CN218470877U - Flight detection device - Google Patents

Abstract

The utility model discloses a flight detection device, including unmanned aerial vehicle and ground control device. Be equipped with total controller and be used for contacting the first extension of waiting to test the electrical equipment on the unmanned aerial vehicle. An electricity testing sensor is arranged on the first extending part. The master controller is respectively in communication connection with the electricity testing sensor and the ground control device. The utility model discloses set up the first extension that has the electroscope on unmanned aerial vehicle, fly and be close to the aerial electrical equipment that waits to test through ground control device control unmanned aerial vehicle when using, rely on the electroscope of first extension to treat to test electrical equipment and test the electric detection, with the result feedback to ground control device on for the operation personnel need not to climb to the high altitude and just can directly test the electricity, reduce the operation degree of difficulty of testing the electricity when improving the electricity accuracy of testing.

Description

Flight detection device

Technical Field

The utility model relates to an electrified high altitude construction technical field, in particular to flight detection device.

Background

In some power system environments, such as substations, aerial work is a common mode of operation. In order to guarantee the personal safety of operating personnel, most of high-altitude operations need to be carried out in a power failure mode, and the power failure needs to test electricity of equipment. However, some electrical devices with 330kV and above are too high in position, the operation difficulty of direct electricity test is large, and the danger coefficient is high.

For this reason, the existing practice is: and adopting indirect electroscopy. However, compared with direct electroscopy, indirect electroscopy has poor accuracy, complex operation and more condition restrictions. Therefore, how to reduce the operation difficulty of electricity testing while improving the electricity testing accuracy becomes an urgent problem to be solved.

SUMMERY OF THE UTILITY MODEL

The utility model discloses the technical problem that will solve is: the utility model provides a flight detection device reduces the operation degree of difficulty of testing electricity when improving the accuracy of testing electricity.

In order to solve the technical problem, the utility model discloses a technical scheme be:

a flight detection device comprises an unmanned aerial vehicle and a ground control device;

the unmanned aerial vehicle is provided with a master controller and a first extension part for contacting the equipment to be tested;

an electricity testing sensor is arranged on the first extending part;

and the master controller is in communication connection with the electricity testing sensor and the ground control device respectively.

Further, a second extension part is further arranged on the unmanned aerial vehicle;

and an SF6 gas leakage detection sensor is arranged on the second extension part, and the SF6 gas leakage detection sensor is in communication connection with the master controller.

Further, a third extending part and a fourth extending part which are adjacent to each other are further arranged on the unmanned aerial vehicle;

zero value detection sensors are arranged on the third extending part and the fourth extending part and are in communication connection with the master controller.

Further, first extension is the unmanned aerial vehicle supporting legs, be provided with the truckle on the unmanned aerial vehicle supporting legs.

Further, the device also comprises an indicator light;

the pilot lamp set up in on the unmanned aerial vehicle and with master controller electricity is connected.

Further, the device also comprises a camera device;

the camera device set up in on the unmanned aerial vehicle and with master controller communication connection.

Further, the ground control device comprises a handheld remote controller and a voice prompter;

and the handheld remote controller is in communication connection with the master controller and the voice prompter respectively.

The beneficial effects of the utility model reside in that: the utility model provides a flight detection device, set up the first extension that has the electroscope on unmanned aerial vehicle, through ground control device control unmanned aerial vehicle flight and be close to the aerial to be tested the electric equipment when using, rely on the electroscope of first extension to treat to test the electric equipment and test the electric detection, feed back the result to ground control device on for the operation personnel need not to climb to the high altitude and just can directly test the electricity, reduce the operation degree of difficulty of testing the electricity when improving the electricity accuracy.

Drawings

Fig. 1 is a front view of a flight detection apparatus according to an embodiment of the present invention;

fig. 2 is a top view of a flight detection apparatus according to an embodiment of the present invention;

fig. 3 is a system block diagram of a flight detection apparatus according to an embodiment of the present invention;

fig. 4 is a schematic view of a flight detection device according to an embodiment of the present invention performing direct electricity testing;

fig. 5 is a schematic view of a flight detection device according to an embodiment of the present invention for detecting air leakage;

fig. 6 is a schematic diagram of a flight detection device according to an embodiment of the present invention performing zero value detection.

Description of reference numerals:

1. an unmanned aerial vehicle; 2. a ground control device; 3. a master controller; 4. a first extension portion; 5. an electroscopy sensor; 6. a second extension portion; 7. an SF6 gas leakage detection sensor; 8. a third extension portion; 9. a fourth extension portion; 10. a zero-value detection sensor; 11. a caster wheel; 12. an indicator light; 13. a camera device; 14. a hand-held remote controller; 15. a voice prompter; 16. a device to be tested; 17. SF6 gas plant; 18. and (6) an insulator to be tested.

Detailed Description

In order to explain the technical content, the objects and the effects of the present invention in detail, the following description is made with reference to the accompanying drawings in combination with the embodiments.

