Unmanned aerial vehicle pipeline inspection device

By designing clamping components and marking components in the UAV pipeline inspection device, the problem that the prior art cannot accurately mark the problem pipeline, and the convenience of accurate marking of the pipeline and subsequent maintenance is achieved.

CN222539016UActive Publication Date: 2025-02-28SHANGHAI INST OF SPECIAL EQUIP INSPECTION & TECHN RES
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Patent Information

Application Number
CN202421299114.6
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-07
Publication Date
2025-02-28
Estimated Expiration
2034-06-07

AI Technical Summary

Technical Problem

The existing drone pipeline inspection device cannot accurately mark the pipelines with problems, resulting in inconvenience in subsequent maintenance.

Method used

A drone piping inspection device is designed, equipped with clamping components and marking components. The clamping assembly drives the clamping block to clamp the pipe through the cylinder to ensure positioning between the drone and the pipe. The marking assembly uses atomizing spray head to spray marking liquid onto the surface of the pipe to avoid inaccurate marking caused by dripping.

Benefits of technology

Accurate marking of problem pipelines is achieved, the convenience and efficiency of subsequent maintenance is improved, and inaccurate problems caused by labeling liquid drops are avoided.

✦ Generated by Eureka AI based on patent content.

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    Figure CN222539016U_ABST
Patent Text Reader

Abstract

The utility model relates to an unmanned aerial vehicle pipeline inspection device which comprises an unmanned aerial vehicle body, a mounting rack, a marking assembly, a gas detection module, a clamping assembly and a controller, the mounting rack is mounted on the side, close to the ground, of the unmanned aerial vehicle body, the marking assembly, the gas detection module and the controller are mounted in the mounting rack, and a supporting plate is mounted on the mounting rack; the clamping assembly is installed on the supporting plate and clamps the pipeline, and the controller is electrically connected with the marking assembly, the gas detection module and the clamping assembly. Compared with the prior art, the pipeline marking device has the advantages that the pipeline is inspected through the gas detection module, the defective pipeline is marked through the marking assembly after being clamped by the clamping assembly, and accurate marking of the defective pipeline is achieved; the marking liquid is sprayed to the surface of the gas pipeline through the atomizing nozzle after being pressurized, so that the problem that the marking liquid easily falls to the ground in a dripping mode is avoided; and the buffer springs form buffering between the clamping blocks and the connecting plates, so that excessive extrusion on the pipeline is avoided, and the like.
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Description

Technical Field

[0001] The utility model relates to unmanned aerial vehicle inspection technology, in particular to an unmanned aerial vehicle pipeline inspection device. Background Art

[0002] At present, in order to ensure the safe transportation of gas, the gas pipelines and equipment in the city need to be inspected once every 5 days during use. However, the existing inspection methods are mostly manual inspection methods, which require a lot of manpower and material resources to barely complete the inspection tasks, and the inspection results are not very ideal.

[0003] After searching, the authorization announcement number CN218086035U discloses an inspection drone, which specifically discloses: including a drone body, a camera, a gas detection device, a laser ranging device and a controller; wherein the first support device includes a mounting bracket, a first steering gear, a vertical bracket, a second steering gear, a U-shaped bracket, a third steering gear and a support plate; through the inspection drone of this application, it can fly to the corresponding position of the pipeline, and then collect images of the pipeline and monitoring instruments through the camera, and detect whether the combustible gas near the pipeline exceeds the standard through the gas detection device, thereby replacing manual inspection work to improve inspection efficiency. However, this existing technology cannot mark the pipeline with problems, which is not convenient for subsequent maintenance.

[0004] Authorization announcement number CN219120358U discloses a pipeline inspection drone, specifically including: a drone body equipped with a GPS positioning module, a rotatable camera, a gas detection device and a marking device, and a controller installed inside the drone body. This prior art replaces the manual inspection method, thereby saving the time of manual inspection along the gas pipeline, improving work efficiency, and avoiding the potential safety hazards of line inspectors during mountain inspections, thereby ensuring personal safety. However, when the pipeline inspection drone is in use, due to the small size of the gas pipeline, the dripping method makes it easy for the marking liquid to not drip accurately on the gas pipeline, reducing the marking effect.

