Protection device for unmanned aerial vehicle high-voltage line inspection
By designing a protective device including lower protection ring pipe, upright pipe and upper protection ring pipe, rubber airbags provide 360-degree protection, the problem that drones cannot be fully protected in the prior art is solved, and the drone is significantly improved Protection effect on falling.
Patent Information
- Application Number
- CN202421339795.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-13
- Publication Date
- 2025-02-07
- Estimated Expiration
- 2034-06-13
AI Technical Summary
The existing airbag protection device for high-voltage line patrol inspection of drones cannot provide 360-degree buffering protection for drones, resulting in easy damage to the wing structure.
A protective device including a lower protection ring tube, a vertical pipe and an upper protection ring tube is designed. Each ring tube is equipped with a rubber airbag, which can inflate and control the airbag through an inflatable cylinder and a microcontroller control board, and when the drone is out of control When falling, the airbag will inflate and provide 360-degree protection to the drone.
It effectively avoids damage to the drone host and fan blade mechanism when falling, and achieves a 360-degree protection effect.
Smart Images

Figure CN222432612U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of unmanned aerial vehicle protection, in particular to a protection device for unmanned aerial vehicle high-voltage line inspection. Background Art
[0002] In recent years, with the development of industry-level drone technology, the inspection of overhead transmission lines is shifting from manual inspection to a collaborative inspection mode dominated by drones. Power inspection drones have extensive and irreplaceable applications in transmission line channel hidden danger inspection, line autonomous inspection, disaster accident special inspection, drone laser point cloud modeling, etc. Most inspection drones are equipped with expensive equipment such as camera gimbals, infrared temperature measurement equipment, and lidar equipment to assist in inspection operations.
[0003] When a drone inspects a high-voltage line, existing structures will use special structures to protect the drone, such as a buffer device for a drone published in announcement CN 218806724 U, whose main features are: it includes an inflatable component and an airbag component; the first side and the second side of the airbag component are symmetrically arranged, and the first side and the second side are respectively provided with pop-up windows for the airbag to pop out; the inflatable component is connected to the third side of the airbag component, and the inflatable component is provided with an air inlet and an inflation port connected to the airbag component, so that the airflow passes through the air inlet, the inflatable component and the inflation port in sequence and enters the airbag component.
[0004] During use of the above-mentioned drone airbag protection device, the applicant found that when the inspection drone falls, the above-mentioned airbag structure will open at the bottom of the drone, and it is impossible to provide 360-degree buffering protection for the drone. When the drone falls, the wing structure of the drone is easily damaged due to collision, and the protection is not comprehensive enough. In order to solve the above-mentioned problems, a protection device for drone high-voltage line inspection is provided. Utility Model Content
[0005] The purpose of the utility model is to provide a protection device for high-voltage line inspection by an unmanned aerial vehicle in order to solve the above-mentioned problems.
[0006] The technical solution adopted by the utility model is as follows: a protective device for unmanned aerial vehicle high-voltage line inspection, including an inspection unmanned aerial vehicle, a landing gear is provided at the lower part of the inspection unmanned aerial vehicle, a plurality of air distribution pipes are fixedly connected to the landing gear, the inner end of the air distribution pipe is fixedly connected to an air distribution seat, a mounting frame is fixedly connected to the landing gear, the air distribution seat is fixedly installed on the mounting frame, an inflatable bottle is fixedly connected to the air distribution seat, the outer end of the air distribution pipe is fixedly connected to a lower protective ring tube, the outer wall of the lower protective ring tube is provided with a plurality of rubber airbags 1, the lower protective ring tube is fixedly connected to a vertical pipe, the outer wall of the vertical pipe is provided with a rubber airbag 2, the upper end of the vertical pipe is fixedly connected to an upper protective ring tube, and the outer wall of the upper protective ring tube is provided with a rubber airbag 3.
[0007] In a preferred embodiment, a tilt angle sensor and a single-chip microcomputer control board are fixedly mounted on the landing gear, and the tilt angle sensor and the gas bottle are electrically connected to the single-chip microcomputer control board.
