CN211943742U - Unmanned aerial vehicle for solar power station - Google Patents
Unmanned aerial vehicle for solar power station Download PDFInfo
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- CN211943742U CN211943742U CN202020587406.5U CN202020587406U CN211943742U CN 211943742 U CN211943742 U CN 211943742U CN 202020587406 U CN202020587406 U CN 202020587406U CN 211943742 U CN211943742 U CN 211943742U
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Abstract
The utility model provides an unmanned aerial vehicle for a solar power station, which comprises an unmanned aerial vehicle main body and a charging seat, wherein the unmanned aerial vehicle main body comprises a machine body, rotor wings arranged around the machine body, an imaging device arranged at the bottom of the machine body and landing supports arranged at the two ends of the bottom of the machine body, and the imaging device comprises a fixing frame and a camera; the landing bracket comprises a supporting rod extending outwards, a vertical rod fixed at the bottom of the supporting rod and a bottom rod fixed at the bottom of the vertical rod; a charging plate extends inwards from the top of the upright rod, a first charging terminal is fixed at the bottom of the charging plate, and the first charging terminal is connected to a battery inside the unmanned aerial vehicle main body through a lead; the two sides of the top of the charging stand are provided with a landing slot corresponding to the landing bracket, the section size of the landing slot corresponds to the bottom rod, the depth of the landing slot corresponds to the upright rod, and the inner side of the landing slot is provided with a second charging terminal corresponding to the first charging terminal; the device has the advantages of convenient detection, high efficiency, convenient charging and energy conservation.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to unmanned aerial vehicle for solar power station.
Background
With the development of new energy technology, photovoltaic power stations with larger and larger scale are built, and the number of panels installed on the photovoltaic power stations is large. Taking a 30 mw photovoltaic plant as an example, the number of panels installed may be as high as 12 million. The panel is the most important power generation unit of the photovoltaic power station, and the power generation loss of the photovoltaic power station can be caused by the faults of the panel, so that the fault inspection and the timely processing of the panel of the power station are realized, and the important significance for improving the power generation of the photovoltaic power station is realized.
Common panel failures include subfissure, shading, dust, backplane scratches, low efficiency wafers, short circuiting of bus bars within the assembly, junction box diode breakdown, and the like. For panel fault detection, usually, in a manual inspection mode, inspection personnel can manually hold an infrared thermal imager to inspect the panel of the photovoltaic power station, shoot the surface of the panel in the panel, record related information and finally analyze the faults of the photovoltaic power station according to shot pictures.
In the present scheme, the fault detection of the photovoltaic power station cell panel is carried out in a manual inspection mode, so that the problems of time consumption, labor consumption and low efficiency can be caused.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a solar power station uses unmanned aerial vehicle to solve current photovoltaic power station panel detection means, waste time and energy and the problem of inefficiency.
The utility model provides a following technical scheme:
an unmanned aerial vehicle for a solar power station comprises an unmanned aerial vehicle main body and a charging seat, wherein the unmanned aerial vehicle main body comprises a machine body, rotor wings arranged on the periphery of the machine body, an imaging device arranged at the bottom of the machine body and landing supports arranged at two ends of the bottom of the machine body, the imaging device comprises a fixing frame and a camera, and the fixing frame comprises fixing plates symmetrically arranged at two sides; the camera is fixed between the fixing frames and is connected to the fixing plates on the two sides through the rotating shaft; the descending support comprises a supporting rod extending outwards, a vertical rod fixed at the bottom of the supporting rod and a bottom rod fixed at the bottom of the vertical rod; a charging plate extends inwards from the top of the upright rod, a first charging terminal is fixed at the bottom of the charging plate, and the first charging terminal is connected to a battery inside the unmanned aerial vehicle main body through a lead; the charging stand is characterized in that two sides of the top of the charging stand correspond to the landing support and are provided with landing grooves, the cross-sectional dimensions of the landing grooves correspond to the bottom rods, the depth of the landing grooves corresponds to the vertical rods, and the inner sides of the landing grooves are provided with second charging terminals corresponding to the first charging terminals.
