Solar panel array supporting device

Abstract

The utility model belongs to the technical field of solar energy, and provides a solar panel array supporting device which comprises an inclined supporting frame, a vertical support, inclined supporting arms and an I-shaped plate, the inclined supporting frame comprises inclined supporting arms and bottom supporting arms, column piles are arranged below the high ends of the inclined supporting arms, the bottom supporting arms are transversely arranged above the low ends of the inclined supporting arms, the inclined supporting arms are arranged side by side at intervals, and the I-shaped plate is arranged on the vertical support. The inclined supporting arms are connected into a whole through the bottom supporting arm; the vertical support is arranged between the high end of the inclined supporting arm and the top of the column pile, the inclined supporting arm is arranged between the low end of the inclined supporting arm and the bottom of the column pile, and the length direction of the inclined supporting arm is perpendicular to the length direction of the inclined supporting arm so that the high end of the inclined supporting arm can abut against the lower portion of the low end of the inclined supporting arm. The solar panel assembling device is simple in structure, convenient to assemble and arrange, capable of rapidly assembling solar panels in a side-by-side array state, extremely low in manpower consumption, capable of effectively reducing the labor intensity of workers and high in practical value.

Description

Technical Field

[0001] This utility model belongs to the field of solar energy technology, specifically relating to a solar panel array support device. Background Technology

[0002] A solar panel is a thin photovoltaic semiconductor sheet that generates electricity directly using sunlight. It is an assembly consisting of several solar cells assembled on a plate in a certain way. In order to increase the power generation of solar panels, multiple solar panel arrays are usually used. When using multiple solar panel arrays, they need to be tilted and supported. The support device is set up to both assemble the array of solar panels into a whole and to ensure the light absorption effect of the solar panels.

[0003] Currently, traditional support devices for solar panel arrays have numerous components, making assembly inconvenient. Furthermore, the process of assembling solar panel arrays in a supported state is cumbersome, resulting in low work efficiency. At the same time, it requires a large amount of labor, increasing the labor intensity of workers.

[0004] Therefore, there is a need to provide an improved technical solution that addresses the shortcomings of the existing technology. Utility Model Content

[0005] The purpose of this invention is to overcome the problems of traditional support devices for solar panel arrays being inconvenient to assemble, having a cumbersome process for assembling solar panel arrays in a supported state, low work efficiency, and requiring a large amount of labor, thus increasing the labor intensity of workers. This invention provides a support device for solar panel arrays.

[0006] To achieve the above objectives, this utility model provides the following technical solution:

[0007] A solar panel array support device includes: a diagonal brace, a vertical support, diagonal arms, and an I-beam. The diagonal brace includes: a diagonal support arm and a bottom support arm. A column is provided below the high end of the diagonal support arm, and the bottom support arm is horizontally positioned above the low end of the diagonal support arm. Multiple diagonal support arms are provided and arranged side-by-side at intervals, connecting the multiple diagonal support arms into one unit via the bottom support arm. The vertical support is located between the high end of the diagonal support arm and the top of the column, and the diagonal support arm is located between the low end of the diagonal support arm and the bottom of the column. The length direction of the diagonal support arm is perpendicular to the length direction of the diagonal support arm, so that the high end of the diagonal support arm touches the low end of the diagonal support arm. The I-beam is composed of a middle plate and a pair of wing plates. The two wing plates are arranged parallel to each other at both ends of the middle plate. The middle plate is obliquely inserted into the lower end of the oblique support arm corresponding to the oblique support arm, and the end of the middle plate protrudes outward. A sliding hole is provided in the middle of the middle plate along the length direction. The upper end of the oblique support arm passes through the wing plate at the lower end of the middle plate and extends into the sliding hole, so that the middle plate can slide along the axial direction of the oblique support arm. The solar panel is located between the middle plates on two adjacent oblique support arms. When the middle plate slides along the axial direction of the oblique support arm, the aluminum frame of the solar panel can be pressed and fixed by the wing plate at the upper end of the middle plate.