[0008] In a preferred embodiment, a plurality of air outlet holes 1 are provided on the lower protective ring tube, and the air outlet holes 1 are arranged in the rubber airbag 1.
[0009] In a preferred embodiment, a plurality of air outlet holes 2 are formed on the vertical pipe, and the air outlet holes 2 are arranged in the rubber airbag 2.
[0010] In a preferred embodiment, a plurality of air outlet holes three are opened on the upper protective ring tube, and the air outlet holes three are arranged in the rubber airbag three.
[0011] In a preferred embodiment, the gas distribution pipe, the gas distribution seat, the lower protective ring pipe, the vertical pipe and the upper protective ring pipe are all made of aluminum alloy.
[0012] In a preferred embodiment, the inspection drone is arranged in a frame composed of the lower protective ring tube, the vertical pipe and the upper protective ring tube.
[0013] In a preferred embodiment, a patrol camera is fixedly mounted on the bottom of the mounting frame.
[0014] In summary, due to the adoption of the above technical solution, the beneficial effects of the utility model are:
[0015] 1. In the utility model, the rubber airbag 1 of the lower protective ring tube, the rubber airbag 2 of the vertical tube and the rubber airbag 3 of the upper protective ring tube are inflated and collided, so that when the inspection drone 1 loses control and falls, the rubber airbags 2 around the inspection drone will provide 360-degree protection for the inspection drone, thereby preventing the inspection drone host and its fan blade mechanism from being damaged. The 360-degree protection can better protect the inspection drone. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;
[0017] Figure 2 This is a schematic diagram of the front view structure of the utility model;
[0018] Figure 3 The utility model is a schematic diagram of the three-dimensional structure of the frame composed of the gas distribution pipe, the gas distribution seat, the lower protective ring pipe, the vertical pipe and the upper protective ring pipe.
[0019] Markings in the figure: 1-inspection drone, 2-air distribution pipe, 3-air distribution seat, 4-inflating bottle, 5-lower protective ring tube, 6-rubber airbag 1, 7-vertical pipe, 8-rubber airbag 2, 9-upper protective ring tube, 10-rubber airbag 3, 11-landing gear, 12-tilt angle sensor, 13-single-chip microcomputer control board, 14-air outlet 1, 15-air outlet 2, 16-air outlet 3, 17-mounting frame, 18-inspection camera. DETAILED DESCRIPTION
[0020] In order to make the purpose, technical solution and advantages of the embodiments of the utility model clearer, the technical solution in the embodiments of the utility model will be clearly and completely described below in combination with the embodiments of the utility model. Obviously, the described embodiments are part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of 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] The following will be combined Figure 1-Figure 3 A protection device for high-voltage line inspection by an unmanned aerial vehicle in an embodiment of the utility model is described in detail.
[0022] Example:
[0023] The utility model provides a protection device for high-voltage line inspection by an unmanned aerial vehicle, referring to Figure 1 and Figure 2 As shown, it includes an inspection drone 1, a landing gear 11 is provided at the bottom of the inspection drone 1, and an inspection camera 17 is fixedly installed at the bottom of the mounting frame 17. This structure utilizes the inspection drone 1 to drive the inspection camera 17 on the landing gear 11 to move, thereby inspecting the high-voltage line and ensuring the safe use of the high-voltage line.
