CN212875718U - Solar photovoltaic board fixed bolster - Google Patents
Solar photovoltaic board fixed bolster Download PDFInfo
- Publication number
- CN212875718U CN212875718U CN202021764543.8U CN202021764543U CN212875718U CN 212875718 U CN212875718 U CN 212875718U CN 202021764543 U CN202021764543 U CN 202021764543U CN 212875718 U CN212875718 U CN 212875718U
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- CN
- China
- Prior art keywords
- solar photovoltaic
- aircraft
- photovoltaic board
- pivot
- fixedly connected
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 230000035939 shock Effects 0.000 claims abstract description 15
- 239000006096 absorbing agent Substances 0.000 claims abstract description 12
- 238000003466 welding Methods 0.000 claims abstract description 7
- 238000005260 corrosion Methods 0.000 claims description 4
- 238000000576 coating method Methods 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 4
- 238000010248 power generation Methods 0.000 description 4
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000004570 mortar (masonry) Substances 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
Classifications
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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
- Y02E10/40—Solar thermal energy, e.g. solar towers
- Y02E10/47—Mountings or tracking
-
- 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
Landscapes
- Photovoltaic Devices (AREA)
Abstract
The utility model discloses a solar photovoltaic board fixed bolster, including base and pad foot, pad foot welding sets up in the base top, pad foot top embedding is provided with the bearing axle, the bearing axle top is rotated and is connected with the bumper shock absorber, the welding of bumper shock absorber top is provided with electric putter, the inside supporting flexible interior pole that is provided with of electric putter, pole top fixed mounting has the pivot in the flexibility, base rear top fixedly connected with support, support and pivot top rotate jointly and are connected with the horizontal pole, the horizontal pole both sides are rotated respectively and are connected with the aircraft son and detain and the aircraft box, horizontal pole top fixed mounting has the backup pad, backup pad top fixedly connected with solar photovoltaic board. The utility model has the advantages of being scientific and reasonable in structural design, convenient operation can change the angle of solar photovoltaic board through the mode of going up and down, and the omnidirectional utilizes solar energy, has improved the photoelectric conversion efficiency of solar photovoltaic board.
Description
Technical Field
The utility model belongs to the technical field of the solar photovoltaic board, specifically be a solar photovoltaic board fixed bolster.
Background
With the continuous development of science and technology, fossil energy is increasingly scarce, solar energy is more and more paid attention to people as clean energy which does not pollute the environment, the solar energy obtained by the earth per second is equivalent to the energy generated by burning 500 million tons of high-quality coal, China is one of the most abundant countries of the world, the total solar energy irradiation amount of China is more than 502 million focal square meters, the area with the annual sunshine duration of 2200 hours in China approximately accounts for more than 2/3 in the national soil area of China, particularly in the western area, the annual sunshine duration reaches more than 3000 hours, the full utilization of solar energy resources gradually becomes the trend of advancing development of the society, and therefore the solar photovoltaic panel assembly is produced by operation.
The solar photovoltaic panel is a power generation device which can generate direct current under the sun, and is composed of thin solid photovoltaic cells made of semiconductor materials (such as silicon), the solar photovoltaic panel is taken as an important component in the solar power generation device, the installation angle of the solar photovoltaic panel can directly influence the power generation efficiency of the solar power generation device, in addition, in different regions or different seasons, the optimal angles of the solar photovoltaic panel are different, most of solar volt-ampere assemblies in the prior art are complex to install, the angle adjustment difficulty and the anti-seismic effect are lower, therefore, a solar photovoltaic panel fixing support is needed, the irradiation angle of the solar photovoltaic panel can be adjusted more conveniently and rapidly, and the absorption and conversion efficiency of the solar photovoltaic panel to sunlight are enhanced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: in order to solve the problem that the angle of the existing solar photovoltaic panel fixing support is difficult to adjust, and the problem that the anti-seismic effect is poor due to no connection between supports, a novel solar photovoltaic panel fixing support is provided.
