CN-121995102-A - Electricity testing device, unmanned plane-based electricity testing method, equipment, medium and product

CN121995102ACN 121995102 ACN121995102 ACN 121995102ACN-121995102-A

Abstract

The embodiment of the application provides an electricity testing device, an unmanned aerial vehicle-based electricity testing method, equipment, a medium and a product. The electricity testing device comprises an electricity testing body, a flexible thin rod, an angle adjusting mechanism, a touch assembly and a communication module, wherein the electricity testing body is arranged on an unmanned aerial vehicle foot stand and used for conducting electricity testing on an electric line to be tested when the flexible touch assembly is in contact with the electric line to be tested, the flexible thin rod is arranged on the unmanned aerial vehicle foot stand and clamped on the unmanned aerial vehicle foot stand through the angle adjusting mechanism and used for fixing the touch assembly, the angle adjusting mechanism is two clamps fixed at the tail end of the flexible thin rod and used for adjusting angles of the flexible thin rod and the touch assembly, the touch assembly is arranged at the top end of the flexible thin rod and electrically connected with the electricity testing body to enable a contact of the electricity testing device to extend, and the communication module is arranged in the electricity testing body and used for conducting wireless communication with a ground end receiver. The reliable contact of the electroscope and the lead is guaranteed, and the radio transmission of the electroscope is realized.

Inventors

CHEN ZHIYONG
HUANG XIAOFA
LIN YANCHENG
CHEN XIAOGUANG
WANG XIAOXIAO
QIU HANFENG
CHEN YIGE
QIN ZHIQIANG
Lin Renpu
ZHANG JIANFENG
XU PENGLEI
GAO SHISEN
WANG WEICONG
LIAO CHENGJIU
LUO QINGXIONG
LAN GANG
LIN HAINAN
CHEN XIAORU
ZHONG SENMIAO

Assignees

广东电网有限责任公司惠州供电局

Dates

Publication Date: 20260508
Application Date: 20260119

Claims (10)

1. The electroscope device is characterized by comprising an electroscope body, a flexible thin rod, an angle adjusting mechanism, a touch assembly and a communication module; The electroscope body is arranged on the tripod of the unmanned aerial vehicle and is used for conducting electroscope on the to-be-tested electric line when the flexible touch assembly is in contact with the to-be-tested electric line; the flexible thin rod is arranged on the unmanned aerial vehicle foot rest, clamped on the unmanned aerial vehicle foot rest through the angle adjusting mechanism and used for fixing the touch assembly; the angle adjusting mechanism is two clamps fixed at the tail end of the flexible thin rod and used for adjusting the angles of the flexible thin rod and the touch assembly; the touch assembly is arranged at the top end of the flexible thin rod and is connected with the electroscope body to realize the contact extension of the electroscope; The communication module is arranged in the electroscope body and is used for carrying out wireless communication with a ground end receiver.
2. The electrical verification device of claim 1, wherein the touch assembly is made of wire; the touch assembly is mechanically connected with the flexible thin rod, and one end of the metal wire is in contact with the to-be-tested electric line; the flexible thin rod is made of composite carbon fiber materials and has good flexibility and fatigue resistance.
3. The electroscope of claim 1, wherein the angular adjustment of the angular adjustment structure is in the range of 0 ° to 45 °.
4. An electricity testing method based on an unmanned aerial vehicle, applied to unmanned aerial vehicle control equipment, wherein the unmanned aerial vehicle control equipment is used for controlling a first unmanned aerial vehicle and a second unmanned aerial vehicle to fly, the second unmanned aerial vehicle is provided with an image acquisition device, and an electricity testing device as claimed in any one of claims 1-3 is provided below the first unmanned aerial vehicle, and the method comprises the following steps: Simultaneously sending flight control instructions to the first unmanned aerial vehicle and the second unmanned aerial vehicle so as to enable the first unmanned aerial vehicle and the second unmanned aerial vehicle to fly to two opposite sides of an electric circuit to be tested; receiving a first image sent by the second unmanned aerial vehicle, wherein the first image at least comprises the to-be-tested line image and the first unmanned aerial vehicle image; According to the first image, an adjustment control instruction is sent to the first unmanned aerial vehicle to adjust the pose of the first unmanned aerial vehicle relative to the to-be-tested electric line until the flexible touch component of the to-be-tested electric line of the electric testing device carried by the first unmanned aerial vehicle touches the to-be-tested electric line; receiving a second image sent by the second unmanned aerial vehicle; After the flexible touch assembly is determined to deform according to the second image, an electroscope signal is sent to an electroscope device of the first unmanned aerial vehicle, so that the electroscope device performs electroscope on the to-be-detected electric line, and an electroscope result is obtained; And receiving the electricity testing result sent by the electricity testing device.
5. The method of claim 4, wherein the sending an adjustment control instruction to the first drone based on the first image, comprises: Determining a relative position relationship between the first unmanned aerial vehicle and the circuit to be tested based on the first unmanned aerial vehicle image and the circuit to be tested in the first image; determining attitude adjustment information and position adjustment information of the first unmanned aerial vehicle according to the relative position relation; Generating the adjustment control instruction according to the posture adjustment information and the position adjustment information; and sending the adjustment control instruction to the first unmanned aerial vehicle.
6. The method of claim 4, wherein determining the deformation of the flexible touch assembly from the second image comprises: identifying a first shape of the flexible touch assembly in the second image; Determining the similarity of the first shape and a preset shape; and when the similarity accords with a preset threshold value, determining that the flexible touch assembly deforms.
7. The method of claim 4, wherein after the receiving the electricity test result sent by the electricity test device, the method further comprises: and sending out a warning signal when the electricity test result is that the to-be-tested line is electrified, wherein the warning signal is an acousto-optic warning and/or the warning signal is warning information.
8. An electronic device is characterized by comprising a memory and a processor; The memory stores computer-executable instructions; The processor executing computer-executable instructions stored in the memory, causing the processor to perform the method of any one of claims 4-7.
9. A computer readable storage medium having stored therein computer executable instructions which when executed are adapted to implement the method of any of claims 4-7.
10. A computer program product comprising a computer program which, when executed, implements the method of any of claims 4-7.

