Insulator resistance value high-efficiency detection device

By designing a high-efficiency insulator resistance detection device and utilizing the innovative structure of the drone body and detection components, the safety hazards and applicability issues in the drone detection process were solved, achieving safe and reliable insulator detection.

CN224066895UActive Publication Date: 2026-03-31CUTTING EDGE INTELLIGENT TECH (SHANDONG) CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-04-11
Publication Date
2026-03-31

AI Technical Summary

Technical Problem

Existing insulator testing methods pose safety hazards, especially when drones are close to the insulators, making them prone to breakdown. Furthermore, the testing process is not adjustable and has poor applicability.

Method used

A high-efficiency insulator resistance detection device was designed, which adopts a drone body, mounting frame, detection components and probe bracket. The probe bracket is adjusted by a dial to ensure that the probe is in close contact with the insulator, and the probe can be pulled out during the detection process. It is combined with the pipe rack and gimbal shell for safe connection and communication, reducing the risk of drone crash.

Benefits of technology

It improves the safety and applicability of the detection process, reduces the risk of drone crashes, lowers the difficulty and cost of operation, and enhances flight stability and control safety.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an insulator resistance value high-efficiency detection device, which belongs to the technical field of electrical variable measurement, and comprises an unmanned aerial vehicle main body, the bottom end of the unmanned aerial vehicle main body is fixedly provided with a mounting rack in a threaded manner, the bottom end of the mounting rack is fixedly provided with a detection assembly, and the detection assembly comprises a first insulating rod. The tail of one end of the first insulating rod is connected with an electric control box, and a second insulating rod is inserted into an inner hole of the other end of the first insulating rod. The probe bracket detection part in the detection device can rotate and adjust the probe bracket corresponding to the dial according to different mounting modes of insulator strings in detection so as to ensure that the probe is in close contact with steel caps at the two ends of the insulator, and in the detection process, when the probe is carelessly clamped on an insulator sheet, the probe bracket can be rotated to adjust the probe bracket. The unmanned aerial vehicle is increased in power and flies backwards, the probe can be pulled out, the air crash risk is reduced, meanwhile, connection is conducted in cooperation with a pipe hanging frame made of insulating materials, the safety of the detection process is further improved, and potential safety hazards such as breakdown are reduced.
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Description

Technical Field

[0001] This utility model relates to the field of electrical variable measurement technology, specifically to an efficient insulator resistance detection device. Background Technology

[0002] In electrical variable measurement operations, measuring transmission lines involves measuring multiple electrical variables, including but not limited to voltage, current, impedance, and capacitance. Among these, the inspection of insulators is crucial. Insulators primarily support conductors and prevent current leakage; they can withstand mechanical loads and electrical stresses, ensuring the safe and stable operation of the power system. High-quality insulators reduce energy loss, prevent short circuits and grounding faults, improve transmission efficiency, and ensure grid reliability. However, with prolonged loads and exposure to high-altitude environments, including sunlight, wind, rain, and snow, insulators can experience resistance degradation, seriously threatening the operational safety of transmission lines. Therefore, periodic inspections are necessary. The insulator inspection industry commonly employs traditional manual inspection, combined drone-mounted robot inspection, and drone-mounted inspection with loads.

[0003] China Patent Network (patent publication number CN108896887B) discloses a tension insulator testing device and method, including a drone, a first camera, a processing module, a flight control system, sensors, and a testing device. The drone includes a drone body, an arm, a propeller, and landing gear. One end of the arm is connected to the drone body, and the other end is connected to the propeller. The landing gear is located at the bottom of the drone body. The first camera is located on the outside of the drone body. The processing module is used to receive the images captured by the first camera. The flight control system is used to receive the processing results of the processing module. The sensors are located on the drone body, and the testing device is connected to the drone body.

[0004] The above-mentioned testing method requires operating a drone to fly above the insulator, controlling the landing gear to be parallel to the insulator, and then controlling the drone to align its testing part with the insulator before automatically landing for testing. This testing method requires the drone to be very close to the insulator. In case of accidental discharge from the line, the drone may be damaged, leading to a crash, which poses a safety hazard. In addition, the testing process is not adjustable, and its applicability will be reduced if the insulator installation angle is different. Therefore, we propose a high-efficiency insulator resistance testing device. Utility Model Content

[0005] The summary section of this application is intended to provide a brief overview of the concepts, which will be described in detail in the detailed description section below. This summary section is not intended to identify key or essential features of the claimed technical solutions, nor is it intended to limit the scope of the claimed technical solutions.

