CN213677156U - Wind turbine generator system inspection device based on unmanned aerial vehicle - Google Patents
Wind turbine generator system inspection device based on unmanned aerial vehicle Download PDFInfo
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- CN213677156U CN213677156U CN202022118118.8U CN202022118118U CN213677156U CN 213677156 U CN213677156 U CN 213677156U CN 202022118118 U CN202022118118 U CN 202022118118U CN 213677156 U CN213677156 U CN 213677156U
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Abstract
The utility model discloses a wind turbine generator system inspection device based on unmanned aerial vehicle, including the unmanned aerial vehicle body, the unmanned aerial vehicle body passes through the control of external control maincenter system, and fixedly connected with support frame can all be dismantled to unmanned aerial vehicle body bottom both sides, and support frame bottom fixedly connected with buffering subassembly, unmanned aerial vehicle body bottom are connected with the mounting panel, and the aerial photograph camera is installed to the mounting panel bottom, and unmanned aerial vehicle body top is equipped with slope warning subassembly, slope warning subassembly and external control maincenter system wireless connection; monitoring the slope condition of unmanned aerial vehicle body through slope warning subassembly, when unmanned aerial vehicle body inclination is too big, can the transmitting signal give outside external control maincenter system, remind staff unmanned aerial vehicle body this moment to be in unusual tilt state, need adjust, be equipped with the buffering subassembly simultaneously, can play the effect of buffering when unmanned aerial vehicle body descends, prevent that the unmanned aerial vehicle body from receiving the damage.
Description
Technical Field
The utility model relates to a wind turbine generator system patrols and examines technical field, specifically is wind turbine generator system inspection device based on unmanned aerial vehicle.
Background
In recent years, the development of wind power in emerging markets is rapid. Under the background of national policy support and energy supply tension, the Chinese wind power industry, particularly the wind power equipment manufacturing industry, also rises rapidly, and becomes the most active place of wind power in the world.
In wind turbine generator system's use, regular needs patrol and examine wind turbine generator system, so that in time discover the trouble, because wind turbine generator system's blade is located the high altitude, consequently all adopt installation camera of taking photo by plane on unmanned aerial vehicle to patrol and examine, current unmanned aerial vehicle when high altitude flight, unmanned aerial vehicle is the great slope of taking place sometimes, when unmanned aerial vehicle is in great slope flight, lead to falling of unmanned aerial vehicle easily, and current unmanned aerial vehicle lacks the check out test set whether unusual slope to unmanned aerial vehicle, it is comparatively inconvenient to use.
Based on this, the utility model designs a wind turbine generator system inspection device based on unmanned aerial vehicle to solve the above-mentioned problem of mentioning.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a wind turbine generator system inspection device based on unmanned aerial vehicle, monitor the slope condition of unmanned aerial vehicle body through slope warning subassembly, when unmanned aerial vehicle body inclination is too big, can the transmitting signal give outside external control maincenter system, remind staff unmanned aerial vehicle body this moment to be in unusual tilt state, need adjust, be equipped with the buffering subassembly simultaneously, can play the effect of buffering when unmanned aerial vehicle body descends, prevent that the unmanned aerial vehicle body from receiving the damage, with the problem of proposing in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: wind turbine generator system inspection device based on unmanned aerial vehicle, including the unmanned aerial vehicle body, the unmanned aerial vehicle body passes through external control maincenter system control, fixedly connected with support frame all can be dismantled to unmanned aerial vehicle body bottom both sides, support frame bottom fixedly connected with buffering subassembly, unmanned aerial vehicle body bottom is connected with the mounting panel, the camera of taking photo by plane is installed to the mounting panel bottom, unmanned aerial vehicle body top is equipped with slope warning subassembly, slope warning subassembly and external control maincenter system wireless connection.
Preferably, the buffering subassembly includes the shell, roof fixedly connected with spring in the shell, there is even board spring bottom butt, even board bottom fixedly connected with connecting rod, the connecting rod passes the shell, connecting rod bottom fixedly connected with shock attenuation board.
Preferably, a friction cushion is bonded at the bottom of the damping plate.
Preferably, the slope warning subassembly includes insulating urceolus, insulating urceolus and unmanned aerial vehicle body top fixed connection, be equipped with metal sleeve in the insulating urceolus, the roof articulates there is the metal bar in the insulating urceolus, roof left side is equipped with the battery in the insulating urceolus, roof right side is equipped with wireless transmitter in the insulating urceolus.
Preferably, the positive electrode of the storage battery is electrically connected with the metal rod, the negative electrode of the storage battery is electrically connected with the wireless signal transmitter and the metal sleeve, and the wireless signal transmitter is wirelessly connected with the external control center system.
