CN210681155U - Aircraft for power line inspection and maintenance - Google Patents
Aircraft for power line inspection and maintenance Download PDFInfo
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- CN210681155U CN210681155U CN201921164910.8U CN201921164910U CN210681155U CN 210681155 U CN210681155 U CN 210681155U CN 201921164910 U CN201921164910 U CN 201921164910U CN 210681155 U CN210681155 U CN 210681155U
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- 238000012423 maintenance Methods 0.000 title claims abstract description 16
- 238000007689 inspection Methods 0.000 title abstract description 10
- 230000000694 effects Effects 0.000 claims abstract 2
- 230000005540 biological transmission Effects 0.000 claims description 4
- 238000009413 insulation Methods 0.000 claims description 2
- 230000008092 positive effect Effects 0.000 abstract 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model relates to an electric power inspection technical field just discloses an aircraft that is used for power line to patrol maintenance usefulness, which comprises a bod, the side fixed mounting at the positive top of organism has first rotor, the positive fixed mounting of organism has controlling means, the side fixed mounting of organism has the back shaft, the side movable mounting of back shaft has the link, the side fixed mounting of link has the second rotor, the positive activity hinge of organism has electric putter, electric putter's the other end is articulated with the medial surface activity of link. This an aircraft for power line tours maintenance usefulness can make the state that the second rotor can be in perpendicular organism impel the organism to move and then improve the continuation of the journey of aircraft when the aircraft hangs on the power line through the cooperation of electric putter and back shaft and link, can make the aircraft hang on the circuit of different diameters through the cooperation of micro motor and screw rod and slide-wire seat.
Description
Technical Field
The utility model relates to an electric power inspection technical field specifically is an aircraft that is used for power line to patrol and maintain usefulness.
Background
With the development of economy and social progress, the structure of a power grid is continuously optimized and upgraded, the number and the length of ultrahigh voltage transmission lines are increased day by day, workers in teams and groups need to complete daily patrol maintenance work, various power failure overhaul, middle inspection and acceptance, completion inspection and acceptance, channel cleaning, hazard source monitoring, seasonal inspection, holiday power protection and other works of the governed lines, the shortage of the workers causes severe overload of the field patrol workers, frequent overtime and point adding sometimes cause the record and maintenance work delay of patrol recording defects, and the detection work of the lines cannot be completed periodically, so that potential hazards are brought to safety production.
At present need artifical the climbing to the circuit when carrying out the circuit inspection on patrol, perhaps adopt the telescope to patrol, the intensity of labour of this kind of patrol mode is big, the telescope patrol produces the careless omission of patrol easily, along with the development of unmanned aerial vehicle technique, now generally use the aircraft to carry out the circuit inspection, unmanned aerial vehicle flies circuit or iron tower department and shoots when the aircraft of using patrols at present, however this kind of mode unmanned aerial vehicle continuation of the journey is not enough when patrolling, work efficiency is low, be unfavorable for carrying out long distance patrol.
Disclosure of Invention
The utility model provides a not enough to prior art, the utility model provides an aircraft for power line patrols maintenance usefulness, it is longer to possess the duration, and unmanned aerial vehicle can closely press close to the circuit, can carry out the advantage of patrolling night, has solved the problem of mentioning in the above background art.