[0006] The purpose of this invention is to provide an efficient insulator resistance detection device to solve the problems mentioned in the background art.

[0007] To achieve the above objectives, this utility model provides the following technical solution: a high-efficiency insulator resistance detection device, comprising a drone body, a mounting bracket threadedly fixed to the bottom end of the drone body, a detection component fixed to the bottom end of the mounting bracket, the detection component comprising a first insulating rod, an electrical control box connected to one end of the first insulating rod, a charging port plug and a switching port plug respectively installed on one side of the electrical control box, a second insulating rod inserted into the inner hole of the other end of the first insulating rod, and an insulating rod connector sleeved at the connection between the first insulating rod and the second insulating rod, a scale plate fixed to one end of the second insulating rod, and a probe bracket attached to one side of the scale plate, probe inserts fixed to both sides of the front end of the probe bracket, and a probe inserted into one end of the probe insert.

[0008] Furthermore, the probe is elastically connected to both sides of the probe holder via a probe plug, and the probe holder is sleeved and rotated with one end of the second insulating rod.

[0009] Furthermore, the electrical control box forms a telescopic structure through the first insulating rod and the second insulating rod, and a detection board is installed inside the electrical control box.

[0010] Furthermore, the main body of the drone includes the drone itself, and a gimbal housing is provided on one side of the bottom of the drone. A quick connector is connected to the top of the gimbal housing, and a gimbal bracket is connected to the top of the quick connector.

[0011] Furthermore, the gimbal housing is fastened to the bottom of the gimbal bracket via a quick connector, and a control board and a communication antenna are installed inside the gimbal housing.

[0012] Furthermore, the mounting frame includes a belly mounting plate, and the top surface of the belly mounting plate is threaded to the bottom belly of the UAV body. Shock absorbers are connected around the bottom surface of the belly mounting plate, and the bottom end of the shock absorbers is connected to an upper carrier connecting plate. The bottom end of the upper carrier connecting plate is connected to a pipe rack, and a lower carrier connecting plate is fixed between the inner walls of the two sides of the pipe rack. Pipe clamps are connected to the two sides of the bottom end of the pipe rack, and a first insulating rod is fastened to the inner wall of the pipe clamp.

[0013] Furthermore, the pipe clamp is fixedly connected to the upper connecting plate of the carrier through the pipe hanger frame, and the pipe clamp is fastened to the middle section of the first insulating rod.

[0014] Compared with the prior art, the beneficial effects of this utility model are:

[0015] The probe bracket in this testing device can be rotated and adjusted according to the different installation methods of the insulator strings during testing, to ensure tight contact between the probe and the steel caps at both ends of the insulator. In addition, if the probe accidentally gets stuck on the insulator sheet during testing, the drone can increase its power and fly backward to pull out the probe, reducing the risk of crash. At the same time, it can be connected with the pipe rack of the insulating material to further improve the safety of the testing process and reduce safety hazards such as puncture.

[0016] This detection device is structured by connecting the drone to the gimbal housing mounted on the gimbal bracket via a wired connection. Communication is achieved through this wired connection, and the issuance of control tasks and feedback of detection results are all displayed on the drone remote controller. This allows for full integration of information, eliminating the need for an additional remote controller for detection, thus reducing costs and operational complexity. The control board and communication antenna inside the gimbal housing communicate wirelessly with the detection components, preventing external high voltage from entering the drone and destroying it, thereby improving operational safety.

