CN215972115U - Unmanned aerial vehicle device for high-altitude high-voltage line fault intelligent recognition - Google Patents
Unmanned aerial vehicle device for high-altitude high-voltage line fault intelligent recognition Download PDFInfo
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- CN215972115U CN215972115U CN202121647275.6U CN202121647275U CN215972115U CN 215972115 U CN215972115 U CN 215972115U CN 202121647275 U CN202121647275 U CN 202121647275U CN 215972115 U CN215972115 U CN 215972115U
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Abstract
The utility model provides an unmanned aerial vehicle device for intelligent high-altitude high-voltage line fault recognition, which comprises a machine body, a left side support, a left side motor, a left side propeller, a right side support, a right side motor, a right side propeller, a fan blade protection frame structure convenient to disassemble, a storage battery, a control chip, a wireless module, a bottom protection frame structure, a side support plate, a buffering support structure and a camera, wherein the left side support and the right side support are respectively installed at four corners of the upper part of the machine body through screws; the left motor screw is arranged on the left upper side of the left bracket; and the left propeller screw is arranged on an output shaft of the left motor. The side mesh enclosures are respectively arranged at the outer sides of the left propeller and the right propeller, so that the side mesh enclosures are beneficial to avoiding the collision between the left propeller or the right propeller and a cable when the left propeller or the right propeller works; the transparent shield is arranged at the lower part of the machine body through screws, so that the transparent shield can be conveniently used for protecting the detection components below the machine body.
Description
Technical Field
The utility model belongs to the technical field of electric power overhaul, and particularly relates to an unmanned aerial vehicle device for intelligent high-altitude high-voltage line fault identification.
Background
In recent years, the application and research of unmanned aerial vehicle widely receive the attention of relevant all aspects, and main country in the world is also in the small-size and miniature unmanned aerial vehicle of impetus development when developing long-endurance unmanned aerial vehicle and combat unmanned aerial vehicle, constantly develops the miniaturized of unmanned aerial vehicle, even miniaturized technique. It is more convenient to utilize unmanned aerial vehicle to detect the high-voltage line.
But the existing unmanned aerial vehicle device has the problems of poor protection effect on fan blades, inconvenience in playing a good protection role on the bottom and no buffer function during landing.
Therefore, the unmanned aerial vehicle device for intelligently identifying the high-altitude high-voltage line fault is very necessary.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problems, the utility model provides an unmanned aerial vehicle device for intelligently identifying faults of high-altitude high-voltage lines, which aims to solve the problems that the existing unmanned aerial vehicle device has poor protection effect on fan blades, is inconvenient to play a good protection role on the bottom and does not have a buffering function when landing. An unmanned aerial vehicle device for intelligent high-altitude high-voltage line fault recognition comprises a machine body, a left side support, a left side motor, a left side propeller, a right side support, a right side motor, a right side propeller, a fan blade protection frame structure convenient to disassemble, a storage battery, a control chip, a wireless module, a bottom protection frame structure, side support plates, a buffer support structure and a camera, wherein the left side support and the right side support are respectively installed at four corners of the upper part of the machine body through screws; the left motor screw is arranged on the left upper side of the left bracket; the left propeller screw is arranged on an output shaft of the left motor; the right motor screw is arranged on the right upper side of the right bracket; the right propeller screw is arranged on an output shaft of the right motor; the fan blade protection frame structure convenient to disassemble is arranged on the outer sides of the left side support and the right side support; the storage battery, the control chip and the wireless module are respectively installed on the inner side of the machine body through screws; the bottom protective frame structure is arranged at the lower part of the machine body; the buffer bracket structure is arranged at the lower part of the side support plate; the camera screw is arranged at the middle lower part of the machine body; the fan blade protection frame structure convenient to disassemble comprises a connecting base plate, connecting bolts, a side mesh enclosure, a reinforcing frame and a middle mesh enclosure, wherein the connecting base plate is respectively arranged at the lower parts of a left side bracket and a right side bracket through the connecting bolts; the side mesh enclosure is glued on the upper part of the connecting base plate; the middle mesh enclosure is mounted on the inner side of the side mesh enclosure through screws.
Preferably, the bottom protection frame structure comprises a transparent protection cover, side insulating protection frames, a mounting frame, a temperature sensor and a humidity sensor, wherein the mounting frame is embedded in the left side and the right side of the transparent protection cover; the temperature sensor and the humidity sensor are respectively installed in the installation frames arranged on the left side and the right side through screws; the side support plate screws are arranged at the lower part of the transparent shield.