[0024] refer to Figure 1 and Figure 2As shown, a plurality of air distribution pipes 2 are fixedly connected to the landing gear 11, an air distribution seat 3 is fixedly connected to the inner ring of the air distribution pipe 2, a mounting frame 17 is fixedly connected to the landing gear 11, the air distribution seat 3 is fixedly installed on the mounting frame 17, an inflatable bottle 4 (the inflatable bottle 4 contains compressed carbon dioxide gas) is fixedly connected to the air distribution seat 3, a lower protective ring tube 5 is fixedly connected to the outer end of the air distribution pipe 2, a plurality of rubber airbags 1 6 are arranged on the outer wall of the lower protective ring tube 5, a vertical pipe 7 is fixedly connected to the lower protective ring tube 5, a rubber airbag 2 8 is arranged on the outer wall of the vertical pipe 7, an upper protective ring tube 9 is fixedly connected to the upper end of the vertical pipe 7, and a rubber airbag 3 10 is arranged on the outer wall of the upper protective ring tube 9, the inspection drone 1 is arranged in a frame composed of the lower protective ring tube 5, the vertical pipe 7 and the upper protective ring tube 9. When the inspection drone 1 with this structure flies normally, the frame structure composed of the lower protective ring tube 5, the vertical pipe 7 and the upper protective ring tube 9 can protect the flying inspection drone 1 and prevent the inspection drone 1 from being damaged when colliding with an object;
[0025] When the inspection unmanned frame 1 is out of control, the internal carbon dioxide is introduced into the gas distribution pipe 2 through the gas distribution seat 3 by using the gas filling bottle 4. The gas distribution pipe 2 will send part of the carbon dioxide into the lower protective ring tube 5, and the lower protective ring tube 5 will send the carbon dioxide into the upper protective ring tube 9 through the vertical pipe 7. At this time, the carbon dioxide gas will cause the rubber airbag 1 6 of the lower protective ring tube 5, the rubber airbag 2 8 of the vertical pipe 7 and the rubber airbag 3 10 of the upper protective ring tube 9 to inflate and collide. Therefore, when the inspection drone 1 loses control and falls, the rubber airbags 2 8 around the inspection drone 1 will provide 360-degree protection for the inspection drone 1, thereby preventing the main machine of the inspection drone 1 and its fan blade mechanism from being damaged. The 360-degree protection can better protect the inspection drone 1.
[0026] refer to Figure 2 As shown, a tilt angle sensor 12 and a single-chip control board 13 are fixedly installed on the landing gear 11. The specific model of the tilt angle sensor 12 is QJ626T. The tilt angle sensor 12 and the gas bottle 4 are electrically connected to the single-chip control board 13. This structure uses the tilt angle sensor 12 to detect the flight tilt angle of the inspection drone 1. When the inspection drone 1 is out of control, the tilt angle sensor 12 detects that the inspection drone 1 exceeds the controllable tilt angle, and then sends a signal to the single-chip control board 13. After receiving the signal, the single-chip control board 13 controls the gas bottle 4 to open, thereby realizing the inflation of the rubber airbag.
[0027] It should be noted that the control devices and programs between the tilt angle sensor 12, the single-chip control board 13 and the gas cylinder 4 in the above-mentioned structure are all prior art, the principles are public, and no improvement is made in this application, so no further introduction is given here.
[0028] refer to Figure 1 and 3As shown, a plurality of air outlet holes 14 are provided on the lower protective ring tube 5 , and the air outlet holes 14 are arranged in the rubber airbag 6 . This structure utilizes the air outlet holes 14 to allow the carbon dioxide in the inflation bottle 4 to enter the rubber airbag 6 .
[0029] refer to Figure 1 and 3 As shown, a plurality of air outlet holes 15 are provided on the vertical pipe 7 , and the air outlet holes 15 are arranged in the rubber airbag 8 . This structure utilizes the air outlet holes 15 to allow the carbon dioxide in the inflation bottle 4 to enter the rubber airbag 8 .
[0030] refer to Figure 1 and 3 As shown, the upper protective ring tube 9 is provided with a plurality of air outlet holes 3 16 , which are arranged in the rubber airbag 3 10 . This structure utilizes the air outlet holes 3 16 to allow the carbon dioxide in the gas bottle 4 to enter the rubber airbag 3 10 .
[0031] refer to Figure 1 As shown, the air distribution pipe 2, the air distribution seat 3, the lower protective ring pipe 5, the vertical pipe 7 and the upper protective ring pipe 9 are all made of aluminum alloy. The aluminum alloy of this structure is light in weight and high in strength, so that the inspection drone 1 will not be overloaded.
[0032] It should be noted that the above-mentioned inspection drone 1 is used for the inspection of high-voltage lines.
