CN219285267U - Unmanned aerial vehicle electricity verification device based on electromagnetic induction principle - Google Patents
Unmanned aerial vehicle electricity verification device based on electromagnetic induction principle Download PDFInfo
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- CN219285267U CN219285267U CN202223271205.2U CN202223271205U CN219285267U CN 219285267 U CN219285267 U CN 219285267U CN 202223271205 U CN202223271205 U CN 202223271205U CN 219285267 U CN219285267 U CN 219285267U
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Abstract
The utility model relates to an unmanned aerial vehicle electricity inspection device based on an electromagnetic induction principle, which comprises an unmanned aerial vehicle, an electromagnetic induction electricity inspection device, a camera, an electromagnetic induction wireless charging device, an energy storage device, a controller, a wireless communication module and a remote terminal, wherein the electromagnetic induction electricity inspection device, the camera, the controller and the communication module are arranged on the unmanned aerial vehicle; the electromagnetic induction electricity testing device and the camera are utilized to realize the convenience and the rapidness of electricity testing, the electromagnetic induction electricity testing device and the camera are utilized to realize the function of unmanned aerial vehicle omnibearing electricity testing, the working efficiency is improved, and the danger of electricity testing operation of constructors is avoided.
Description
Technical Field
The utility model relates to the technical field of electricity testing equipment, in particular to an unmanned aerial vehicle electricity testing device based on an electromagnetic induction principle.
Background
With the continuous development of scientific technology, unmanned aerial vehicle technology has been greatly improved in recent years, unmanned aerial vehicle is unmanned aerial vehicle that utilizes radio remote control equipment or self-contained program control device to control, consequently many intelligent, multi-functional unmanned aerial vehicle have appeared, to the transmission information in some small-scale regions, demand such as monitoring, it is a new concept aircraft in rapid development, and it has flexibility, and the reaction is quick, unmanned flight, advantage that the operation is required low.
The unmanned aerial vehicle can realize real-time image transmission and high-risk area detection functions by carrying various sensors, can be used in various fields, such as electric power, along with the rapid development of industrialization and urbanization in China, the demand of residents for electric power energy is increased year by year, so that the surge of electricity consumption inevitably leads to the construction and development of an electric power network, in particular to a high-voltage transmission line, and the unmanned aerial vehicle has the characteristics of long mileage, multiple nodes and crisscross operation and maintenance work of network allocation personnel, thereby bringing a great deal of workload and safety challenges; when a distribution network worker performs operation detection work of a high-voltage transmission line, the high-voltage transmission line is required to be subjected to electroscopic work at first, but the conventional electroscopic work has the following risks and problems that 1, the worker ascends the height by means of a pole climbing tool or a ladder to fall at high altitude; 2. when the operator does not test electricity, the operator uses an electrician knife to cut open the insulating layer of the insulated wire, so that the operator is at risk of touching the exposed wire; 3. the problem that the insulation layer of the insulated wire is lost or the insulation is reduced during electricity inspection exists; 4. the power-on and power-off time is influenced by overlong power-on and power-off time, so that the problems of power supply reliability and the like are reduced.
Chinese patent publication No. CN112550708B discloses an unmanned aerial vehicle electricity test apparatus, which includes an unmanned aerial vehicle, the unmanned aerial vehicle including a frame; the device comprises a mounting bracket, a first rotating device, a second rotating device and an electricity testing device, wherein the electricity testing device comprises a mounting rod fixed on a first rotating seat and an electricity testing device fixed on the mounting rod, and the device is high in electricity testing efficiency and good in electricity testing safety; and can effectively improve the in-process of checking the electricity, unmanned aerial vehicle's stability to unmanned aerial vehicle's unmanned aerial vehicle equipment of checking the electricity in the unbalanced problem of effectively solving unmanned aerial vehicle because of external force interference, but the laser rangefinder sensor that this patent utilized need adjust unmanned aerial vehicle's angle, and the operation is complicated, and the effect of checking the electricity is limited.
Disclosure of Invention
The utility model provides an unmanned aerial vehicle electricity testing device based on an electromagnetic induction principle, which utilizes the electromagnetic induction electricity testing device to realize the function of omnibearing electricity testing of an unmanned aerial vehicle, improves the working efficiency and avoids the danger of electricity testing operation of constructors.
