Unmanned aerial vehicle for power system maintenance and management system

Abstract

The invention discloses an unmanned aerial vehicle for power system maintenance and a management system, the unmanned aerial vehicle for power system maintenance and the management system comprise a housing, a remote controller and a flight controller, the housing is provided with a plurality of wings, each wing is rotatably provided with a propeller, the housing is rotatably provided with a first gear, and the first gear is rotatably provided with a second gear; a first gear is arranged on the machine shell, a second gear is arranged on the machine shell, the first gear is in meshed connection with the second gear, a rotating rod is arranged on the second gear, a supporting plate is arranged on the rotating rod, a fixing plate is arranged on the supporting plate, a laser device is rotatably arranged on the fixing plate, a support is arranged on the machine shell, and the laser device is arranged on the support. A servo motor is arranged on the machine shell, and an output shaft of the servo motor is connected with the first gear. The remote controller and the flight controller are in communication connection through radio waves, so that the laser can damage an object wound on the electric wire, and meanwhile, the angle of the laser can be conveniently adjusted.

Description

Technical Field

[0001] The present invention relates to the field of unmanned aerial vehicles (UAVs), and in particular to an unmanned aerial vehicle (UAV) and a management system for power system maintenance. Background Art

[0002] The drone used for power system maintenance is a system that combines drone technology with the needs of power inspection. It is mainly used for efficient and accurate inspection of power facilities such as transmission lines and substations. However, sometimes there will be debris entangled in the wires, which need to be destroyed by lasers. However, some drone inspections are just passing inspections, and it is not easy to destroy objects entangled in the wires, and some drone lasers are not easy to adjust the angle. Summary of the invention

[0003] The purpose of the present invention is to provide a drone and management system for power system maintenance, which solves the problem that it is not easy to damage objects wrapped around wires and it is not convenient for the laser to adjust the angle.

[0004] In order to achieve the above-mentioned purpose, the present invention provides an unmanned aerial vehicle and management system for power system maintenance, the unmanned aerial vehicle and management system for power system maintenance comprising a casing, a remote controller and a flight controller, the casing is provided with a plurality of wings, each of the wings is rotatably provided with a propeller, the casing is rotatably provided with a first gear, the casing is provided with a second gear, the first gear is meshingly connected with the second gear, the second gear is provided with a rotating rod, the rotating rod is provided with a supporting plate, the supporting plate is provided with a fixing plate, the fixing plate is rotatably provided with a laser, the casing is provided with a bracket, the casing is provided with a servo motor, and the output shaft of the servo motor is connected with the first gear; the remote controller and the flight controller are connected to each other by radio waves, and the communication frequency is . Hz; the flight controller is connected to the flight controller by wires; the flight controller comprises an electronic speed controller and a sensor, the electronic speed controller is connected to the propeller by a wire, and the electronic speed controller controls the rotation speed of the propeller.

[0005] Preferably, a motor is provided on the wing, and an output shaft of the motor is connected to the propeller.

[0006] Preferably, a battery is provided on the housing, and the battery is electrically connected to the motor.

[0007] Preferably, the flight controller is connected to the battery via a wire.

[0008] Preferably, the sensor includes a rotation sensor, and the rotation sensor is used to detect the tilt degree of the drone.

[0009] Preferably, the sensor also includes an acceleration sensor, and the acceleration sensor is used to sense changes in the speed of the drone.

[0010] Preferably, the sensor also includes an air pressure sensor, and the air pressure sensor is used to detect the altitude of the drone.

[0011] The present invention also provides a management system, the drone management system comprising the drone and management system for power system maintenance according to claims 1-7:

[0012] S1 starts the remote controller first, so that the remote controller controls the flight controller through radio waves. At the same time, the flight controller controls the battery to run. When the battery is running, it controls the motor to run. When the motor is running, it controls the propeller to rotate.

[0013] S2 Then, the flight controller controls the electronic speed controller, and the electronic speed controller controls the rotation speed of the propeller;

[0014] At S3, the flight controller controls the rotation sensor, which is used to detect the tilt of the drone, and controls the acceleration sensor, which is used to sense the speed change of the drone, and controls the air pressure sensor, which is used to detect the height of the drone;

[0015] S4: Then, the servo motor is rotated, so that the servo motor drives the first gear to rotate, and the first gear drives the second gear to rotate during the rotation process, and the second gear drives the laser to move during the rotation process.