Preferably, a charging adapter is arranged in the charging seat, the input end of the charging adapter is externally connected with a solar power generation system of the solar power station, and the output end of the charging adapter is connected with the second charging terminal.
Preferably, a tact switch is further connected between the input end of the charging adapter and a solar power generation system of the solar power station, and the tact switch is arranged at the bottom of the descending tank.
Preferably, be provided with servo motor on the fixed plate, servo motor is rotatory through pivot drive camera, servo motor passes through the wire and is connected to the unmanned aerial vehicle main part.
Preferably, the main body of the unmanned aerial vehicle is further provided with a flight control module, and the flight control module is used for receiving or sending instructions; the flight control module is electrically connected with the camera.
Preferably, a longitudinal extending direction of the first charging terminal and a longitudinal extending direction of the second charging terminal are perpendicular to each other.
Preferably, the openings of the falling grooves are provided with rounded corners.
The utility model has the advantages that:
the utility model relates to an unmanned aerial vehicle for a solar power station can control the main body of the unmanned aerial vehicle and an imaging device to detect the battery board fault of a photovoltaic power station by the mode of personnel operating on the ground, thereby improving the efficiency of battery board fault detection; simultaneously, after the unmanned aerial vehicle main part descends, charge through the charging seat is automatic, adopt the clean energy of solar power station self-production, energy-concerving and environment-protective.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
FIG. 1 is a schematic structural view of the present invention;
labeled as: 1. the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, 11, a vehicle body, 12, a rotor wing, 2, an imaging device, 21, a fixing frame, 22, a camera, 23, a servo motor, 3, a landing bracket, 31, a supporting rod, 32, a vertical rod, 33, a bottom rod, 34, a charging plate, 35, a first charging terminal, 4, a charging seat, 41, a landing groove and 42, and a second charging terminal.
Detailed Description
As shown in fig. 1, an unmanned aerial vehicle for a solar power station comprises an unmanned aerial vehicle main body 1 and a charging seat 4, wherein the unmanned aerial vehicle main body 1 comprises a machine body 11, rotor wings 12 arranged around the machine body 1, an imaging device 2 arranged at the bottom of the machine body 1 and landing supports 3 arranged at two ends of the bottom of the machine body 1; the unmanned aerial vehicle main body 1 is also provided with a flight control module, and the flight control module is used for receiving or sending instructions; the flight control module is electrically connected to the camera 22.
The imaging device 2 comprises a fixed frame 21 and a camera 22, wherein the fixed frame 21 comprises fixed plates which are symmetrically arranged at two sides; the camera 22 is fixed between the fixing frames 21 and is connected to the fixing plates at two sides through a rotating shaft; be provided with servo motor 23 on the fixed plate, servo motor 23 is rotatory through pivot drive camera 22, and servo motor 23 is connected to unmanned aerial vehicle main part 1 through the wire.
The descending support 3 comprises a support rod 31 extending outwards, a vertical rod 32 fixed at the bottom of the support rod 31 and a bottom rod 33 fixed at the bottom of the vertical rod 32; the top of the upright rod 32 extends inwards to form a charging plate 34, a first charging terminal 35 is fixed at the bottom of the charging plate 34, and the first charging terminal 35 is connected to the internal battery of the unmanned aerial vehicle main body 1 through a lead.
The two sides of the top of the charging stand 4 are provided with a landing slot 41 corresponding to the landing bracket 3, the opening of the landing slot 41 is provided with a rounded corner, the section size of the landing slot 41 corresponds to the bottom rod 33, the depth of the landing slot 41 corresponds to the upright rod 32, the inner side of the landing slot 41 is provided with a second charging terminal 42 corresponding to the first charging terminal 35, and the length extension direction of the first charging terminal 35 is perpendicular to that of the second charging terminal 42; the charging base 4 is internally provided with a charging adapter, the input end of the charging adapter is externally connected with a solar power generation system of a solar power station, the output end of the charging adapter is connected with a second charging terminal 42, a tact switch is further connected between the input end of the charging adapter and the solar power generation system of the solar power station, and the tact switch is arranged at the bottom of the falling groove 41.
