Unmanned aerial vehicle with supporting foot stands

By designing a drone tripod with fixed chassis, straps, cushioning pads, springs and elastic steel, the existing drone tripods are solved, and the effect of convenient installation and effective shock absorption is achieved.

CN222756794UActive Publication Date: 2025-04-15HENAN ZEZHONG BIG DATA TECH CO LTD
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Patent Information

Application Number
CN202421489262.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-27
Publication Date
2025-04-15
Estimated Expiration
2034-06-27

AI Technical Summary

Technical Problem

The existing drone tripods are cumbersome when installed and lack shock absorbing devices, which causes the impact force of the drone to be transmitted to the interior when landing, which may cause damage.

Method used

A drone with a support tripod was designed, using a fixed chassis, straps, cushioning pads, springs and elastic steel structures to achieve easy installation and shock absorption effects.

Benefits of technology

By simplifying the installation process and introducing shock absorbing devices, the installation convenience of the drone and the impact absorption capacity during landing are improved, reducing the risk of damage inside the drone.

✦ 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, and discloses an unmanned aerial vehicle with supporting foot stools, which comprises an unmanned aerial vehicle main body, the bottom of the unmanned aerial vehicle main body is movably connected with a fixed chassis, the outer wall of the fixed chassis is respectively and rotatably connected with a bandage I and a bandage II, and the bottom of the fixed chassis is fixedly provided with a connecting rod. A fixing shell is fixedly installed at the bottom of the connecting rod, and a buffering pad is slidably connected to the inner wall of the fixing shell. An unmanned aerial vehicle body is placed above a fixed chassis, a first binding band penetrates through the outer wall of the unmanned aerial vehicle body to reach the top of the unmanned aerial vehicle body, a second binding band penetrates through a fixed block at the top of the first binding band, and at the moment, a ratchet groove moves below a fixed ratchet by pulling the second binding band; when the unmanned aerial vehicle body is fixed through the second binding band and the first binding band, pulling of the second binding band is stopped, the fixing ratchets press downwards through the first spring, the ratchet grooves are fixed, then the second binding band is fixed, and installation of the second binding band is completed.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a supporting tripod. Background Art

[0002] The drone tripod is a derivative product of the drone, and its function is to support the drone when it takes off and lands.

[0003] When installing the existing drone tripod, it is necessary to pre-install a fixing frame on the bottom of the drone for installing the tripod. The installation is complicated in actual use and it is often necessary to install it before reaching the flight area. At the same time, there is no shock-absorbing device inside. When the drone lands, the tripod at the bottom of the drone directly contacts the ground, causing the impact force generated to be transmitted to the inside of the drone, which may cause damage to the inside of the drone. Utility Model Content

[0004] In view of the deficiencies in the prior art, the utility model provides a drone with a supporting tripod, which has the advantages of being easy to install and having a shock-absorbing effect, and solves the problems raised by the above-mentioned background technology.

[0005] The utility model provides the following technical solution: an unmanned aerial vehicle with a supporting tripod, comprising an unmanned aerial vehicle body, the bottom of the unmanned aerial vehicle body is movably connected with a fixed chassis, the outer walls of the fixed chassis are rotatably connected with a first strap and a second strap, the bottom of the fixed chassis is fixedly installed with a connecting rod, the bottom of the connecting rod is fixedly installed with a fixed shell, the inner wall of the fixed shell is slidably connected with a buffer pad, the top of the first strap is fixedly installed with a fixed block, the inner wall of the fixed block is slidably connected with a fixed ratchet, the top of the fixed ratchet is fixedly installed with a pull rod, the top of the fixed ratchet is provided with a first spring, the top of the second strap is provided with a ratchet groove, the top of the buffer pad is fixedly installed with a limiting column, the inner wall of the fixed shell is provided with a second spring, the inner wall of the fixed shell is slidably connected with a sliding block, and the bottom of the sliding block is fixedly installed with elastic steel.