Referring to fig. 1 to 6, a flight detection device includes an unmanned aerial vehicle 1 and a ground control device 2;

the unmanned aerial vehicle 1 is provided with a master controller 3 and a first extension part 4 for contacting with a device 16 to be tested;

an electricity testing sensor 5 is arranged on the first extending part 4;

and the master controller 3 is in communication connection with the electricity testing sensor 5 and the ground control device 2 respectively.

From the above description, the beneficial effects of the present invention are: set up the first extension 4 that has the electroscope 5 on unmanned aerial vehicle, through the flight of ground control device 2 control unmanned aerial vehicle and be close to the aerial electric equipment 16 of waiting to test of height when using, rely on the electroscope 5 of first extension 4 to treat the electroscope 16 and test the electric detection, feed back the result to ground control device 2 on for the operation personnel need not to climb to the height and just can carry out direct electroscope, reduce the operation degree of difficulty of testing the electricity when improving the electroscope degree of accuracy.

Further, a second extension part 6 is further arranged on the unmanned aerial vehicle 1;

and an SF6 gas leakage detection sensor 7 is arranged on the second extension part 6, and the SF6 gas leakage detection sensor 7 is in communication connection with the master controller 3.

As can be seen from the above description, by providing the second extension portion 6 with the SF6 gas leakage detection sensor 7, the unmanned aerial vehicle 1 can also be used for performing gas leakage detection on the SF6 gas equipment 17 in the air, and does not need to have a power failure and let the operator ascend to detect, thereby reducing the number of times of power failure and reducing the operation risk.

Further, a third extending part 8 and a fourth extending part 9 which are adjacent to each other are further arranged on the unmanned aerial vehicle 1;

zero value detection sensors 10 are arranged on the third extending part 8 and the fourth extending part 9, and the zero value detection sensors 10 are in communication connection with the master controller 3.

From the above description, through set up zero value detection sensor 10 on third extension 8 and fourth extension 9 for unmanned aerial vehicle 1 can be used to carry out zero value detection to the high altitude insulator, thereby reduces the operation degree of difficulty that does not have the outage zero value and detect.

Further, first extension 4, second extension 6, third extension 8 and fourth extension 9 are the unmanned aerial vehicle supporting legs, be provided with truckle 11 on the unmanned aerial vehicle supporting legs.

Known from the above description, first extension 4, second extension 6, third extension 8 and fourth extension 9 are the unmanned aerial vehicle supporting legs for can also regard as the support basis that unmanned aerial vehicle 1 parked when testing electricity, gas leakage and zero value and detecting, thereby simplify unmanned aerial vehicle 1's structural component, make its appearance succinct beautiful.

Further, an indicator light 12 is also included;

the pilot lamp 12 set up in on the unmanned aerial vehicle 1 and with total controller 3 electricity is connected.

From the above description, set up pilot lamp 12 on unmanned aerial vehicle 1, carry out physics feedback to testing electric structure etc. through light for the operation personnel can acquire the test electricity result more directly perceived rapidly.

Further, an imaging device 13 is also included;

camera device 13 set up in on unmanned aerial vehicle 1 and with master controller 3 communication connection.

From the above description, still be provided with camera device 13 on unmanned aerial vehicle 1, can real-time recording flight picture etc. the subaerial operation personnel of being convenient for combine image information to operate unmanned aerial vehicle 1, accomplish the operation of testing the electricity conveniently.

Further, the ground control device 2 comprises a hand-held remote controller 14 and a voice prompter 15;

the hand-held remote controller 14 is respectively in communication connection with the master controller 3 and the voice prompter 15.

As can be seen from the above description, the ground control device 2 includes the handheld remote controller 14 and the voice prompt 15, and can perform voice broadcasting on the electricity testing, air leakage, zero value detection results, and the like, and send out warning to the operator.

The utility model discloses a flight detection device can be applicable to the scene of high altitude electroscopy detection operation, explains through specific embodiment below:

referring to fig. 1 to 6, a first embodiment of the present invention is:

a flight detection device comprises an unmanned aerial vehicle (1) and a ground control device (2). As shown in fig. 1 to 3, the unmanned aerial vehicle 1 is provided with a general controller 3, and a first extension portion 4, a second extension portion 6, a third extension portion 8, and a fourth extension portion 9 for contacting an electrical device 16 to be tested. An electroscope sensor 5 is arranged on the first extension part 4, an SF6 gas leakage detection sensor 7 is arranged on the second extension part 6, and zero value detection sensors 10 are arranged on the third extension part 8 and the fourth extension part 9. The master controller 3 is respectively in communication connection with the electricity testing sensor 5, the SF6 gas leakage detection sensor 7, the zero value detection sensor 10 and the ground control device 2.

