Unmanned aerial vehicle hoisting photovoltaic module

Abstract

The utility model relates to the technical field of photovoltaic assembly hoisting, in particular to an unmanned aerial vehicle hoisting photovoltaic assembly, which comprises an unmanned aerial vehicle, the unmanned aerial vehicle comprises a vehicle body, the outer surface of the unmanned aerial vehicle is fixedly connected with a clamping device, the clamping device comprises a fixing plate, the inner surface of the fixing plate is movably connected with a rotating disc, and the rotating disc is fixedly connected with a rotating shaft. A rotating groove is formed in the outer surface of the rotating disc, a connecting piece is fixedly connected to the inner surface of the rotating disc, and a servo motor is fixedly connected to the outer surface of the connecting piece. Through the arrangement of the rotating disc and the clamping jaw, the servo motor is started, the clamping jaw can clamp inwards under the pushing of the servo motor, and the position of the clamping jaw is positioned through the driving of the servo motor, so that the clamping jaw can clamp inwards, and the clamping jaw can clamp inwards. Therefore, the clamping jaw can be effectively prevented from loosening in the long-time use process, and falling and damage of the photovoltaic device in the hoisting process can be effectively avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of photovoltaic component hoisting, in particular to a method for unmanned aerial vehicle hoisting photovoltaic components. Background Art

[0002] Drone transportation is easy to operate, has a fast flight speed, and is not affected by terrain. It effectively solves the problems of difficult material transportation and low labor efficiency in mountain photovoltaic construction, greatly improves work efficiency and reduces labor costs. It is a commonly used and effective means of transportation for mountain photovoltaic project construction.

[0003] The Chinese utility model patent with the authorization announcement number CN220640216U discloses a drone lifting bracket for photovoltaic modules, including a frame, a bottom plate, a cover plate and an adjustment device, wherein the top surface of the frame is provided with a plurality of hanging ears; the bottom plate is fixed to the bottom of the frame for receiving photovoltaic modules; the cover plate is movably connected to the top surface of the frame; the adjustment device includes a push plate and an elastic component, wherein the push plate is arranged on the bottom plate, and the side away from the frame fits the photovoltaic module; one end of the elastic component is connected to the inner side of the frame, and the other end is connected to the side of the push plate close to the frame, generating thrust to the push plate. The utility model has a simple structure and is easy to use. It can be used to lift photovoltaic modules of different sizes through the adjustment device. While ensuring the weight of the lifting bracket, it can also lift the photovoltaic modules horizontally, so that the photovoltaic modules are evenly stressed, which can effectively reduce the probability of hidden cracks and has great promotion value.

[0004] Although the above-mentioned prior art solution is suitable for lifting photovoltaic modules of different sizes through an adjusting device, and can lift the photovoltaic modules horizontally while ensuring the weight of the lifting bracket, so that the photovoltaic modules are evenly stressed, this device uses a frame, a base plate, a cover plate and an adjusting device to fix the photovoltaic modules. However, after long-term use, the built-in elastic components will continue to relax, and thus the optimal clamping and fixing effects cannot be achieved, which makes it very easy for the drone to fall off during the lifting process, resulting in unnecessary losses. Therefore, it is urgent to design a method for lifting photovoltaic modules by drones to solve the above problems. Utility Model Content

[0005] The purpose of the utility model is to provide a method for lifting photovoltaic components by drones, so as to solve the problem that the device proposed in the above background technology adopts a frame, a bottom plate, a cover plate and an adjustment device to fix the photovoltaic components, but after long-term use, the built-in elastic components will continue to relax, thereby failing to achieve the best clamping and fixing effects, which can easily cause the drone to fall off during the lifting process, resulting in unnecessary losses.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical solution, a method for lifting photovoltaic modules by a drone, comprising: a drone, the drone comprising a body, the outer surface of the drone being fixedly connected with a clamping device;

[0007] The clamping device comprises a fixed plate, the inner surface of the fixed plate is movably connected with a rotating disk, the outer surface of the rotating disk is provided with a rotating groove, the inner surface of the rotating disk is fixedly connected with a connecting piece, the outer surface of the connecting piece is fixedly connected with a servo motor, the outer surface of the rotating disk is movably connected with a pushing rod, the outer surface of the pushing rod is fixedly connected with a sliding block, the outer surface of the sliding block is fixedly connected with a limiting plate, the outer surface of the limiting plate is fixedly connected with a clamping claw, the outer surface of the clamping claw is provided with a tooth plate, the outer surface of the sliding block is movably connected with a protective plate, the outer surface of the protective plate is movably connected with a fixing bolt, the outer surface of the protective plate is provided with a first guide groove, and the outer surface of the protective plate is fixedly connected with an adjusting device;

[0008] The adjusting device comprises a bottom plate.