The utility model provides a following technical scheme: an aircraft for power line patrol maintenance comprises an aircraft body, wherein a first rotor wing is fixedly arranged on the side face of the front top of the aircraft body, a control device is fixedly arranged on the front face of the aircraft body, a supporting shaft is fixedly arranged on the side face of the aircraft body, a connecting frame is movably arranged on the side face of the supporting shaft, a second rotor wing is fixedly arranged on the side face of the connecting frame, an electric push rod is movably hinged on the front face of the aircraft body, the other end of the electric push rod is movably hinged with the inner side face of the connecting frame, a first camera is fixedly arranged on the front face of the aircraft body, a supporting rod is fixedly arranged on the front face of the aircraft body, a cavity plate is fixedly arranged on the top of the supporting rod, a micro motor is fixedly arranged on the side face of the cavity plate, the output end of the micro motor penetrates through the cavity plate and extends to the inside of the, the bottom of the machine body is fixedly connected with an electric rotating seat, the bottom of the electric rotating seat is fixedly provided with a longitudinal connecting frame, the inner side surface of the longitudinal connecting frame is fixedly connected with a rotating shaft, the outer surface of the rotating shaft is fixedly provided with a mounting seat, the front surface of the mounting seat is fixedly provided with a second camera, the front surface of the mounting seat is fixedly provided with an infrared scanning head, the front surface of the mounting seat is fixedly provided with an illuminating lamp, the side surface of the longitudinal connecting frame is fixedly provided with a placing cavity, one end of the rotating shaft extends into the placing cavity and is fixedly connected with a connecting shaft, a side gear is fixedly sleeved on the outer surface of the connecting shaft, the miniature speed reducing motor is fixedly installed at the top of the inner cavity of the placing cavity, a straight gear is fixedly sleeved on the outer surface of the output end of the miniature speed reducing motor, and the outer surface of the straight gear is in meshing transmission connection with the outer surface of the side gear.
Preferably, the control device is electrically connected with the electric push rod, the micro motor and the micro speed reducing motor.
Preferably, the screw rod is divided into two sections, the spiral directions of the two sections of screw rod are opposite, the number of the slide wire seats is two, and the two slide wire seats are respectively in one-to-one correspondence with the two sections of screw rod.
Preferably, the length value of the connecting frame is greater than the distance value between the bottom of the mounting seat and the bottom of the machine body.
Preferably, the outer surface of the body is coated with a highly insulating casing.
Compared with the prior art, the utility model discloses possess following beneficial effect:
1. this an aircraft for power line tours maintenance usefulness can make the state that the second rotor can be in perpendicular organism impel the organism to move and then improve the continuation of the journey of aircraft when the aircraft hangs on the power line through the cooperation of electric putter and back shaft and link, can make the aircraft hang on the circuit of different diameters through the cooperation of micro motor and screw rod and slide-wire seat.
2. This an aircraft for power line patrols maintenance usefulness makes the direction of second camera change at will through electronic rotation seat and miniature gear motor, and then can make the second camera can patrol the circuit of next door, can patrol the circuit at night through the light.
Drawings
FIG. 1 is a top view of the present invention;
FIG. 2 is a side view of the structure of the present invention;
fig. 3 is an enlarged view of a position a in the structure diagram 2 of the present invention.
In the figure: 1. a body; 2. a first rotor; 3. a screw; 4. a first camera; 5. a cavity plate; 6. a trolley wire seat; 7. a micro motor; 8. a support shaft; 9. an electric rotating base; 10. a second rotor; 11. a connecting frame; 12. an electric push rod; 13. a control device; 14. a support bar; 15. a rotating shaft; 16. an illuminating lamp; 17. a second camera; 18. a mounting seat; 19. an infrared scanning head; 20. a longitudinal connecting frame; 21. a placement chamber; 22. a spur gear; 23. a miniature speed reduction motor; 24. a side gear; 25. and (7) connecting the shafts.