CN219535980U

CN219535980U - Solar power panel span control mechanism

Info

Publication number: CN219535980U
Application number: CN202320492990.XU
Authority: CN
Inventors: 徐秋华
Original assignee: Tuanche Internet Information Service Beijing Co ltd
Current assignee: Tuanche Internet Information Service Beijing Co ltd
Priority date: 2023-03-15
Filing date: 2023-03-15
Publication date: 2023-08-15
Anticipated expiration: 2033-03-15

Abstract

The utility model provides a solar power panel span control mechanism, comprising: the utility model has the beneficial effects that compared with the prior art, the electric support device has the following beneficial effects that: through setting up pushing mechanism, can be convenient for open or withdraw span main part, operation process is simple and convenient and labour saving and time saving, can reduce artifical intensity of labour, through setting up lifter, fixture block and draw-in groove, when the span main part is withdrawn, the fixture block can block into the draw-in groove, can make the span main part be difficult for removing after withdrawing, promotes the stability after the span main part is withdrawn.

Description

Solar power panel span control mechanism

Technical Field

The utility model belongs to the technical field of solar power panel wingspan, and particularly relates to a solar power panel wingspan control mechanism.

Background

Solar energy, which is a renewable energy source, refers to thermal radiation energy of the sun, and is mainly represented by solar rays, and is generally used as power generation or energy source for solar automobiles in modern times.

The solar power panel span is formed by combining the solar battery panel and the span, and is generally arranged at the top of a solar automobile, so that the paving area of the solar battery panel can be increased.

The span of the solar power panel is that solar radiation energy is directly converted into electric energy by utilizing the photoelectric effect, and a basic device of photoelectric conversion is a solar cell. The solar cell is a device for directly converting solar energy into electric energy due to photovoltaic effect, but when the solar cell is arranged above a solar car, the solar power panel span in the prior art is often required to be manually opened, the solar cell is required to be manually retracted when the solar cell is required to be retracted, the operation process is complicated, the labor intensity of workers is improved, the opening and the retraction processes are time-consuming, the working efficiency is influenced, and therefore, the solar power panel span control mechanism is required to be designed to reduce the labor intensity.

Disclosure of Invention

Aiming at the defects existing in the prior art, the utility model aims to provide a solar power panel span control mechanism which solves the problems in the prior art.

The utility model is realized by the following technical scheme: a solar panel span control mechanism comprising: the device comprises a wingspan main body and a connecting bottom plate, wherein the front side and the rear side below the wingspan main body are respectively provided with a connecting bottom plate, and the upper surfaces of the two connecting bottom plates are respectively provided with a group of pushing mechanisms;

the pushing mechanism comprises an electric stay bar, a lifting rod I, a connecting box and a connecting ring, wherein the electric stay bar is arranged on the left side above the connecting bottom plate, the lifting rod I is arranged on the right side of the electric stay bar, and the lifting rod II is arranged on the right side of the lifting rod I;

two connecting boxes are arranged on the right side of the upper surface of the connecting bottom plate, a central rod is arranged in the middle of the inside of each connecting box, and the lower ends of the lifting rod I and the lifting rod II are respectively connected with the central rod in the connecting box below the connecting rods through connecting rings.

As a preferred embodiment, a clamping groove is respectively formed in the front and the rear of the left side of the lower surface of the wing span main body, a lifting rod is respectively arranged on the left side of the upper surface of the two connecting bottom plates, and a clamping block is respectively connected to the upper ends of the two lifting rods.

As a preferred implementation mode, a plurality of rod openings are formed in the middle of the left sides of the upper surfaces of the connecting boxes, a rod opening II is formed in the middle of the right sides of the upper surfaces of the connecting boxes on the left sides, the front ends of the electric supporting rods are in pin joint with a lifting rod II, the lifting rod I and the lifting rod II are movable mechanisms, and the connecting rings are sleeved on the outer sides of the center rods.

As a preferable implementation mode, the first lifting rod and the second lifting rod are connected with the wingspan main body at the upper ends, the front view surface of the connecting box is of a rectangular structure, and the width of the right view surface of the connecting box is the same as that of the right view surface of the connecting bottom plate.

As a preferable implementation mode, the position of the clamping block and the position of the clamping groove are symmetrical when the wing span main body is retracted, and the bottom view surface of the clamping groove and the front view surface of the clamping block are both rectangular structures.