[0009] Preferably, the fixed plate is fixedly connected to the bottom of the fuselage, the rotating disk is rotatably connected to the inside of the fixed plate, and the rotating groove is opened through the upper and lower ends of the rotating disk.

[0010] Preferably, one end of the connecting member is fixedly connected to the inner wall of the rotating disk, and the other end of the connecting member is sleeved on the output end of the servo motor, and the servo motor is arranged inside the fuselage.

[0011] Preferably, the protective plate is fixedly connected to the upper surface of the fixing plate, the fixing bolt penetrates and is connected to the upper surface of the protective plate, and the protective plate is fixedly connected to the upper surface of the rotating disk.

[0012] Preferably, the push rod is fixedly connected to the bottom of the sliding block, the sliding block is slidably connected inside the first guide groove, and the sliding block is fixedly connected between the push rod and the limiting plate.

[0013] Preferably, the tooth plate is arranged on the inner side of the clamping claws, the clamping claws are arranged in three groups on the upper surface of the protective plate, and the first guide groove is opened through the upper surface of the protective plate.

[0014] Preferably, a second guide groove is provided on the outer surface of the base plate, a sliding groove is provided on the outer surface of the second guide groove, a protective ring is movably connected to the outer surface of the second guide groove, a rotating rod is rotatably connected to the inside of the protective ring, a fixed cylinder is fixedly connected to the outer surface of the rotating rod, a connecting rod is fixedly connected to the outer surface of the fixed cylinder, and a hook is movably connected to the outer surface of the connecting rod.

[0015] Preferably, the hook is rotatably connected to an end of the connecting rod away from the fixing tube, the protective ring is slidably connected to the outer surface of the second guide groove, and the rotating rod is movably connected to the inner side of the sliding groove.

[0016] Compared with the prior art, the beneficial effects of the utility model are:

[0017] By setting the rotating disk and the clamping claw, the servo motor is started. Under the push of the servo motor, the clamping claw can be clamped inward, and the position of the clamping claw is positioned by the drive of the servo motor, thereby effectively preventing the clamping claw from loosening during long-term use, causing the photovoltaic to fall off and be damaged during lifting.

[0018] Through the arrangement of the base plate and the hook, when the clamping claw is clamping, the connecting rod can be rotated from the inside of the base plate, and the hook can be hooked on the packing rope for lifting photovoltaics, which can play a protective role. Even when the clamping claw is loose, the hook will promptly ensure the stability of the photovoltaics. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of a three-dimensional front view of the structure of the utility model;

[0020] Figure 2 It is a three-dimensional schematic diagram of the partial connection structure of the fixing plate and the protective plate of the utility model;

[0021] Figure 3 It is a three-dimensional schematic diagram of the partial connection structure of the protective plate and the clamping claw of the utility model;

[0022] Figure 4 It is a three-dimensional schematic diagram of the partial connection structure of the bottom plate and the connecting rod of the utility model.

[0023] In the figure: 1. UAV; 11. Fuselage; 2. Clamping device; 21. Fixed plate; 22. Rotating disk; 23. Rotating groove; 24. Connecting piece; 25. Servo motor; 26. Push rod; 27. Sliding block; 28. Limiting plate; 29. ​​Clamping claw; 210. Tooth plate; 211. Protective plate; 212. Fixing bolt; 213. First guide groove; 3. Adjusting device; 31. Bottom plate; 32. Second guide groove; 33. Slide groove; 34. Protective ring; 35. Rotating rod; 36. Fixed cylinder; 37. Connecting rod; 38. Hook. DETAILED DESCRIPTION

[0024] 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 in 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.

[0025] See also Figure 1-4 The utility model provides an embodiment: a method for lifting photovoltaic modules by drone, comprising: a drone 1, the drone 1 comprising a body 11, and a clamping device 2 is fixedly connected to the outer surface of the drone 1;

[0026] The clamping device 2 includes a fixed plate 21, the inner surface of the fixed plate 21 is movably connected with a rotating disk 22, the outer surface of the rotating disk 22 is provided with a rotating groove 23, the inner surface of the rotating disk 22 is fixedly connected with a connecting piece 24, the outer surface of the connecting piece 24 is fixedly connected with a servo motor 25, the outer surface of the rotating disk 22 is movably connected with a push rod 26, the outer surface of the push rod 26 is fixedly connected with a sliding block 27, the outer surface of the sliding block 27 is fixedly connected with a limit plate 28, the outer surface of the limit plate 28 is fixedly connected with a clamping claw 29, the outer surface of the clamping claw 29 is provided with a tooth plate 210, the outer surface of the sliding block 27 is movably connected with a protective plate 211, the outer surface of the protective plate 211 is movably connected with a fixing bolt 212, the outer surface of the protective plate 211 is provided with a first guide groove 213, and the outer surface of the protective plate 211 is fixedly connected with an adjusting device 3;

[0027] The adjusting device 3 comprises a bottom plate 31 .