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, an aircraft for power line inspection and maintenance comprises an aircraft body 1, wherein the outer surface of the aircraft body 1 is coated with a high-insulation shell to prevent the aircraft body 1 from being broken through by a high-voltage line, a first rotor wing 2 is fixedly installed on the side surface of the top of the front surface of the aircraft body 1, a control device 13 is fixedly installed on the front surface of the aircraft body 1, a support shaft 8 is fixedly installed on the side surface of the aircraft body 1, a connecting frame 11 is movably installed on the side surface of the support shaft 8, a second rotor wing 10 is fixedly installed on the side surface of the connecting frame 11, an electric push rod 12 is movably hinged on the front surface of the aircraft body 1, the other end of the electric push rod 12 is movably hinged with the inner side surface of the connecting frame 11, and the second rotor wing 10 can be driven to move in a state perpendicular to the aircraft body 1 when the aircraft is, the front of the machine body 1 is fixedly provided with a first camera 4, the front of the machine body 1 is fixedly provided with a support rod 14, the top of the support rod 14 is fixedly provided with a cavity plate 5, the side surface of the cavity plate 5 is fixedly provided with a micro motor 7, the output end of the micro motor 7 penetrates through the cavity plate 5 and extends to the inside of the cavity plate 5 and is fixedly connected with a screw 3, the outer surface of the screw 3 is provided with a slide wire seat 6 in a threaded manner, the screw 3 is divided into two sections, the spiral directions of the two sections of the screw 3 are opposite, the number of the slide wire seats 6 is two, the two slide wire seats 6 are respectively in one-to-one correspondence with the two sections of the screw 3, the aircraft can be hung on lines with different diameters through the matching of the micro motor 7, the screw 3 and the slide wire seats 6, the bottom of the machine body 1 is fixedly connected with an electric rotating seat 9, the bottom, the outer surface of the rotating shaft 15 is fixedly provided with a mounting seat 18, the length value of the connecting frame 11 is larger than the distance value between the bottom of the mounting seat 18 and the bottom of the machine body 1, the front surface of the mounting seat 18 is fixedly provided with a second camera 17, the front surface of the mounting seat 18 is fixedly provided with an infrared scanning head 19, the infrared scanning head 19 can scan the problems on the line and further detect the problems, the front surface of the mounting seat 18 is fixedly provided with an illuminating lamp 16, the line can be patrolled at night through the illuminating lamp 16, the side surface of the longitudinal connecting frame 20 is fixedly provided with a placing cavity 21, one end of the rotating shaft 15 extends to the inside of the placing cavity 21 and is fixedly connected with a connecting shaft 25, the outer surface of the connecting shaft 25 is fixedly provided with a side gear 24, the top of the inner cavity of the placing cavity 21 is fixedly provided with a micro reducing motor 23, the control, the outer fixed surface cover of miniature gear motor 23 output is equipped with spur gear 22, and the surface of spur gear 22 is connected with the surface meshing transmission of side gear 24, makes the direction of second camera 17 change at will through electronic rotation seat 9 and miniature gear motor 23, and then can make second camera 17 can patrol the circuit on next door.
Theory of operation, when near the aircraft flies the circuit, people send signal to controlling means 13 through the remote controller, people control organism 1 through the picture that first camera 4 was shot, make the circuit arrange in between slide wire seat 6, micro motor 7 drives screw rod 3 and rotates, the rotation of screw rod 3 makes two slide wire seats 6 move to the inboard and makes two slide wire seats 6 clip the circuit, first rotor 2 stop work this moment, electric putter 12 drives link 11 and rotates round back shaft 8 and make second rotor 10 be in the vertical state of organism 1, the rotation of second rotor 10 makes organism 1 move along the circuit, drive second camera 17 through electronic rotation seat 9 and adjust horizontal angle this moment, micro gear motor 23 drives spur gear 22 and rotates, spur gear 22 drives side gear 24 and rotates and then drives mount pad 18 through connecting axle 25 and axis of rotation 15 and reciprocate and then make the vertical of second camera 17 adjust horizontal angle, the straight-direction that the straight-tooth gear 17 was driven to the aircraft is reached The angle is adjusted, and the second camera 17 and the infrared scanning head 19 patrol the line and transmit the patrol to the control end.