Damping device carried on unmanned aerial vehicle and having real-time dynamic positioning function

By designing shock-absorbing devices with buffer components and waterproof components on the drone, the problems of unstable drone landing and aging of the locator in rainy days were solved, and stable drone landing was achieved and the life of the locator was extended.

CN223355883UActive Publication Date: 2025-09-19严泽峰
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Patent Information

Application Number
CN202421076601.6
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-17
Publication Date
2025-09-19
Estimated Expiration
2034-05-17

AI Technical Summary

Technical Problem

Drones have poor stability when landing and are prone to rollover and damage, and their positioning devices are prone to aging in rainy days, reducing their service life.

Method used

A shock-absorbing device including a buffer component and a waterproof component was designed. The buffer component realized the buffering of the UAV through a fixing plate, a fixing block, a connecting rod, a connecting plate, a spring and other structures. The waterproof component protected the GPS real-time dynamic locator through a fixing ring, a protective cover and a connecting column.

Benefits of technology

It improves the landing stability of the drone, avoids rollover damage, and protects the locator in rainy days, extending its service life.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a damping device carried on an unmanned aerial vehicle and having a real-time dynamic positioning function, which comprises a vehicle body, and the outer surface of the vehicle body is fixedly connected with supporting legs. Through the arrangement of the fixing plates, the fixing blocks, the connecting rods, the connecting plates, pressing plates, first springs, limiting columns, telescopic rods, second springs and non-slip mats, when the unmanned aerial vehicle lands, the fixing plates and the fixing blocks are driven to press downwards due to the gravity of the unmanned aerial vehicle, the fixing blocks press downwards to drive the connecting rods to rotate, and the connecting rods rotate to drive the two connecting plates to move towards the opposite sides; and then through cooperative use of a telescopic rod and a second spring, the effect of improving the landing stability of the unmanned aerial vehicle is achieved, and the situation that when the unmanned aerial vehicle lands on the ground, the bottom of the unmanned aerial vehicle is likely to be unstable, and the unmanned aerial vehicle is damaged is avoided. The unmanned aerial vehicle is not buffered, so that the unmanned aerial vehicle is damaged due to rollover.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a shock absorbing device carried on an UAV and having a real-time dynamic positioning function. Background Art

[0002] A drone is an aircraft that can be remotely controlled or flown autonomously. A drone is an autonomous system capable of performing tasks without human intervention. There are many different types of drones and their applications include reconnaissance, surveillance, traffic control, firefighting, agriculture, and entertainment.

[0003] However, the existing technology for drones also has the disadvantage of being difficult to improve the landing stability of the drone. When in use, the bottom of the drone is easily unstable when landing on the ground, and there is no cushioning, which causes the drone to roll over and be damaged. Moreover, the existing technology for drones also has the disadvantage of being difficult to improve the service life of the locator. When in use, rainwater falls on the surface of the locator on rainy days, which easily causes it to age, resulting in a reduction in the service life of the locator. Utility Model Content

[0004] The purpose of the present invention is to provide a shock absorbing device with a real-time dynamic positioning function carried on an unmanned aerial vehicle, so as to solve the problems raised in the above-mentioned background technology.

[0005] To achieve the above objectives, the present invention provides the following technical solutions:

[0006] A shock absorbing device with real-time dynamic positioning function carried on an unmanned aerial vehicle, comprising

[0007] The cam is fixedly connected to the bottom of the base plate, and the cam is fixedly connected to the bottom of the base plate, wherein the cam comprises a fixing plate, a fixing block, a connecting rod, a connecting plate, a pressure plate, a first spring, a limiting column, a telescopic rod, a second spring and an anti-slip pad. The top of the fixing plate is fixedly connected to the bottom of the base plate, one side of the fixing plate is fixedly connected to the fixing block, the outer surface of the fixing block is rotatably connected to the connecting rod, one side of the surface of the connecting rod is rotatably connected to the connecting plate, one side of the connecting plate is fixedly connected to the pressure plate, one side of the pressure plate is fixedly connected to the first spring, the inner side wall of the first spring is sleeved with the limiting column, one side of the bottom of the base plate is fixedly connected to the telescopic rod, the outer surface of the telescopic rod is fixedly connected to the second spring, and the bottom of the second spring is fixedly connected to the anti-slip pad.