[0005] To sum up, how to design a UAV pipeline inspection device that can inspect pipelines and accurately mark problematic pipelines is a technical problem that needs to be solved. Utility Model Content

[0006] The purpose of the utility model is to provide a UAV pipeline inspection device in order to overcome the defect of the above-mentioned prior art that the problematic pipeline cannot be accurately marked.

[0007] The purpose of the utility model can be achieved through the following technical solutions:

[0008] According to one aspect of the utility model, a UAV pipeline inspection device is provided, including a UAV body equipped with a positioning module, the device also including a mounting frame, a marking component, a gas detection module, a clamping component and a controller, the mounting frame is installed on the side of the UAV body close to the ground, the marking component, the gas detection module and the controller are installed in the mounting frame, a support plate is installed on the side of the mounting frame close to the ground, the clamping component is installed on the support plate, the clamping component clamps the pipeline, and the controller is electrically connected to the marking component, the gas detection module and the clamping component.

[0009] As a preferred technical solution, the device also includes a first camera, a second camera and a wireless communicator, all of which are electrically connected to the controller; the first camera is installed on the side of the mounting frame close to the ground; the second camera is installed on the side of the drone body, and the second camera is rotatable; the wireless communicator is installed on the side of the mounting frame close to the drone body, and communicates with the control background.

[0010] As a preferred technical solution, the marking assembly includes a liquid storage bottle, a solenoid valve, a first connecting pipe, a micro high-pressure pump, a second connecting pipe and an atomizing nozzle connected in sequence, the liquid storage bottle, the solenoid valve, the first connecting pipe and the micro high-pressure pump are installed inside the mounting frame, the second connecting pipe and the atomizing nozzle are installed outside the mounting frame, and the atomizing nozzle faces the pipe and is located on the side of the pipe clamped by the clamping assembly away from the ground.

[0011] As a preferred technical solution, one end of the second connecting pipe connected to the atomizing nozzle is clamped with an elastic buckle, and the elastic buckle is fixed on the edge of the mounting frame on the side close to the ground.

[0012] As a preferred technical solution, the device also includes a cylinder, which is mounted on the support plate and has an output end that passes through the support plate and is connected to the clamping assembly.

[0013] As a preferred technical solution, the clamping assembly includes two sets of jaws, and the two sets of jaws are clamped on both sides of the pipe.

[0014] As a preferred technical solution, the clamp includes a connecting plate, a buffer spring, a clamping block and a sliding rod; the output end of the cylinder is connected to one side of the connecting plate, the buffer spring is sleeved on the outer surface of the sliding rod, one end is fixedly connected to the other side of the connecting plate, and the other end is fixedly connected to the clamping block; one end of the sliding rod is connected to the clamping block, and the other end passes through the connecting plate and forms a moving pair with the connecting plate; the clamping block clamps the pipe.

[0015] As a preferred technical solution, the buffer spring and the slide rod are both in number and are symmetrically installed between the clamping block and the connecting plate, and the cylinder output end is connected to the center of the connecting plate.

[0016] As a preferred technical solution, one side of the clamping block that clamps the pipe is an arc surface.

[0017] As a preferred technical solution, a support frame is fixedly connected to one side of the support plate close to the ground, and a buffer pad is provided on one side of the support frame close to the ground.