The utility model adopts the technical scheme as follows: the utility model provides a solar photovoltaic board fixed bolster, includes base and pad foot, pad foot welding sets up in the base top, its characterized in that: the solar energy photovoltaic aircraft is characterized in that a bearing shaft is embedded into the upper portion of the pad foot, a shock absorber is connected to the upper portion of the bearing shaft in a rotating mode, an electric push rod is welded to the upper portion of the shock absorber, a telescopic inner rod is arranged inside the electric push rod in a matched mode, a rotating shaft is fixedly mounted on the upper portion of the telescopic inner rod, a support is fixedly connected to the upper portion of the rear portion of the base, a cross rod is connected to the support and the upper portion of the rotating shaft in a rotating mode, an aircraft male buckle and an aircraft female buckle are connected to the two sides of the cross rod.
As a further scheme of the utility model, the equal fixedly connected with telescopic link of aircraft box opposite side is detained to the aircraft son, and the spherical pivot of telescopic link opposite side fixedly connected with, and spherical pivot is provided with corresponding mortar shape groove in the supporting horizontal pole both sides.
As a further proposal of the utility model, the outside of the bracket, the electric push rod and the telescopic inner rod is coated with an anti-corrosion coating.
As a further proposal of the utility model, the aircraft is buckled and is set up between the aircraft box.
As a further aspect of the present invention, the support and the cross bar connection are also embedded and provided with a bearing shaft.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses in, through being equipped with electric putter above the base, can change the angle of solar photovoltaic board through the mode of going up and down, can make solar photovoltaic board make full use of sunlight, eliminated traditional solar photovoltaic board defect that the angle is difficult to adjust in the use effectively, the omnidirectional utilizes solar energy, has improved the photoelectric conversion efficiency of solar photovoltaic board.
2. The utility model discloses in, through rotating the connection bumper shock absorber above holding the pivot, can make the mount more firm, when receiving external irresistance power factor, protection solar photovoltaic board does not receive the damage, increases the life of solar photovoltaic board, reduces cost of maintenance.
3. The utility model discloses in, through setting up the aircraft son in horizontal pole both sides and detaining with the aircraft box, can make two or two above horizontal poles splice together, and more stable between two or more than two supports, and then the combined action has better shock resistance.
Drawings
FIG. 1 is a schematic diagram of the side structure of the present invention;
FIG. 2 is a schematic diagram of a rear view structure of the present invention;
the labels in the figure are: 1. a base; 2. a foot pad; 201. a rotating shaft; 202. an electric push rod; 203. a telescopic inner rod; 204. a bearing shaft; 3. a shock absorber; 301. a support; 302. a cross bar; 303. airplane buttons; 304. an airplane female buckle; 4. a support plate; 5. a solar photovoltaic panel.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some examples of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work all belong to the protection scope of the present invention.
The utility model discloses in bumper shock absorber (3), aircraft son knot (303), aircraft box (304), solar photovoltaic board (5) all can be obtained in market or private order.
Referring to FIGS. 1-2: the utility model provides a solar photovoltaic board fixed bolster, including base 1 and pad foot 2, pad foot 2 welding sets up in base 1 top, pad foot 2 top embedding is provided with bearing axle 204, bearing axle 204 top is rotated and is connected with bumper shock absorber 3, bumper shock absorber 3 top welding is provided with electric putter 202, the inside supporting pole 203 in stretching out and drawing back that is provided with of electric putter 202, pole 203 top fixed mounting has pivot 201 in the stretching out and drawing back, 1 rear top fixedly connected with support 301 of base, support 301 and pivot 201 top rotate jointly and are connected with horizontal pole 302, horizontal pole 302 both sides are rotated respectively and are connected with the aircraft and detain 303 and aircraft box 304, horizontal pole 302 top fixed mounting has backup pad 4, backup pad 4 top fixedly connected with solar photovoltaic board 5.
Further, the equal fixedly connected with telescopic link of aircraft secondary knot 303 and aircraft box 304 opposite side, and the spherical pivot of telescopic link opposite side fixedly connected with, and spherical pivot is provided with corresponding mortar groove in the supporting horizontal pole 302 both sides, can make two supports splice together fast, more has stability.
