CN105336815B - Manufacturing method of photovoltaic hyperboloidal double-glass module - Google Patents
Manufacturing method of photovoltaic hyperboloidal double-glass module Download PDFInfo
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- CN105336815B CN105336815B CN201510700182.8A CN201510700182A CN105336815B CN 105336815 B CN105336815 B CN 105336815B CN 201510700182 A CN201510700182 A CN 201510700182A CN 105336815 B CN105336815 B CN 105336815B
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- 239000011521 glass Substances 0.000 title claims abstract description 62
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 41
- 239000011265 semifinished product Substances 0.000 claims abstract description 18
- 238000007789 sealing Methods 0.000 claims abstract description 8
- 238000000034 method Methods 0.000 claims description 34
- 230000000712 assembly Effects 0.000 claims description 32
- 238000000429 assembly Methods 0.000 claims description 32
- 238000007711 solidification Methods 0.000 claims description 31
- 230000008023 solidification Effects 0.000 claims description 31
- 238000003466 welding Methods 0.000 claims description 23
- 230000001939 inductive effect Effects 0.000 claims description 16
- 239000000853 adhesive Substances 0.000 claims description 15
- 230000001070 adhesive effect Effects 0.000 claims description 15
- 239000002390 adhesive tape Substances 0.000 claims description 7
- 239000002023 wood Substances 0.000 claims description 6
- 241000700608 Sagitta Species 0.000 claims description 5
- 239000004744 fabric Substances 0.000 claims description 5
- 238000003856 thermoforming Methods 0.000 claims description 4
- 238000012360 testing method Methods 0.000 claims description 2
- 238000010030 laminating Methods 0.000 abstract description 3
- 239000012790 adhesive layer Substances 0.000 abstract 2
- 230000003247 decreasing effect Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- 238000004806 packaging method and process Methods 0.000 abstract 1
- 238000005201 scrubbing Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 4
- 238000011161 development Methods 0.000 description 3
- 238000013139 quantization Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 230000032798 delamination Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000013467 fragmentation Methods 0.000 description 2
- 238000006062 fragmentation reaction Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 239000012528 membrane Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 208000000884 Airway Obstruction Diseases 0.000 description 1
- 206010017577 Gait disturbance Diseases 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000013083 solar photovoltaic technology Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- GOLXNESZZPUPJE-UHFFFAOYSA-N spiromesifen Chemical compound CC1=CC(C)=CC(C)=C1C(C(O1)=O)=C(OC(=O)CC(C)(C)C)C11CCCC1 GOLXNESZZPUPJE-UHFFFAOYSA-N 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 230000003319 supportive effect Effects 0.000 description 1
- 210000003437 trachea Anatomy 0.000 description 1
Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/042—PV modules or arrays of single PV cells
- H01L31/048—Encapsulation of modules
- H01L31/0488—Double glass encapsulation, e.g. photovoltaic cells arranged between front and rear glass sheets
-
- 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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- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a manufacturing method of a photovoltaic hyperboloidal double-glass module. The manufacturing method specifically comprises the steps of: placing a photovoltaic adhesive layer on lower cover plate curved glass, and laying a battery string on the lower photovoltaic adhesive layer; laminating the strips to form a module rudiment; packaging the module rudiment; placing the packaged module rudiment in vacuum bag, placing a vacuum suction nozzle on an air guiding mat above the module rudiment, and sealing the module rudiment with the vacuum bag completely; connecting the vacuum suction nozzle with a vacuum pump for vacuumizing the vacuum bag to form a module semi-finished product; placing the module semi-finished product into a curing furnace for thermal forming; reducing the module semi-finished product to the normal temperature, and disassembling and scrubbing the module semi-finished product; and finally placing the module semi-finished product into an autoclave for secondary curing. Through the application of the manufacturing method, the produced hyperboloidal double-glass module can be well combined with an installation structure, the quantitative production of the hyperboloidal double-glass module is ensured, the scrapping rate of the module is reduced, the production cost of the module is decreased, and the market competitiveness of the hyperboloidal double-glass module is increased.
Description
Technical field
The present invention relates to solar photovoltaic technology field, particularly a kind of manufacture method of solar double-glass assemblies.