As a preferred embodiment, the type of the main body of the span is SFP95-18 solar power panel span, the type of the electric supporting rod is DTZ2500 type electric pushing rod, and the type of the lifting rod is ANT-35 small type electric pushing rod.

After the technical scheme is adopted, the utility model has the beneficial effects that: through setting up pushing mechanism, can be convenient for open or withdraw span main part, operation process is simple and convenient and labour saving and time saving, can reduce artifical intensity of labour, through setting up lifter, fixture block and draw-in groove, when the span main part is withdrawn, the fixture block can block into the draw-in groove, can make the span main part be difficult for removing after withdrawing, promotes the stability after the span main part is withdrawn.

Drawings

In order to more clearly illustrate the embodiments of the utility model or the technical solutions of the prior art, the drawings which are used in the description of the embodiments or the prior art will be briefly described, it being obvious that the drawings in the description below are only some embodiments of the utility model, and that other drawings can be obtained according to these drawings without inventive faculty for a person skilled in the art.

FIG. 1 is a schematic view of the overall structure of a solar panel span control mechanism of the present utility model.

FIG. 2 is a schematic top view of a junction box in a solar panel span control mechanism according to the present utility model.

FIG. 3 is an enlarged schematic view of section A of a solar panel span control mechanism of the present utility model.

Fig. 4 is a schematic view of a spanwise body of a solar panel spanwise control mechanism of the present utility model from below.

In the figure, a 1-span main body, a 2-connecting bottom plate, a 3-pushing mechanism, a 4-electric supporting rod, a 5-lifting rod I, a 6-lifting rod II, a 7-connecting box, an 8-center rod, a 9-connecting ring, a 10-rod opening, an 11-lifting rod, a 12-clamping block and a 13-clamping groove are arranged.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1 to 4, the present utility model provides a technical solution: a solar panel span control mechanism comprising: the device comprises a wingspan main body 1 and connecting bottom plates 2, wherein the front side and the rear side below the wingspan main body 1 are respectively provided with one connecting bottom plate 2, and the upper surfaces of the two connecting bottom plates 2 are respectively provided with a group of pushing mechanisms 3;

the pushing mechanism 3 comprises an electric stay bar 4, a lifting rod I5, a connecting box 7 and a connecting ring 9, wherein the electric stay bar 4 is arranged on the left side above the connecting bottom plate 2, the lifting rod I5 is arranged on the right side of the electric stay bar 4, and the lifting rod II 6 is arranged on the right side of the lifting rod I5;

two connecting boxes 7 are arranged on the right side of the upper surface of the connecting bottom plate 2, a center rod 8 is arranged in the middle of the inside of each connecting box 7, and the lower ends of the lifting rod I5 and the lifting rod II 6 are respectively connected with the center rod 8 in the connecting box 7 below the connecting bottom plate through connecting rings 9.

A clamping groove 13 is respectively formed in the front and the rear of the left side of the lower surface of the wingspan main body 1, a jacking rod 11 is respectively arranged on the left side of the upper surface of the two connecting bottom plates 2, and clamping blocks 12 are respectively connected to the upper ends of the two jacking rods 11.

A rod opening 10 is formed in the middle of the left sides of the upper surfaces of the connecting boxes 7, a rod opening II is formed in the middle of the right sides of the upper surfaces of the left connecting boxes 7, the front ends of the electric supporting rods 4 are in pin joint with the lifting rods II 6, the lifting rods I5 and the lifting rods II 6 are movable mechanisms, and the connecting rings 9 are sleeved on the outer sides of the center rods 8.

The upper ends of the lifting rod I5 and the lifting rod II 6 are connected with the wingspan main body 1, the front view surface of the connecting box 7 is of a rectangular structure, and the width of the right view surface of the connecting box is the same as that of the right view surface of the connecting bottom plate 2.

The position of the clamping block 12 and the position of the clamping groove 13 are mutually symmetrical when the wingspan main body 1 is retracted, and the bottom view surface of the clamping groove 13 and the front view surface of the clamping block 12 are both rectangular structures.

The model of the wingspan main body 1 is an SFP95-18 solar power panel wingspan, the model of the electric supporting rod 4 is a DTZ2500 type electric push rod, and the model of the jacking rod 11 is an ANT-35 small type electric push rod.

