CN214729642U - Insulator fault detection's unmanned aerial vehicle - Google Patents
Insulator fault detection's unmanned aerial vehicle Download PDFInfo
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- CN214729642U CN214729642U CN202120877106.5U CN202120877106U CN214729642U CN 214729642 U CN214729642 U CN 214729642U CN 202120877106 U CN202120877106 U CN 202120877106U CN 214729642 U CN214729642 U CN 214729642U
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- 238000001514 detection method Methods 0.000 title claims abstract description 36
- 239000012212 insulator Substances 0.000 title claims abstract description 22
- 230000005540 biological transmission Effects 0.000 claims abstract description 15
- 230000004044 response Effects 0.000 claims abstract description 9
- 239000000523 sample Substances 0.000 claims abstract description 8
- 238000012360 testing method Methods 0.000 claims abstract description 4
- 238000009434 installation Methods 0.000 claims abstract description 3
- 238000012545 processing Methods 0.000 claims description 12
- 230000006698 induction Effects 0.000 claims description 8
- 238000000034 method Methods 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 4
- 230000004888 barrier function Effects 0.000 description 4
- 230000006870 function Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008447 perception Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
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Abstract
The utility model discloses an insulator fault detection's unmanned aerial vehicle, concretely relates to unmanned air vehicle technique field, including the unmanned aerial vehicle body, one side fixed mounting of unmanned aerial vehicle body has the span, the top surface of span is rotated and is installed the wing, the top surface demountable installation of unmanned aerial vehicle body has a pole, the one end fixed mounting of a pole has the detector shell, one side fixed mounting of unmanned aerial vehicle body has the response radar. In the above-mentioned scheme, unmanned aerial vehicle body itself has manual remote operation's function, can easily go to any eminence, and cooperation response radar and camera can perceive where the insulator is located to pass through data transmission module with this signal and transmit to the computer end, avoid the high altitude sight not good, the detection error appears and probably causes danger even, through test probe and detection stick and establish single chip microcomputer controller in, can realize the accurate effect that detects out the insulator fault problem, light swift, the practicality is strong.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically say, the utility model relates to an insulator fault detection's unmanned aerial vehicle.
Background
The unmanned plane is called as an unmanned plane for short, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device, and at present, for the insulator detection of a high-voltage line, a maintainer needs to operate at high altitude, so that the unmanned plane has the risk of falling and the possible electric shock condition, and the danger coefficient is extremely high; lack the device at present, can combine unmanned aerial vehicle and detection device, realize artifical remote operation.
Therefore, it is urgently needed to provide an unmanned aerial vehicle for insulator fault detection.
SUMMERY OF THE UTILITY MODEL
In order to overcome the above-mentioned defect of prior art, the embodiment of the utility model provides an insulator fault detection's unmanned aerial vehicle to solve prior art and lack the problem of the device that can combine unmanned aerial vehicle and detection mechanism together.
In order to solve the technical problem, the utility model provides a following technical scheme: the utility model provides an insulator fault detection's unmanned aerial vehicle, includes the unmanned aerial vehicle body, one side fixed mounting of unmanned aerial vehicle body has the span, the top surface of span is rotated and is installed the wing, the top surface demountable installation of unmanned aerial vehicle body has a pole, the one end fixed mounting of a pole has the detector shell, one side fixed mounting of unmanned aerial vehicle body has the response radar, one side fixed mounting that the unmanned aerial vehicle body is close to the response radar has the camera, the inside of camera is equipped with the photography module of making a video recording, the inside of unmanned aerial vehicle body is equipped with image processing module and data transmission module.
Preferably, a signal line is fixedly installed on one side of the detector shell, a detection rod is fixedly installed on the other side of the detector shell, a detection probe is fixedly sleeved on the outer wall of the detection rod, and a single chip microcomputer controller is arranged inside the detector shell.
Preferably, the inside of unmanned aerial vehicle body is equipped with the controller, the output and the controller electric connection of response radar, the output of controller and image processing module's input electric connection, the output of the photographic module of making a video recording and the input electric connection of controller, image processing module's output and data transmission module's input electric connection.