The working process of the specific embodiment is as follows:
the working personnel send instructions to the flight control module through the remote control equipment to control the unmanned aerial vehicle main body 1 to take off, inspect the unmanned aerial vehicle above the solar power station and shoot through the imaging device 2; after shooting work is completed, the unmanned aerial vehicle main body 1 lands on the charging seat 4, the landing support 3 enters the landing groove 41, the first charging terminal 35 and the second charging terminal 42 are connected at the moment, the bottom rod 33 presses the touch switch, the solar power generation system of the solar power station, the touch switch, the charging adapter, the second charging terminal 42, the first charging terminal 35 and the internal battery of the unmanned aerial vehicle main body 1 are sequentially connected, and charging is carried out.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (7)
1. An unmanned aerial vehicle for a solar power station is characterized by comprising an unmanned aerial vehicle main body and a charging seat, wherein the unmanned aerial vehicle main body comprises a machine body, rotor wings arranged around the machine body, an imaging device arranged at the bottom of the machine body and landing brackets arranged at two ends of the bottom of the machine body, the imaging device comprises a fixed frame and a camera, and the fixed frame comprises fixed plates symmetrically arranged at two sides; the camera is fixed between the fixing frames and is connected to the fixing plates on the two sides through the rotating shaft; the descending support comprises a supporting rod extending outwards, a vertical rod fixed at the bottom of the supporting rod and a bottom rod fixed at the bottom of the vertical rod; a charging plate extends inwards from the top of the upright rod, a first charging terminal is fixed at the bottom of the charging plate, and the first charging terminal is connected to a battery inside the unmanned aerial vehicle main body through a lead; the charging stand is characterized in that two sides of the top of the charging stand correspond to the landing support and are provided with landing grooves, the cross-sectional dimensions of the landing grooves correspond to the bottom rods, the depth of the landing grooves corresponds to the vertical rods, and the inner sides of the landing grooves are provided with second charging terminals corresponding to the first charging terminals.
2. The unmanned aerial vehicle for a solar power plant according to claim 1, wherein a charging adapter is provided inside the charging base, an input end of the charging adapter is externally connected to a solar power generation system of the solar power plant, and an output end of the charging adapter is connected to the second charging terminal.
3. The unmanned aerial vehicle for the solar power station as claimed in claim 2, wherein a tact switch is further connected between the input end of the charging adapter and a solar power generation system of the solar power station, and the tact switch is arranged at the bottom of the landing slot.
4. The unmanned aerial vehicle for the solar power station as claimed in claim 1, wherein a servo motor is disposed on the fixing plate, the servo motor drives the camera to rotate through a rotating shaft, and the servo motor is connected to the unmanned aerial vehicle main body through a lead.
5. The unmanned aerial vehicle for the solar power station as claimed in claim 1, wherein the unmanned aerial vehicle body is further provided with a flight control module, and the flight control module is used for receiving or sending instructions; the flight control module is electrically connected with the camera.
6. The unmanned aerial vehicle for a solar power plant according to claim 1, wherein a length extending direction of the first charging terminal and a length extending direction of the second charging terminal are perpendicular to each other.
7. The unmanned aerial vehicle for the solar power plant as claimed in claim 1, wherein the openings of the landing slots are provided with rounded corners.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020587406.5U CN211943742U (en) | 2020-04-17 | 2020-04-17 | Unmanned aerial vehicle for solar power station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020587406.5U CN211943742U (en) | 2020-04-17 | 2020-04-17 | Unmanned aerial vehicle for solar power station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211943742U true CN211943742U (en) | 2020-11-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020587406.5U Active CN211943742U (en) | 2020-04-17 | 2020-04-17 | Unmanned aerial vehicle for solar power station |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211943742U (en) |
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2020
- 2020-04-17 CN CN202020587406.5U patent/CN211943742U/en active Active
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