[0017] The carrier plate of this testing device is connected to the fuselage mounting plate by a shock absorber, which prevents the overall vibration of the testing components from being transmitted to the UAV during the testing process and affecting the UAV's flight attitude. At the same time, the hanging pipe clamp on the first insulating rod is the center of gravity of the entire testing system, thereby reducing the power consumption of the UAV for stabilization and improving flight stability. Attached Figure Description

[0018] Figure 1 This is a three-dimensional structural diagram of the main body of the UAV of this utility model;

[0019] Figure 2 This is a three-dimensional structural diagram of the mounting bracket of this utility model;

[0020] Figure 3 This is a three-dimensional structural diagram of the detection component of this utility model;

[0021] Figure 4 This is a three-dimensional structural diagram of the probe holder in the detection component of this utility model;

[0022] Figure 5 This is a schematic diagram of the probe side view structure in the detection assembly of this utility model;

[0023] Figure 6 This is a three-dimensional structural diagram of the first detection process of this utility model;

[0024] Figure 7 This is a three-dimensional structural diagram of the second detection process of this utility model.

[0025] In the diagram: 1. UAV body; 101. UAV; 102. Gimbal shell; 103. Quick connector; 104. Gimbal bracket; 2. Mounting frame; 201. Underbody mounting plate; 202. Shock absorber; 203. Upper connecting plate of the carrier; 204. Suspension pipe frame; 205. Lower connecting plate of the carrier; 206. Suspension pipe clamp; 3. Detection components; 301. First insulating rod; 302. Electrical control box; 303. Charging port plug; 304. Switch port plug; 305. Second insulating rod; 306. Insulating rod connector; 307. Dial; 308. Probe bracket; 309. Probe plug; 310. Probe. Detailed Implementation

[0026] Embodiments of this disclosure will now be described in more detail with reference to the accompanying drawings. While some embodiments of this disclosure are shown in the drawings, it should be understood that this disclosure can be implemented in various forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided to provide a more thorough and complete understanding of this disclosure. It should be understood that the accompanying drawings and embodiments of this disclosure are for illustrative purposes only and are not intended to limit the scope of protection of this disclosure.

[0027] It should also be noted that, for ease of description, only the parts relevant to the invention are shown in the accompanying drawings. Unless otherwise specified, the embodiments and features described in this disclosure can be combined with each other.

[0028] It should be noted that the concepts of "first" and "second" mentioned in this disclosure are used only to distinguish different devices, modules, or units, and are not used to limit the order of functions performed by these devices, modules, or units or their interdependencies.

[0029] It should be noted that the terms "a" and "a plurality of" used in this disclosure are illustrative rather than restrictive, and those skilled in the art should understand that, unless otherwise expressly indicated in the context, they should be understood as "one or more".

[0030] This disclosure will now be described in detail with reference to the accompanying drawings and embodiments.

[0031] This utility model provides, for example Figure 1-7The device for high-efficiency detection of insulator resistance shown includes a drone body 1, a mounting bracket 2 is threadedly fixed to the bottom end of the drone body 1, a detection component 3 is fixed to the bottom end of the mounting bracket 2, the drone body 1 includes a drone 101, and a gimbal shell 102 is provided on one side of the bottom of the drone 101, a quick connector 103 is connected to the top end of the gimbal shell 102, and a gimbal bracket 104 is connected to the top end of the quick connector 103.

[0032] To provide a stable wireless control process and reduce detection operations, such as Figure 1 As shown, this detection device structure is wiredly connected to the gimbal housing 102 mounted on the gimbal bracket 104 via the drone 101. Communication is achieved through this wired connection, and the issuance of control tasks and feedback of detection results are all displayed on the drone remote controller. This allows for full integration of information, eliminating the need for an additional remote controller for detection, thus reducing costs and operational complexity. Communication with the detection component 3 is achieved wirelessly via the control board and communication antenna inside the gimbal housing 102, preventing external high voltage from entering the drone and destroying it, thereby improving operational safety.

[0033] like Figure 2 As shown, the mounting frame 2 includes a belly mounting plate 201, and the top surface of the belly mounting plate 201 is threaded to the bottom belly of the UAV body 1. Shock absorbers 202 are connected around the bottom surface of the belly mounting plate 201. The bottom end of the shock absorber 202 is connected to the upper connecting plate 203 of the carrier. The bottom end of the upper connecting plate 203 of the carrier is connected to the pipe rack 204. The lower connecting plate 205 of the carrier is fixed between the inner walls on both sides of the pipe rack 204. The bottom ends of the pipe rack 204 are connected to the pipe clamps 206. The inner wall of the pipe clamps 206 is fastened with a first insulating rod 301.