Preferably, the output end of the data transmission module is electrically connected with a data receiving module, and the data receiving module is located inside the computer end.
The utility model discloses an above-mentioned technical scheme's beneficial effect as follows:
in the above-mentioned scheme, unmanned aerial vehicle body itself has manual remote operation's function, can easily go to any eminence, and cooperation response radar and camera can perceive where the insulator is located to pass through data transmission module with this signal and transmit to the computer end, avoid the high altitude sight not good, the detection error appears and probably causes danger even, through test probe and detection stick and establish single chip microcomputer controller in, can realize the accurate effect that detects out the insulator fault problem, light swift, the practicality is strong.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural view of the unmanned aerial vehicle body of the present invention;
fig. 3 is a schematic side view of the unmanned aerial vehicle body of the present invention;
fig. 4 is a system block diagram of the present invention.
[ reference numerals ]
1. An unmanned aerial vehicle body; 2. a wing span; 3. an airfoil; 4. a support rod; 5. a detector housing; 6. a signal line; 7. detecting a probe; 8. a detection rod; 9. an induction radar; 10. a camera; 11. a camera shooting module; 12. an image processing module; 13. and a data transmission module.
Detailed Description
In order to make the technical problems, technical solutions and advantages of the present invention more clear, the following detailed description is given with reference to the accompanying drawings and specific embodiments, and the description of this section is only exemplary and explanatory and should not be taken as limiting the scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
The embodiment of the utility model provides an unmanned aerial vehicle for insulator fault detection as shown in fig. 1-4, including unmanned aerial vehicle body 1, one side of unmanned aerial vehicle body 1 is fixedly installed with span 2, the top surface of span 2 is rotated and is installed with wing 3, the top surface of unmanned aerial vehicle body 1 can be dismantled and installed with prop-out pole 4, one end of prop-out pole 4 is fixedly installed with detector shell 5, one side of unmanned aerial vehicle body 1 is fixedly installed with induction radar 9, one side of unmanned aerial vehicle body 1 near induction radar 9 is fixedly installed with camera 10, the inside of camera 10 is equipped with camera shooting module 11, the inside of unmanned aerial vehicle body 1 is equipped with image processing module 12 and data transmission module 13; one side fixed mounting of detector shell 5 has signal line 6, and the opposite side fixed mounting of detector shell 5 has detection stick 8, and the outer wall of detection stick 8 is fixed to be cup jointed with test probe 7, and the inside of detector shell 5 is equipped with single chip controller.
Specifically, during actual detection, the top surface of unmanned aerial vehicle body 1 still needs to be equipped with fixture, and fixture can fix whole device on the cable, when avoiding detecting, takes place to rock, influences detection efficiency or the detection data error appears.
Specifically, unmanned aerial vehicle is still including the remote controller that control unmanned aerial vehicle body 1 removed, when needs examine the insulator of high altitude electric wire, can fly through remote controller control unmanned aerial vehicle body 1, and response radar 9 can the perception barrier, avoids unmanned aerial vehicle body 1 and barrier to collide, and the camera can be in real time with video data upload to the computer end, through video content, adjusts unmanned aerial vehicle body 1's position.
The unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, an induction radar 9, an image processing module 12, a camera shooting module 11, a data transmission module 13 and a controller, wherein the controller is arranged in the unmanned aerial vehicle body 1, the output end of the induction radar 9 is electrically connected with the controller, the output end of the controller is electrically connected with the input end of the image processing module 12, the output end of the camera shooting module 11 is electrically connected with the input end of the controller, and the output end of the image processing module 12 is electrically connected with the input end of the data transmission module 13; the output end of the data transmission module 13 is electrically connected with a data receiving module, and the data receiving module is located inside the computer end.
As shown in fig. 4, specifically, the controller, the camera module 11, the image processing module 12 and the data slave transmission module 13 may be connected by a line, so as to achieve an effect of transmitting video data in real time, and avoid detection errors caused by poor high-altitude sight.