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. An aircraft for power line patrol maintenance, comprising an airframe (1), characterized in that: the side fixed mounting at the positive top of organism (1) has first rotor (2), the positive fixed mounting of organism (1) has controlling means (13), the side fixed mounting of organism (1) has back shaft (8), the side movable mounting of back shaft (8) has link (11), the side fixed mounting of link (11) has second rotor (10), the positive movable hinge of organism (1) has electric putter (12), the other end of electric putter (12) is articulated with the medial surface activity of link (11), the positive fixed mounting of organism (1) has first camera (4), the positive fixed mounting of organism (1) has bracing piece (14), the top fixed mounting of bracing piece (14) has cavity board (5), the side fixed mounting of cavity board (5) has micro motor (7), the output end of the micro motor (7) penetrates through the cavity plate (5) and extends to the inside of the cavity plate (5) and the fixedly connected screw (3), the outer surface thread of the screw (3) is provided with the slide wire seat (6), the bottom fixedly connected with electric rotating seat (9) of the machine body (1), the bottom fixedly connected with of the electric rotating seat (9) is provided with a longitudinal connecting frame (20), the inner side surface of the longitudinal connecting frame (20) is fixedly connected with a rotating shaft (15), the outer surface of the rotating shaft (15) is fixedly provided with a mounting seat (18), the front of the mounting seat (18) is fixedly provided with a second camera (17), the front of the mounting seat (18) is fixedly provided with an infrared scanning head (19), the front of the mounting seat (18) is fixedly provided with an illuminating lamp (16), the side fixedly provided with a placing cavity (21) of the longitudinal connecting frame (20), the one end of axis of rotation (15) extends to the inside and fixedly connected with connecting axle (25) of placing chamber (21), the external fixed surface cover of connecting axle (25) is equipped with side gear (24), the top fixed mounting of placing chamber (21) inner chamber has miniature gear motor (23), the external fixed surface cover of miniature gear motor (23) output is equipped with straight-teeth gear (22), the surface of straight-teeth gear (22) is connected with the surface engagement transmission of side gear (24).
2. An aircraft for power line patrol maintenance according to claim 1, characterized in that: the control device (13) is electrically connected with the electric push rod (12), the micro motor (7) and the micro speed reducing motor (23).
3. An aircraft for power line patrol maintenance according to claim 1, characterized in that: the screw rod (3) is divided into two sections, the spiral directions of the two sections of screw rods (3) are opposite, the number of the slide wire seats (6) is two, and the two slide wire seats (6) are respectively in one-to-one correspondence with the two sections of screw rods (3).
4. An aircraft for power line patrol maintenance according to claim 1, characterized in that: the length value of the connecting frame (11) is larger than the distance value between the bottom of the mounting seat (18) and the bottom of the machine body (1).
5. An aircraft for power line patrol maintenance according to claim 1, characterized in that: the outer surface of the machine body (1) is coated with a high-insulation shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921164910.8U CN210681155U (en) | 2019-07-24 | 2019-07-24 | Aircraft for power line inspection and maintenance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921164910.8U CN210681155U (en) | 2019-07-24 | 2019-07-24 | Aircraft for power line inspection and maintenance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210681155U true CN210681155U (en) | 2020-06-05 |
Family
ID=70890719
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921164910.8U Expired - Fee Related CN210681155U (en) | 2019-07-24 | 2019-07-24 | Aircraft for power line inspection and maintenance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210681155U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114094490A (en) * | 2021-11-16 | 2022-02-25 | 国家电网有限公司 | System and method for quickly fixing broken strands of conducting wires and ground wires of overhead transmission line |
| CN117682120A (en) * | 2024-02-01 | 2024-03-12 | 国网吉林省电力有限公司白山供电公司 | A nighttime lighting mounting device for drones used for power inspections |
-
2019
- 2019-07-24 CN CN201921164910.8U patent/CN210681155U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114094490A (en) * | 2021-11-16 | 2022-02-25 | 国家电网有限公司 | System and method for quickly fixing broken strands of conducting wires and ground wires of overhead transmission line |
| CN117682120A (en) * | 2024-02-01 | 2024-03-12 | 国网吉林省电力有限公司白山供电公司 | A nighttime lighting mounting device for drones used for power inspections |
| CN117682120B (en) * | 2024-02-01 | 2024-04-16 | 国网吉林省电力有限公司白山供电公司 | Unmanned aerial vehicle night illumination mounting device for electric power inspection |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200605 |
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| CF01 | Termination of patent right due to non-payment of annual fee |