[0034] To maintain stability during the connection and flight control process, such as Figure 2 As shown, the structure of this testing device features a pipe clamp 206 installed in the middle of the first insulating rod 301. The clamp is installed in a semi-open manner, which facilitates the assembly and disassembly of the insulating rod. At the same time, the pipe clamp 206, the pipe frame 204, and the connecting plate 203 on the carrier are fixedly connected together, improving the overall rigidity and structural stability. The connecting plate 203 on the carrier is connected to the fuselage mounting plate 201 through a shock absorber 202, which prevents the overall vibration of the testing component 3 from being transmitted to the UAV 101 during the testing process, thus avoiding any impact on the flight attitude of the UAV 101. In addition, the pipe clamp 206 on the first insulating rod 301 is the center of gravity of the entire testing system, thereby reducing the power consumption of the UAV for stabilization and improving flight stability. The pipe frame 204 is also made of insulating material to prevent external high voltage from being transmitted to the testing component 3 and penetrating the UAV 101 along the pipe frame 204, causing a crash.

[0035] like Figure 3-7As shown, the detection component 3 includes a first insulating rod 301. One end of the first insulating rod 301 is connected to an electrical control box 302. A charging port plug 303 and a switch port plug 304 are respectively installed at the charging port and switch port on one side of the electrical control box 302. A second insulating rod 305 is inserted into the inner hole of the other end of the first insulating rod 301. An insulating rod connector 306 is sleeved at the connection between the first insulating rod 301 and the second insulating rod 305. A scale 307 is fixed to one end of the second insulating rod 305. A probe bracket 308 is attached to one side of the scale 307. Probe inserts 309 are fixed to both sides of the front end of the probe bracket 308. A probe 310 is inserted into one end of the probe insert 309.

[0036] Finally, to further improve the safety and adjustability of the detection process, such as... Figure 3-7 As shown, the probe bracket 308 of this testing device is fixed to the head end of the second insulating rod 305 by a clamping method. A scale line is provided on the upper rear side of the probe bracket. A scale 307, which is mounted next to the second insulating rod 305, allows the probe bracket 308 to rotate according to the reading on the scale 307 after the clamping screw is loosened. Depending on the installation method of the insulator string during testing, the probe bracket 308 is rotated and adjusted according to the scale 307 to ensure tight contact between the probe 310 and the steel caps at both ends of the insulator. Furthermore, each probe 310 is equipped with a probe clamp in the middle section, reducing the length of the probe cantilever beam, thereby improving the rigidity of the probe 310, reducing vibration amplitude, and facilitating operation. Each probe 310 has an "eight"-shaped tip, which serves as a guide when it comes into contact with the insulator during operation, improving the error tolerance of the pilot's operation. The end of the probe 310 is embedded in the probe plug 309 by an irregular bending method. The probe 310 is inserted and removed by elastic deformation, which facilitates the installation of the probe 310. If the probe 310 is accidentally stuck on the insulator sheet, the UAV 101 can increase its power and fly backward to pull out the probe 310, reducing the risk of crash. The probe plug 309 has holes on the inside, which allow the wires inside the probe bracket 308 to contact the end of the probe 310, so that the probe 310 can be connected to the board in the control box 302 for stable testing.

[0037] In summary, the structure of this testing device, during use, firstly, the gimbal housing 102 containing the control board and communication antenna is installed on the gimbal bracket 104. The entire testing component 3 is fixed to the belly of the UAV via the belly mounting bracket 2. The second insulating rod 305 is pulled out from the first insulating rod 301 to a suitable length, and the screws of the insulating rod connector 306 are tightened to fix the two insulating rods together. Then, the probe 310 is inserted into the probe plug 309. Depending on the different operating scenarios and the installation method of the insulator, the probe bracket 308 is rotated so that the two probes 310 and the insulator string are always kept on the same horizontal line. When testing the tension horizontal insulator string, the probe bracket 308 is kept horizontal, and the probe 310 is in close contact with the steel caps on both sides of the insulator for testing. When testing the suspension insulator string, the probe bracket 308 is rotated 90 degrees to keep it vertical, and the probe 310 is in close contact with the steel caps at the top and bottom ends of the insulator for testing.

