CN217693140U - Flexible support with space stable structure - Google Patents
Flexible support with space stable structure Download PDFInfo
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- CN217693140U CN217693140U CN202221174437.3U CN202221174437U CN217693140U CN 217693140 U CN217693140 U CN 217693140U CN 202221174437 U CN202221174437 U CN 202221174437U CN 217693140 U CN217693140 U CN 217693140U
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- stranded wire
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
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Abstract
The utility model discloses a flexible support with a space stable structure, which is formed by a plurality of groups of stress support units which are transversely arranged in parallel, each group of stress support unit comprises a first steel strand, a second steel strand and a third steel strand which are parallel to each other, the second steel strand is higher than the first steel strand, and a plane formed by the first steel strand and the second steel strand forms an inclination angle with a horizontal plane; each group of stressed bracket units also comprises a space stabilizing structure, and the space stabilizing structure forms the space stabilizing structure of an inverted space triangular pyramid or space quadrangular pyramid by taking the support connecting rod as a bevel edge and taking the pull rod as a bottom edge according to the space positions of the first steel strand, the second steel strand and the third steel strand. The utility model discloses can carry out longitudinal tie with transverse arrangement's atress support unit, make each flexible support unit even become unified atress structure to guarantee photovoltaic module safe operation under the wind load effect.
Description
Technical Field
The utility model relates to a solar photovoltaic technology field especially relates to a flexible support with space stable structure.
Background
In recent years, the photovoltaic industry in China is rapidly developed, available land resources are less and less, and the traditional fixed support cannot meet the market demand. The method for installing the photovoltaic module by adopting the flexible support is more and more accepted by the market, however, the flexible support is installed by adopting the steel strand and has larger span, and the difficult problem of how to ensure the safe operation of the photovoltaic module under the action of wind load is needed to be solved urgently.
Disclosure of Invention
The utility model aims at providing a flexible support with space stable structure, this space stable structure can carry out longitudinal tie with transverse arrangement's atress support unit, makes each flexible support unit link into unified atress structure to guarantee photovoltaic module safe operation under the wind load effect.
In order to achieve the above purpose, the technical scheme of the utility model is that:
a flexible support with a space stable structure is used for supporting a solar photovoltaic panel, and is formed by transversely arranging a plurality of groups of stress support units in parallel, wherein each group of stress support units comprises a first steel strand, a second steel strand and a third steel strand which are parallel to each other, the second steel strand is higher than the first steel strand, a plane formed by the first steel strand and the second steel strand forms an inclination angle with a horizontal plane, photovoltaic modules are arranged on the first steel strand and the second steel strand to meet the installation requirements of different inclination angles of the modules, and the third steel strand is positioned right below the central lines of the first steel strand and the second steel strand;
each group of stressed bracket units also comprises a space stabilizing structure, the space stabilizing structure forms a space stabilizing structure of an inverted space triangular pyramid or a space quadrangular pyramid by taking a supporting connecting rod as a bevel edge and taking a pull rod as a bottom edge according to the space positions of the first steel stranded wire, the second steel stranded wire and the third steel stranded wire, and each angular point of the space stabilizing structure is respectively connected with the first steel stranded wire, the second steel stranded wire and the third steel stranded wire through cable clamps;
preferably, the bottom corner point of one space stabilization structure and the top corner point of an adjacent space stabilization structure are obliquely connected through longitudinal oblique rods between the adjacent stress support units, so that the side turning of the space stabilization structures is prevented.
More preferably, the device also comprises a longitudinal connecting rod, wherein the longitudinal connecting rod is respectively connected with the space stabilizing structure of each stressed bracket unit through a hoop, and all the stressed bracket units are connected into a unified stressed structure.
According to a further preferable technical scheme, the connection between each corner point of the space stabilizing structure is connected through a check bolt.
The utility model has the advantages that:
the utility model discloses can carry out longitudinal tie with transversal arrangement's atress support unit, make each flexible support unit even become unified atress structure to guarantee photovoltaic module safe operation under the wind load effect.
Drawings
Fig. 1 is a schematic structural diagram of embodiment 1 of the present invention;
fig. 2 is a schematic structural diagram of embodiment 2 of the present invention.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings.