[0016] The present invention provides an unmanned aerial vehicle and management system for electric power system maintenance, the unmanned aerial vehicle and management system for electric power system maintenance comprising a casing, a remote controller and a flight controller, the casing is provided with a plurality of wings, each of the wings is rotatably provided with a propeller, the casing is rotatably provided with a first gear, the casing is provided with a second gear, the first gear is meshingly connected with the second gear, the second gear is provided with a rotating rod, the rotating rod is provided with a supporting plate, the supporting plate is provided with a fixing plate, the fixing plate is rotatably provided with a laser, the casing is provided with a bracket, the casing is provided with a servo motor, the output shaft of the servo motor is connected with the first gear; the remote controller and the flight controller are connected to each other by radio waves, and the communication frequency is . Hz; the flight controller is connected to the flight controller by wires; the flight controller comprises an electronic speed controller and a sensor, the electronic speed controller is connected to the propeller by wires, The electronic speed controller controls the rotation speed of the propeller. When using the device, first start the remote control so that the remote control controls the flight controller through radio waves. At the same time, the flight controller controls the operation of the battery. When the battery is running, the motor is controlled to run. When the motor is running, the propeller is controlled to rotate. Then, the flight controller controls the electronic speed controller, and the electronic speed controller controls the rotation speed of the propeller. At the same time, the flight controller controls the rotation sensor, which is used to detect the tilt degree of the drone and control the acceleration sensor. The acceleration sensor is used to sense the speed change of the drone and control the air pressure sensor. The air pressure sensor is used to detect the height of the drone. Then, rotate the servo motor so that the servo motor drives the first gear to rotate. The first gear drives the second gear to rotate during the rotation process. The second gear drives the laser to move during the rotation process. Through a simple structure, the laser can destroy objects wrapped around the wire, and it is also convenient for the laser to adjust the angle.

[0017] Other features and advantages of the present invention will be described in detail in the following detailed description. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the following specific embodiments, they are used to explain the present invention but do not constitute a limitation of the present invention. In the accompanying drawings:

[0019] Figure 1 This is a first-person perspective structural diagram of the UAV for power system maintenance provided by the present invention;

[0020] Figure 2 This is a second perspective structural diagram of the UAV for power system maintenance provided by the present invention;

[0021] Figure 3 yes Figure 2 The structure diagram at A is enlarged;

[0022] Figure 4 It is a system diagram of the UAV for power system maintenance provided by the present invention.

[0023] Description of Reference Numerals

[0024] 1. Casing; 2. Wings; 3. Propellers; 4. Motors; 5. Batteries; 6. First gear; 7. Second gear; 8. Rotating rod; 9. Support plate; 10. Fixing plate; 11. Laser; 12. Bracket. DETAILED DESCRIPTION

[0025] The specific implementation of the present invention is described in detail below in conjunction with the accompanying drawings. It should be understood that the specific implementation described here is only used to illustrate and explain the present invention, and is not used to limit the present invention.

[0026] like Figure 1-4 As shown: The present invention provides an unmanned aerial vehicle for power system maintenance and a management system, the unmanned aerial vehicle for power system maintenance comprises a housing 1, a remote controller and a flight controller, the housing 1 is provided with a plurality of wings 2, each of the wings 2 is rotatably provided with a propeller 3, the housing 1 is rotatably provided with a first gear 6, the housing 1 is provided with a second gear 7, the first gear 6 is meshed and connected with the second gear 7, the second gear 7 is provided with a rotating rod 8, the rotating rod 8 is provided with a supporting plate 9, the supporting plate 9 is provided with a fixing plate 10, the fixing plate 10 is rotatably provided with a laser 11, the housing 1 is provided with a bracket 12, the housing 1 is provided with a servo motor, the output shaft of the servo motor is connected to the first gear 6; the remote controller and the flight controller are communicated via radio waves, and the communication frequency is 2.4 Hz; the flight controller is connected to the flight controller via wires; the flight controller includes an electronic speed controller and a sensor, the electronic speed controller is connected to the propeller 3 via a wire, and the electronic speed controller controls the rotation speed of the propeller 3.

[0027] The working principle of the present invention is as follows: when using the device, first start the remote control so that the remote control controls the flight controller through radio waves, and at the same time the flight controller controls the battery to run, and when the battery is running, controls the motor to run, and when the motor is running, controls the propeller to rotate; then, the flight controller controls the electronic speed controller, and the electronic speed controller controls the rotation speed of the propeller; at the same time, the flight controller controls the rotation sensor, which is used to detect the tilt degree of the drone, and controls the acceleration sensor, which is used to sense the speed change of the drone, and controls the air pressure sensor, which is used to detect the height of the drone; then, rotate the servo motor, so that the servo motor drives the first gear to rotate, and the first gear drives the second gear to rotate during the rotation process, and the second gear drives the laser to move during the rotation process, and through a simple structure, the laser can destroy objects wrapped around the wire, and it is also convenient for the laser to adjust the angle.

[0028] In a preferred embodiment of the present invention, a motor 4 is provided on the wing 2, and an output shaft of the motor 4 is connected to the propeller 3, so as to facilitate the motor to drive the propeller to rotate.

[0029] In a preferred embodiment of the present invention, a battery 5 is disposed on the housing 1, and the battery 5 is electrically connected to the motor 4, so that the battery can drive the motor to rotate.

[0030] In a preferred embodiment of the present invention, the flight controller is connected to the battery 5 via a wire, which is to facilitate the flight controller to control the battery.

[0031] In a preferred embodiment of the present invention, the sensor includes a rotation sensor, and the rotation sensor is used to detect the tilt degree of the drone, which is to facilitate the observation of the tilt condition of the drone during flight.

