Photovoltaic product inspection device

Abstract

The utility model provides a photovoltaic product inspection device which comprises a machine body, movable wings and an inspection assembly, the left front side, the left rear side, the right front side and the right rear side of the machine body are hinged to the movable wings respectively, the inspection assembly used for photovoltaic inspection is installed on the lower side of the machine body, and the machine body comprises a bottom plate, a top plate and a battery. Compared with the prior art, the photovoltaic routing inspection device has the following beneficial effects that by arranging the clamping pieces, the wind resistance in a strong wind environment can be effectively reduced, and the whole device can smoothly complete a photovoltaic routing inspection task in strong wind weather or when flying against wind; compared with traditional fixed wings, the movable wings can select the opening degree of the wings according to weather conditions, so that the movable wings can still perform normal inspection tasks in windy weather, and the flight stability of the whole device in windy weather is improved.

Description

Technical Field

[0001] The utility model belongs to the technical field of photovoltaic inspection equipment, and particularly relates to a photovoltaic product inspection device. Background Art

[0002] Photovoltaic inspection devices refer to professional equipment and technical means used to regularly inspect and maintain the operating status of various equipment and systems in photovoltaic power plants. These devices usually combine advanced sensing technology, drone inspections, image recognition, data analysis, and Internet and Internet of Things (IoT) technologies to efficiently and accurately monitor and evaluate the health and performance of photovoltaic power plants, using drones equipped with high-resolution cameras, infrared thermal imagers and other sensors to conduct comprehensive and rapid aerial inspections of photovoltaic panels. Drones can cover large areas of photovoltaic arrays, quickly identify problems such as damage, hot spots, stains, and occlusions on panels, and accurately locate faults through image analysis technology.

[0003] Existing mission-specific drones used for photovoltaic inspections use a multi-rotor design (such as quad-rotors, hexacopters, etc.). These drones control their flight attitude and direction by adjusting the rotation speed of each rotor. However, drones with this design structure may affect the stability and endurance of the drone in extreme weather conditions (such as strong winds), limiting its inspection capabilities in specific time periods or areas. Therefore, we hope to design a photovoltaic product inspection device with a new structure to solve this problem. Utility Model Content

[0004] In view of the deficiencies in the prior art, the purpose of the present invention is to provide a photovoltaic product inspection device to solve the problems raised in the above-mentioned background technology.

[0005] The utility model is realized by the following technical scheme: a photovoltaic product inspection device, comprising: a body, a movable wing and an inspection component, wherein the left front side, the left rear side, the right front side and the right rear side of the body are respectively hinged with a movable wing, and the lower side of the body is equipped with an inspection component for photovoltaic inspection;

[0006] The machine body comprises a bottom plate, a top plate and a battery, the top plate is fixed on the upper side of the top plate, and the battery is installed in the middle of the upper side of the top plate;

[0007] The movable wing comprises a wing rod and a rotor, and a rotor is installed at the end of each wing rod. The inspection component comprises a camera and a remote control adjustment frame, and a camera is movably installed at the lower end of the remote control adjustment frame.

[0008] As a preferred embodiment, a mounting frame is installed on the upper end of the remote control adjustment frame, and the remote control adjustment frame is fixed in the middle of the lower surface of the base plate through the mounting frame. The camera is movably mounted below the middle of the base plate through the remote control adjustment frame and the mounting frame. A high-resolution camera can be selected, and its specific model can be selected according to actual usage requirements. The camera and the remote control adjustment frame are both existing products on the market that meet usage requirements.

[0009] As a preferred embodiment, a support leg is welded on the left and right sides of the lower surface of the base plate, the height of the lowest end of the camera is higher than the height of the lowest end of the support leg, and a mounting block is fixed on the middle front and rear sides of the upper surface of the base plate.

[0010] As a preferred embodiment, the left rear side and the right rear side of each mounting block are damping-hinged with a wing rod close to the front end of the fuselage, and a clamping piece is respectively installed on the left front side and the left rear side of the front end of the base plate, and a clamping piece is respectively installed on the right front side and the right rear side of the front end of the base plate.

[0011] As a preferred embodiment, each of the clamping parts is composed of a clamping block 1 and a clamping block 2, and the distance between the clamping block 1 and the clamping block 2 in the clamping part on the front side of the base plate is greater than the distance between the clamping block 1 and the clamping block 2 in the clamping part on the rear side of the base plate. In actual use, the parts where the clamping blocks 1 and 2 are clamped to the hollow rod will be deformed during clamping, and when the hollow rod is fully inserted, the deformation will be reset, so that the hollow rod can be firmly clamped and will not fall off during flight.

[0012] As a preferred embodiment, the specifications of the clamping block 1 in each of the clamping parts are the same as the specifications of the clamping block 2, a clamping groove 1 is provided on the side of the clamping block 1 close to the clamping block 2, and a clamping groove 2 is provided on the side of the clamping block 2 close to the clamping block 1, and the specifications of the clamping groove 1 are the same as the specifications of the clamping groove 2.