Preferably, the aerial camera is an FPV aerial model aerial camera, and the model of the aerial camera is RS-HD1818C 6-5V.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model is not only novel in structure, monitor the slope condition of unmanned aerial vehicle body through slope warning subassembly, when unmanned aerial vehicle body inclination is too big, can the transmitting signal give outside external control maincenter system, remind staff unmanned aerial vehicle body this moment to be in unusual tilt state, need adjust, be equipped with the buffering subassembly simultaneously, can play the effect of buffering when unmanned aerial vehicle body descends, prevent that the unmanned aerial vehicle body from receiving the damage.
2. The utility model discloses in, during the flight of unmanned aerial vehicle body, when the inclination of unmanned aerial vehicle body is too big, contact between metal bar and the metal sleeve, the wireless signal transmitter circular telegram starts, and wireless signal transmitter transmission signal gives outside external control maincenter system, reminds staff unmanned aerial vehicle body this moment to be in unusual tilt state, needs to adjust the flight state of unmanned aerial vehicle body, prevents that the unmanned aerial vehicle body from appearing falling, and the security is high.
3. The utility model discloses in, when the unmanned aerial vehicle body descends, the friction cushion contacts with ground earlier, and the damping plate upward movement, damping plate pass through the connecting rod and drive even board upward movement, and the spring is compressed, and friction cushion, damping plate and spring can play the effect of buffering, cause the unmanned aerial vehicle body to receive the damage because of the speed is too fast when preventing that the unmanned aerial vehicle body from descending.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the tilt warning assembly of the present invention;
fig. 3 is a schematic view of the structure of the buffer assembly of the present invention.
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 of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Please refer to fig. 1-3, the utility model provides a wind turbine inspection device technical scheme based on unmanned aerial vehicle: including unmanned aerial vehicle body 1, unmanned aerial vehicle body 1 is through external control maincenter system control, fixedly connected with support frame 5 all can be dismantled to 1 bottom both sides of unmanned aerial vehicle body, support frame 5 bottom fixedly connected with buffering subassembly 4 can play the effect of buffering when unmanned aerial vehicle body 1 descends, prevents that unmanned aerial vehicle body 1 from receiving the damage, 1 bottom of unmanned aerial vehicle body is connected with mounting panel 2, aerial photograph camera 3 is installed to 2 bottoms of mounting panel, 1 top of unmanned aerial vehicle body is equipped with slope warning subassembly 6, slope warning subassembly 6 and external control maincenter system wireless connection, when 1 inclination of unmanned aerial vehicle body is too big, can the transmitting signal give external control maincenter system, remind staff unmanned aerial vehicle body 1 this moment to be in unusual tilt state.
Wherein, buffer unit 4 includes shell 41, roof fixedly connected with spring 42 in the shell 41, spring 42 bottom butt has even board 43, even board 43 bottom fixedly connected with connecting rod 44, connecting rod 44 passes shell 41, connecting rod 44 bottom fixedly connected with shock attenuation board 45, shock attenuation board 45 bottom bonds and has friction cushion 46, when unmanned aerial vehicle body 1 descends, friction cushion 46 contacts with ground earlier, shock attenuation board 45 upward movement, shock attenuation board 45 drives even board 43 upward movement through connecting rod 44, spring 42 is compressed, friction cushion 46, shock attenuation board 45 and spring 42 can play the effect of buffering, cause unmanned aerial vehicle body 1 to receive the damage because of the speed is too fast when preventing unmanned aerial vehicle body 1 from descending.
Wherein, the inclination warning component 6 comprises an insulating outer cylinder 61, the insulating outer cylinder 61 is fixedly connected with the top of the unmanned aerial vehicle body 1, a metal sleeve 62 is arranged in the insulating outer cylinder 61, a metal rod 64 is hinged with the inner top wall of the insulating outer cylinder 61, a storage battery 63 is arranged on the left side of the inner top wall of the insulating outer cylinder 61, a wireless signal transmitter 65 is arranged on the right side of the inner top wall of the insulating outer cylinder 61, the positive electrode of the storage battery 63 is electrically connected with the metal rod 64, the negative electrode of the storage battery 63 is electrically connected with the wireless signal transmitter 65 and the metal sleeve 62, the wireless signal transmitter 65 is wirelessly connected with an external control center system, when the inclination angle of the unmanned aerial vehicle body 1 is too large, the metal rod 64 is contacted with the metal sleeve 62, and at the moment, a closed loop is formed among the, the wireless signal transmitter 65 transmits a signal to an external control hub system.
The aerial photography camera 3 is an FPV aerial photography camera, the model of the aerial photography camera 3 is RS-HD1818C6-5V, and the shooting effect is good.