In this embodiment, as shown in fig. 2, the first extension portion 4, the second extension portion 6, the third extension portion 8, and the fourth extension portion 9 are four drone supporting legs of the drone 1, respectively. Every unmanned aerial vehicle supporting legs all is provided with truckle 11. The first extension portion 4, the second extension portion 6, the third extension portion 8 and the fourth extension portion 9 are all tubular structures and can be freely stretched and folded.

In this embodiment, a flight detection device is used as follows:

as shown in fig. 4, when directly testing electricity, the operator operates the ground control device 2, controls the unmanned aerial vehicle 1 to fly to the side of the electrical equipment 16 to be tested, and makes the electrical sensor 5 on the first extension part 4 contact the electrical equipment 16 to be tested, so as to test electricity and detect, and feeds back the result to the ground control device 2 through the master controller 3.

As shown in fig. 5, when performing gas leakage detection, the operator operates the ground control device 2, controls the unmanned aerial vehicle 1 to fly to the side of the SF6 gas device 17 to be subjected to gas leakage detection, makes the SF6 gas leakage detection sensor 7 on the second extension portion 6 close to the SF6 gas device 17 to perform gas leakage detection, and feeds back the result to the ground control device 2 through the master controller 3.

As shown in fig. 6, when performing zero-value detection, the operator operates the ground control device 2 to control the unmanned aerial vehicle 1 to fly to the side of the insulator 18 to be detected, and the zero-value detection sensors 10 on the third extending portion 8 and the fourth extending portion 9 respectively touch the two ends of the insulator to be detected, perform zero-value detection, and feed back the result to the ground control device 2 through the master controller 3.

In this embodiment, as shown in fig. 1, three indicator lights 12 are disposed on the unmanned aerial vehicle 1 and are all electrically connected with the general controller 3. The three indicator lights 12 are respectively a red light, a yellow light and an orange light, correspond to the electroscope sensor 5, the SF6 gas leakage detection sensor 7 and the zero value detection sensor 10, and feed back the detection result through the light.

In the present embodiment, as shown in fig. 1 and 3, an imaging device 13 is further included. Camera device 13 sets up on unmanned aerial vehicle 1 and with total controller 3 communication connection. Camera device 13 record unmanned aerial vehicle 1's flight picture, and the supplementary operation personnel accomplish the operation of testing the electricity.

In the present embodiment, as shown in fig. 3, the ground control device 2 includes a hand-held remote controller 14 and a voice prompter 15. The hand-held remote controller 14 is respectively connected with the general controller 3 and the voice prompter 15 in a communication way. The voice prompter 15 can perform voice feedback on the detection result. For example, when the electricity testing sensor 5 detects that the equipment 16 to be tested has electricity, the voice prompter 15 sends out voice: "Please note, there is a power! ". At this time, the indicator lamp 12 may blink red correspondingly. The air leakage detection and the zero value detection are performed similarly to the voice prompt process described above.

To sum up, the utility model provides a pair of flight detection device, set up the first extension that has the electricity test sensor on unmanned aerial vehicle, third extension and fourth extension that have the gaseous gas leakage of SF6 and detect the second extension of sensor and have zero value and detect the sensor, control unmanned aerial vehicle when using and remove and be close to electrical equipment, thereby accomplish the electricity test and detect, gas leakage detects, the insulator surveys operation such as zero, feed back to ground controlling means with the result on, and have light instruction, functions such as voice broadcast, make the operation personnel need not to climb to the high altitude and just can directly test electricity, gas leakage detection, the insulator surveys operation such as zero, improve the electricity test, reduce the operation degree of difficulty when gas leakage detection and the insulator measure the degree of accuracy of zero.

The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.

Claims (7)

1. A flight detection device is characterized by comprising an unmanned aerial vehicle and a ground control device;

the unmanned aerial vehicle is provided with a master controller and a first extension part for contacting the equipment to be tested;

an electricity testing sensor is arranged on the first extending part;

and the master controller is in communication connection with the electricity testing sensor and the ground control device respectively.

2. A flight detection apparatus according to claim 1, wherein the drone is further provided with a second extension;

and an SF6 gas leakage detection sensor is arranged on the second extension part, and the SF6 gas leakage detection sensor is in communication connection with the master controller.

3. The flight detection device according to claim 1, wherein the unmanned aerial vehicle is further provided with a third extension part and a fourth extension part which are adjacent to each other;

zero value detection sensors are arranged on the third extending part and the fourth extending part and are in communication connection with the master controller.

4. A flight detection apparatus according to claim 1, wherein the first extension is an unmanned aerial vehicle support foot on which a castor is provided.

5. A flight detection device according to claim 1, further comprising an indicator light;

the pilot lamp set up in on the unmanned aerial vehicle and with master controller electricity is connected.

6. A flight detection device according to claim 1, further comprising a camera device;

the camera device set up in on the unmanned aerial vehicle and with master controller communication connection.

7. A flight detection apparatus according to claim 1, wherein the ground control apparatus comprises a hand-held remote control and a voice prompt;

and the handheld remote controller is in communication connection with the master controller and the voice prompter respectively.

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