[0008] The top of the body is fixedly connected to a waterproof component, which includes a fixing ring, a protective cover, a connecting column and a GPS real-time dynamic locator. The bottom of the fixing ring is fixedly connected to the top of the body, the top surface of the fixing ring is threadedly connected to the protective cover, the inner side wall of the fixing ring is fixedly connected to the connecting column, and one end of the connecting column is fixedly connected to the GPS real-time dynamic locator.

[0009] Preferably, a connecting slot is provided on the top of the anti-slip pad, and the bottom of the limiting column is fixedly connected to the inside of the connecting slot.

[0010] Preferably, the top of the second spring is fixedly connected to one side of the bottom of the base plate, and the bottom of the second spring is fixedly connected to one side of the top of the anti-slip pad.

[0011] Preferably, a circular slot is provided on one side of the top of the anti-slip pad, and the bottom of the telescopic rod is fixedly connected to the inside of the circular slot.

[0012] Preferably, a slot is provided inside the connecting plate, and the outer surface of the connecting rod is rotatably connected to the inside of the slot.

[0013] Preferably, a threaded ring is provided on the top of the surface of the fixing ring, and the bottom of the inner wall of the protective cover is threadedly connected to the outer surface of the threaded ring.

[0014] Compared with the prior art, the beneficial effects of the present invention are:

[0015] 1. A shock absorbing device with a real-time dynamic positioning function carried on a drone, through the arrangement of a fixed plate, a fixed block, a connecting rod, a connecting plate, a pressure plate, a first spring, a limiting column, a telescopic rod, a second spring and an anti-slip pad. When the drone lands, its own gravity drives the fixed plate and the fixed block to press downward, and the downward pressure of the fixed block drives the connecting rod to rotate. The rotation of the connecting rod drives the two connecting plates to move toward the opposite side, and then drives the two pressure plates to be squeezed toward the opposite side, drives the first spring to contract, and then the first spring rebounds and resets to cushion the drone. The telescopic rod and the second spring are used in conjunction with each other to achieve the effect of improving the landing stability of the drone, thereby avoiding the situation where the bottom of the drone is easily unstable when landing on the ground and is not cushioned, resulting in the drone rolling over and causing damage.

[0016] 2. This shock absorbing device with real-time dynamic positioning function carried on a UAV is equipped with a fixing ring, a protective cover, a connecting column and a GPS real-time dynamic locator. On rainy days, the operator can rotate the protective cover and fix it on the surface of the fixing ring. The protective cover can effectively protect the GPS real-time dynamic locator from rain, and the connecting column supports and fixes the GPS real-time dynamic locator, thereby achieving the effect of increasing the service life of the locator and avoiding rainwater falling on the surface of the locator on rainy days, which easily causes it to age and thus reduces the service life of the locator. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the three-dimensional appearance of the utility model;

[0018] Figure 2 This is an enlarged schematic diagram of the buffer component of the present utility model;

[0019] Figure 3 This is a schematic diagram of the partial structure of the buffer component of the utility model;

[0020] Figure 4 For the utility model Figure 2 A in the middle is an enlarged schematic diagram;

[0021] Figure 5 This is a schematic diagram of the disassembly of the waterproof component of the utility model;

[0022] Figure 6 This is a schematic diagram of the positioning system of the present utility model.

[0023] In the figure: 1. Body; 2. Support legs; 3. Bottom plate; 4. Fixing plate; 5. Fixing block; 6. Connecting rod; 7. Connecting plate; 8. Pressing plate; 9. First spring; 10. Limiting column; 11. Telescopic rod; 12. Second spring; 13. Anti-slip pad; 14. Fixing ring; 15. Protective cover; 16. Connecting column; 17. GPS real-time dynamic positioning device; 18. Threaded ring. DETAILED DESCRIPTION

[0024] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0025] See also Figures 1-6 As shown, the utility model provides a technical solution:

[0026] A shock absorbing device with real-time dynamic positioning function carried on an unmanned aerial vehicle, comprising