Preferably, the buffer support structure comprises a movable frame, a positioning ring, a buffer spring, a T-shaped movable rod, a rubber support leg and an insulating sheath, wherein the movable frame is embedded in the lower part of the side support plate; the positioning ring screw is arranged at the lower part of the movable frame; the T-shaped movable rod penetrates through the positioning ring and is inserted into the inner side of the movable frame; the rubber support leg is connected to the lower part of the T-shaped movable rod in an adhesive mode.
Preferably, the side mesh enclosure is respectively arranged at the outer sides of the left propeller and the right propeller.
Preferably, the transparent shield screw is mounted at the lower part of the fuselage.
Preferably, the buffer spring is arranged at the upper part of the inner side of the movable frame.
Preferably, the side insulating protective frames are respectively installed at the connecting positions of the transparent protective cover and the connecting base plate through screws.
Preferably, the upper end and the lower end of the insulating sheath are respectively glued to the lower part of the outer side of the side support plate and the upper part of the outer side of the rubber support leg.
Preferably, the reinforcing frame is installed on the front side and the rear side of the side mesh enclosure through screws.
Preferably, control chip and sensor, humidity transducer, camera, left side motor, right side motor and battery electric connection, control chip and wireless module electric connection, wireless module and remote control module electric connection, the remote control module adopt one kind of smart mobile phone, panel computer or notebook computer.
Compared with the prior art, the utility model has the beneficial effects that:
1. in the utility model, the side mesh enclosures are respectively arranged at the outer sides of the left propeller and the right propeller, so that the collision between the left propeller or the right propeller and a cable during working can be avoided when the side mesh enclosures are used.
2. In the utility model, the transparent shield screw is arranged at the lower part of the machine body, so that the transparent shield can be conveniently used for protecting detection parts below the machine body.
3. In the utility model, the buffer spring is arranged at the upper part of the inner side of the movable frame, so that the buffer spring can be used for playing a good role in damping and buffering the T-shaped movable rod when in use.
4. According to the utility model, the side insulating protection frames are respectively installed at the connecting positions of the transparent shield and the connecting base plate through screws, so that the side insulating protection frames can be conveniently used for protecting cables in use.
5. In the utility model, the upper end and the lower end of the insulating sheath are respectively glued to the lower part of the outer side of the side support plate and the upper part of the outer side of the rubber support leg, so that the rubber support leg and the side support plate can be conveniently protected when in use, and sundries are prevented from entering the inner sides of the side support plate and the rubber support leg.
6. In the utility model, the reinforcing frame screws are arranged on the front side and the rear side of the side mesh enclosure, so that the reinforcing frame can be used for reinforcing the side mesh enclosure when in use.
Drawings
Fig. 1 is a schematic structural view of the present invention.
FIG. 2 is a schematic structural view of the fan blade protection frame structure convenient for disassembly.
Fig. 3 is a schematic structural view of the bottom protective frame structure of the present invention.
Fig. 4 is a schematic structural view of a buffer bracket structure of the present invention.
In the figure:
1. a body; 2. a left side bracket; 3. a left side motor; 4. a left propeller; 5. a right side bracket; 6. a right motor; 7. a right side propeller; 8. the fan blade protection frame structure is convenient to disassemble; 81. connecting the base plate; 82. a connecting bolt; 83. a side net cover; 84. a reinforcing frame; 85. a middle net cover; 9. a storage battery; 10. a control chip; 11. a wireless module; 12. a bottom guard frame structure; 121. a transparent shield; 122. a side insulating protective frame; 123. installing a frame; 124. a temperature sensor; 125. a humidity sensor; 13. a side support plate; 14. a buffer support structure; 141. a movable frame; 142. a positioning ring; 143. a buffer spring; 144. a T-shaped movable rod; 145. a rubber foot; 146. an insulating sheath; 15. a camera is provided.