[0008] In the solar panel array support device described above, preferably, the vertical support includes: a horizontal support leg and a pair of vertical support legs, the horizontal support leg being located at the top of the column, and the two vertical support legs being arranged parallel to each other at both ends of the horizontal support leg.

[0009] Preferably, the upper ends of both vertical support legs are aligned with the lower end of the upper end of the inclined support arm;

[0010] The lower ends of the two vertical support legs and the lower end of the inclined support arm are fixed to the column pile by clamps.

[0011] Preferably, the top and bottom of the pile are provided with annular grooves that fit with the clamp;

[0012] The clamp is located within the annular groove.

[0013] Preferably, the intermediate plate is perpendicular to the inclined support arm.

[0014] Preferably, the inclined support arm is a threaded rod.

[0015] Preferably, a traction disc is provided in the center of the side of the wing plate at the lower end of the intermediate plate facing the column.

[0016] Preferably, the traction disc has a through hole in the middle for the inclined support arm to pass through.

[0017] Preferably, the external thread of the inclined arm is fitted with a threaded tube.

[0018] Preferably, a gap is provided between the traction disc and the adjacent wing plate;

[0019] The high end of the solenoid has a circular cavity that fits into the traction disc, so that the high end of the solenoid is fitted between the traction disc and the adjacent wing plate.

[0020] Beneficial effects: This utility model has a simple structure, is easy to assemble and arrange. It can also quickly assemble solar panels in a side-by-side array with very low manpower consumption, effectively reducing the labor intensity of workers and has high practical value. Attached Figure Description

[0021] The accompanying drawings, which form part of this application, are used to provide a further understanding of the present invention. The illustrative embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an undue limitation of the present invention. Wherein:

[0022] Figure 1 This is the front view of the present invention;

[0023] Figure 2 This is a schematic diagram of the present invention integrated with a solar panel array;

[0024] Figure 3 This is a schematic diagram of the overall design of this utility model;

[0025] Figure 4 for Figure 3 Another perspective illustration;

[0026] Figure 5 This is a front sectional view of the present invention;

[0027] Figure 6 for Figure 5 Enlarged view of point A in the middle;

[0028] Figure 7 This is an overall schematic diagram of the I-beam structure of this utility model;

[0029] Figure 8 This is a schematic diagram of the overall structure of the column pile of this utility model.

[0030] In the diagram: 1. Inclined support arm; 2. Bottom support arm; 3. Column pile; 4. Inclined support arm; 5. Intermediate plate; 6. Wing plate; 7. Sliding hole; 8. Horizontal support leg; 9. Vertical support leg; 10. Clamp; 11. Annular groove; 12. Traction disc; 13. Screw tube. Detailed Implementation

[0031] The technical solutions in the embodiments of this utility model will be clearly and completely described below. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art are within the protection scope of this utility model.

[0032] In the description of this utility model, the terms "longitudinal," "lateral," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," and "bottom," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are used only for the convenience of describing this utility model and do not require that this utility model be constructed and operated in a specific orientation; therefore, they should not be construed as limitations on this utility model. The terms "connected" and "linked" used in this utility model should be interpreted broadly. For example, they can refer to a fixed connection or a detachable connection; they can refer to a direct connection or an indirect connection through intermediate components. Those skilled in the art can understand the specific meaning of the above terms according to the specific circumstances.

[0033] The present invention will now be described in detail with reference to the accompanying drawings and embodiments. It should be noted that, unless otherwise specified, the embodiments and features described herein can be combined with each other.

[0034] This embodiment aims to provide a solar panel array support device, whose main function is to have a simple structure that is easy to arrange on site, and at the same time, it can quickly assemble solar panels in array state, reducing manpower consumption.