[0027] The body 1 is fixedly connected to the outer surface of the body 1 with a support leg 2, the bottom of the support leg 2 is fixedly connected to the bottom of the bottom plate 3, and the bottom of the bottom plate 3 is fixedly connected to a buffer assembly, which includes a fixed plate 4, a fixed block 5, a connecting rod 6, a connecting plate 7, a pressure plate 8, a first spring 9, a limiting column 10, a telescopic rod 11, a second spring 12 and an anti-slip pad 13. The top of the fixed plate 4 is fixedly connected to the bottom of the bottom plate 3, and one side of the fixed plate 4 is fixedly connected to the fixed block 5. The outer surface of the fixed block 5 is rotatably connected to the connecting rod 6, and one side of the surface of the connecting rod 6 is rotatably connected to the connecting plate 7. One side of the connecting plate 7 is fixedly connected to the pressure plate 8, and one side of the pressure plate 8 is fixedly connected to the first spring 9. The inner side wall of the first spring 9 is sleeved with the limiting column 10. The bottom side of the bottom plate 3 is fixed A telescopic rod 11 is fixedly connected, and a second spring 12 is fixedly connected to the outer surface of the telescopic rod 11. The bottom of the second spring 12 is fixedly connected to an anti-slip pad 13. When the drone lands, the fixed plate 4 and the fixed block 5 are pressed downward due to their own gravity. The downward pressure of the fixed block 5 drives the connecting rod 6 to rotate. The rotation of the connecting rod 6 drives the two connecting plates 7 to move to the opposite side, thereby driving the two pressure plates 8 to squeeze to the opposite side, driving the first spring 9 to contract, and then the first spring 9 rebounds and resets to cushion the drone. The coordinated use of the telescopic rod 11 and the second spring 12 achieves the effect of improving the landing stability of the drone, avoiding the situation where the bottom of the drone is easily unstable when landing on the ground and there is no buffering, resulting in the drone rolling over and causing damage;

[0028] The top of the body 1 is fixedly connected with a waterproof component, which includes a fixing ring 14, a protective cover 15, a connecting column 16 and a GPS real-time dynamic locator 17. The bottom of the fixing ring 14 is fixedly connected to the top of the body 1, and the top of the surface of the fixing ring 14 is threadedly connected with the protective cover 15. The inner side wall of the fixing ring 14 is fixedly connected with the connecting column 16. One end of the connecting column 16 is fixedly connected with the GPS real-time dynamic locator 17. On rainy days, the operator can rotate the protective cover 15 and fix it to the surface of the fixing ring 14. The protective cover 15 can effectively protect the GPS real-time dynamic locator 17 from rain, and the connecting column supports and fixes the GPS real-time dynamic locator 17, thereby achieving the effect of improving the service life of the locator and avoiding rainwater falling on the surface of the locator on rainy days, which easily causes it to age and thus reduces the service life of the locator.

[0029] In this embodiment, preferably, a connecting slot is provided on the top of the anti-slip pad 13, and the bottom of the limiting column 10 is fixedly connected to the inside of the connecting slot;

[0030] In this embodiment, preferably, the top of the second spring 12 is fixedly connected to the bottom side of the bottom plate 3, and the bottom of the second spring 12 is fixedly connected to the top side of the anti-slip pad 13;

[0031] In this embodiment, preferably, a circular slot is opened on one side of the top of the anti-slip pad 13, and the bottom of the telescopic rod 11 is fixedly connected to the inside of the circular slot;

[0032] In this embodiment, preferably, a slot is opened inside the connecting plate 7, and the outer surface of the connecting rod 6 is rotatably connected to the inside of the slot;

[0033] In this embodiment, preferably, a threaded ring 18 is provided on the top of the surface of the fixing ring 14 , and the bottom of the inner wall of the protective cover 15 is threadedly connected to the outer surface of the threaded ring 18 .