[0018] Compared with the prior art, the utility model has the following beneficial effects:

[0019] 1) The utility model inspects the pipeline through the gas detection module. When natural gas is detected, the clamping component clamps the problematic pipeline, and then marks it through the marking component, thereby achieving accurate marking of the problematic pipeline;

[0020] 2) The utility model uses the first camera and the second camera to shoot the on-site situation of the pipeline, which is convenient for the back-end operator to control the drone pipeline inspection device more accurately and conveniently through the wireless communication device;

[0021] 3) After the electromagnetic valve is activated, the marking liquid in the liquid storage bottle flows into the micro high-pressure pump through the first connecting pipe. The micro high-pressure pump pressurizes the marking liquid and sprays it onto the surface of the gas pipeline through the atomizing nozzle, thereby avoiding the problem of inaccurate marking caused by the marking liquid dripping to the ground;

[0022] 4) The clamping assembly of the utility model drives the connecting plates to approach each other through the cylinder, so that the clamping block is clamped on the gas pipeline, thereby completing the positioning between the drone body and the gas pipeline, which is convenient for subsequent marking work. The buffer spring forms a buffer between the clamping block and the connecting plate to prevent the cylinder from causing excessive squeezing of the gas pipeline;

[0023] 5) The utility model is provided with a support frame and a buffer pad to prevent the UAV pipeline inspection device from being damaged due to a large impact force when landing. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 This is a front view of a UAV pipeline inspection device of the utility model;

[0025] Figure 2 This is a side view of a UAV pipeline inspection device of the utility model;

[0026] Figure 3 It is the assembly drawing of the marking components of the utility model;

[0027] Figure 4 This is an assembly diagram of the clamping assembly of the utility model;

[0028] The numbers in the figure show:

[0029] 1. UAV body, 2. Mounting frame, 3. Marking assembly, 31. Liquid storage bottle, 32. Solenoid valve, 33. First connecting pipe, 34. Micro high-pressure pump, 35. Second connecting pipe, 36. Atomizing nozzle, 4. Gas detection module, 5. First camera, 6. Support plate, 7. Cylinder, 8. Clamping assembly, 81. Connecting plate, 82. Buffer spring, 83. Clamping block, 84. Slide rod, 9. Second camera, 10. Wireless communicator, 11. Controller, 12. Support frame, 13. Buffer pad, 14. Elastic buckle. DETAILED DESCRIPTION

[0030] 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 part of the embodiments of the utility model, not all of them. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work should fall within the scope of protection of the utility model.

[0031] like Figure 1 and Figure 2 As shown, the utility model provides a UAV pipeline inspection device, including a UAV body 1 equipped with a positioning module, a mounting frame 2, a marking component 3, a gas detection module 4, a cylinder 7, a clamping component 8, a controller 11, a first camera 5, a second camera 9 and a wireless communicator 10. The second camera 9 is rotatable and mounted on the front side of the UAV body 1.

[0032] The mounting frame 2 is a cubic frame structure, which is installed on the bottom surface of the drone body 1 (i.e., the side close to the ground) by bolts, and the marking assembly 3, the gas detection module 4, the controller 11, the first camera 5 and the wireless communicator 10 are installed on it. Two support plates 6 are installed at both ends of the bottom surface of the mounting frame 2 by bolts. The support frame 12 is installed at both ends of the bottom surface of the support plate 6 by bolts, and the buffer pad 13 is bonded to the bottom surface of the support frame 12.

[0033] like Figure 3As shown, the marking assembly 3 is installed in the middle of the top wall of the mounting frame 2, including a liquid storage bottle 31, a solenoid valve 32, a first connecting pipe 33, a micro high-pressure pump 34, a second connecting pipe 35, an atomizing nozzle 36 and an elastic buckle 14; the liquid storage bottle 31 is threadedly connected to the middle of the top wall of the mounting frame 2, the solenoid valve 32 is threadedly connected to the bottom surface of the liquid storage bottle 31, the first connecting pipe 33 is threadedly connected to the bottom surface of the solenoid valve 32, the first connecting pipe 33 is threadedly connected to the micro high-pressure pump 34 at one end away from the solenoid valve 32, the micro high-pressure pump 34 is installed at the rear end of the inner surface of the mounting frame 2 by bolts, the second connecting pipe 35 is threadedly connected to the rear side of the micro high-pressure pump 34, the atomizing nozzle 36 is threadedly connected to the end of the second connecting pipe 35 away from the micro high-pressure pump 34, the atomizing nozzle 36 faces the pipeline and is located directly above the pipeline clamped by the clamping assembly 8, the elastic buckle 14 is clamped with the end of the second connecting pipe 35 close to the atomizing nozzle 36, and is installed in the middle of the left bottom surface of the mounting frame 2 by bolts.

