CN205029628U - Radiating area is independently divided detached laminate assembly - Google Patents
Radiating area is independently divided detached laminate assembly Download PDFInfo
- Publication number
- CN205029628U CN205029628U CN201520713628.6U CN201520713628U CN205029628U CN 205029628 U CN205029628 U CN 205029628U CN 201520713628 U CN201520713628 U CN 201520713628U CN 205029628 U CN205029628 U CN 205029628U
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- CN
- China
- Prior art keywords
- radiating area
- frame
- solar panel
- panel laminate
- radiating
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- 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
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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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- Photovoltaic Devices (AREA)
Abstract
The utility model relates to a radiating area is by independent detached laminate assembly, laminate assembly include solar panel lamination piece and with the sealed frame that four sides of solar panel lamination piece closely cooperated, be provided with solar energy component terminal box and two radiating area separators that are parallel to each other on the backplate face of solar panel lamination piece, direct contact not between the sealed frame of radiating area separator and solar energy component to cut apart into the independent heat radiation region of a plurality of with solar panel lamination piece, be equipped with radiating fin on the backplate face between the radiating area separator. The radiating area has greatly been simplified the frame design that is used for the protective layer casting die by independent detached laminate assembly, makes its heat dissipation function that does not influence subassembly backplate face, can make subassembly during operation verso very easily dispel the heat, and the temperature of subassembly will obviously be less than with the conventional subassembly under the environment.
Description
Technical field
The utility model relates to technical field of solar batteries, is specifically related to a kind of radiating area by the independent point of laminated compenent separated.
Background technology
Current known crystal silicon solar assembly, the structure adopted is: crystal silicon solar component layer laminate assembling aluminum alloy frame forms.
Solar components can be operationally heat energy most of light energy conversion, assembly is caused to generate heat, and the temperature of assembly can affect the operating efficiency of assembly, in general, under identical operational environment, the higher then operating efficiency of temperature of assembly is lower, and the working temperature therefore reducing assembly has become the important method improving component efficiency.
Present solar components has on the market been generally frame assembly, different according to the area aluminum alloy frame thickness of assembly, but it is minimum also at about 25mm, large area assembly reaches about 50mm, because solar panel laminate surrounding shelves have been lived by aluminum alloy frame, add mounting bracket when part is installed and be parallel to that face of aluminium frame installing hole, the extreme influence cooling system at the solar components back side, thus temperature when causing component operation is very high.
Utility model content
The purpose of this utility model is to overcome defect of the prior art, designs a kind ofly under the prerequisite meeting basic sealing and protection, can have cost low simultaneously; easy to process; easy for installation, be widely used, the radiating area of the advantages such as highly versatile is by the independent point of laminated compenent separated.
For achieving the above object, the technical scheme that the utility model adopts is:
A kind of radiating area is by the independent point of laminated compenent separated, it is characterized in that, described laminated compenent comprise solar panel laminate and with described solar panel laminate four close-fitting sealed frames of side, the backboard face of described solar panel laminate is provided with solar assembly junction box and two radiating area separators be parallel to each other, described radiating area separator does not directly contact with between solar components sealed frame, and solar panel laminate is divided into each and every one independently heat dissipation region some, backboard face between the separator of radiating area is provided with radiating fin.
Wherein preferred technical scheme is, described solar components sealed frame is by long margin frame and short frame is combined and spliced forms, the side of described short frame offers the first groove that cross section is rectangle along its length, the thickness of described groove and the thickness of solar panel laminate match, and the two ends of described short frame are respectively arranged with the first screw away from the position of slot opening;
The side of described long margin frame offers the second groove that cross section is rectangle along its length, and the part that the two ends of described long margin frame are positioned at the second bottom portion of groove is extended one section of protuberance respectively to the length direction of both sides along long margin frame and this protuberance is provided with second screw corresponding with described first screw.
Preferred technical scheme is that described short frame is less than or equal to 10mm along the thickness perpendicular to the first slot opening direction further, and described long margin frame is less than or equal to 10mm along the thickness perpendicular to the second slot opening direction.
