Unmanned aerial vehicle contact electricity testing device

Through the drone contact power inspection device, the intelligent joystick and contact components are used to achieve efficient and safe power inspection operations, solving the problems of power inspection difficulty and safety hazards in high altitude operations, and improving the accuracy and operation and maintenance level of power inspection .

CN222259455UActive Publication Date: 2024-12-27MAINTENANCE CO STATE GRID QINGHAI ELECTRIC POWER +2
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Patent Information

Application Number
CN202420141340.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-01-19
Publication Date
2024-12-27
Estimated Expiration
2034-01-19

AI Technical Summary

Technical Problem

Most of the existing power inspection work are high altitude operations, and it is easy to shake when operating the electrical inspection appliance and it is difficult to align the power inspection point, which increases the difficulty of work and poses safety hazards.

Method used

A drone contact power inspection device is designed, including electrical tester, power inspection base, flash light, speaker, installation component and probe. It is moved to the measurement point through the intelligent joystick of the drone and used contact components to realize it. Accurate power verification, including contact rods, housings and locking screws, ensure that the probe is in contact with the transmission line and triggers induction.

Benefits of technology

It improves the accuracy and efficiency of power inspection, reduces operating costs, enhances safety, and improves the level of power grid operation and maintenance.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of electricity testing, in particular to an unmanned aerial vehicle contact electricity testing device, which comprises an electroscope, an electricity testing seat body, a flashing light, a loudspeaker, a mounting assembly and a probe, and is characterized in that the electroscope is in threaded connection with the electricity testing seat body and is positioned on one side of the electricity testing seat body, and the flashing light is fixedly connected with the electricity testing seat body and is embedded in one side of the electricity testing seat body; the loudspeaker is fixedly connected with the electricity testing seat body and embedded in one side of the electricity testing seat body, the installation assembly is fixedly connected with the electricity testing seat body and located on one side of the electricity testing seat body, and the probe is fixedly connected with the electroscope and located at one end of the electroscope. The device is simple in structure, light in weight and small in size, can be fixed to the end part of an intelligent control rod of the unmanned aerial vehicle, is driven by the unmanned aerial vehicle to move to one side of a measurement point, improves the electricity testing efficiency and accuracy, is high in intelligent degree, is high in electricity testing efficiency, is high in safety, is low in operation cost, and can improve the operation and maintenance level of a power grid.
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Description

Technical Field

[0001] The utility model relates to the technical field of electricity testing, in particular to a contact electricity testing device for unmanned aerial vehicles. Background Art

[0002] At present, maintenance personnel often perform power outage maintenance work in their daily work. Before the power outage maintenance work, they must use a tester to verify that the line has been powered off, and then install the grounding wire to ensure the personal safety of the maintenance personnel. Maintenance personnel must strictly abide by the safety operating rules during power outage maintenance work to ensure their own personal safety and the normal operation of the equipment.

[0003] However, in the prior art, most of the electrical testing work is high-altitude work. When the workers operate the electrical tester, it is easy to shake and difficult to aim at the testing point, which increases the difficulty of the work and is prone to safety hazards during the electrical testing process. Utility Model Content

[0004] The purpose of the utility model is to provide a contact electrical testing device for unmanned aerial vehicles, aiming to solve the technical problems that most of the electrical testing work in the prior art is high-altitude operation, and when the staff operates the electrical tester, it is easy to shake and difficult to align the electrical testing point, which increases the difficulty of the work, and there are potential safety hazards during the electrical testing process.

[0005] To achieve the above-mentioned purpose, the utility model adopts a contact electrical test device for unmanned aerial vehicles, including an electrical tester, an electrical tester seat, a strobe light, a horn, a mounting assembly and a probe, the electrical tester is threadedly connected to the electrical tester seat and is located on one side of the electrical tester seat, the strobe light is fixedly connected to the electrical tester seat and embedded in one side of the electrical tester seat, the horn is fixedly connected to the electrical tester seat and embedded in one side of the electrical tester seat, the mounting assembly is fixedly connected to the electrical tester seat and is located on one side of the electrical tester seat, and the probe is fixedly connected to the electrical tester and is located at one end of the electrical tester.