Background technology
Solar electrical energy generation is a kind of new forms of energy, with environmental protection, energy-conservation, it is inexhaustible the features such as, working as previous existence
Under boundary's wide resource environment in short supply, solar electrical energy generation has won the favor of more and more user with which the characteristics of intrinsic, because
This solar components arises at the historic moment, and its effect is exactly that solar energy is changed into electric energy.With the continuous progress of people's environmental protection concept,
Also increasingly it is subject to people's attention by the photovoltaic application system that solar components are constituted, especially this year, country went into overdrive to renovate
Haze, increasingly payes attention to the development of clean energy resource, encourages the development of pure electric vehicle, curved surface solar double-glass assemblies mutually to tie with various vehicles
Close, it is installed in the top of car, not only attractive in appearance but also can generate electricity.But the unstability of the unicity and production technology of curved surface solar double-glass assemblies
Become restriction stumbling-block preventing the development, the quantization of demand curved surface solar double-glass assemblies produces the quantization life of especially hyperboloid solar double-glass assemblies
Production. art becomes the important problem of photovoltaic industry.
But photovoltaic curved surface solar double-glass assemblies in the market are more based on plane, single-curved surface, single solar double-glass assemblies can only
The size of single adjustment curved surface length, modeling structure are single, and can not combine with mounting structure completely；In addition, also receiving
To the restriction of radian, it is impossible to meet the market demand to greatest extent.Photovoltaic hyperboloid solar double-glass assemblies have filled up curved surface from structure
The blank of solar double-glass assemblies, meets the demand in market.
Traditional solar double-glass assemblies can only be laminated using flat board tradition laminating machine, or be entered using vacuum cushion rubber in production
Row is fixed, and edge carries out bonding with high temperature gummed tape, be easily caused in evacuation process edge cell piece take out partially, vacuum cushion rubber leaks
The problems such as gas, vacuum trachea are blocked during evacuation occurs, and component scrappage is high.In addition, for the double glass of photovoltaic hyperboloid
For component, double curved glass and component are all that, with cambered structure, moulding is complicated, and traditional processing technology cannot meet hyperboloid
The production of solar double-glass assemblies, yield rate are low, and cost is high, cannot realize mass production always, it is impossible to form competitiveness.
The content of the invention
The technical problem to be solved in the invention is to provide a kind of manufacture method suitable for hyperboloid solar double-glass assemblies, is protecting
On the basis of the card component quality of production, the yield rate of component is improved, reduce the production cost of component, improve its market competitiveness.
For solving above-mentioned technical problem, the technical solution used in the present invention is as follows.
A kind of manufacture method of photovoltaic hyperboloid solar double-glass assemblies, the manufacture method specifically include following steps：
A. on lower cover bend glass place photovoltaic adhesive linkage,
B. battery strings are laid above lower floor's photovoltaic adhesive linkage；
C. piece is closed, component just shape is formed；
D. wrap up component just shape；
E. by the component for wrapping, just shape is placed in vacuum bag, and vacuum slot is placed on the inducing QI above the first shape of component
It is on felt then complete with vacuum bag sealing；
F. connect vacuum slot with vacuum pump, to bag vacuum, form component semi-finished product；
G. component semi-finished product are put into into curing oven thermoforming；
H., after being down to room temperature, Wipe assembly semi-finished product are dismantled；
I. being finally putting in autoclave carries out secondary solidification.
A kind of manufacture method of above-mentioned photovoltaic hyperboloid solar double-glass assemblies, described in step B, the welding manner of battery strings is：By electricity
Pond piece scribing, lays scribing cell piece along lower cover bend glass radian, forms battery strings using welding connection scribing cell piece,
In welding process, welding sagitta is less than 1mm；Bonding fritter is placed between welding, and the corner placement corner of scribing cell piece is little
Block, places adhesive strip between battery strings；Finally it is welded as a whole with busbar.
A kind of manufacture method of above-mentioned photovoltaic hyperboloid solar double-glass assemblies, the operating process for closing piece described in step C is：Will successively
Upper strata photovoltaic adhesive linkage, upper cover plate bend glass are placed in battery strings and form component just shape；Then to component, just shape is carried out
EL is tested, and until component, just shape is intact.
A kind of manufacture method of above-mentioned photovoltaic hyperboloid solar double-glass assemblies, step D are concretely comprised the following steps：First, at the beginning of component
Shape surrounding wraps up not sticky cloth film；In component, just inducing QI gauze is wrapped up on shape surface again, and is fixed with wood grain adhesive tape；Then again in inducing QI
Gauze outer layer covers inducing QI felt, and fixed with wood grain adhesive tape.
A kind of manufacture method of above-mentioned photovoltaic hyperboloid solar double-glass assemblies, it is when in step F to bag vacuum, cold to find time
For 60～80min, vacuum is not less than 98kpa.