Further preferred technical scheme also has, described radiating area separator by silica gel or adhered by double sided plaster on a side of described solar panel laminate.
Preferred technical scheme also has, and the material of described solar components sealed frame is the one in aluminium, engineering plastics or polyurethane.
Advantage of the present utility model and beneficial effect are: described radiating area is by the independent point of laminated compenent separated; greatly simplify the frame design for the protection of laminate; it is made not affect the heat sinking function in assembly backboard face; when can make component operation, very easily dispel the heat in the back side, and the temperature of assembly will be starkly lower than the general components under same environment.The feature of the design of this programme is, the heat dissipation region of general components back side entirety is divided into relatively uniform independently three regions again, the relatively conventional aluminium frame in region on both sides, because side section bar does not have the restriction in C face, be beneficial to ventilation and heat, the heat that backboard distributes can be transmitted in air very soon and go, and the heat distributed unlike general components is all gone back by frame gear, particularly module edge part heat radiation difficulty especially, thus affect component power;
The heat radiation of zone line, the area relatively conventional full wafer assembly area that need dispel the heat due to middle region part is much smaller, and do not have C face to design due to the frame of assembly side, result of ventilating heat dissipation is very good, adding and installing section bar is aluminium section bar, and heat transfer is very good, integrates, radiating effect is well more a lot of than routine, so this design can reduce module operating temperature to a great extent.
Accompanying drawing explanation
Fig. 1 is Facad structure figure of the present utility model;
Fig. 2 is the structure chart of short frame in the utility model;
Fig. 3 is the end view in the utility model under short frame using state;
Fig. 4 is the structure chart of long margin frame in the utility model;
Fig. 5 is the end view in the utility model under long margin frame using state;
Fig. 6 is the connection diagram of length frame in the utility model;
In figure: 1, solar panel laminate; 2, long margin frame; 3, short frame; 4, radiating area separator; 5, solar components connecting box; 6, radiating fin; 21, the second groove; 22, protuberance; 23, the second screw; 31, the first groove; 32, the first screw.
Embodiment
Below in conjunction with drawings and Examples, embodiment of the present utility model is further described.Following examples only for clearly the technical solution of the utility model being described, and can not limit protection range of the present utility model with this.
As shown in accompanying drawing 1 ~ 6: the utility model is that radiating area is by the independent point of laminated compenent separated, comprise solar panel laminate 1 and with the close-fitting solar components sealed frame of solar panel laminate 1 four sides, the backboard face of solar panel laminate 1 is provided with solar components connecting box 5 and two radiating area separators 4 be parallel to each other, do not contact between radiating area separator 4 with solar components sealed frame, and solar panel laminate 1 is divided at least three independently heat dissipation region, backboard face between the separator of radiating area is provided with radiating fin 6, radiating area separator 4 by silica gel or adhered by double sided plaster on a side of solar panel laminate 1, the material of solar components sealed frame is aluminium, one in engineering plastics or polyurethane.
Solar components sealed frame is by long margin frame 2 and short frame 3 is combined and spliced forms, the side of short frame 3 offers the first groove 31 that cross section is rectangle along its length, the thickness of the first groove 31 and the thickness of solar panel laminate 1 match, and the two ends of short frame 3 are respectively arranged with the first screw 32 away from the position of slot opening;
The side of long margin frame 2 offers the second groove 21 that cross section is rectangle along its length, the thickness of the second groove 21 and the thickness of solar panel laminate 1 match, and the part that the two ends of long margin frame 2 are positioned at bottom the second groove 21 is extended one section of protuberance 22 respectively to the length direction of both sides along long margin frame 2 and this protuberance 22 is provided with second screw 23 corresponding with the first screw 32;
In the surrounding of laminate, single trough rim frame is set, the frame of the relative general components of single trough rim frame, there is no B face and C face, reduce frame so to greatest extent to the impact of assembly radiating, simultaneously, there is again the effect of common frame protective layer casting die, relative to which one side adhesive tape edge sealing without frame assembly, this solar energy solar components reliability is higher, life-span is longer, use safer, reliability particularly in transport and installation process will far above without frame assembly, be different from the installing hole of conventional aluminium frame, the hole such as ground hole and apopore is designed, section bar of the present utility model is without any the design of aspect, hole, also just not relevant main equipment and manufacturing process, reduce the production cost of aluminium frame.