[0028] Furthermore, the fixed plate 21 is fixedly connected to the bottom of the fuselage 11, the rotating disk 22 is rotatably connected to the inside of the fixed plate 21, and the rotating groove 23 is opened through the upper and lower ends of the rotating disk 22. Through the setting of the fixed plate 21, the clamping device 2 can be fixedly connected to the bottom of the fuselage 11, thereby playing the role of a fixing device, effectively improving the stability of the device.

[0029] Furthermore, one end of the connecting member 24 is fixedly connected to the inner wall of the rotating disk 22, and the other end of the connecting member 24 is sleeved on the output end of the servo motor 25. The servo motor 25 is arranged inside the fuselage 11. Through the setting of the servo motor 25, under the rotation of the servo motor 25, the rotating disk 22 can push the pushing rod 26 to produce displacement, so that the clamping claw 29 forms a clamp.

[0030] Furthermore, the protective plate 211 is fixedly connected to the upper surface of the fixed plate 21, the fixing bolt 212 penetrates and is connected to the upper surface of the protective plate 211, the protective plate 211 is fixedly connected to the upper surface of the rotating disk 22, and through the setting of the fixing bolt 212, the fixing bolt 212 is fixedly connected to the protective plate 211 and the fixed plate 21, and the rotating disk 22 is rotatably connected between the protective plate 211 and the fixed plate 21.

[0031] Furthermore, the pushing rod 26 is fixedly connected to the bottom of the sliding block 27, the sliding block 27 is slidably connected to the inside of the first guide groove 213, the sliding block 27 is fixedly connected between the pushing rod 26 and the limiting plate 28, and through the setting of the pushing rod 26, the pushing rod 26 is movably connected to the inner side of the rotating groove 23. Under the rotation of the rotating disk 22, the pushing rod 26 can push the clamping claw 29 to produce displacement.

[0032] Furthermore, the tooth plate 210 is arranged on the inner side of the clamping claw 29, and the clamping claw 29 is arranged in three groups on the upper surface of the protective plate 211. The first guide groove 213 is opened through the upper surface of the protective plate 211. Through the setting of the first guide groove 213, it can effectively play a guiding role when the clamping claw 29 is displaced.

[0033] Furthermore, a second guide groove 32 is formed on the outer surface of the base plate 31, a sliding groove 33 is provided on the outer surface of the second guide groove 32, a protective ring 34 is movably connected to the outer surface of the second guide groove 32, a rotating rod 35 is rotatably connected to the inside of the protective ring 34, a fixed cylinder 36 is fixedly connected to the outer surface of the rotating rod 35, a connecting rod 37 is fixedly connected to the outer surface of the fixing cylinder 36, and a hook 38 is movably connected to the outer surface of the connecting rod 37. The second guide groove 32 can play a guiding role during the sliding of the connecting rod 37, thereby effectively improving the stability of the device.

[0034] Furthermore, the hook 38 is rotatably connected to one end of the connecting rod 37 away from the fixed tube 36, the protective ring 34 is slidably connected to the outer surface of the second guide groove 32, and the rotating rod 35 is movably connected to the inner side of the slide groove 33. Through the setting of the protective ring 34, it can play a limiting role during the sliding process of the connecting rod 37, thereby avoiding the disconnection of the connecting rod 37 during the sliding process, thereby effectively improving the practicability of the device.

[0035] Working principle: During use, when the photovoltaic needs to be lifted, the drone 1 is stopped above the photovoltaic, and the servo motor 25 is started. The servo motor 25 drives the rotating disk 22 to rotate. During the rotation of the rotating disk 22, the push rod 26 movably connected to the inside of the rotating groove 23 will be pushed by the rotating disk 22, and the push rod 26 will push the clamping claw 29 to slide on the inside of the first guide groove 213, so that the clamping claw 29 clamps inward. Under the action of the tooth plate 210, it can effectively play a role in anti-slip and enhanced friction. Conversely, reversing the servo motor 25 can make the clamping claw 29 slide outward, so that the clamping claw 29 releases the clamped photovoltaic.

[0036] Rotate the connecting rod 37 and turn it out from the inner side of the second guide groove 32. Connect the hook 38 and the connecting rod 37 by threaded rotation. Hook the hook 38 on the photovoltaic packing rope, which can effectively enhance the stability of the photovoltaic during the lifting process. The rotating rod 35 can drive the connecting rod 37 to slide in the slide groove 33, so that the position of the connecting rod 37 can be slidably adjusted to adapt to the connection at different positions.

[0037] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

Claims

1. A method for lifting photovoltaic modules by drone, comprising: An unmanned aerial vehicle (1), characterized in that the unmanned aerial vehicle (1) comprises a body (11), and a clamping device (2) is fixedly connected to an outer surface of the unmanned aerial vehicle (1); The clamping device (2) comprises a fixed plate (21), the inner surface of the fixed plate (21) is movably connected to a rotating disk (22), the outer surface of the rotating disk (22) is provided with a rotating groove (23), the inner surface of the rotating disk (22) is fixedly connected to a connecting piece (24), the outer surface of the connecting piece (24) is fixedly connected to a servo motor (25), the outer surface of the rotating disk (22) is movably connected to a push rod (26), the outer surface of the push rod (26) is fixedly connected to a sliding block (27), and the The outer surface of the sliding block (27) is fixedly connected to a limit plate (28), the outer surface of the limit plate (28) is fixedly connected to a clamping claw (29), the outer surface of the clamping claw (29) is provided with a tooth plate (210), the outer surface of the sliding block (27) is movably connected to a protective plate (211), the outer surface of the protective plate (211) is movably connected to a fixing bolt (212), the outer surface of the protective plate (211) is provided with a first guide groove (213), and the outer surface of the protective plate (211) is fixedly connected to an adjustment device (3); An adjusting device (3), wherein the adjusting device (3) comprises a bottom plate (31).

2. The method for lifting photovoltaic modules by drone according to claim 1, characterized in that: The fixed plate (21) is fixedly connected to the bottom of the body (11), the rotating disk (22) is rotatably connected to the inside of the fixed plate (21), and the rotating groove (23) is opened through the upper and lower ends of the rotating disk (22).

3. The method for lifting photovoltaic modules by drone according to claim 1, characterized in that: One end of the connecting member (24) is fixedly connected to the inner wall of the rotating disk (22), and the other end of the connecting member (24) is sleeved on the output end of the servo motor (25), and the servo motor (25) is arranged inside the machine body (11).

4. The method for lifting photovoltaic modules by drone according to claim 1, characterized in that: The protective plate (211) is fixedly connected to the upper surface of the fixing plate (21), the fixing bolt (212) penetrates and is connected to the upper surface of the protective plate (211), and the protective plate (211) is fixedly connected to the upper surface of the rotating disk (22).

5. The method for lifting photovoltaic modules by drone according to claim 1, characterized in that: The push rod (26) is fixedly connected to the bottom of the sliding block (27), the sliding block (27) is slidably connected inside the first guide groove (213), and the sliding block (27) is fixedly connected between the push rod (26) and the limiting plate (28).

6. The method for lifting photovoltaic modules by drone according to claim 1, characterized in that: The tooth plate (210) is arranged on the inner side of the clamping claw (29), the clamping claw (29) is arranged in three groups on the upper surface of the protective plate (211), and the first guide groove (213) is opened through the upper surface of the protective plate (211).

7. The method for lifting photovoltaic modules by drone according to claim 6, characterized in that: The outer surface of the bottom plate (31) is provided with a second guide groove (32), the outer surface of the second guide groove (32) is provided with a slide groove (33), the outer surface of the second guide groove (32) is movably connected to a protective ring (34), the interior of the protective ring (34) is rotatably connected to a rotating rod (35), the outer surface of the rotating rod (35) is fixedly connected to a fixing cylinder (36), the outer surface of the fixing cylinder (36) is fixedly connected to a connecting rod (37), and the outer surface of the connecting rod (37) is movably connected to a hook (38).

8. The method for lifting photovoltaic modules by drone according to claim 7, characterized in that: The hook (38) is rotatably connected to an end of the connecting rod (37) away from the fixing tube (36), the protective ring (34) is slidably connected to the outer surface of the second guide groove (32), and the rotating rod (35) is movably connected to the inner side of the sliding groove (33).

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