[0034] The shock absorbing device of this embodiment, which is mounted on a drone and has a real-time dynamic positioning function, is used. When the drone lands, its own gravity drives the fixing plate 4 and the fixing block 5 to press downward. The downward pressure of the fixing block 5 drives the connecting rod 6 to rotate. The rotation of the connecting rod 6 drives the two connecting plates 7 to move toward opposite sides, thereby driving the two pressure plates 8 to squeeze toward opposite sides, driving the first spring 9 to contract, and then the first spring 9 rebounds and resets to cushion the drone. The telescopic rod 11 and the second spring 12 cooperate with each other to achieve the effect of improving the landing stability of the drone, thereby avoiding the situation where the bottom of the drone is easily unstable when landing on the ground and there is no cushioning, resulting in the drone rolling over and causing damage. In rainy days, the operator can rotate the protective cover 15 and fix it to the surface of the fixing ring 14. The protective cover 15 can effectively protect the GPS real-time dynamic locator 17 from rain, and the connecting column supports and fixes the GPS real-time dynamic locator 17, thereby achieving the effect of improving the service life of the locator, thereby avoiding the situation where rainwater falls on the surface of the locator on rainy days, easily causing it to age, thereby reducing the service life of the locator.

[0035] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely preferred examples of the present invention and are not intended to limit the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention, and such changes and improvements fall within the scope of the present invention. The scope of protection claimed in the present invention is defined by the appended claims and their equivalents.

Claims

1. A shock absorbing device with real-time dynamic positioning function mounted on an unmanned aerial vehicle, characterized by: The device comprises a body (1), the outer surface of the body (1) is fixedly connected to a support leg (2), the bottom of the support leg (2) is fixedly connected to a base plate (3), the bottom of the base plate (3) is fixedly connected to a buffer assembly, the buffer assembly comprises a fixed plate (4), a fixed block (5), a connecting rod (6), a connecting plate (7), a pressure plate (8), a first spring (9), a limiting column (10), a telescopic rod (11), a second spring (12) and an anti-slip pad (13), the top of the fixed plate (4) is fixedly connected to the bottom of the base plate (3), and one side of the fixed plate (4) is fixedly connected to a fixed Block (5), the outer surface of the fixed block (5) is rotatably connected to a connecting rod (6), one side of the surface of the connecting rod (6) is rotatably connected to a connecting plate (7), one side of the connecting plate (7) is fixedly connected to a pressure plate (8), one side of the pressure plate (8) is fixedly connected to a first spring (9), the inner side wall of the first spring (9) is sleeved with a limiting column (10), one side of the bottom of the bottom plate (3) is fixedly connected to a telescopic rod (11), the outer surface of the telescopic rod (11) is fixedly connected to a second spring (12), and the bottom of the second spring (12) is fixedly connected to an anti-slip pad (13); The top of the body (1) is fixedly connected to a waterproof component, and the waterproof component includes a fixing ring (14), a protective cover (15), a connecting column (16) and a GPS real-time dynamic positioning device (17). The bottom of the fixing ring (14) is fixedly connected to the top of the body (1), the top of the surface of the fixing ring (14) is threadedly connected to the protective cover (15), the inner side wall of the fixing ring (14) is fixedly connected to the connecting column (16), and one end of the connecting column (16) is fixedly connected to the GPS real-time dynamic positioning device (17).

2. The shock absorbing device with real-time dynamic positioning function mounted on an unmanned aerial vehicle according to claim 1, characterized in that: A connecting slot is provided on the top of the anti-slip pad (13), and the bottom of the limiting column (10) is fixedly connected to the inside of the connecting slot.

3. The shock absorbing device with real-time dynamic positioning function mounted on an unmanned aerial vehicle according to claim 1, characterized in that: The top of the second spring (12) is fixedly connected to one side of the bottom of the bottom plate (3), and the bottom of the second spring (12) is fixedly connected to one side of the top of the anti-slip pad (13).

4. The shock absorbing device with real-time dynamic positioning function mounted on an unmanned aerial vehicle according to claim 1, characterized in that: A circular slot is provided on one side of the top of the anti-slip pad (13), and the bottom of the telescopic rod (11) is fixedly connected to the inside of the circular slot.

5. The shock absorbing device with real-time dynamic positioning function mounted on an unmanned aerial vehicle according to claim 1, characterized in that: A slot is provided inside the connecting plate (7), and the outer surface of the connecting rod (6) is rotatably connected to the inside of the slot.

6. The shock absorbing device with real-time dynamic positioning function mounted on an unmanned aerial vehicle according to claim 1, characterized in that: A threaded ring (18) is provided on the top of the surface of the fixing ring (14), and the bottom of the inner wall of the protective cover (15) is threadedly connected to the outer surface of the threaded ring (18).