[0006] Among them, the electrical test seat body includes a base, a switch button, a charging interface and a power display. The switch button is fixedly connected to the base and embedded in one side of the base. The charging interface is fixedly connected to the base and embedded in one side of the base. The power display is fixedly connected to the base and embedded in one side of the base.

[0007] Wherein, the installation assembly includes a fastener seat, a buckle and a locking bolt, the fastener seat is fixedly connected to the base and is located on one side of the base, one end of the buckle is rotatably connected to the fastener seat, and one end of the buckle is embedded in the interior of the fastener seat, the other end of the buckle contacts the fastener seat through the locking bolt, and the buckle is limited by the locking bolt.

[0008] The drone contact electrical testing device further comprises a contact component, which is sleeved on the outer wall of the probe and located at the end of the electrical tester.

[0009] Among them, the contact component includes a contact rod, a shell and a locking screw. The shell is sleeved on the outer wall of the probe, one end of the contact rod is embedded in the interior of the shell, and there are multiple locking screws. Each locking screw is threadedly connected to the shell and is located on one side of the shell.

[0010] The beneficial effects of the drone contact electrical testing device of the utility model are: lightweight and miniaturized design, which can be fixed to the end of the drone's intelligent joystick, and moved to one side of the measuring point under the drive of the drone, thereby improving the efficiency and accuracy of electrical testing, with high intelligence, fast electrical testing efficiency, strong safety and low operating cost, which can improve the operation and maintenance level of the power grid. BRIEF DESCRIPTION OF THE DRAWINGS

[0011] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0012] Figure 1 The utility model is a structural schematic diagram of a contact electrical testing device for an unmanned aerial vehicle.

[0013] Figure 2 The utility model is a side view of a contact electrical testing device for an unmanned aerial vehicle.

[0014] Figure 3 The utility model is a partial structural schematic diagram of a UAV contact electrical testing device.

[0015] 1-electrical tester, 2-base, 3-switch button, 4-charging port, 5-power indicator, 6-strobe light, 7-speaker, 8-fastener seat, 9-clip, 10-locking bolt, 11-probe, 12-contact rod, 13-housing, 14-locking screw. DETAILED DESCRIPTION

[0016] See also Figures 1 to 3The utility model provides a contact electric test device for unmanned aerial vehicles, including an electric tester 1, an electric tester seat, a flashing light 6, a speaker 7, a mounting assembly and a probe 11. The electric tester 1 is threadedly connected to the electric tester seat and is located on one side of the electric tester seat. The flashing light 6 is fixedly connected to the electric tester seat and embedded in one side of the electric tester seat. The speaker 7 is fixedly connected to the electric tester seat and embedded in one side of the electric tester seat. The mounting assembly is fixedly connected to the electric tester seat and is located on one side of the electric tester seat. The probe 11 is fixedly connected to the electric tester 1 and is located at one end of the electric tester 1.

[0017] Furthermore, the electrical test seat body includes a base 2, a switch button 3, a charging interface 4 and a power display 5, the switch button 3 is fixedly connected to the base 2 and embedded in one side of the base 2, the charging interface 4 is fixedly connected to the base 2 and embedded in one side of the base 2, and the power display 5 is fixedly connected to the base 2 and embedded in one side of the base 2.

[0018] Furthermore, the mounting assembly includes a fastener seat 8, a buckle 9 and a locking bolt 10. The fastener seat 8 is fixedly connected to the base 2 and is located on one side of the base 2. One end of the buckle 9 is rotatably connected to the fastener seat 8, and one end of the buckle 9 is embedded in the inside of the fastener seat 8. The other end of the buckle 9 contacts the fastener seat 8 through the locking bolt 10, and the buckle 9 is limited by the locking bolt 10.