[0035] Reference Figure 1-4 The system includes: a diagonal brace, a vertical support, a diagonal support arm 4, and an I-beam. The diagonal brace includes: a diagonal support arm 1 and a bottom support arm 2. Both the diagonal support arm 1 and the bottom support arm 2 are metal square tubes. A column pile 3 is erected below the high end of the diagonal support arm 1. The bottom support arm 2 is horizontally welded above the low end of the diagonal support arm 1. There are multiple diagonal support arms 1, which are arranged side by side at intervals. The multiple diagonal support arms 1 are connected into one unit by the bottom support arm 2. The diagonal support arm 4 is a threaded rod. The diagonal support arm 4 is located between the low end of the diagonal support arm 1 and the bottom of the column pile 3. The length direction of the diagonal support arm 4 is perpendicular to the length direction of the diagonal support arm 1, so that the high end of the diagonal support arm 4 touches the low end of the diagonal support arm 1.

[0036] Reference Figure 1 , Figure 4 and Figure 8The vertical support is located between the high end of the inclined support arm 1 and the top of the column 3. Specifically, the vertical support includes a horizontal support leg 8 and a pair of vertical support legs 9. The horizontal support leg 8 is located at the center of the top of the column 3. The two vertical support legs 9 are welded parallel to each other at both ends of the horizontal support leg 8. The upper ends of the two vertical support legs 9 are welded to the lower end of the high end of the inclined support arm 1. The lower ends of the two vertical support legs 9 and the lower end of the inclined support arm 4 are fixed to the column 3 by clamps 10. The top and bottom of the column 3 are provided with annular grooves 11 that fit with the clamps 10 so that the clamps 10 can be embedded in the annular grooves 11, thereby increasing the lateral stress support strength of the vertical support and the anti-slip ability of the lower clamps 10.

[0037] Reference Figure 1-6 The I-beam plate consists of a middle plate 5 and a pair of wing plates 6. The two wing plates 6 are welded parallel to each other at both ends of the middle plate 5. The middle plate 5 is inserted obliquely into the lower end of the oblique support arm 1, corresponding to the oblique support arm 4, to ensure that the middle plate 5 and the oblique support arm 4 remain perpendicular and that the end of the middle plate 5 protrudes outward to leave room for movement. The middle plate 5 has a sliding hole 7 along its length in the middle. The width of the sliding hole 7 matches the diameter of the oblique support arm 4 so that the upper end of the oblique support arm 4 passes through the wing plate 6 at the lower end of the middle plate 5 and extends into the sliding hole 7. At the same time, the middle plate 5 can slide along the axial direction of the oblique support arm 4. Based on this, the solar panel is placed between the middle plates 5 on two adjacent oblique support arms 1. When the middle plate 5 slides along the axial direction of the oblique support arm 4, that is, obliquely downward, the aluminum frame of the solar panel can be pressed and fixed by the wing plate 6 at the upper end of the middle plate 5.

[0038] In this embodiment, refer to Figure 2-7 A traction disc 12 is welded to the center of the wing plate 6 at the lower end of the middle plate 5, facing the column 3, with a pre-existing gap between the traction disc 12 and the adjacent wing plate 6. The traction disc 12 has a through hole in the middle for the inclined support arm 4 to pass through. A threaded tube 13 is threaded onto the outside of the inclined support arm 4. The high end of the threaded tube 13 has a cavity that fits with the traction disc 12, so that the high end of the threaded tube 13 is fitted between the traction disc 12 and the adjacent wing plate 6. Thus, when the threaded tube 13 is rotated and moved on the inclined support arm 4, the I-beam will be pulled downward or pushed upward by the direction of movement of the threaded tube 13. When the I-beam is pulled downward by the threaded tube 13, it is used to press the aluminum frame of the solar panel. When the I-beam is pushed upward by the threaded tube 13, it is used to adjust the distance between the wing plate 6 at the high end of the middle plate 5 and the adjacent inclined support arm 1, so that the solar panel is placed between the middle plates 5 on the two adjacent inclined support arms 1.