In order to achieve the above purpose, the utility model is realized by adopting the following technical scheme:
the unmanned aerial vehicle electricity inspection device based on the electromagnetic induction principle comprises an unmanned aerial vehicle, an electromagnetic induction electricity inspection device, a camera, a controller, a wireless communication module and a remote terminal, wherein the electromagnetic induction electricity inspection device, the camera, the controller and the communication module are arranged on the unmanned aerial vehicle, the electromagnetic induction electricity inspection device and the camera are used for connecting an output signal wire with an IO interface of the controller, electromagnetic induction electricity inspection and shooting are carried out on the wire, and then electricity inspection information is transmitted to the controller, a communication port of the controller is connected with the wireless communication module, and the wireless communication module is connected with the remote terminal of an operator in a wireless manner;
the wireless charging device of electromagnetic induction charges for energy storage device, and energy storage device is unmanned vehicles, electromagnetic induction electricity test device, camera, controller and wireless communication module power supply.
Further, unmanned vehicles includes fuselage, horn subassembly and rotor power pack, and unmanned vehicles fuselage is including the inside casing that has the holding chamber, and the horn subassembly rotates to be connected at the wall of casing, and rotor power pack installs on the horn subassembly.
Further, the electromagnetic induction electricity inspection device comprises an electromagnetic induction circuit, an audible and visual alarm device and a vibration sensor, wherein the electromagnetic induction circuit is used for inducing an electromagnetic field around the electricity inspection circuit, and an output port of the electromagnetic induction circuit is connected with the vibration sensor and the audible and visual alarm device to be connected with an interface of the controller.
Further, the electromagnetic induction lines are four and are respectively fixed on four horn arms of the unmanned aerial vehicle.
Further, the controller selects an ARM chip, a UART port is connected with a communication port, and an IO interface is connected with the camera, the vibration sensor and the audible and visual alarm.
Compared with the prior art, the utility model has the beneficial effects that:
1) The electromagnetic induction electricity testing device and the camera are utilized to realize an omnibearing electricity testing mode of the unmanned aerial vehicle, so that the unmanned aerial vehicle is convenient and quick;
2) The efficiency of checking electricity has been improved greatly, has avoided operating personnel to check the danger of electricity.
Drawings
Fig. 1 is a block diagram of the structure of the present utility model.
Fig. 2 is a schematic structural view of the unmanned aerial vehicle according to the present utility model.
Fig. 3 is a circuit diagram of an electromagnetic inductor according to the present utility model.
Fig. 4 is a schematic diagram of the controller connection according to the present utility model.
In the figure: 1. unmanned aerial vehicle 2, horn assembly 3, rotor power assembly 4, electromagnetic induction coil 5, camera 6, electromagnetic induction wireless charging device 7, conductor long rod 8 power indicator lamp
Detailed Description
The following is a further description of embodiments of the utility model, taken in conjunction with the accompanying drawings:
see fig. 1 for a block diagram of the structure of the present utility model. The utility model discloses an unmanned aerial vehicle electricity inspection device based on an electromagnetic induction principle, which comprises an unmanned aerial vehicle 1, an electromagnetic induction electricity inspection device, a camera 5, a controller, a wireless communication module and a remote terminal, wherein the electromagnetic induction electricity inspection device, the camera 5, the controller and the communication module are arranged on the unmanned aerial vehicle, the output end of the electromagnetic induction electricity inspection device is connected with a controller IO interface, the camera 5 adopts a 360-degree high-definition camera, an output signal wire is connected with the controller IO interface, and after electromagnetic induction electricity inspection and shooting are carried out on the circuit, electricity inspection information is transmitted to the controller, a communication port of the controller is connected with the wireless communication module, and the wireless communication module is wirelessly connected with the remote terminal of an operator;
the unmanned aerial vehicle further comprises an electromagnetic induction wireless charging device 6 and an energy storage device, wherein the electromagnetic induction wireless charging device 6 cuts an electricity inspection line by utilizing a conductor long rod 7 to generate electromotive force to charge the energy storage device, the energy storage device charges the unmanned aerial vehicle and the electromagnetic induction electricity inspection device, and a power indicator 8 of the unmanned aerial vehicle 1 displays whether the unmanned aerial vehicle 1 has electricity or not.
See fig. 2, further, unmanned aerial vehicle includes fuselage, horn subassembly 2 and rotor power pack 3, and the unmanned aerial vehicle fuselage is including inside having the casing that holds the chamber, and horn subassembly 2 rotates to be connected the wall at the casing, and rotor power pack 3 installs on horn subassembly 2, unmanned aerial vehicle adopts light structure, and horn subassembly 2 directly articulate on the casing, and the casing bears the rotor power pack on horn subassembly 2 and the horn subassembly 2.