[0006] As a preferred technical solution of the utility model, a rectangular groove is provided on the outer wall of the fixing block, and the rectangular groove passes through the fixing block, and the shape of the rectangular groove on the outer wall of the fixing block is adapted to the shape of the second binding strap.

[0007] As a preferred technical solution of the utility model, the top of the pull rod passes through the fixed block, and there are two pull rods and spring one, the two pull rods and spring one are symmetrically distributed inside the fixed block, and connecting plates are provided on the tops of the two pull rods to connect the two pull rods.

[0008] As a preferred technical solution of the utility model, the fixed ratchet is located above the ratchet groove, and the size of the fixed ratchet is matched with that of the ratchet groove.

[0009] As a preferred technical solution of the utility model, the number of the sliding blocks is two, and the two sliding blocks are connected to the two ends of the elastic steel, and the bottom of the elastic steel overlaps the top surface of the buffer pad.

[0010] As a preferred technical solution of the utility model, the top of the limiting column penetrates the top of the fixed shell, and an extension ring is provided on the top of the limiting column. The diameter of the extension ring on the top of the limiting column is larger than the through hole through which the limiting column penetrates the fixed shell.

[0011] Compared with the prior art, the utility model has the following beneficial effects:

[0012] 1. The drone with a supporting tripod is installed by placing the drone body above a fixed chassis, passing the first strap through the outer wall of the drone body to the top of the drone body, passing the second strap through the fixed block on the top of the first strap, and pulling the second strap to move the ratchet groove below the fixed ratchet. When the second strap and the first strap fix the drone body, stop pulling the second strap, and the fixed ratchet is pressed downward by the first spring to fix the ratchet groove, thereby fixing the second strap, and completing the installation.

[0013] 2. When the drone with a supporting tripod lands on the ground with the drone body, the buffer pad faces the ground. When the buffer pad contacts the ground, the buffer pad is pushed upward by the impact force. At this time, the buffer pad moves upward to drive the limit column to move upward, thereby causing the second spring to contract and at the same time press the top surface of the elastic steel upward to deform the elastic steel, thereby causing the two ends of the elastic steel to move to both sides, driving the two sliding blocks to move to both sides, and absorbing the impact force during landing through the elastic steel and the second spring. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0015] Figure 2 This is a schematic diagram of the fixed chassis structure of the utility model;

[0016] Figure 3 This is a schematic diagram of the structure of the fixed block of the utility model;

[0017] Figure 4 This is a schematic diagram of the elastic steel structure of the utility model;

[0018] Figure 5 This is a schematic diagram of the ratchet groove structure of the utility model.

[0019] In the figure: 1. UAV body; 2. Fixed chassis; 3. Strap 1; 4. Strap 2; 5. Connecting rod; 6. Fixed shell; 7. Buffer pad; 8. Fixed block; 9. Fixed ratchet; 10. Pull rod; 11. Spring 1; 12. Ratchet groove; 13. Limiting column; 14. Spring 2; 15. Elastic steel; 16. Sliding block. DETAILED DESCRIPTION

[0020] 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.

[0021] See also Figure 1 - Figure 5 A drone with a supporting tripod comprises a drone body 1, a fixed chassis 2 is movably connected to the bottom of the drone body 1, a strap 1 3 and a strap 2 4 are rotatably connected to the outer wall of the fixed chassis 2, a connecting rod 5 is fixedly installed at the bottom of the fixed chassis 2, a fixed shell 6 is fixedly installed at the bottom of the connecting rod 5, a buffer pad 7 is slidably connected to the inner wall of the fixed shell 6, a fixed block 8 is fixedly installed at the top of the strap 1 3, a fixed ratchet 9 is slidably connected to the inner wall of the fixed block 8, a pull rod 10 is fixedly installed on the top of the fixed ratchet 9, a spring 11 is provided on the top of the strap A ratchet groove 12 is provided on the top of the second 4, a limiting column 13 is fixedly installed on the top of the buffer pad 7, a spring second 14 is provided on the inner wall of the fixed shell 6, a sliding block 16 is slidably connected to the inner wall of the fixed shell 6, and an elastic steel 15 is fixedly installed on the bottom of the sliding block 16. In the above structure, there are two connecting rods 5, fixed shells 6, buffer pads 7, limiting columns 13, springs second 14, elastic steel 15 and sliding blocks 16, and the two connecting rods 5, fixed shells 6, buffer pads 7, limiting columns 13, springs second 14, elastic steel 15 and sliding blocks 16 are symmetrically distributed on both sides of the bottom of the fixed chassis 2.