A kind of manufacture method of above-mentioned photovoltaic hyperboloid solar double-glass assemblies, in step G, the solidification process of curing oven is divided into three
Stage：First stage, solidification temperature are 90 degree, are kept for 30 minutes；Second stage, solidification temperature are 100 degree, are kept for 100 minutes；
Phase III, solidification temperature 120 are kept for 120 minutes；During solidification, the vacuum of component semi-finished product is not less than 98kpa.
A kind of manufacture method of above-mentioned photovoltaic hyperboloid solar double-glass assemblies, the solidification process of step I mesohigh kettle are divided into three
Stage：First stage, pressure value are 0.6Mpa, and solidification temperature is 70 degree, is kept for 30 minutes；Second stage, pressure value is
0.8Mpa, solidification temperature are 90 degree, are kept for 20 minutes；Phase III, pressure value is 1Mpa, 130 degree of solidification temperature, is kept for 50 points
Clock；Discharge temperature is 40 degree.
As a result of above technical scheme, the invention technological progress is as follows.
The present invention abandons vacuum cushion rubber, is increased bonding fritter, is increased inducing QI gauze using control welding sagitta, component internal
With the mode of production such as inducing QI felt, the cold evacuation of vacuum bag, the secondary solidification of curing oven thermoforming, autoclave, solve cell piece it is broken,
Welding bending, cell piece corner take out partially, vacuum cushion rubber gas leakage, the technical problem such as vacuum airway obstruction, make the hyperboloid pair of production
Glass component can be good at combining with mounting structure, it is ensured that the quantization production of hyperboloid solar double-glass assemblies, reduce component
Scrappage, reduces the production cost of component, improves the market competitiveness of hyperboloid solar double-glass assemblies.
Specific embodiment
Below in conjunction with specific embodiment, the present invention will be described in further detail.
A kind of manufacture method of photovoltaic hyperboloid solar double-glass assemblies, is applied to field of photovoltaic power generation, difficult to reduce production technology
Degree, enables photovoltaic hyperboloid solar double-glass assemblies to quantify production.The manufacture method of the present invention specifically includes following steps：
A. on lower cover bend glass place photovoltaic adhesive linkage.
Lower cover bend glass is cleaned first, and dried lower cover bend glass is placed on the table；Then will
Lower floor's photovoltaic adhesive linkage of well cutting is laid in cover plate bend glass.In the present invention, photovoltaic adhesive linkage can adopt PVB glued membranes.
B. battery strings are laid above lower floor's photovoltaic adhesive linkage, specifically includes following steps.
B1. select cell piece, in election process, must assure that the solid colour of cell piece, cell piece can not occur chipping,
The problem of appearance such as unfilled corner.
B2. the cell piece scribing to having no problem.
B3. scribing cell piece is laid along lower cover bend glass radian, battery is formed using welding connection scribing cell piece
String.During placing battery plate scribing, stress difference should be avoided the occurrence of, placing battery is avoided in the larger position of glass radian
Piece, is replaced with the welding of middle connection.During welding, it is necessary to adopt manual welding, two finger forces are uniform, per root bead band handss
Finger is gently promoted, it is ensured that welding sagitta is consistent, height ＜ 1mm, and welding does not allow to offset main gate line.
B4. bonding fritter is placed between welding, the corner of scribing cell piece is placed corner fritter, placed between battery strings
Adhesive strip；Finally it is welded as a whole with busbar.Each bonding fritter is placed centrally, bonding fritter and left and right welding away from
From being advisable in 5 millimeters, play a part of cushioning supportive while, it is to avoid bonding fritter incorporate during by welding bending.It is viscous
Narrow bars should be placed centrally, while keeping 3-5 millimeters to be advisable.
C. piece is closed, component just shape is formed.
Close piece operating process be：Upper strata photovoltaic adhesive linkage, upper cover plate bend glass are placed on into shape in battery strings successively
Into the first shape of component；Then to component, just shape carries out EL tests, and until component, just shape is intact.
During piece is closed, it is ensured that the phenomenons such as immovable or fragmentation occurs in cell piece, glass combination is concordant, no
Allow the scene for wrong piece occur；When EL is tested, component will gently be lifted and be put down gently, it is found that problematic cell piece will be changed in time, change
After to tested, till having no problem.If it was found that component internal has debris, glass surrounding is inhaled using sucker simultaneously
Rise, remove impurity removing, forbid glass is lifted impurity removing to prevent the glass other end stress from excessively concentrating, crush battery
Piece.