See fig. 3, further, electromagnetic induction electroscope includes electromagnetic induction circuit, audible and visual alarm device, vibration sensor, electromagnetic induction circuit is four, fix respectively on four horn subassemblies 2 of unmanned vehicles, electromagnetic induction circuit includes electromagnetic induction coil 4L1, resistance-capacitance absorbing device R1 and C3, divider resistor R2 and amplifier VT, electromagnetic induction coil 4L1 senses the magnetic field signal of circuit around the circuit, after the amplifier amplifies the output connection controller analog interface AIN1-AIN7 arbitrary pin, vibration sensor connection controller analog input interface, whether the output unmanned vehicles bumps, audible and visual alarm device connects the digital output interface of controller, send the warning to electroscope result.
Referring to fig. 4, further, the controller selects an ARM chip, and the chip model is: CH32F103, its IO interface PA3, PA4 connect the serial port of the camera, receive the image information that the camera transmits, IO interface PD0 connects the signal output part of the audible and visual alarm, IO interface AIN0 connects the output part of the vibration sensor.
Further, the wireless communication module adopts a chip model E103-W02, and communication ports GPIO1 and GPIO2 of the wireless communication module are connected with UART transmission ports PA10 and PA11 of the controller.
The above examples are implemented on the premise of the technical scheme of the present utility model, and detailed implementation manners and specific operation processes are given, but the protection scope of the present utility model is not limited to the above examples. The methods used in the above examples are conventional methods unless otherwise specified.
Claims (5)
1. The unmanned aerial vehicle electricity inspection device based on the electromagnetic induction principle is characterized by comprising an unmanned aerial vehicle, an electromagnetic induction electricity inspection device, a camera, a controller, a wireless communication module and a remote terminal, wherein the electromagnetic induction electricity inspection device, the camera, the controller and the communication module are arranged on the unmanned aerial vehicle, the electromagnetic induction electricity inspection device and the camera are used for connecting an output signal wire with an IO interface of the controller, electromagnetic induction electricity inspection is carried out on the wire, and after shooting, electricity inspection information is transmitted to the controller, a communication port of the controller is connected with the wireless communication module, and the wireless communication module is connected with the remote terminal of an operator in a wireless way;
the wireless charging device of electromagnetic induction charges for energy storage device, and energy storage device is unmanned vehicles, electromagnetic induction electricity test device, camera, controller and wireless communication module power supply.
2. The unmanned aerial vehicle electricity inspection device based on the electromagnetic induction principle according to claim 1, wherein the unmanned aerial vehicle comprises a body, a horn assembly and a rotor power assembly, the unmanned aerial vehicle body comprises a shell with a containing cavity inside, the horn assembly is rotationally connected to the wall surface of the shell, and the rotor power assembly is installed on the horn assembly.
3. The unmanned aerial vehicle electricity test device based on the electromagnetic induction principle according to claim 1, wherein the electromagnetic induction electricity test device comprises an electromagnetic induction circuit, an audible and visual alarm device and a vibration sensor, the electromagnetic induction circuit induces an electromagnetic field around the electricity test circuit, and an output port of the electromagnetic induction circuit is connected with the vibration sensor and the audible and visual alarm device to an interface of a controller.
4. The unmanned aerial vehicle electricity inspection device based on the electromagnetic induction principle according to claim 3, wherein four electromagnetic induction lines are respectively fixed on four horn arms of the unmanned aerial vehicle.
5. The unmanned aerial vehicle electricity inspection device based on the electromagnetic induction principle according to claim 1, wherein the controller is an ARM chip, a UART port is connected with a communication port, and an IO interface is connected with a camera, a vibration sensor and an audible and visual alarm.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202223271205.2U CN219285267U (en) | 2022-12-07 | 2022-12-07 | Unmanned aerial vehicle electricity verification device based on electromagnetic induction principle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202223271205.2U CN219285267U (en) | 2022-12-07 | 2022-12-07 | Unmanned aerial vehicle electricity verification device based on electromagnetic induction principle |
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| CN219285267U true CN219285267U (en) | 2023-06-30 |
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| CN202223271205.2U Active CN219285267U (en) | 2022-12-07 | 2022-12-07 | Unmanned aerial vehicle electricity verification device based on electromagnetic induction principle |
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