[0022] In a preferred embodiment, a rectangular groove is provided on the outer wall of the fixing block 8, and the rectangular groove passes through the fixing block 8. The shape of the rectangular groove on the outer wall of the fixing block 8 is adapted to the shape of the strap 2 4. In the above structure, by passing the strap 2 4 through the square groove on the outer wall of the fixing block 8, it passes through the square groove on the outer wall of the fixing block 8 to reach the other side of the fixing block 8. At this time, pulling the strap 2 4 can adjust the length of the strap 2 4 passing through the fixing block 8, so that the tightness between the strap 2 4 and the strap 1 3 can be adjusted.

[0023] In a preferred embodiment, the top of the pull rod 10 passes through the fixed block 8, and the number of the pull rods 10 and the spring 11 is two, the two pull rods 10 and the spring 11 are symmetrically distributed inside the fixed block 8, and the tops of the two pull rods 10 are provided with connecting plates to connect the two pull rods 10. In the above structure, by pulling the connecting plate on the top of the pull rod 10 upward, the two pull rods 10 are driven to move upward, and then the fixed ratchet 9 is driven to move upward, so that the spring 11 on the top of the fixed ratchet 9 contracts.

[0024] In a preferred embodiment, the fixed ratchet 9 is located above the ratchet groove 12, and the fixed ratchet 9 is adapted to the size of the ratchet groove 12. In the above structure, the ratchet groove 12 at the top of the strap 2 4 is moved by pulling the strap 2 4, and the ratchet groove 12 is moved so that the fixed ratchet 9 is squeezed upward by the movement of the ratchet groove 12, so that the strap 2 4 can be pulled. When the strap 2 4 stops pulling, the fixed ratchet 9 is bounced between the ratchet grooves 12 by the downward elastic force of the spring 11, and the ratchet direction of the fixed ratchet 9 and the ratchet direction of the ratchet groove 12 make the ratchet groove 12 fixed by the fixed ratchet 9.

[0025] In a preferred embodiment, there are two sliding blocks 16, and the two sliding blocks 16 are connected to the two ends of the elastic steel 15, and the bottom of the elastic steel 15 overlaps the top surface of the buffer pad 7. In the above structure, when the buffer pad 7 contacts the ground, the buffer pad 7 moves upward, thereby driving the bottom of the elastic steel 15 to move upward, so that the two ends of the elastic steel 15 expand, driving the two sliding blocks 16 to move to both sides, and absorbing the impact force.

[0026] In a preferred embodiment, the top of the limiting column 13 penetrates the top of the fixed shell 6, and an extension ring is provided on the top of the limiting column 13. The diameter of the extension ring on the top of the limiting column 13 is larger than the through hole through which the limiting column 13 penetrates the fixed shell 6. In the above structure, the limiting column 13 is limited by the extension ring on the top of the limiting column 13, so that the limiting column 13 cannot be separated from the fixed shell 6.

