4 As shown, this embodiment further illustrates Example 1, a pressing block 11 is provided at the bottom of the frame 1, a locking block 12 is fixedly connected to the top of the pressing block 11, a third spring 13 is fixedly connected to one side of the locking block 12, a connecting column 14 is slidably connected to the outer wall of the locking block 12, a fourth spring 15 is fixedly connected to one side of the pressing block 11, a supporting column 16 is fixedly connected to the bottom of the frame 1, a bracket 17 is fixedly connected to the bottom end of the supporting column 16, a connecting rod 18 is fixedly connected to the outer wall of the frame 1, a blade 19 is provided at one end of the connecting rod 18, and a camera 20 is fixedly connected to the top of the frame 1.

[0033] Among them, Figure 4 As shown, the connecting column 14 is provided with a sliding groove that matches the pressing block 11. The pressing block 11 forms a sliding structure with the connecting column 14 through the fourth spring 15, which is conducive to pressing the pressing block 11 to retract it back into the groove of the connecting column 14, so that the connecting column 14 is separated from the bottom of the frame 1 and the disassembly and maintenance are completed.

[0034] Among them, Figure 1 As shown, the frame 1 is provided with a sliding groove that matches the locking block 12. The locking block 12 forms a snap-fit ​​structure with the frame 1 through the pressing block 11 and the third spring 13, which is conducive to inserting the locking block 12 into the groove of the frame 1 to complete the fixation and facilitate installation.

[0035] When in use: First, when the drone lands, the positioning cone 10 will first contact the ground, so that the bottom of the positioning cone 10 is inserted into the ground, which has a certain stabilizing effect and prevents the drone from bouncing and rolling. The length of the support can be controlled by rotating the threaded column 3. At this time, the impact force of landing will cause the sliding column 5 to shrink into the groove of the contraction column 6, and the first spring 7 will play a buffering support effect. At the same time, the telescopic column 8 shrinks and relies on the second spring 9 to play an elastic support effect, which can buffer the side, reduce the impact force, and protect the drone equipment;

[0036] Finally, the user inserts the connecting column 14 into the groove at the bottom of the frame 1, and the locking block 12 shrinks back into the groove of the connecting column 14. When the position is reached, the locking block 12 pops out from the groove of the connecting column 14 by the elastic force of the third spring 13, and is inserted into the slot of the frame 1 to complete the fixation. Then, the locking block 12 shrinks back into the groove of the connecting column 14 by pressing the pressing block 11, and the connecting column 14 can be quickly installed and disassembled, which is convenient for its inspection and maintenance.

[0037] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device.

[0038] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A drone landing protection device, comprising a frame (1) and a buffer mechanism arranged at the bottom of the frame (1), characterized in that: The buffer mechanism comprises a working component and a buffer component; The working assembly comprises a connection plate (2), the bottom of the frame (1) is provided with the connection plate (2), the bottom of the connection plate (2) is fixedly connected with a threaded column (3), and the outer wall of the threaded column (3) is spirally connected with a fixed plate (4); The buffer assembly comprises a sliding column (5), the bottom of the fixed plate (4) is fixedly connected to the sliding column (5), the outer wall of the sliding column (5) is slidably connected to a contraction column (6), the outer wall of the contraction column (6) is provided with a first spring (7), the bottom of the fixed plate (4) is rotatably connected to a telescopic column (8), the outer wall of the telescopic column (8) is provided with a second spring (9), and the bottom end of the contraction column (6) is fixedly connected to a positioning cone (10).

2. The UAV landing protection device according to claim 1, characterized in that: A pressing block (11) is provided at the bottom of the frame (1), a locking block (12) is fixedly connected to the top of the pressing block (11), a third spring (13) is fixedly connected to one side of the locking block (12), a connecting column (14) is slidably connected to the outer wall of the locking block (12), a fourth spring (15) is fixedly connected to one side of the pressing block (11), a supporting column (16) is fixedly connected to the bottom of the frame (1), a bracket (17) is fixedly connected to the bottom end of the supporting column (16), a connecting rod (18) is fixedly connected to the outer wall of the frame (1), a blade (19) is provided at one end of the connecting rod (18), and a camera (20) is fixedly connected to the top of the frame (1).

3. The UAV landing protection device according to claim 1, characterized in that: The fixed disk (4) and the sliding column (5) are in a fixed connection relationship, and the fixed disk (4) and the sliding column (5) are provided with a thread groove that matches the thread column (3).

4. The UAV landing protection device according to claim 1, characterized in that: The shrinkage column (6) is provided with a sliding groove that matches the sliding column (5), and the sliding column (5) forms a buffer structure with the shrinkage column (6) through the first spring (7).

5. The UAV landing protection device according to claim 1, characterized in that: Three groups of positioning cones (10) are provided, and the positions of the three groups of positioning cones (10) are symmetrically distributed about the center of the frame (1), and the positioning cones (10) have a conical appearance.

6. The UAV landing protection device according to claim 2, characterized in that: The connecting column (14) is provided with a sliding groove that matches the pressing block (11), and the pressing block (11) forms a sliding structure with the connecting column (14) via a fourth spring (15).

7. The UAV landing protection device according to claim 2, characterized in that: The frame (1) is provided with a sliding groove that matches the locking block (12); the locking block (12) forms a locking structure with the frame (1) via a pressing block (11) and a third spring (13).

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