D. wrap up component just shape.
First, check to laying the glass assembly for finishing, after confirmation does not have appearance quality, in the first shape four of component
Week wraps up not sticky cloth film；In component, just inducing QI gauze is wrapped up on shape surface again, and is fixed with wood grain adhesive tape；Then again in inducing QI gauze
Outer layer covers inducing QI felt, and fixed with wood grain adhesive tape.The parcel completely first shape of component, the gas for being conducive to component internal unnecessary and
Moisture is fully derived.
E. by the component for wrapping, just shape is placed in vacuum bag, and vacuum slot is placed on the inducing QI above the first shape of component
It is on felt then complete with vacuum bag sealing.
In the present embodiment, should be without obvious foreign body, without breakage from vacuum bag.At the beginning of parcel component, the method for shape is：By vacuum
On the table, by component, just shape is placed in the middle of vacuum bag for bag tiling, it is ensured that just shape surrounding has enough positions to carry out height to component
The bonding of warm sealing joint strip；On the inducing QI felt that vacuum slot is put in above component；Elevated-temperature seal adhesive tape is adhered to into vacuum bag
Edge；Then the another side of vacuum bag is picked up carries out doubling, carries out bonding with sealing joint strip to vacuum bag；Bonding is complete
Sealing joint strip to be extruded after finishing, it is ensured that generation of the two-layer vacuum diaphragm without gas leak phenomenon up and down.
F. connect vacuum slot with vacuum pump, and using sealing joint strip seal vacuum pump and the junction of vacuum slot；It is right
Bag vacuum, cold to find time as 60～80min, vacuum is not less than 98kpa, forms component semi-finished product.
G. component semi-finished product are put into into curing oven thermoforming.
Component semi-finished product are put into into truck, progradation should avoid component from encountering truck frame and scratch vacuum bag；By group
After part is put into truck, position of the observation assembly on truck sees whether can enter in stove, it is to avoid component encounters stove during charging
Wall output component fragmentation；Equipment regularly will be patrolled and examined during working, must not be unattended for a long time.
Solidification process is divided into three phases：First stage, solidification temperature are 90 degree, are kept for 30 minutes；Second stage, solidification
Temperature is 100 degree, is kept for 100 minutes；Phase III, solidification temperature 120 are kept for 120 minutes；Component semi-finished product during solidification
Vacuum is not less than 98kpa.
H., after being down to room temperature, Wipe assembly semi-finished product are dismantled.
After the completion of solidification, truck is released, remove vacuum slot, component is carried off, lowered the temperature.Treat that assembly surface is down to
Dismounting Wipe assembly is carried out after room temperature, notes firmly uniform when not sticky cloth is dismantled, in order to avoid pull the glued membrane of glass edge.
I. being finally putting in autoclave carries out secondary solidification.
Successful component will be solidified to be put in autoclave, secondary solidification is carried out, the adhesive strength of stiffener assembly prevents component
Occur the quality problems such as delamination of coming unglued in use.During autoclave operation：First stage, pressure value are 0.6Mpa,
Solidification temperature is 70 degree, is kept for 30 minutes；Second stage, pressure value are 0.8Mpa, and solidification temperature is 90 degree, is kept for 20 minutes；
Phase III, pressure value is 1Mpa, 130 degree of solidification temperature, is kept for 50 minutes；Discharge temperature is 40 degree.
The present invention is by controlling welding sagitta, the portion for being combined between cell piece, adding between cell piece corner, battery strings
Part, it is to avoid the broken possibility of cell piece, while having reached the straight effect of welding, makes component facade more attractive in appearance.Using leading
Gas gauze and inducing QI felt, having reached derives the purpose of excessive gas and moisture in component, improves the vacuum of component, enhances
The bonding degree of component, it is to avoid component comes unglued, the generation of delamination problems.Using carrying out cold taking out in outdoor after component machine-shaping
It is empty, it is to avoid component vacuum bag gas leakage in evacuation process, while improve the vacuum strength of component, it is to avoid air bubble problem
Produce, improve component production efficiency.The laminating machine replaced using curing oven so that the life of photovoltaic double curved glass solar double-glass assemblies
Product is possibly realized.
The present invention instead of vacuum cushion rubber using vacuum bag, it is to avoid the limitation and non-plasticity of cushion rubber, reduce group
The production cost of part, solves vacuum cushion rubber and comes off the phenomenon of vacuum reduction, it is ensured that photovoltaic hyperboloid solar double-glass assemblies go out
Product rate；Replace the big curvature that vacuum cushion rubber can also adapt to component to require using vacuum bag, the double glass of hyperbolic can be further compensated for
Photovoltaic module blank commercially, improves competitiveness.