[0033] The implementation principle of the protection device for high-voltage line inspection of an unmanned aerial vehicle in the embodiment of the present application is as follows: when in use, the tilt angle sensor 12 detects the flight tilt angle of the inspection unmanned aerial vehicle 1. When the inspection unmanned aerial vehicle 1 is out of control, the tilt angle sensor 12 detects that the inspection unmanned aerial vehicle 1 exceeds the controllable tilt angle, and then sends a signal to the single-chip control board 13. After the single-chip control board 13 receives the signal, it controls the gas bottle 4 to open, and the gas bottle 4 allows the internal carbon dioxide to enter the gas distribution pipe 2 through the gas distribution seat 3, and the gas distribution pipe 2 will send part of the carbon dioxide into the lower protective ring pipe 5, the lower protection ring tube 5 will send carbon dioxide into the upper protection ring tube 9 through the vertical pipe 7. At this time, the carbon dioxide gas will inflate and collide with the rubber airbag 1 6 of the lower protection ring tube 5, the rubber airbag 2 8 of the vertical pipe 7 and the rubber airbag 3 10 of the upper protection ring tube 9. Therefore, when the inspection drone 1 loses control and falls, the rubber airbags 2 8 around the inspection drone 1 will provide 360-degree protection for the inspection drone 1, thereby preventing the main machine of the inspection drone 1 and its fan blade mechanism from being damaged. The 360-degree protection can better protect the inspection drone 1.
[0034] The above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that the technical solutions described in the aforementioned embodiments may still be modified, or some of the technical features may be replaced by equivalents. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.
Claims
1. A protection device for high-voltage line inspection by an unmanned aerial vehicle, comprising an inspection unmanned aerial vehicle (1), characterized in that: The lower part of the inspection drone (1) is provided with a landing gear (11), and a plurality of air distribution pipes (2) are fixedly connected to the landing gear (11), and the inner end of the air distribution pipe (2) is fixedly connected to an air distribution seat (3), and a mounting frame (17) is fixedly connected to the landing gear (11), and the air distribution seat (3) is fixedly mounted on the mounting frame (17), and an air filling bottle (4) is fixedly connected to the air distribution seat (3), and the outer end of the air distribution pipe (2) is fixedly connected to a lower protective ring tube (5), and the outer wall of the lower protective ring tube (5) is provided with a plurality of rubber airbags (1) (6), and the lower protective ring tube (5) is fixedly connected to a vertical tube (7), and the outer wall of the vertical tube (7) is provided with a rubber airbag (2) (8), and the upper end of the vertical tube (7) is fixedly connected to an upper protective ring tube (9), and the outer wall of the upper protective ring tube (9) is provided with a rubber airbag (3) (10).
2. A protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: An inclination angle sensor (12) and a single-chip microcomputer control board (13) are fixedly mounted on the landing gear (11); the inclination angle sensor (12) and the gas filling bottle (4) are electrically connected to the single-chip microcomputer control board (13).
3. A protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: The lower protective ring tube (5) is provided with a plurality of air outlet holes (14), and the air outlet holes (14) are arranged in the rubber airbag (6).
4. A protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: The vertical pipe (7) is provided with a plurality of air outlet holes (15), and the air outlet holes (15) are arranged in the rubber airbag (8).
5. The protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: The upper protective ring tube (9) is provided with a plurality of air outlet holes (3) (16), and the air outlet holes (3) (16) are arranged in the rubber airbag (3) (10).
6. A protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: The gas distribution pipe (2), the gas distribution seat (3), the lower protective ring pipe (5), the vertical pipe (7) and the upper protective ring pipe (9) are all made of aluminum alloy.
7. A protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: The inspection drone (1) is arranged in a frame formed by the lower protective ring tube (5), the vertical tube (7) and the upper protective ring tube (9).
8. The protection device for high-voltage line inspection by an unmanned aerial vehicle according to claim 1, characterized in that: A patrol camera (18) is fixedly mounted on the bottom of the mounting frame (17).
Citation Information
Patent Citations
A buffer device for drones
CN218806724U
Cited By
Electric cruise unmanned aerial vehicle
CN223721190U