[0019] Furthermore, the drone contact electrical testing device further comprises a contact component, which is sleeved on the outer wall of the probe 11 and located at the end of the electrical tester 1 .

[0020] Furthermore, the contact assembly includes a contact rod 12, a sleeve 13 and a locking screw 14, the sleeve 13 is sleeved on the outer wall of the probe 11, one end of the contact rod 12 is embedded in the sleeve 13, and there are multiple locking screws 14, each of which is threadedly connected to the sleeve 13 and is located on one side of the sleeve 13.

[0021] In this embodiment, the buckle 9 and the fastener seat 8 are sleeved on the outer wall of the drone smart pole, and the buckle 9 and the fastener seat 8 are fixed by the locking bolt 10, the shell 13 is sleeved on the outer wall of the probe 11, and the contact rod 12 is inserted into the interior of the shell 13, and the probe 11 contacts the contact rod 12, and the shell 13 is locked by the locking screw 14, so that the contact rod 12 and the probe 11 are clamped. When the contact rod 12 and the probe 11 contact or approach the power transmission line, the contact induction generates induced charges of the same polarity, and the two-pole platinum sheet at the other end of the contact repel each other due to the charges of the same polarity, so the conductive platinum sheet opens, causing the detection circuit to be instantly turned on, thereby realizing the electrical detection of the wire. During the electrical detection process, the flashing light 6 and the speaker 7 can be used for warning, and the power display 5 can run through the remaining power of the current device, and the switch button 3 controls the opening and closing of the device, and the charging interface 4 charges the device.

[0022] The above disclosure is only a preferred embodiment of the present invention, and certainly cannot be used to limit the scope of rights of the present invention. Ordinary technicians in this field can understand that all or part of the processes of the above embodiment and equivalent changes made according to the claims of the present invention still fall within the scope covered by the utility model.

Claims

1. A drone contact electrical testing device, characterized in that: It includes an electrician, an electrician socket, a flashing light, a horn, a mounting assembly and a probe. The electrician is threadedly connected to the electrician socket and is located on one side of the electrician socket. The flashing light is fixedly connected to the electrician socket and embedded in one side of the electrician socket. The horn is fixedly connected to the electrician socket and embedded in one side of the electrician socket. The mounting assembly is fixedly connected to the electrician socket and is located on one side of the electrician socket. The probe is fixedly connected to the electrician and is located at one end of the electrician.

2. A drone contact electrical testing device as claimed in claim 1, characterized in that: The electrical test seat body includes a base, a switch button, a charging interface and a power display. The switch button is fixedly connected to the base and embedded in one side of the base. The charging interface is fixedly connected to the base and embedded in one side of the base. The power display is fixedly connected to the base and embedded in one side of the base.

3. A drone contact electrical testing device as claimed in claim 2, characterized in that: The mounting assembly includes a fastener seat, a buckle and a locking bolt. The fastener seat is fixedly connected to the base and is located on one side of the base. One end of the buckle is rotatably connected to the fastener seat, and one end of the buckle is embedded in the interior of the fastener seat. The other end of the buckle contacts the fastener seat through the locking bolt, and the buckle is limited by the locking bolt.

4. A drone contact electrical testing device as claimed in claim 3, characterized in that: The unmanned aerial vehicle contact electrical testing device further comprises a contact type component, which is sleeved on the outer wall of the probe and located at the end of the electrical tester.

5. A drone contact electrical testing device as claimed in claim 4, characterized in that: The contact assembly includes a contact rod, a sleeve and a locking screw. The sleeve is sleeved on the outer wall of the probe, one end of the contact rod is embedded in the interior of the sleeve, and there are multiple locking screws. Each locking screw is threadedly connected to the sleeve and is located on one side of the sleeve.

Citation Information

Cited By

  • Unmanned aerial vehicle electricity testing device

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