Example 1:
as shown in fig. 1, the utility model discloses a flexible support with space stabilization structure, include and transversely form side by a plurality of groups of atress support units, every group atress support unit includes a steel strand wires 1, a steel strand wires 2 and a steel strand wires 3 that are parallel to each other, no. two steel strand wires 2 are highly higher than a steel strand wires 1, the plane that a steel strand wires 1 and a steel strand wires 2 formed forms the inclination with the horizontal plane promptly, arrange photovoltaic module above a steel strand wires 1 and a steel strand wires 2, can satisfy the installation requirement at the different inclinations of subassembly, no. three steel strand wires 3 are located under a steel strand wires 1 and a steel strand wires 2 central line;
the space stabilizing structure is formed by a support connecting rod 4 and a pull rod 5 according to the space positions of a first steel strand 1, a second steel strand 2 and a third steel strand 3, the support connecting rod is used as a bevel edge of the space stabilizing structure, the pull rod 5 is used as a bottom edge of the space stabilizing structure, the formed space stabilizing structure is an inverted space triangular pyramid, and each angular point of the space stabilizing structure is connected with the first steel strand 1, the second steel strand 2 and the third steel strand 3 through cable clamps;
the longitudinal diagonal rod 6 is used for obliquely connecting a bottom corner point of one space stabilizing structure with a top corner point of an adjacent space stabilizing structure so as to prevent the space stabilizing structure from turning laterally;
and the longitudinal connecting rod 7 is connected with the space stabilizing structure in a hoop mode and connects all the stress support units into a unified stress structure.
In some embodiments, each corner point of the space stabilizing structure is provided with a cable clamp for connecting a steel strand, and the space stabilizing structure is fixed on the space suspension cable bracket.
The longitudinal connecting rod 7, the inclined rod 6 and one support rod 4 of the space stabilizing structure form a plane triangular stabilizing structure.
The stay bar 4, the pull rod 5, the inclined rod 6 and the longitudinal connecting rod 7 in the space stabilizing structure can be made of square pipes or round pipes.
The longitudinal connecting rod 7 is connected with the space stabilizing structure in a hoop mode, and the influence of construction errors on a stress system is reduced.
The spatial stabilization structure angular points are connected through anti-loosening bolts.
This embodiment can carry out longitudinal connection with transversely arranged's atress supporting element, makes each flexible support unit link into unified atress structure to guarantee photovoltaic module safe operation under the wind load effect.
Example 2:
fig. 2 is a schematic structural diagram of another embodiment of the present invention, as shown in fig. 2, on the basis that the rest of the structures are the same as those of embodiment 1, the difference lies in the space stable structure, according to the spatial positions of the first steel strand 1, the second steel strand 2 and the third steel strand 3, the space stable structure is formed by the support link 4 and the pull rod 5, the support link 4 is the bevel edge of the space stable structure, the pull rod 5 is the base edge of the space stable structure, and the formed space stable structure is an inverted space quadrangular pyramid.
Under the development of this embodiment, the space-stable structure can also adopt other space centrum, but from stability and economy, it is all good as the structure listed in embodiment 1 and embodiment 2 of the present invention, but the improvement made on this basis all belongs to the protection scope of the present invention.
The described embodiments are only some, but not all embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Claims (4)
1. A flexible support with a space stable structure is used for supporting a solar photovoltaic panel and is characterized in that the flexible support is formed by a plurality of groups of stress support units in a transverse parallel mode, each group of stress support units comprises a first steel stranded wire, a second steel stranded wire and a third steel stranded wire which are parallel to each other, the height of the second steel stranded wire is higher than that of the first steel stranded wire, a plane formed by the first steel stranded wire and the second steel stranded wire forms an inclination angle with a horizontal plane, photovoltaic modules are arranged on the first steel stranded wire and the second steel stranded wire to meet the installation requirements of different inclination angles of the modules, and the third steel stranded wire is positioned right below the central line of the first steel stranded wire and the central line of the second steel stranded wire;
every group atress support unit still includes a space stable structure, space stable structure according to the spatial position of a steel strand wires, no. two steel strand wires and No. three steel strand wires, make the hypotenuse by the supporting rod, make the base by the pull rod, form the space stable structure of the space triangle pyramid or the space quadrangle of handstand, every angular point of space stable structure is connected with a steel strand wires, no. two steel strand wires and No. three steel strand wires respectively through the cable clip.
2. The flexible support with the space stabilizing structure as claimed in claim 1, wherein the bottom corner point of one space stabilizing structure and the top corner point of the adjacent space stabilizing structure are connected obliquely by the longitudinal diagonal rods between the adjacent stressed support units, so as to prevent the space stabilizing structure from side turning over.
3. The flexible support with space stabilization structure of claim 1, further comprising a longitudinal connecting rod, wherein the longitudinal connecting rod is connected with the space stabilization structure of each force-bearing support unit through a hoop, and the force-bearing support units are connected into a unified force-bearing structure.
4. A flexible support with a spatially stable structure according to claim 1, characterized in that the connection between each corner point of the spatially stable structure is by means of a locking bolt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221174437.3U CN217693140U (en) | 2022-05-07 | 2022-05-07 | Flexible support with space stable structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221174437.3U CN217693140U (en) | 2022-05-07 | 2022-05-07 | Flexible support with space stable structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217693140U true CN217693140U (en) | 2022-10-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221174437.3U Active CN217693140U (en) | 2022-05-07 | 2022-05-07 | Flexible support with space stable structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217693140U (en) |
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2022
- 2022-05-07 CN CN202221174437.3U patent/CN217693140U/en active Active
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