Short frame 3 is less than or equal to 10mm along the thickness perpendicular to the first groove 31 opening direction, and long margin frame 2 is less than or equal to 10mm along the thickness perpendicular to the second groove 21 opening direction.
Being different from conventional solar energy aluminium frame length frame uses corner brace to connect, the utility model can adopt self-tapping screw to connect the length frame of aluminium section bar, frame does not need imprint process after installing, and dismounting aluminium frame can not cause cell piece to break or hiddenly to split, technique is simple, can adapt to not have the batch production under frame loader condition.
The above is only preferred implementation of the present utility model; should be understood that; for those skilled in the art; under the prerequisite not departing from the utility model know-why; can also make some improvements and modifications, these improvements and modifications also should be considered as protection range of the present utility model.
Claims (5)
1. a radiating area is by the independent point of laminated compenent separated, it is characterized in that, described laminated compenent comprise solar panel laminate and with described solar panel laminate four close-fitting sealed frames of side, the backboard face of described solar panel laminate is provided with solar assembly junction box and two radiating area separators be parallel to each other, described radiating area separator does not directly contact with between solar components sealed frame, and solar panel laminate is divided into each and every one independently heat dissipation region some, backboard face between the separator of radiating area is provided with radiating fin.
2. radiating area as claimed in claim 1 is by the independent point of laminated compenent separated, it is characterized in that, described solar components sealed frame is by long margin frame and short frame is combined and spliced forms, the side of described short frame offers the first groove that cross section is rectangle along its length, the thickness of described groove and the thickness of solar panel laminate match, and the two ends of described short frame are respectively arranged with the first screw away from the position of slot opening;
The side of described long margin frame offers the second groove that cross section is rectangle along its length, and the part that the two ends of described long margin frame are positioned at the second bottom portion of groove is extended one section of protuberance respectively to the length direction of both sides along long margin frame and this protuberance is provided with second screw corresponding with described first screw.
3. radiating area as claimed in claim 2 is by the independent point of laminated compenent separated, it is characterized in that, described short frame is less than or equal to 10mm along the thickness perpendicular to the first slot opening direction, and described long margin frame is less than or equal to 10mm along the thickness perpendicular to the second slot opening direction.
4. the radiating area as described in claim 1 or 3, by independent point of laminated compenent separately, is characterized in that, described radiating area separator by silica gel or adhered by double sided plaster on a side of described solar panel laminate.
5. radiating area as claimed in claim 1 is by the independent point of laminated compenent separated, and it is characterized in that, the material of described solar components sealed frame is the one in aluminium, engineering plastics or polyurethane.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520713628.6U CN205029628U (en) | 2015-09-16 | 2015-09-16 | Radiating area is independently divided detached laminate assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201520713628.6U CN205029628U (en) | 2015-09-16 | 2015-09-16 | Radiating area is independently divided detached laminate assembly |
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CN205029628U true CN205029628U (en) | 2016-02-10 |
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CN201520713628.6U Expired - Fee Related CN205029628U (en) | 2015-09-16 | 2015-09-16 | Radiating area is independently divided detached laminate assembly |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106411256A (en) * | 2016-12-17 | 2017-02-15 | 许昌学院 | Photovoltaic cell pack structure facilitating installation of heat dissipation device |
-
2015
- 2015-09-16 CN CN201520713628.6U patent/CN205029628U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106411256A (en) * | 2016-12-17 | 2017-02-15 | 许昌学院 | Photovoltaic cell pack structure facilitating installation of heat dissipation device |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160210 Termination date: 20190916 |
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CF01 | Termination of patent right due to non-payment of annual fee |