[0034] The gas detection module 4 is installed on the front end of the inner surface of the mounting frame 2 by means of bolts to detect whether there is natural gas near the pipeline.

[0035] There are two cylinders 7, which are respectively installed on the outer sides of the two support plates 6 by bolts, and the output ends thereof pass through the support plates 6 to the inner sides of the support plates 6 and are connected to the clamping assembly 8.

[0036] like Figure 4 As shown, the clamping assembly 8 has two sets of clamping jaws, which clamp on both sides of the pipe. The clamping jaws include a connecting plate 81, a buffer spring 82, a clamping block 83 and a slide bar 84. The connecting plate 81 is installed on the telescopic end of the cylinder 7 by bolts. One end of the two buffer springs 82 is welded to the side of the connecting plate 81 away from the cylinder 7, and the other end is welded to the clamping block 83. The two slide bars 84 are installed on the side of the clamping block 83 where the buffer spring 82 is welded by bolts. The buffer spring 82 is sleeved on the slide bar 84. The end of the slide bar 84 away from the clamping block 83 passes through the connecting plate 81 and is slidably connected to the connecting plate 81. The side where the clamping block 83 is connected to the slide bar 84 is a plane, and the side where the pipe is clamped is an arc surface.

[0037] The controller 11 is installed on the front end of the top wall of the mounting frame 2 by bolts, and is electrically connected to the solenoid valve 32, the micro high-pressure pump 34, the gas detection module 4, the first camera 5, the cylinder 7, the second camera 9, and the wireless communicator 10.

[0038] The first camera 5 is installed at the middle of the bottom surface of the mounting frame 2 by bolts; the wireless communicator 10 is installed at the rear end of the top wall of the mounting frame 2 by bolts to communicate with the control background.

[0039] The working process of this utility model is as follows:

[0040] When the drone is inspecting, if the gas detection module 4 detects the presence of natural gas near the gas pipeline, the gas detection module 4 sends a signal to the controller 11, and the controller 11 sends the location information to the background through the GPS positioning module. The staff controls the drone body 1 to descend until the gas pipeline is located between the clamping components 8; the staff controls the external control system to send a signal to the controller 11 through the wireless communication device 10 to start the cylinder 7, and the cylinder 7 drives the connecting plates 81 to approach each other, so that the clamping block 83 is clamped on the gas pipeline, thereby completing the positioning between the drone body 1 and the gas pipeline, which is convenient for subsequent marking work. The buffer spring 82 forms a buffer between the clamping block 83 and the connecting plate 81 to prevent the cylinder 7 from causing excessive squeezing of the gas pipeline; the solenoid valve 32 is started, and the marking liquid in the liquid storage bottle 31 flows into the micro high-pressure pump 34 through the first connecting pipe 33. The micro high-pressure pump 34 pressurizes the marking liquid and sprays it onto the surface of the gas pipeline through the atomizing nozzle 36, thereby avoiding the problem that the marking liquid easily falls to the ground in a dripping manner.

[0041] The utility model is easy to use and has good use effect.

[0042] The above is only a specific implementation of the utility model, but the protection scope of the utility model is not limited thereto. Any technician familiar with the technical field can easily think of various equivalent modifications or replacements within the technical scope disclosed by the utility model, and these modifications or replacements should be included in the protection scope of the utility model. Therefore, the protection scope of the utility model should be based on the protection scope of the claims.