Detailed Description
The utility model is further described below with reference to the accompanying drawings:
example (b):
as shown in figures 1 and 2
The utility model provides an unmanned aerial vehicle device for intelligently identifying faults of high-altitude high-voltage lines, which comprises a machine body 1, a left side support 2, a left side motor 3, a left side propeller 4, a right side support 5, a right side motor 6, a right side propeller 7, a fan blade protection frame structure 8 convenient to disassemble, a storage battery 9, a control chip 10, a wireless module 11, a bottom protection frame structure 12, a side support plate 13, a buffering support structure 14 and a camera 15, wherein the left side support 2 and the right side support 5 are respectively installed at four corners of the upper part of the machine body 1 through screws; the left motor 3 is mounted on the left upper side of the left bracket 2 through a screw; the left propeller 4 is mounted on the output shaft of the left motor 3 through a screw; the right motor 6 is mounted on the right upper side of the right bracket 5 through a screw; the right propeller 7 is mounted on an output shaft of the right motor 6 through a screw; the fan blade protection frame structure 8 convenient to disassemble is arranged on the outer sides of the left side support 2 and the right side support 5; the storage battery 9, the control chip 10 and the wireless module 11 are respectively installed on the inner side of the machine body 1 through screws; the bottom protective frame structure 12 is arranged at the lower part of the machine body 1; the buffer bracket structure 14 is arranged at the lower part of the side support plate 13; the camera 15 is mounted at the middle lower part of the machine body 1 through a screw; the fan blade protection frame structure 8 convenient to disassemble comprises a connecting backing plate 81, a connecting bolt 82, a side mesh enclosure 83, a reinforcing frame 84 and a middle mesh enclosure 85, wherein the connecting backing plate 81 is respectively arranged at the lower parts of the left side support 2 and the right side support 5 through the connecting bolt 82; the side mesh enclosures 83 are respectively arranged at the outer sides of the left propeller 4 and the right propeller 7, so that the left propeller 4 or the right propeller 7 can be prevented from colliding with cables during working; the reinforcing frames 84 are mounted on the front side and the rear side of the side mesh enclosure 83 through screws, and when the side mesh enclosure 83 is used, the reinforcing frames 84 can be utilized to reinforce the side mesh enclosure 83; the side mesh enclosure 83 is glued on the upper part of the connecting backing plate 81; the middle mesh enclosure 85 is mounted on the inner side of the side mesh enclosure 83 by screws.
As shown in fig. 3, in the above embodiment, specifically, the bottom protection frame structure 12 includes a transparent shield 121, a side insulating protection frame 122, a mounting frame 123, a temperature sensor 124 and a humidity sensor 125, the transparent shield 121 is mounted at the lower part of the body 1 by screws, and the transparent shield 121 is used to protect the detection components below the body 1; the side insulating protective frames 122 are respectively installed at the connecting positions of the transparent protective cover 121 and the connecting backing plate 81 through screws, so that the side insulating protective frames 122 can be used for protecting cables when in use; the mounting frames 123 are embedded in the left and right sides of the transparent shield 121; the temperature sensor 124 and the humidity sensor 125 are respectively installed in the installation frames 123 arranged at the left and right sides by screws; the side support plate 13 is mounted on the lower portion of the transparent shield 121 by screws.
In the above embodiment, as shown in fig. 4, specifically, the buffer bracket structure 14 includes a movable frame 141, a positioning ring 142, a buffer spring 143, a T-shaped movable rod 144, a rubber leg 145 and an insulating sheath 146, wherein the movable frame 141 is embedded in the lower portion of the side support plate 13; the positioning ring 142 is mounted at the lower part of the movable frame 141 by screws; the buffer spring 143 is arranged at the upper part of the inner side of the movable frame 141, and the buffer spring 143 can be used for playing a good role in damping and buffering the T-shaped movable rod 144 when in use; the T-shaped movable rod 144 penetrates through the positioning ring 142 and is inserted into the inner side of the movable frame 141; the rubber support leg 145 is glued to the lower part of the T-shaped movable rod 144; the upper end and the lower end of the insulating sheath 146 are respectively glued on the lower part of the outer side of the side support plate 13 and the upper part of the outer side of the rubber support leg 145, so that the rubber support leg 145 and the side support plate 13 are conveniently protected when in use, and sundries are prevented from entering the inner sides of the side support plate 13 and the rubber support leg 145.
Principle of operation
In the working process, when the intelligent remote detection device is used, the side insulating protective frame 122 can be used for protecting the two sides of the machine body 1, the side mesh enclosure 83 and the middle mesh enclosure 85 can be used for protecting the outer sides of the left propeller 4 and the right propeller 7, then the camera 15, the temperature sensor 124 and the humidity sensor 125 are used for detecting the surrounding environment and the temperature and humidity, and then the wireless module 11 is used for sending signals to the remote control module through the control chip 10 so as to realize the remote intelligent detection function.
The technical solutions of the present invention or similar technical solutions designed by those skilled in the art based on the teachings of the technical solutions of the present invention are all within the scope of the present invention.