Furthermore, the outside of the bracket 301, the electric push rod 202 and the telescopic inner rod 203 are coated with anti-corrosion coatings, so that the anti-corrosion performance of the bracket can be enhanced, and the service life of the bracket can be prolonged.
Furthermore, the aircraft button 303 and the aircraft button 304 are matched, so that the aircraft button is convenient to detach and mount.
Further, the bearing shaft 204 is embedded in the joint of the bracket 301 and the cross rod 302, and the height of the solar photovoltaic panel 5 can be adjusted by the driving of the electric push rod 202.
When the solar photovoltaic panel fixing support provided by the utility model is used, firstly, the telescopic inner rod 203 which is matched and arranged inside the electric push rod 202 moves up and down to drive the rotating shaft 201 and the bearing shaft 204 to start moving to adjust the position of the solar photovoltaic panel 5, the shock absorber 3 which is rotatably connected above the bearing shaft 204 plays a shock absorption effect at the moment, the protection effect on the solar photovoltaic panel 5 is enhanced, and finally, the aircraft male button 303 and the aircraft female button 304 are respectively connected with the two sides of the cross bar 302 in a rotating way, when another support needs to be connected, the aircraft male buckle 303 and the aircraft female buckle 304 are connected in a matching way and then are fixed in a telescopic way, the supports are mutually connected, the utility model has better shock resistance, the structure design is scientific and reasonable, the operation is convenient, the angle of the solar photovoltaic panel can be changed in a lifting mode, solar energy is utilized in an all-dimensional mode, and photoelectric conversion efficiency of the solar photovoltaic panel is improved.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.
Claims (5)
1. The utility model provides a solar photovoltaic board fixed bolster, includes base (1) and pad foot (2), pad foot (2) welding sets up in base (1) top, its characterized in that: the embedding of foot pad (2) top is provided with and holds pivot (204), it is connected with bumper shock absorber (3) to hold pivot (204) top rotation, bumper shock absorber (3) top welding is provided with electric putter (202), electric putter (202) inside supporting interior pole (203) that stretches out and draws back that is provided with, pole (203) top fixed mounting has pivot (201) in stretching out and drawing back, base (1) rear top fixedly connected with support (301), support (301) and pivot (201) top rotate jointly and are connected with horizontal pole (302), horizontal pole (302) both sides are rotated respectively and are connected with the aircraft and detain (303) and aircraft box (304), horizontal pole (302) top fixed mounting has backup pad (4), backup pad (4) top fixedly connected with solar photovoltaic board (5).
2. The solar photovoltaic panel fixing bracket of claim 1, wherein: the aircraft secondary button (303) and the aircraft primary button (304) are fixedly connected with telescopic rods on the other sides, spherical rotating shafts are fixedly connected on the other sides of the telescopic rods, and corresponding mortar-shaped grooves are formed in the two sides of the cross rod (302) in a matched mode through the spherical rotating shafts.
3. The solar photovoltaic panel fixing bracket of claim 1, wherein: and the support (301), the electric push rod (202) and the telescopic inner rod (203) are coated with anti-corrosion coatings.
4. The solar photovoltaic panel fixing bracket of claim 1, wherein: the airplane male buckle (303) and the airplane female buckle (304) are arranged in a matched mode.
5. The solar photovoltaic panel fixing bracket of claim 1, wherein: and a bearing shaft (204) is also embedded at the joint of the bracket (301) and the cross rod (302).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021764543.8U CN212875718U (en) | 2020-08-21 | 2020-08-21 | Solar photovoltaic board fixed bolster |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021764543.8U CN212875718U (en) | 2020-08-21 | 2020-08-21 | Solar photovoltaic board fixed bolster |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212875718U true CN212875718U (en) | 2021-04-02 |
Family
ID=75189867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021764543.8U Expired - Fee Related CN212875718U (en) | 2020-08-21 | 2020-08-21 | Solar photovoltaic board fixed bolster |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212875718U (en) |
-
2020
- 2020-08-21 CN CN202021764543.8U patent/CN212875718U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210402 Termination date: 20210821 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |