Rapid balance loading mechanism for photovoltaic module transportation of unmanned aerial vehicle

Abstract

The utility model belongs to the technical field of photovoltaic assembly transportation, and particularly relates to a rapid balance loading mechanism for photovoltaic assembly transportation of an unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, the bottom end of the unmanned aerial vehicle main body is fixedly connected with an upper clamping plate through four nylon ropes, and a lower box body is arranged below the upper clamping plate. The lower box body is used for placing a photovoltaic module, the outer wall of the lower box body is provided with a hanging assembly, the hanging assembly comprises four groups of connecting ropes and two sliding tables, one end of each connecting rope is fixedly connected with the outer wall of the lower box body, and the other end of each connecting rope is fixedly connected with a clamping ring; the upper clamping plate covers the top end of the lower box body, the clamping ring is connected with the clamping hook, and the connecting rope is pulled through the sliding table to keep tight, so that the upper clamping plate and the lower box body are rapidly connected, the unmanned aerial vehicle body transports the photovoltaic module by hoisting the lower box body, and meanwhile the photovoltaic module in the lower box body is prevented from falling off through the upper clamping plate.

Description

TECHNICAL FIELD

[0001] The utility model relates to transport photovoltaic module transportation technical field, concretely is a kind of quick balance load mechanism for unmanned aerial vehicle transport photovoltaic module. BACKGROUND

[0002] Mountain photovoltaic power station component installation, due to the restriction of mountain terrain slope, also need to meet the time limit and efficiency demand, will use improved version unmanned aerial vehicle for installation operation photovoltaic module transport.

[0003] But photovoltaic module is hung on unmanned aerial vehicle and is transported, because of wind speed change, air turbulence, terrain undulation, temperature gradient and other factors, the stability, balance, safety of the photovoltaic module hung are significantly influenced;Therefore, aiming at the above problems, a kind of quick balance load mechanism for unmanned aerial vehicle transport photovoltaic module is provided. UTILITY MODEL CONTENTS

[0004] In order to make up for the deficiency of prior art, solve the technical problems proposed above, the utility model provides a kind of quick balance load mechanism for unmanned aerial vehicle transport photovoltaic module.

[0005] The utility model discloses a kind of quick balance load mechanisms for unmanned aerial vehicle transport photovoltaic module, including unmanned aerial vehicle main body, the bottom of the unmanned aerial vehicle main body is fixedly connected with upper clamping plate by four nylon ropes, the lower box body is installed in the lower of the upper clamping plate, the lower box body is used to place photovoltaic module, the outer wall of the lower box body is installed with hanging component, the hanging component includes four groups of connecting ropes and two sliding platforms, the outer wall of the lower box body is fixedly connected with the one end of connecting rope, and the other end of connecting rope is fixedly connected with snap ring, two the sliding platform is slidably installed on the upper surface of upper clamping plate, the center of two the sliding platform is threadedly connected with two-way screw rod, the two-way screw rod is penetrated and is rotationally connected with upper clamping plate, the sidewall of the upper clamping plate is fixedly connected with driver, and the driving end of driver is fixedly connected with the one end of two-way screw rod, the upper surface of the sliding platform is fixedly connected with two clamping hooks.

[0006] Preferably, the lower box body includes L-shaped support main body, L-shaped side baffle is arranged on the both sides of the support main body respectively, a plurality of support columns are fixedly connected to the bottom end of the side baffle, and the other end of the support column is penetrated into the inside of the support main body.

[0007] Preferably, the bottom end of the side baffle is higher than the bottom end of the support main body, the sidewall of the side baffle is fixedly connected with telescopic limiting rod, and the other end of the telescopic limiting rod is fixedly connected with the support main body.

[0008] Preferably, one end of the side baffle is fixedly connected with convex layer.

[0009] Preferably, the lower box body and the upper clamping plate are respectively provided with an opening for reducing weight.

[0010] Preferably, the upper clamping plate is provided with a pressing assembly, the pressing assembly comprises two grooves provided on the surface of the upper clamping plate, and the two sides of the grooves are respectively connected with a pressing frame through a shaft.

[0011] Preferably, a top plate is arranged above the pressing frame, the center of the top plate is fixedly connected with an electric push rod, and the bottom end of the electric push rod is fixedly connected with the upper clamping plate.

[0012] Preferably, the lower surface of the top plate is rotatably connected with four groups of connecting rods through a shaft, and the bottom end of the connecting rod is rotatably connected with the pressing frame through a shaft.

[0013] The utility model discloses the beneficial effect lies in:

[0014] 1. The utility model discloses a lower box body is transported photovoltaic module through the hoisting, and the photovoltaic module in the lower box body is prevented from falling through the upper clamping plate, reaches the purpose that photovoltaic module is transported fast, stably and safely, thereby speeds up the construction progress of photovoltaic installation, reduces photovoltaic module damage, improves the security when photovoltaic module is transported.

[0015] 2. The utility model discloses the bottom end of pressing frame is driven to resist the top end of the uppermost photovoltaic module through the electric push rod contraction, thereby carries out the top limiting to the photovoltaic module in the lower box body, prevents the photovoltaic module in the lower box body from shaking too big range and causing damage. DRAWINGS

[0016] In order to more clearly illustrate the technical scheme in the embodiment of the utility model or prior art, the following will briefly introduce the drawing needed to be used in the embodiment or prior art description, obviously, the drawing in the following description only is some embodiments of the utility model, for ordinary skilled person in the art, under the premise of not paying the creative labor, still can obtain other drawings according to these drawings.

[0017] Figure 1 It is the whole structure schematic diagram of the utility model;

[0018] Figure 2 It is the upper clamping plate and lower box body structure schematic diagram of the utility model;

[0019] Figure 3 It is the mounting assembly structure schematic diagram of the utility model;

[0020] Figure 4The utility model discloses a lower box body structure schematic diagram.

[0021] Figure 5 The utility model discloses a compression assembly structure schematic diagram.

[0022] In the drawing: 1, unmanned plane main body, 2, upper clamping plate, 3, lower box body, 31, support main body, 32, side baffle, 33, support column, 34, telescopic limit rod, 36, protruding layer, 4, mounting assembly, 41, connecting rope, 42, sliding table, 43, two -way screw rod, 44, clamping hook, 45, snap ring, 5, driver, 7, compression assembly, 71, slot, 72, compression frame, 73, top plate, 74, electric push rod, 75, connecting rod. DETAILED DESCRIPTION

[0023] The technical scheme in the embodiments of the utility model will be apparently and completely described below with the drawings in the embodiments of the utility model, and apparently, the described embodiments are only a part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by the ordinary skill in the art without making creative labor belong to the range of protection of the utility model.

[0024] Embodiment one

[0025] Please refer to Figures 1-4 As shown in the drawing, a kind of quick balance load mechanism for unmanned plane transport photovoltaic module, including unmanned plane main body 1, the bottom end of unmanned plane main body 1 is fixedly connected with upper clamping plate 2 by four nylon ropes, and upper clamping plate 2 is installed with lower box body 3 below, and lower box body 3 is used to place photovoltaic module, and mounting assembly 4 is installed on the outer wall of lower box body 3, and mounting assembly 4 includes four groups of connecting ropes 41 and two sliding tables 42, one end of connecting rope 41 is fixedly connected with the outer wall of lower box body 3, and the other end of connecting rope 41 is fixedly connected with snap ring 45, two sliding tables 42 are slidably installed on the upper surface of upper clamping plate 2, two -way screw rod 43 is screw-connected at the center of two sliding tables 42, and two -way screw rod 43 is connected with upper clamping plate 2 rotationally, the side wall of upper clamping plate 2 is fixedly connected with driver 5, and the driving end of driver 5 is fixedly connected with one end of two -way screw rod 43, the upper surface of sliding table 42 is fixedly connected with two clamping hooks 44 symmetrically, the size of the internal space of lower box body 3 is consistent with the size of photovoltaic module, and driver 5 is electrically connected with the control system of unmanned plane main body 1.

[0026] Specifically, the two sliding platforms 42 slide to the two sides of the upper clamping plate 2, thereby reducing the distance between the clamping hooks 44 and the clamping rings 45, facilitating the connection of the two, and placing the photovoltaic modules in the lower box body 3. The unmanned aerial vehicle body 1 takes off and lifts the upper clamping plate 2, then the upper clamping plate 2 is covered on the top of the lower box body 3, and then the clamping ring 45 is placed in the corresponding clamping hook 44. After the placement is completed, the operation of the driver 5 drives the rotation of the bidirectional screw rod 43, and the bidirectional screw rod 43 drives the synchronous opposite sliding of the two sliding platforms 42. The sliding of the sliding platform 42 drives the sliding of the clamping hook 44, the clamping hook 44 drives the movement of the clamping ring 45, the clamping ring 45 moves upward to tighten the connecting rope 41, until the connecting rope 41 is kept tight, thereby quickly connecting the upper clamping plate 2 and the lower box body 3, so that the unmanned aerial vehicle body 1 transports the photovoltaic modules by lifting the lower box body 3, and at the same time, the photovoltaic modules in the lower box body 3 are prevented from falling by the upper clamping plate 2, achieving the purpose of quickly, stably and safely transporting the photovoltaic modules, thereby speeding up the construction progress of photovoltaic installation, reducing the damage of photovoltaic modules, and improving the safety of photovoltaic module transportation.