[0039] In use, the inclined support arm 1, vertical bracket, I-beam and inclined support arm 4 are assembled into one unit in advance. Then the vertical bracket is placed on the top of the column pile 3 and fixed by the clamp 10. At the same time, the lower end of the inclined support arm 4 is hinged to the clamp 10 at the bottom of the column pile 3. This method is repeated on each column pile 3. Finally, the lower end of all the inclined support arms 1 is welded to the bottom support arm 2. The bottom support arm 2 is to prevent the solar panel from slipping. In this way, the solar panel can be quickly placed and fixed on the top of two adjacent inclined support arms 1.

[0040] The support device provided in this embodiment has a simple structure, is easy to assemble and arrange. It can also quickly assemble solar panels in a side-by-side array, with very low manpower consumption, effectively reducing the labor intensity of workers and making it highly practical.

[0041] It is understood that the above description is merely exemplary and the embodiments of this application do not limit the scope of the application.

[0042] The above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model shall be within the scope of protection of the pending claims of the present utility model.

Claims

1. A solar panel array support device, characterized in that, include: The diagonal bracing frame includes: a diagonal support arm and a bottom support arm. A column is provided below the high end of the diagonal support arm, and the bottom support arm is horizontally positioned above the low end of the diagonal support arm. Multiple diagonal support arms are provided and arranged side by side at intervals. The multiple diagonal support arms are connected into one unit by the bottom support arm. A vertical support is provided between the high end of the inclined support arm and the top of the column pile; An inclined support arm is provided between the lower end of the inclined support arm and the bottom of the column pile. The length direction of the inclined support arm is perpendicular to the length direction of the inclined support arm, so that the upper end of the inclined support arm touches the lower end of the inclined support arm. The I-beam plate consists of a middle plate and a pair of wing plates. The two wing plates are arranged parallel to each other at both ends of the middle plate. The middle plate is obliquely inserted into the lower end of the oblique support arm corresponding to the oblique support arm, and the end of the middle plate protrudes outward. A sliding hole is provided in the middle of the middle plate along the length direction. The upper end of the oblique support arm passes through the wing plate at the lower end of the middle plate and extends into the sliding hole, so that the middle plate slides along the axial direction of the oblique support arm. The solar panel is located between the intermediate plates on two adjacent inclined support arms. When the intermediate plate slides along the axial direction of the inclined support arm, the aluminum frame of the solar panel can be pressed and fixed by the wing plate at the high end of the intermediate plate.

2. The solar panel array support device according to claim 1, characterized in that, The vertical support includes a horizontal support leg and a pair of vertical support legs. The horizontal support leg is located at the top of the column, and the two vertical support legs are arranged parallel to each other at both ends of the horizontal support leg.

3. The solar panel array support device according to claim 2, characterized in that, The upper ends of both vertical support legs are connected to the lower part of the upper end of the inclined support arm; The lower ends of the two vertical support legs and the lower end of the inclined support arm are fixed to the column pile by clamps.

4. The solar panel array support device according to claim 3, characterized in that, The top and bottom of the pile are provided with annular grooves that fit with the clamp. The clamp is located within the annular groove.

5. The solar panel array support device according to claim 1, characterized in that, The intermediate plate is perpendicular to the inclined support arm.

6. The solar panel array support device according to claim 1, characterized in that, The inclined support arm is a threaded rod.

7. The solar panel array support device according to claim 6, characterized in that, A traction disc is centrally located on the side of the wing plate at the lower end of the intermediate plate facing the column.

8. The solar panel array support device according to claim 7, characterized in that, The traction disc has a through hole in the middle for the inclined support arm to pass through.

9. The solar panel array support device according to claim 8, characterized in that, The external thread of the inclined arm is fitted with a threaded tube.

10. The solar panel array support device according to claim 9, characterized in that, There is a gap between the traction disc and the adjacent wing plate; The high end of the solenoid has a circular cavity that fits into the traction disc, so that the high end of the solenoid is fitted between the traction disc and the adjacent wing plate.

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