[0027] Working principle: when using the device, the drone body 1 is placed above the fixed chassis 2, and the strap 1 3 is placed on the top of the drone body 1, and the strap 2 4 is passed through the square groove on the outer wall of the fixed block 8, so that it passes through the square groove on the outer wall of the fixed block 8 to reach the other side of the fixed block 8, and the ratchet groove 12 at the top of the strap 2 4 is moved by pulling the ratchet groove 12, and the ratchet groove 12 squeezes the fixed ratchet 9 upward through the movement of the ratchet groove 12, so that the strap 2 4 can be pulled, and when the strap 2 4 stops pulling, the fixed ratchet 9 is bounced into between the ratchet grooves 12 by the downward elastic force of the spring 11, and the ratchet direction of the fixed ratchet 9 and the ratchet direction of the ratchet groove 12 make the ratchet groove 12 be fixed The ratchet The tooth 9 is fixed. At this time, the drone body 1 is fixed on the top of the fixed chassis 2 by the strap 1 3 and the strap 2 4. Then, the drone body 1 is installed. The drone body 1 can be manipulated to make it fly. When the drone body 1 is landing, the fixed chassis 2 is facing downward, and the buffer pad 7 is in contact with the bottom surface. When the buffer pad 7 is in contact with the ground, the buffer pad 7 moves upward, thereby driving the bottom of the elastic steel 15 to move upward, so that the two ends of the elastic steel 15 expand, and drive the two sliding blocks 16 to move to both sides. At the same time, due to the upward movement of the buffer pad 7, the limit column 13 is driven to move upward, so that the spring 2 14 contracts, and the impact force during landing is absorbed by the spring 2 14 and the elastic steel 15, so that the impact force on the drone body 1 is reduced.

[0028] 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 with a supporting tripod, comprising a drone body (1), characterized in that: The bottom of the drone body (1) is movably connected to a fixed chassis (2); the outer wall of the fixed chassis (2) is rotatably connected to a first strap (3) and a second strap (4); a connecting rod (5) is fixedly installed at the bottom of the fixed chassis (2); a fixed shell (6) is fixedly installed at the bottom of the connecting rod (5); a buffer pad (7) is slidably connected to the inner wall of the fixed shell (6); a fixed block (8) is fixedly installed at the top of the first strap (3); the inner wall of the fixed block (8) is slidably connected to A fixed ratchet (9), a pull rod (10) is fixedly installed on the top of the fixed ratchet (9), a spring 1 (11) is provided on the top of the fixed ratchet (9), a ratchet groove (12) is provided on the top of the second strap (4), a limit column (13) is fixedly installed on the top of the buffer pad (7), a spring 2 (14) is provided on the inner wall of the fixed shell (6), a sliding block (16) is slidably connected to the inner wall of the fixed shell (6), and an elastic steel (15) is fixedly installed on the bottom of the sliding block (16).

2. The UAV with a supporting tripod according to claim 1, characterized in that: The outer wall of the fixing block (8) is provided with a rectangular groove, and the rectangular groove passes through the fixing block (8), and the shape of the rectangular groove on the outer wall of the fixing block (8) is compatible with the shape of the second binding belt (4).

3. The UAV with a supporting tripod according to claim 1, characterized in that: The top of the pull rod (10) passes through the fixed block (8), and the number of the pull rod (10) and the spring one (11) is two. The two pull rods (10) and the spring one (11) are symmetrically distributed inside the fixed block (8), and a connecting piece is provided on the top of the two pull rods (10) to connect the two pull rods (10).

4. The UAV with a supporting tripod according to claim 1, characterized in that: The fixed ratchet (9) is located above the ratchet groove (12), and the fixed ratchet (9) and the ratchet groove (12) are matched in size.

5. The UAV with a supporting tripod according to claim 1, characterized in that: The number of the sliding blocks (16) is two, and the two sliding blocks (16) are connected to the two ends of the elastic steel (15), and the bottom of the elastic steel (15) overlaps the top surface of the buffer pad (7).

6. The UAV with a supporting tripod according to claim 1, characterized in that: The top of the limiting column (13) penetrates the top of the fixed shell (6), and an extension ring is provided on the top of the limiting column (13). The diameter of the extension ring on the top of the limiting column (13) is larger than the through hole through which the limiting column (13) penetrates the fixed shell (6).