The working process of the utility model is as follows:
when the insulator of the high-altitude electric wire needs to be detected, the unmanned aerial vehicle body 1 can be controlled to fly through the remote controller, the induction radar 9 can sense the barrier, the collision between the unmanned aerial vehicle body 1 and the barrier is avoided, the camera can upload video data to a computer end in real time, the position of the unmanned aerial vehicle body 1 is adjusted through video content, and finally the insulator is detected through the detection probe 7 and the detection rod 8, in the scheme, the unmanned aerial vehicle body 1 has the function of manual remote operation and can easily go to any high place, the position of the insulator can be sensed by matching the induction radar 9 and the camera 10, the signal is transmitted to the computer end through the data transmission module 13 for further confirmation, the poor high-altitude sight is avoided, the detection error is caused and even danger is possibly caused, and the detection probe 7, the detection rod 8 and the built-in single chip microcomputer controller are adopted, the effect of detecting the insulator fault problem fast and accurately can be realized, and the method is easy and fast and has strong practicability.
The points to be finally explained are: the terms "central," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like are used in a generic and descriptive sense only and not for purposes of limitation, the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like are used in the description and are used in a generic and descriptive sense only and not for purposes of limitation, the term "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," and the like. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases for a person of ordinary skill in the art;
secondly, the method comprises the following steps: in the drawings of the disclosed embodiments of the present invention, only the structures related to the disclosed embodiments are referred to, and other structures can refer to the common design, and under the condition of no conflict, the same embodiment and different embodiments of the present invention can be combined with each other;
and finally: the above description is only for the preferred embodiment of the present invention and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (4)
1. The utility model provides an insulator fault detection's unmanned aerial vehicle, includes unmanned aerial vehicle body (1), one side fixed mounting of unmanned aerial vehicle body (1) has span (2), the top surface of span (2) is rotated and is installed wing (3), its characterized in that, the top surface demountable installation of unmanned aerial vehicle body (1) has a pole (4), the one end fixed mounting of pole (4) has detector shell (5), one side fixed mounting of unmanned aerial vehicle body (1) has response radar (9), one side fixed mounting that unmanned aerial vehicle body (1) is close to response radar (9) has camera (10), the inside of camera (10) is equipped with makes a video recording photography module (11), the inside of unmanned aerial vehicle body (1) is equipped with image processing module (12) and data transmission module (13).
2. The insulator fault detection unmanned aerial vehicle of claim 1, characterized in that, one side fixed mounting of detector shell (5) has signal line (6), the other side fixed mounting of detector shell (5) has detection stick (8), the outer wall of detection stick (8) is fixed to be cup jointed with test probe (7), the inside of detector shell (5) is equipped with single chip microcomputer controller.
3. The unmanned aerial vehicle for insulator fault detection according to claim 1, wherein a controller is arranged inside the unmanned aerial vehicle body (1), the output end of the induction radar (9) is electrically connected with the controller, the output end of the controller is electrically connected with the input end of the image processing module (12), the output end of the camera shooting module (11) is electrically connected with the input end of the controller, and the output end of the image processing module (12) is electrically connected with the input end of the data transmission module (13).
4. The unmanned aerial vehicle for insulator fault detection according to claim 1, wherein the output end of the data transmission module (13) is electrically connected with a data receiving module, and the data receiving module is located inside a computer end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120877106.5U CN214729642U (en) | 2021-04-26 | 2021-04-26 | Insulator fault detection's unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120877106.5U CN214729642U (en) | 2021-04-26 | 2021-04-26 | Insulator fault detection's unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214729642U true CN214729642U (en) | 2021-11-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120877106.5U Expired - Fee Related CN214729642U (en) | 2021-04-26 | 2021-04-26 | Insulator fault detection's unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214729642U (en) |
-
2021
- 2021-04-26 CN CN202120877106.5U patent/CN214729642U/en not_active Expired - Fee Related
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211116 |
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| CF01 | Termination of patent right due to non-payment of annual fee |