Claims (9)
1. The unmanned aerial vehicle device for the intelligent high-altitude high-voltage line fault recognition is characterized by comprising a machine body (1), a left side support (2), a left side motor (3), a left side propeller (4), a right side support (5), a right side motor (6), a right side propeller (7), a fan blade protection frame structure (8) convenient to disassemble, a storage battery (9), a control chip (10), a wireless module (11), a bottom protection frame structure (12), side support plates (13), a buffering support structure (14) and a camera (15), wherein the left side support (2) and the right side support (5) are respectively installed at four corners of the upper part of the machine body (1) through screws; the left motor (3) is arranged on the left upper side of the left bracket (2) through a screw; the left propeller (4) is arranged on an output shaft of the left motor (3) through a screw; the right motor (6) is arranged on the right upper side of the right bracket (5) through a screw; the right propeller (7) is arranged on an output shaft of the right motor (6) through a screw; the fan blade protection frame structure (8) convenient to disassemble is arranged on the outer sides of the left side support (2) and the right side support (5); the storage battery (9), the control chip (10) and the wireless module (11) are respectively installed on the inner side of the machine body (1) through screws; the bottom protective frame structure (12) is arranged at the lower part of the machine body (1); the buffer bracket structure (14) is arranged at the lower part of the side support plate (13); the camera (15) is mounted at the middle lower part of the machine body (1) through a screw; the fan blade protection frame structure (8) convenient to disassemble comprises a connecting base plate (81), a connecting bolt (82), a side mesh enclosure (83), a reinforcing frame (84) and a middle mesh enclosure (85), wherein the connecting base plate (81) is respectively arranged at the lower parts of a left side bracket (2) and a right side bracket (5) through the connecting bolt (82); the side mesh enclosure (83) is glued on the upper part of the connecting backing plate (81); the middle mesh enclosure (85) is mounted on the inner side of the side mesh enclosure (83) through screws.
2. The unmanned aerial vehicle device for intelligent high altitude high voltage line fault recognition of claim 1, wherein the bottom protective frame structure (12) comprises a transparent shield (121), a side insulating protective frame (122), a mounting frame (123), a temperature sensor (124) and a humidity sensor (125), wherein the mounting frame (123) is embedded in the left side and the right side of the transparent shield (121); the temperature sensor (124) and the humidity sensor (125) are respectively installed in the installation frames (123) arranged on the left side and the right side through screws; the side support plate (13) is mounted at the lower part of the transparent shield (121) through screws.
3. The unmanned aerial vehicle device for intelligent high-altitude high-voltage line fault identification as claimed in claim 1, wherein the buffer support structure (14) comprises a movable frame (141), a positioning ring (142), a buffer spring (143), a T-shaped movable rod (144), a rubber leg (145) and an insulating sheath (146), wherein the movable frame (141) is embedded in the lower portion of the side support plate (13); the positioning ring (142) is arranged at the lower part of the movable frame (141) through a screw; the T-shaped movable rod (144) penetrates through the positioning ring (142) and is inserted into the inner side of the movable frame (141); the rubber support leg (145) is connected to the lower part of the T-shaped movable rod (144) in a gluing mode.
4. The unmanned aerial vehicle device for high altitude high voltage line fault intelligent recognition of claim 1, characterized in that, the side screen panel (83) set up respectively in the outside of left side screw propeller (4) and right side screw propeller (7).
5. The unmanned aerial vehicle device for high altitude high voltage line fault intelligent recognition of claim 2, characterized in that transparent guard shield (121) screw installation in the lower part of fuselage (1).
6. The unmanned aerial vehicle device for high altitude high voltage line fault intelligent recognition of claim 3, characterized in that, buffer spring (143) set up in the inboard upper portion of movable frame (141).
7. The unmanned aerial vehicle device for high altitude high voltage line fault intelligent recognition of claim 2, characterized in that, the side insulating protection frame (122) respectively screw-mounted in the junction of transparent guard shield (121) and connection backing plate (81).
8. The unmanned aerial vehicle device for intelligent high-altitude high-voltage line fault identification as claimed in claim 3, wherein the upper end and the lower end of the insulating sheath (146) are respectively glued to the lower portion of the outer side of the side support plate (13) and the upper portion of the outer side of the rubber support leg (145).
9. The unmanned aerial vehicle device for high altitude high voltage line fault intelligent recognition of claim 1, characterized in that, the reinforcing frame (84) screw installation in the front and back both sides of side screen panel (83).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121647275.6U CN215972115U (en) | 2021-07-19 | 2021-07-19 | Unmanned aerial vehicle device for high-altitude high-voltage line fault intelligent recognition |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121647275.6U CN215972115U (en) | 2021-07-19 | 2021-07-19 | Unmanned aerial vehicle device for high-altitude high-voltage line fault intelligent recognition |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215972115U true CN215972115U (en) | 2022-03-08 |
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ID=80577624
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121647275.6U Active CN215972115U (en) | 2021-07-19 | 2021-07-19 | Unmanned aerial vehicle device for high-altitude high-voltage line fault intelligent recognition |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215972115U (en) |
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2021
- 2021-07-19 CN CN202121647275.6U patent/CN215972115U/en active Active
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