Description

Electricity testing device, unmanned plane-based electricity testing method, equipment, medium and product Technical Field The application relates to the technical field of electric power inspection, in particular to an electricity inspection device, an unmanned aerial vehicle-based electricity inspection method, equipment, a medium and a product. Background In a power system, the electricity inspection of a line is an important link for guaranteeing the safety of operators and ensuring the normal operation of power equipment. Although power outage measures have typically been performed prior to operation, the lines may still be live due to potential risks of breaker failure, mishandling, induced voltage, reverse power delivery, etc. If the electricity inspection confirmation is not performed at this time, the operator may misjudge as a safe state and directly contact the line, thereby causing electric shock accidents, serious personal injury and even death accidents. Therefore, the line electricity inspection is a first defense line for guaranteeing the safety of electric power operation, and is also an essential link for the operation, maintenance and management of an electric power system. With the development of unmanned aerial vehicle technology, unmanned aerial vehicle electricity inspection gradually becomes a new solution. In the prior art, a method for carrying out electricity inspection on a circuit by using an unmanned aerial vehicle generally adopts a rigid probe to directly contact with a wire, an electroscope is fixed on the unmanned aerial vehicle through an insulating rod, one end of the insulating rod is fixed on the unmanned aerial vehicle, and the electroscope is arranged at the other end of the insulating rod, so that the electricity inspection is carried out on the circuit through the electroscope. However, the existing method for testing the line has low efficiency, and the design of the electrical testing device is unreasonable, so that the electrical testing device cannot adapt to the problem of complex environment. Disclosure of Invention The embodiment of the application provides an electricity testing device, an unmanned aerial vehicle-based electricity testing method, equipment, a medium and a product, which are used for solving the problems that the efficiency is low, the design of the electricity testing device is unreasonable, and the complex environment cannot be adapted in the prior art. In a first aspect, an embodiment of the present application provides an electroscope device, the electroscope device including an electroscope body, a flexible wand, an angle adjustment mechanism, a touch assembly, and a communication module; The electroscope body is arranged on the tripod of the unmanned aerial vehicle and is used for conducting electroscope on the to-be-tested electric line when the flexible touch assembly is in contact with the to-be-tested electric line; the flexible thin rod is arranged on the unmanned aerial vehicle foot rest, clamped on the unmanned aerial vehicle foot rest through the angle adjusting mechanism and used for fixing the touch assembly; the angle adjusting mechanism is two clamps fixed at the tail end of the flexible thin rod and used for adjusting the angles of the flexible thin rod and the touch assembly; The touch assembly is arranged at the top end of the flexible thin rod and is electrically connected with the electroscope body to realize the contact extension of the electroscope; The communication module is arranged in the electroscope body and is used for carrying out wireless communication with a ground end receiver. In one possible embodiment, the touch assembly is made of wire; the touch assembly is mechanically connected with the flexible thin rod, and one end of the metal wire is in contact with the to-be-tested electric line; the flexible thin rod is made of composite carbon fiber materials and has good flexibility and fatigue resistance. In one possible embodiment, the angle adjustment structure has an angle adjustment range of 0 ° to 45 °. In a second aspect, an embodiment of the present application provides an electricity testing method based on an unmanned aerial vehicle, which is applied to an unmanned aerial vehicle control device, where the unmanned aerial vehicle control device is used for controlling a first unmanned aerial vehicle and a second unmanned aerial vehicle to fly, and an electricity testing device in the first aspect is mounted below the first unmanned aerial vehicle, and the electricity testing method includes: Simultaneously sending flight control instructions to the first unmanned aerial vehicle and the second unmanned aerial vehicle so as to enable the first unmanned aerial vehicle and the second unmanned aerial vehicle to fly to two opposite sides of an electric circuit to be tested; receiving a first image sent by the second unmanned aerial vehicle, wherein the first image at least comprises the to-be-tested line i