[0013] As a preferred embodiment, the wing rod comprises a hollow rod and a hinged joint, a hinged joint is fixed to a side of the hollow rod close to the mounting block, and the hollow rod is damping-hinged with the rear side of the mounting block through the hinged joint;

[0014] The diameter of the hollow rod matches the size of the first clamping groove and the second clamping groove.

[0015] After adopting the above technical solution, the beneficial effects of the utility model are: by setting the card connector, the wind resistance in a windy environment can be effectively reduced, ensuring that the entire device can successfully complete the task of photovoltaic inspection in windy weather or against the wind;

[0016] Compared with traditional fixed wings, the movable wing setting can choose the wing opening degree according to weather conditions, so that it can still perform normal inspection tasks in windy weather, improving the flight stability of the entire device in windy weather. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative labor.

[0018] Figure 1 The utility model is a schematic diagram of the overall structure of a photovoltaic product inspection device.

[0019] Figure 2 It is a schematic diagram of the rear side structure of a photovoltaic product inspection device of the utility model.

[0020] Figure 3 It is a schematic diagram of the connection between a clamping piece and a movable wing of a photovoltaic product inspection device of the utility model.

[0021] Figure 4 This is a schematic diagram of the optional component structure of a photovoltaic product inspection device of the utility model.

[0022] In the figure, 100-body, 110-bottom plate, 120-top plate, 130-battery, 140-leg, 150-mounting block, 160-clip-joint, 161-clip-joint block 1, 162-clip-joint block 2;

[0023] 200-movable wing, 210-wing rod, 211-hollow rod, 212-hinge joint, 220-rotor;

[0024] 300-inspection component, 310-mounting bracket, 320-remote control adjustment bracket, 330-camera. DETAILED DESCRIPTION

[0025] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0026] See also Figures 1 to 4The utility model provides a technical solution: a photovoltaic product inspection device, comprising: a body 100, a movable wing 200 and an inspection component 300, wherein the left front side, the left rear side, the right front side and the right rear side of the body 100 are respectively hinged with a movable wing 200, and the lower side of the body 100 is equipped with an inspection component 300 for photovoltaic inspection;

[0027] The body 100 includes a bottom plate 110, a top plate 120 and a battery 130, a top plate 120 is fixed on the upper side of the top plate 120, and a battery 130 is installed in the middle of the upper surface of the top plate 120;

[0028] The movable wing 200 includes a wing rod 210 and a rotor 220 , and a rotor 220 is installed at the end of each wing rod 210 . The inspection component 300 includes a camera 330 and a remote control adjustment frame 320 , and a camera 330 is movably installed at the lower end of the remote control adjustment frame 320 .

[0029] See also Figures 1 to 4 A mounting frame 310 is installed on the upper end of the remote control adjustment frame 320, and the remote control adjustment frame 320 is fixed to the middle of the lower surface of the base plate 110 through the mounting frame 310. The camera 330 is movably installed below the middle of the base plate 110 through the remote control adjustment frame 320 and the mounting frame 310. A high-resolution camera 330 can be selected for the camera 330, and its specific model can be selected according to actual usage requirements. The camera 330 and the remote control adjustment frame 320 both use existing products on the market to meet usage requirements.

[0030] A support leg 140 is welded to the left and right sides of the lower surface of the bottom plate 110 , respectively. The height of the lowest end of the camera 330 is higher than the height of the lowest end of the support leg 140 . A mounting block 150 is fixed to the front and rear sides of the middle of the upper surface of the bottom plate 110 .

[0031] The left rear side and the right rear side of each mounting block 150 are damping hinged with a wing rod 210 near the front end of the fuselage 100, and a clamping member 160 is respectively installed on the left front side and the left rear side of the front end of the base plate 110, and a clamping member 160 is respectively installed on the right front side and the right rear side of the front end of the base plate 110.

[0032] Each of the clamping parts 160 is composed of a clamping block 161 and a clamping block 162. The distance between the clamping block 161 and the clamping block 162 in the clamping part 160 on the front side of the base plate 110 is greater than the distance between the clamping block 161 and the clamping block 162 in the clamping part 160 on the rear side of the base plate 110. In actual use, the parts where the clamping blocks 161, 162 and the hollow rod 211 are clamped will be deformed during the clamping. When the hollow rod 211 is fully clamped in, the deformation will be reset, so that the hollow rod 211 can be firmly clamped and will not fall off during flight.

[0033] The specifications of the clamping block 1 161 in each clamping member 160 are the same as those of the clamping block 2 162. A clamping groove 1 is provided on the side of the clamping block 161 close to the clamping block 2 162, and a clamping groove 2 is provided on the side of the clamping block 1 162 close to the clamping block 1 161. The specifications of the clamping groove 1 are the same as those of the clamping groove 2.