Claims

1. A drone pipeline inspection device, comprising a drone body (1) equipped with a positioning module, characterized in that: The device further comprises a mounting frame (2), a marking component (3), a gas detection module (4), a clamping component (8) and a controller (11); the mounting frame (2) is mounted on a side of the drone body (1) close to the ground; the marking component (3), the gas detection module (4) and the controller (11) are mounted in the mounting frame (2); a support plate (6) is mounted on a side of the mounting frame (2) close to the ground; the clamping component (8) is mounted on the support plate (6); the clamping component (8) clamps the pipeline; and the controller (11) is electrically connected to the marking component (3), the gas detection module (4) and the clamping component (8).

2. The unmanned aerial vehicle pipeline inspection device according to claim 1 is characterized in that: The device also includes a first camera (5), a second camera (9) and a wireless communicator (10), all of which are electrically connected to a controller (11); the first camera (5) is mounted on a side of a mounting frame (2) close to the ground; the second camera (9) is mounted on a side of a drone body (1), and the second camera (9) is rotatable; the wireless communicator (10) is mounted on a side of the mounting frame (2) close to the drone body (1), and communicates with a control background.

3. The unmanned aerial vehicle pipeline inspection device according to claim 1 is characterized in that: The marking assembly (3) comprises a liquid storage bottle (31), a solenoid valve (32), a first connecting pipe (33), a micro high-pressure pump (34), a second connecting pipe (35) and an atomizing nozzle (36) which are connected in sequence; the liquid storage bottle (31), the solenoid valve (32), the first connecting pipe (33) and the micro high-pressure pump (34) are installed inside the mounting frame (2); the second connecting pipe (35) and the atomizing nozzle (36) are installed outside the mounting frame (2); the atomizing nozzle (36) faces the pipeline and is located on the side of the pipeline clamped by the clamping assembly (8) away from the ground.

4. The unmanned aerial vehicle pipeline inspection device according to claim 3 is characterized in that: One end of the second connecting pipe (35) connected to the atomizing nozzle (36) is clamped with an elastic buckle (14), and the elastic buckle (14) is fixed on the edge of the mounting frame (2) close to the ground.

5. The unmanned aerial vehicle pipeline inspection device according to claim 1 is characterized in that: The device also comprises a cylinder (7), which is mounted on the support plate (6), and an output end of the cylinder (7) passes through the support plate (6) and is connected to a clamping assembly (8).

6. The unmanned aerial vehicle pipeline inspection device according to claim 5 is characterized in that: The clamping assembly (8) comprises two sets of clamping jaws, and the two sets of clamping jaws are clamped on both sides of the pipeline.

7. The unmanned aerial vehicle pipeline inspection device according to claim 6 is characterized in that: The clamping claw comprises a connecting plate (81), a buffer spring (82), a clamping block (83) and a sliding rod (84); the output end of the cylinder (7) is connected to one side of the connecting plate (81); the buffer spring (82) is sleeved on the outer surface of the sliding rod (84), one end of which is fixedly connected to the other side of the connecting plate (81), and the other end of which is fixedly connected to the clamping block (83); one end of the sliding rod (84) is connected to the clamping block (83), and the other end passes through the connecting plate (81) and forms a moving pair with the connecting plate (81); the clamping block (83) clamps the pipeline.

8. The unmanned aerial vehicle pipeline inspection device according to claim 7 is characterized in that: The buffer spring (82) and the slide rod (84) are both in two pieces and are symmetrically installed between the clamping block (83) and the connecting plate (81). The output end of the cylinder (7) is connected to the center of the connecting plate (81).

9. The unmanned aerial vehicle pipeline inspection device according to claim 7, characterized in that: The side of the clamping block (83) that clamps the pipe is an arc surface.

10. The unmanned aerial vehicle pipeline inspection device according to claim 1, characterized in that: A support frame (12) is fixedly connected to one side of the support plate (6) close to the ground, and a buffer pad (13) is provided on one side of the support frame (12) close to the ground.

Citation Information

Patent Citations

  • Inspection unmanned aerial vehicle

    CN218086035U

  • Pipeline inspection unmanned aerial vehicle

    CN219120358U