[0032] In a preferred embodiment of the present invention, the sensor further includes an acceleration sensor, and the acceleration sensor is used to sense the speed change of the drone, which is to facilitate the observation of the speed change of the drone flight.

[0033] In a preferred embodiment of the present invention, the sensor further includes an air pressure sensor, and the air pressure sensor is used to detect the altitude of the drone to prevent the drone from flying too high.

[0034] The present invention also provides a management system, the drone management system comprising the drone and management system for power system maintenance according to claims 1-7:

[0035] S1 first starts the remote controller so that the remote controller controls the flight controller through radio waves, and at the same time the flight controller controls the battery 5 to operate, and when the battery 5 is operating, the motor 4 is controlled to operate, and when the motor 4 is operating, the propeller 3 is controlled to rotate;

[0036] S2 Next, the flight controller controls the electronic speed controller, and the electronic speed controller controls the rotation speed of the propeller 3;

[0037] At S3, the flight controller controls the rotation sensor, which is used to detect the tilt of the drone, and controls the acceleration sensor, which is used to sense the speed change of the drone, and controls the air pressure sensor, which is used to detect the height of the drone;

[0038] S4: Then, the servo motor is rotated, so that the servo motor drives the first gear 6 to rotate, and the first gear 6 drives the second gear 7 to rotate during the rotation process, and the second gear 7 drives the laser 11 to move during the rotation process.

[0039] The preferred embodiments of the present invention are described in detail above in conjunction with the accompanying drawings. However, the present invention is not limited to the specific details in the above embodiments. Within the technical concept of the present invention, a variety of simple modifications can be made to the technical solution of the present invention, and these simple modifications all belong to the protection scope of the present invention.

[0040] It should also be noted that the various specific technical features described in the above specific embodiments can be combined in any suitable manner without contradiction. In order to avoid unnecessary repetition, the present invention will not further describe various possible combinations.

[0041] In addition, various embodiments of the present invention may be arbitrarily combined, and as long as they do not violate the concept of the present invention, they should also be regarded as the contents disclosed by the present invention.

Claims

1. A drone for power system maintenance, characterized in that: The unmanned aerial vehicle and management system for power system maintenance comprises a housing (1), a remote controller and a flight controller, the housing (1) being provided with a plurality of wings (2), each of the wings (2) being rotatably provided with a propeller (3), the housing (1) being rotatably provided with a first gear (6), the housing (1) being provided with a second gear (7), the first gear (6) being meshingly connected with the second gear (7), the second gear (7) being provided with a rotating rod (8), the rotating rod (8) being provided with a supporting plate (9), the supporting plate (9) being provided with a fixing plate (10), the fixing plate (10) being rotatably provided with a laser (11), the housing (1) being provided with a bracket (12), the housing (1) being provided with a servo motor, the output shaft of the servo motor being connected with the first gear (6); The remote controller and the flight controller are connected to each other by radio waves, and the communication frequency is 2.4 Hz; The flight controller is connected to the flight controller via a wire; The flight controller comprises an electronic speed controller and a sensor. The electronic speed controller is connected to the propeller (3) via a wire, and the electronic speed controller controls the rotation speed of the propeller (3).

2. The power system maintenance drone according to claim 1, characterized in that: A motor (4) is provided on the wing (2), and an output shaft of the motor (4) is connected to the propeller (3).

3. The power system maintenance drone according to claim 2, characterized in that: A battery (5) is arranged on the housing (1), and the battery (5) is electrically connected to the motor (4).

4. The power system maintenance drone according to claim 3, characterized in that: The flight controller is connected to the battery (5) via a wire.

5. The power system maintenance drone according to claim 4, characterized in that: The sensor includes a rotation sensor, and the rotation sensor is used to detect the tilt degree of the drone.

6. The UAV for power system maintenance according to claim 5, characterized in that: The sensor also includes an acceleration sensor, which is used to sense the speed change of the drone.

7. The UAV for power system maintenance according to claim 6, characterized in that: The sensor also includes an air pressure sensor, which is used to detect the height of the drone.

8. A drone management system, characterized in that: The drone management system comprises the drone and management system for power system maintenance according to claims 1-7: S1 first starts the remote controller, so that the remote controller controls the flight controller through radio waves, and at the same time the flight controller controls the battery (5) to operate, and when the battery (5) is operating, the motor (4) is controlled to operate, and when the motor (4) is operating, the propeller (3) is controlled to rotate; S2 Then, the flight controller controls the electronic speed controller, and the electronic speed controller controls the rotation speed of the propeller (3); At S3, the flight controller controls the rotation sensor, which is used to detect the tilt of the drone, and controls the acceleration sensor, which is used to sense the speed change of the drone, and controls the air pressure sensor, which is used to detect the height of the drone; S4: Then, the servo motor is rotated so that the servo motor drives the first gear (6) to rotate, and the first gear (6) drives the second gear (7) to rotate during the rotation process, and the second gear (7) drives the laser (11) to move during the rotation process.

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