[0034] As the first embodiment of the utility model, in actual use, if it is in windless weather or when inspecting with the wind, the user can pry the wing rod 210 of the movable wing 200 to disengage the previously engaged clamping block 1 161 or clamping block 2 162, and clamp the wing rod 210 on the front side of the base plate 110 and the wing rod 210 on the rear side to the clamping groove 1 on the clamping block 1 161 in the corresponding clamping member 160 (the four clamping members 160 on the base plate 110 are distributed in an axially symmetrical structure, and the multiple clamping blocks 1 161 and clamping blocks 2 162 on the left and right sides of the base plate 110 are also distributed in an axially symmetrical structure). At this time, the four movable wings 200 are in the maximum open mode, When inspecting in windy weather or against the wind, the user moves the wing rod 210 of the movable wing 200, and engages the wing rod 210 on the front side and the wing rod 210 on the rear side of the base plate 110 with the corresponding engaging groove 2 on the engaging block 2 162 in the engaging member 160. At this time, the four movable wings 200 are in a folded mode, which can effectively reduce the wind resistance in a windy environment and ensure that the entire device can successfully complete the photovoltaic inspection task in windy weather or against the wind (the above-mentioned body 100 is adapted with a shell on the outside, and the shell will not cause movement interference to the adjustment of the movable wing 200, and the body 100 is equipped with corresponding electronic components. The above are all existing technologies and will not be repeated here).

[0035] See also Figures 1 to 3 The wing rod 210 includes a hollow rod 211 and a hinge joint 212. The hinge joint 212 is fixed to one side of the hollow rod 211 close to the mounting block 150. The hollow rod 211 is hinged to the rear side of the mounting block 150 through the hinge joint 212.

[0036] The diameter of the hollow rod 211 matches the size of the first clamping groove and the second clamping groove.

[0037] As the second embodiment of the utility model, based on the above-mentioned first embodiment, in actual use, since the end of the hollow rod 211 close to the mounting block 150 is hinged to the base plate 110 through the hinge joint 212, when it is necessary to adjust the opening degree of the movable wing 200, the movable hollow rod 211 helps the user to quickly adjust the position of the movable wing 200. Compared with the traditional fixed wing, it can select the wing opening degree according to the weather conditions, so that it can still perform normal inspection tasks in windy weather, thereby improving the flight stability of the entire device in windy weather.

[0038] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A photovoltaic product inspection device, comprising: A machine body (100), a movable wing (200), and an inspection component (300), characterized in that a movable wing (200) is hingedly connected to the left front side, the left rear side, the right front side, and the right rear side of the machine body (100), respectively, and an inspection component (300) for photovoltaic inspection is installed on the lower side of the machine body (100); The machine body (100) comprises a bottom plate (110), a top plate (120) and a battery (130); the top plate (120) is fixed on the upper side of the top plate (120); and the battery (130) is installed in the middle of the upper surface of the top plate (120); The movable wing (200) comprises a wing rod (210) and a rotor (220), and a rotor (220) is installed at the end of each wing rod (210). The inspection component (300) comprises a camera (330) and a remote control adjustment frame (320), and the camera (330) is movably installed at the lower end of the remote control adjustment frame (320).

2. A photovoltaic product inspection device as claimed in claim 1, characterized in that: The remote control adjustment frame (320) is provided with a mounting frame (310) at the upper end thereof; the remote control adjustment frame (320) is fixed to the middle of the lower surface of the bottom plate (110) via the mounting frame (310); and the camera (330) is movably mounted below the middle of the bottom plate (110) via the remote control adjustment frame (320) and the mounting frame (310).

3. A photovoltaic product inspection device as claimed in claim 2, characterized in that: A support leg (140) is welded to the left and right sides of the lower surface of the bottom plate (110), respectively; the height of the lowest end of the camera (330) is higher than the height of the lowest end of the support leg (140); and a mounting block (150) is fixed to the middle front and rear sides of the upper surface of the bottom plate (110), respectively.

4. A photovoltaic product inspection device as claimed in claim 3, characterized in that: The left rear side and the right rear side of each mounting block (150) are damping-hinged with a wing rod (210) close to the front end of the fuselage (100); a clamping piece (160) is respectively installed on the left front side and the left rear side of the front end of the base plate (110); and a clamping piece (160) is respectively installed on the right front side and the right rear side of the front end of the base plate (110).

5. A photovoltaic product inspection device as claimed in claim 4, characterized in that: Each of the clamping parts (160) is composed of a first clamping block (161) and a second clamping block (162), and the distance between the first clamping block (161) and the second clamping block (162) in the clamping part (160) on the front side of the base plate (110) is greater than the distance between the first clamping block (161) and the second clamping block (162) in the clamping part (160) on the rear side of the base plate (110).

6. A photovoltaic product inspection device as claimed in claim 5, characterized in that: The specifications of the first clamping block (161) in each of the clamping parts (160) are the same as those of the second clamping block (162); a first clamping groove is provided on a side of the first clamping block (161) close to the second clamping block (162); a second clamping groove is provided on a side of the second clamping block (162) close to the first clamping block (161); and the specifications of the first clamping groove are the same as those of the second clamping groove.

7. A photovoltaic product inspection device as claimed in claim 6, characterized in that: The wing rod (210) comprises a hollow rod (211) and a hinge joint (212); the hinge joint (212) is fixed to a side of the hollow rod (211) close to the mounting block (150); The hollow rod (211) is damping-hinged with the rear side of the mounting block (150) via a hinge joint (212); the diameter of the hollow rod (211) matches the size of the first clamping groove and the second clamping groove.

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