The specific working principle is as follows:
when the unmanned aerial vehicle is used, the flight path of the unmanned aerial vehicle body 1 is controlled through the external control center system, the wind turbine generator is subjected to camera inspection through the aerial camera 3, when the inclination angle of the unmanned aerial vehicle body 1 is too large, the metal rod 64 is in contact with the metal sleeve 62, a closed loop is formed among the storage battery 63, the metal rod 64, the metal sleeve 62 and the wireless signal transmitter 65 at the moment, the wireless signal transmitter 65 transmits a signal to the external control center system to remind a worker that the unmanned aerial vehicle body 1 is in an abnormal inclination state at the moment, the flight state of the unmanned aerial vehicle body 1 needs to be adjusted, the unmanned aerial vehicle body 1 is prevented from falling, the safety is high, when the unmanned aerial vehicle body 1 descends, the friction cushion 46 is firstly in contact with the ground, the damping plate 45 moves upwards, and the damping plate 45 drives the connecting plate 43 to move upwards through, spring 42 is compressed, and the effect of buffering can be played to friction cushion 46, shock attenuation board 45 and spring 42, causes unmanned aerial vehicle body 1 to receive the damage because of the speed is too fast when preventing unmanned aerial vehicle body 1 from descending.
In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The present invention is limited only by the claims and their full scope and equivalents.
Claims (6)
1. Wind turbine generator system inspection device based on unmanned aerial vehicle, including unmanned aerial vehicle body (1), unmanned aerial vehicle body (1) is through external control maincenter system control, its characterized in that: fixedly connected with support frame (5) all can be dismantled to unmanned aerial vehicle body (1) bottom both sides, support frame (5) bottom fixedly connected with buffering subassembly (4), unmanned aerial vehicle body (1) bottom is connected with mounting panel (2), camera (3) of taking photo by plane are installed to mounting panel (2) bottom, unmanned aerial vehicle body (1) top is equipped with slope warning subassembly (6), slope warning subassembly (6) and external control maincenter system wireless connection.
2. The unmanned aerial vehicle-based wind turbine inspection device according to claim 1, wherein: buffer unit (4) include shell (41), roof fixedly connected with spring (42) in shell (41), spring (42) bottom butt has even board (43), even board (43) bottom fixedly connected with connecting rod (44), shell (41) is passed in connecting rod (44), connecting rod (44) bottom fixedly connected with shock attenuation board (45).
3. The unmanned aerial vehicle-based wind turbine inspection device according to claim 2, wherein: and a friction cushion (46) is bonded at the bottom of the damping plate (45).
4. The unmanned aerial vehicle-based wind turbine inspection device according to claim 1, wherein: slope warning subassembly (6) are including insulating urceolus (61), insulating urceolus (61) and unmanned aerial vehicle body (1) top fixed connection, be equipped with metal sleeve (62) in insulating urceolus (61), the roof articulates in insulating urceolus (61) has metal rod (64), roof left side is equipped with battery (63) in insulating urceolus (61), roof right side is equipped with radio signal transmitter (65) in insulating urceolus (61).
5. The unmanned aerial vehicle-based wind turbine inspection device according to claim 4, wherein: the positive pole of the storage battery (63) is electrically connected with the metal rod (64), the negative pole of the storage battery (63) is electrically connected with the wireless signal transmitter (65) and the metal sleeve (62), and the wireless signal transmitter (65) is wirelessly connected with an external control center system.
6. The unmanned aerial vehicle-based wind turbine inspection device according to claim 1, wherein: the aerial photography camera (3) is an FPV aerial photography camera, and the model of the aerial photography camera (3) is RS-HD1818C 6-5V.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022118118.8U CN213677156U (en) | 2020-09-24 | 2020-09-24 | Wind turbine generator system inspection device based on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022118118.8U CN213677156U (en) | 2020-09-24 | 2020-09-24 | Wind turbine generator system inspection device based on unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN213677156U true CN213677156U (en) | 2021-07-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202022118118.8U Expired - Fee Related CN213677156U (en) | 2020-09-24 | 2020-09-24 | Wind turbine generator system inspection device based on unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114476104A (en) * | 2021-12-27 | 2022-05-13 | 北京卓翼智能科技有限公司 | Carry on nanopi system unmanned aerial vehicle |
-
2020
- 2020-09-24 CN CN202022118118.8U patent/CN213677156U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114476104A (en) * | 2021-12-27 | 2022-05-13 | 北京卓翼智能科技有限公司 | Carry on nanopi system unmanned aerial vehicle |
| CN114476104B (en) * | 2021-12-27 | 2023-11-24 | 北京卓翼智能科技有限公司 | Carry on nano system unmanned aerial vehicle |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210713 |