As a first embodiment of the present utility model: in order to solve the problems that when the solar power panel wingspan in the prior art is installed above a solar automobile, the wingspan is required to be opened manually, the wingspan is required to be retracted manually, the operation process is complicated, the labor intensity of workers is increased, the opening and retraction process is time-consuming, and the working efficiency is affected, when the solar power panel wingspan is used, two electric supporting rods 4 are started, the electric supporting rods 4 push the lifting rods II 6 rightwards, the lifting rods II 6 can push the wingspan main body 1 rightwards, so that the wingspan main body 1 is opened, the wingspan main body 1 moves and drives the lifting rods I5 to move rightwards, meanwhile, the lower ends of the lifting rods I5 and II 6 respectively drive the connecting rings 9 below the lifting rods to rotate outside the center rod 8, when the wingspan main body 1 is required to be retracted, the two electric supporting rods 4 drive the lifting rods II 6 to move leftwards, the wingspan main body 1 is driven to move leftwards, and the wingspan main body 1 is retracted, and the final effect is that the labor intensity of workers can be opened or the wingspan main body 1 conveniently and the operation is reduced, and the labor intensity of workers can be saved.

As a second embodiment of the present utility model: in combination with the first embodiment, when the wingspan main body 1 is retracted, the lower end of the lifting rod one 5 and the lower end of the lifting rod two 6 are respectively located at the left rod opening 10, meanwhile, as the position of the clamping block 12 and the position of the clamping groove 13 are symmetrical when the wingspan main body 1 is retracted, the clamping block 12 is driven to ascend by the lifting rod 11, so that the wingspan main body 1 is not easy to move after being retracted, the stability of the wingspan main body 1 after being retracted is improved, and when the wingspan main body 1 needs to be opened, the lower end of the clamping block 12 is driven by the lifting rod 11, so that the wingspan main body 1 is separated from the clamping groove 13.

The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the utility model.

Claims

1. A solar panel span control mechanism comprising: span main part (1) and connecting plate (2), span main part (1) below front side and rear side are provided with a connecting plate (2) respectively, its characterized in that: the upper surfaces of the two connecting bottom plates (2) are respectively provided with a group of pushing mechanisms (3);

the pushing mechanism (3) comprises an electric stay bar (4), a lifting rod I (5), a connecting box (7) and a connecting ring (9), wherein the electric stay bar (4) is arranged on the left side above the connecting bottom plate (2), the lifting rod I (5) is arranged on the right side of the electric stay bar (4), and the lifting rod II (6) is arranged on the right side of the lifting rod I (5);

two connecting boxes (7) are arranged on the right side of the upper surface of the connecting bottom plate (2), a center rod (8) is arranged in the middle of the inside of each connecting box (7), and the lower ends of the lifting rod I (5) and the lifting rod II (6) are respectively connected with the center rod (8) in the connecting boxes (7) below the connecting boxes through connecting rings (9).

2. A solar panel span control mechanism as recited in claim 1, wherein: a clamping groove (13) is formed in the front and the rear of the left side of the lower surface of the wingspan main body (1), a jacking rod (11) is mounted on the left side of the upper surface of the connecting bottom plate (2), and clamping blocks (12) are connected to the upper ends of the jacking rods (11) respectively.

3. A solar panel span control mechanism as recited in claim 1, wherein: a plurality of pole mouth (10) have all been seted up in the middle of connecting box (7) upper surface left side, wherein the left side pole mouth second has been seted up in the middle of connecting box (7) upper surface right side, electronic vaulting pole (4) front end and lifting rod second (6) pin joint, lifting rod first (5) and lifting rod second (6) are a movable mechanism, go-between (9) cover is in the outside of center rod (8).

4. A solar panel span control mechanism as recited in claim 3, wherein: the upper ends of the lifting rod I (5) and the lifting rod II (6) are connected with the wingspan main body (1), the front view surface of the connecting box (7) is of a rectangular structure, and the width of the right view surface of the connecting box is the same as that of the right view surface of the connecting bottom plate (2).

5. A solar panel span control mechanism as recited in claim 2, wherein: the position of the clamping block (12) and the position of the clamping groove (13) are mutually symmetrical when the wingspan main body (1) is retracted, and the upward viewing surface of the clamping groove (13) and the forward viewing surface of the clamping block (12) are both rectangular structures.

6. A solar panel span control mechanism as recited in claim 1, wherein: the model of the wingspan main body (1) is SFP95-18 solar power panel wingspan, the model of the electric supporting rod (4) is DTZ2500 type electric push rod, and the model of the jacking rod (11) is ANT-35 small type electric push rod.