[0027] The lower box body 3 comprises an L-shaped support body 31, and L-shaped side plates 32 are arranged on the two sides of the support body 31 respectively. A plurality of support columns 33 are fixedly connected to the bottom end of the side plates 32, and the other ends of the support columns 33 penetrate into the inside of the support body 31. The bottom end of the side plate 32 is higher than the bottom end of the support body 31. The side wall of the side plate 32 is fixedly connected with a telescopic limiting rod 34, and the other end of the telescopic limiting rod 34 is fixedly connected with the support body 31. The telescopic range of the telescopic limiting rod 34 is smaller than the length of the support column 33.

[0028] Specifically, the telescopic limiting rod 34 limits the outward sliding distance of the side plate 32, so as to avoid the disconnection of the side plate 32 and the support body 31. The support column 33 is used to slidably connect the support body 31 and the side plate 32. When carrying the photovoltaic modules, the side plate 32 is pulled outward to increase the space inside the lower box body 3, so as to facilitate the construction personnel to carry the photovoltaic modules. When lifting, the side plate 32 is pushed inward to close the side plate 32 and the support body 31. The upper clamping plate 2 is covered on the lower box body 3 to limit the side plate 32, so as to prevent the side plate 32 from sliding open during transportation, thereby achieving the effect of automatically fixing the side plate 32.

[0029] One end of the side plate 32 is fixedly connected with a protruding layer 36.

[0030] Specifically, the protruding layer 36 is used to laterally limit the photovoltaic modules to prevent the photovoltaic modules from falling.

[0031] The surfaces of the lower box body 3 and the upper clamping plate 2 are respectively provided with openings, which are used to reduce the weight.

[0032] Example two

[0033] For comparison with example one, please refer toFigure 5 As shown, the utility model provides another embodiment, the surface of upper clamping plate 2 is equipped with compression assembly 7, compression assembly 7 includes two slot 71, slot 71 is equipped in the surface of upper clamping plate 2, the both sides of slot 71 are connected with compression frame 72 through shaft rotation respectively, the top of compression frame 72 is installed with top plate 73, the center of top plate 73 is fixedly connected with electric push rod 74, the bottom end of electric push rod 74 is fixedly connected with upper clamping plate 2, the lower surface of top plate 73 is connected with four groups of connecting rods 75 through shaft rotation, the bottom end of connecting rod 75 is connected with compression frame 72 through shaft rotation, electric push rod 74 is electrically connected with the control system of unmanned aerial vehicle main body 1.

[0034] Specifically, after upper clamping plate 2 is connected with lower box body 3, electric push rod 74 is controlled to retract through the remote controller of unmanned aerial vehicle, electric push rod 74 retraction drives top plate 73 to descend, top plate 73 descends drive connecting rod 75 to move downwards, connecting rod 75 moves downwards and pushes compression frame 72 to rotate downwards, until the bottom end of compression frame 72 abuts against the top end of the uppermost photovoltaic module, thereby limiting the top of photovoltaic module inside lower box body 3, preventing photovoltaic module inside lower box body 3 from being damaged due to excessive shaking amplitude.

[0035] The parts not involved in the device are the same as or can be realized by the prior art.

[0036] Working principle, photovoltaic module is placed in the inside of lower box body 3, upper clamping plate 2 is lifted by unmanned aerial vehicle main body 1, then upper clamping plate 2 is covered on the top end of lower box body 3, then snap ring 45 is placed in the inside of corresponding hook 44, after placement, drive 5 is controlled to run through the remote controller of unmanned aerial vehicle, drive 5 drives bidirectional screw rod 43 to rotate, bidirectional screw rod 43 drives two sliding tables 42 to slide synchronously, sliding table 42 slides and drives hook 44 to slide, hook 44 drives snap ring 45 to move, snap ring 45 moves and tightens connecting rope 41 upwards, until connecting rope 41 keeps tight, thereby quickly connecting upper clamping plate 2 and lower box body 3, so that unmanned aerial vehicle main body 1 transports photovoltaic module by lifting lower box body 3, and photovoltaic module inside lower box body 3 is prevented from falling by upper clamping plate 2, so that the purpose of quickly, stably and safely transporting photovoltaic module is achieved, thereby speeding up the construction progress of photovoltaic installation, reducing photovoltaic module damage, and improving the safety of photovoltaic module transportation.