[0038] After preparation, the detection system is switched on, and the pilot controls the detection unit via the drone remote controller and control system to begin operation. The pilot then controls the drone to take off, carrying the device, and flies to the vicinity of the insulator. Two probes contact the steel caps at both ends of the insulator. Upon contact, the device automatically performs the detection and displays the measured values ​​in real-time on the remote controller. Simultaneously, the drone's video recording function is activated, capturing the appearance of the target insulator. When the insulator resistance falls below the set threshold, an audible and visual alarm will sound on the remote controller to notify the pilot.

[0039] The above description is merely a selection of preferred embodiments of this disclosure and an explanation of the technical principles employed. Those skilled in the art should understand that the scope of application in the embodiments of this disclosure is not limited to technical solutions formed by specific combinations of the above-described technical features, but should also cover other technical solutions formed by arbitrary combinations of the above-described technical features or their equivalents without departing from the above practical concept. For example, technical solutions formed by substituting the above-described features with (but not limited to) technical features with similar functions disclosed in the embodiments of this disclosure.

Claims

1. An insulator resistance efficient detection device, comprising a UAV main body (1), characterized in that: The bottom end of the unmanned aerial vehicle body (1) is fixedly provided with a mounting rack (2), and the bottom end of the mounting rack (2) is fixedly provided with a detection assembly (3), the detection assembly (3) comprises a first insulating rod (301), one end of the first insulating rod (301) is connected with an electric control box (302), one side of the electric control box (302) is provided with a charging port and a switch port, and the charging port and the switch port are respectively provided with a charging port plug (303) and a switch port plug (304), the other end of the first insulating rod (301) is inserted into a second insulating rod (305), and the first insulating rod (301) and the second insulating rod (305) are connected with an insulating rod connecting piece (306), one end of the second insulating rod (305) is fixedly provided with a scale disc (307), and a probe support (308) is attached to one side of the scale disc (307), and the probe support (308) is fixedly provided with a probe plug-in (309) on the front end of the two sides, and one end of the probe plug-in (309) is inserted with a probe (310).

2. The high-accuracy insulator resistance detection device according to claim 1, characterized in that: The probe (310) is elastically inserted into the probe support (308) through the probe plug-in (309), and the probe support (308) is sleeved and rotationally connected with the second insulating rod (305).

3. The high-accuracy insulator resistance detection device according to claim 1, characterized in that: The electric control box (302) is connected with the first insulating rod (301) and the second insulating rod (305) in a telescopic mode, and a detection board is arranged in the electric control box (302).

4. The high-accuracy insulator resistance detection device according to claim 1, characterized in that: The unmanned aerial vehicle body (1) comprises an unmanned aerial vehicle (101), and a holder shell (102) is arranged on one side of the bottom of the unmanned aerial vehicle (101), the top end of the holder shell (102) is connected with a quick connector (103), and the top end of the quick connector (103) is connected with a holder support (104).

5. The high-accuracy insulator resistance detection device according to claim 4, characterized in that: The holder shell (102) is buckled with the holder support (104) at the bottom end through the quick connector (103), and the holder shell (102) is internally provided with a control board and a communication antenna.

6. The high-accuracy insulator resistance detection device according to claim 1, characterized in that: The mounting rack (2) comprises a belly mounting plate (201), and the top surface of the belly mounting plate (201) is fixedly connected with the bottom belly of the unmanned aerial vehicle body (1) in a threaded mode, the bottom surface of the belly mounting plate (201) is connected with shock absorbers (202) around, the bottom end of the shock absorber (202) is connected with an upper carrier connecting plate (203), the bottom end of the upper carrier connecting plate (203) is connected with a pipe hanger (204), the bottom end of the pipe hanger (204) is fixedly provided with a lower carrier connecting plate (205) between the inner walls of the two sides, the bottom end of the pipe hanger (204) is connected with pipe hanger clamps (206) on the two sides, and the inner wall of the pipe hanger clamp (206) is buckled with the first insulating rod (301).

7. The high-accuracy insulator resistance detection device according to claim 6, characterized in that: The pipe hanger clamp (206) is fixedly connected with the pipe hanger (204) and the upper carrier connecting plate (203), and the pipe hanger clamp (206) is buckled in the middle section of the first insulating rod (301).

Citation Information

Patent Citations

  • A kind of tension insulator detection device and method

    CN108896887B