[0037] The outer sliding distance of the side baffle 32 is limited by the telescopic limiting rod 34, avoiding the disconnection of the side baffle 32 and the support body 31, and the support body 31 and the side baffle 32 are slidably connected through the support column 33; when carrying the photovoltaic module, the side baffle 32 is pulled outward, the space inside the lower box body 3 is increased, the photovoltaic module is conveniently carried by the construction personnel, when hoisting, the side baffle 32 is pushed inward, the side baffle 32 is closed with the support body 31, the side baffle 32 is limited by covering the upper clamping plate 2 on the lower box body 3, the side baffle 32 is prevented from sliding and opening during transportation, and the effect of automatically fixing the side baffle 32 is achieved.

[0038] After the upper clamping plate 2 is connected with the lower box body 3, the electric push rod 74 is controlled to shrink through the remote controller of the unmanned aerial vehicle, the electric push rod 74 is driven to shrink and the top plate 73 is lowered, the top plate 73 is driven to lower and the connecting rod 75 is moved downward, the connecting rod 75 is driven to move downward and the pressing frame 72 is rotated downward until the bottom end of the pressing frame 72 abuts against the top end of the uppermost photovoltaic module, so that the photovoltaic module in the lower box body 3 is limited at the top, and the photovoltaic module in the lower box body 3 is prevented from being damaged due to too large shaking amplitude.

[0039] In the description of the present specification, the description of the terms "one embodiment", "example", "specific example" and the like means that the specific features, structures, materials or characteristics described in combination with the embodiment or example are contained in at least one embodiment or example of the present application. In the present specification, the illustrative description of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0040] The basic principles, main features and advantages of the present application are shown and described above. It should be understood by those skilled in the art that the present application is not limited by the above embodiments, and the above embodiments and descriptions in the specification are only to illustrate the principles of the present application. Without departing from the spirit and scope of the present application, various changes and improvements can be made to the present application, and these changes and improvements all fall within the scope of the claimed present application.

Claims

1. A quick balancing load mechanism for unmanned aerial vehicle transportation of photovoltaic modules comprising of an unmanned aerial vehicle body (1) characterized by: The bottom end of the unmanned aerial vehicle body (1) is fixedly connected with an upper clamping plate (2) through four nylon ropes, a lower box body (3) is installed below the upper clamping plate (2), the lower box body (3) is used for placing a photovoltaic module, a mounting assembly (4) is installed on the outer wall of the lower box body (3), the mounting assembly (4) comprises four groups of connecting ropes (41) and two sliding tables (42), one end of the connecting rope (41) is fixedly connected with the outer wall of the lower box body (3), and the other end of the connecting rope (41) is fixedly connected with a snap ring (45), the two sliding tables (42) are slidingly installed on the upper surface of the upper clamping plate (2), a bidirectional lead screw (43) is threadedly connected at the center of the two sliding tables (42), the bidirectional lead screw (43) penetrates and is rotationally connected with the upper clamping plate (2), a drive (5) is fixedly connected with the side wall of the upper clamping plate (2), and the driving end of the drive (5) is fixedly connected with one end of the bidirectional lead screw (43), two clamping hooks (44) are fixedly connected on the upper surface of the sliding table (42) in a symmetrical manner.

2. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 1, wherein: The lower box body (3) comprises an L-shaped support body (31), L-shaped side baffles (32) are arranged on the two sides of the support body (31) respectively, a plurality of support columns (33) are fixedly connected to the bottom end of the side baffle (32), and the other end of the support column (33) penetrates into the inside of the support body (31).

3. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 2, wherein: The bottom end of the side baffle (32) is higher than the bottom end of the support body (31), the side wall of the side baffle (32) is fixedly connected with a telescopic limiting rod (34), and the other end of the telescopic limiting rod (34) is fixedly connected with the support body (31).

4. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 2, wherein: One end of the side baffle (32) is fixedly connected with a convex layer (36).

5. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 2, wherein: The surfaces of the lower box body (3) and the upper clamping plate (2) are respectively provided with openings, and the openings are used to reduce the weight.

6. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 1, wherein: A pressing assembly (7) is arranged on the surface of the upper clamping plate (2), the pressing assembly (7) comprises two grooves (71), the grooves (71) are arranged on the surface of the upper clamping plate (2), and pressing frames (72) are rotationally connected to the two sides of the groove (71) through shafts.

7. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 6, wherein: A top plate (73) is installed above the pressing frame (72), an electric push rod (74) is fixedly connected to the center of the top plate (73), and the bottom end of the electric push rod (74) is fixedly connected with the upper clamping plate (2).

8. The quick balancing payload mechanism for drone transportation of photovoltaic modules of claim 7, wherein: Four groups of connecting rods (75) are rotationally connected to the bottom end of the pressing frame (72) through shafts.

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