Claims (6)
1. a kind of manufacture method of photovoltaic hyperboloid solar double-glass assemblies, it is characterised in that the manufacture method specifically includes following step
Suddenly：
A. on lower cover bend glass place photovoltaic adhesive linkage,
B. battery strings are laid above lower floor's photovoltaic adhesive linkage；
C. piece is closed, component just shape is formed；
D. wrap up component just shape；First, in component, just shape surrounding wraps up not sticky cloth film；In component, just inducing QI yarn is wrapped up on shape surface again
Cloth, and fixed with wood grain adhesive tape；Then again in inducing QI gauze outer layer covers inducing QI felt, and fixed with wood grain adhesive tape；
E. by the component for wrapping, just shape is placed in vacuum bag, and vacuum slot is placed on the inducing QI felt above the first shape of component
On, then it is complete with vacuum bag sealing；
F. connect vacuum slot with vacuum pump, to bag vacuum, form component semi-finished product；
G. component semi-finished product are put into into curing oven thermoforming；
H., after being down to room temperature, Wipe assembly semi-finished product are dismantled；
I. being finally putting in autoclave carries out secondary solidification.
2. a kind of manufacture method of photovoltaic hyperboloid solar double-glass assemblies according to claim 1, it is characterised in that step B institute
The welding manner for stating battery strings is：By cell piece scribing, scribing cell piece is laid along lower cover bend glass radian, using welding
Connection scribing cell piece forms battery strings, and in welding process, welding sagitta is less than 1mm；Bonding fritter is placed between welding, is drawn
Corner fritter is placed in the corner of piece cell piece, places adhesive strip between battery strings；Finally it is welded as a whole with busbar.
3. a kind of manufacture method of photovoltaic hyperboloid solar double-glass assemblies according to claim 1, it is characterised in that step C institute
State close piece operating process be：Successively upper strata photovoltaic adhesive linkage, upper cover plate bend glass are placed in battery strings and form component
First shape；Then to component, just shape carries out EL tests, and until component, just shape is intact.
4. the manufacture method of a kind of photovoltaic hyperboloid solar double-glass assemblies according to claim 1, it is characterised in that in step F
During to bag vacuum, cold to find time as 60 ~ 80min, vacuum is not less than 98 kpa.
5. the manufacture method of a kind of photovoltaic hyperboloid solar double-glass assemblies according to claim 1, it is characterised in that in step G
The solidification process of curing oven is divided into three phases：First stage, solidification temperature are 90 degree, are kept for 30 minutes；Second stage, solidification
Temperature is 100 degree, is kept for 100 minutes；Phase III, solidification temperature 120 are kept for 120 minutes；Component semi-finished product during solidification
Vacuum is not less than 98 kpa.
6. the manufacture method of a kind of photovoltaic hyperboloid solar double-glass assemblies according to claim 1, it is characterised in that in step I
The solidification process of autoclave is divided into three phases：First stage, pressure value are 0.6Mpa, and solidification temperature is 70 degree, is kept for 30 points
Clock；Second stage, pressure value are 0.8Mpa, and solidification temperature is 90 degree, is kept for 20 minutes；Phase III, pressure value are 1Mpa, Gu
Change 130 degree of temperature, kept for 50 minutes；Discharge temperature is 40 degree.
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| CN201510700182.8A CN105336815B (en) | 2015-10-26 | 2015-10-26 | Manufacturing method of photovoltaic hyperboloidal double-glass module |
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| CN201510700182.8A CN105336815B (en) | 2015-10-26 | 2015-10-26 | Manufacturing method of photovoltaic hyperboloidal double-glass module |
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| CN105336815B true CN105336815B (en) | 2017-03-22 |
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| CN111883620B (en) * | 2020-08-12 | 2022-06-21 | 夏能科技(北京)有限公司 | Preparation method of curved-surface solar module |
| CN114371125A (en) * | 2022-01-27 | 2022-04-19 | 江苏铁锚玻璃股份有限公司 | Method for testing TPU bonding strength |
| CN114497284A (en) * | 2022-02-11 | 2022-05-13 | 深圳嘉盛赋能科技有限公司 | Photovoltaic module automation line |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1564816A1 (en) * | 2004-02-16 | 2005-08-17 | Curvet SPA | Curved photovoltaic module and its production method |
| CN102779876A (en) * | 2012-08-01 | 2012-11-14 | 保定嘉盛光电科技有限公司 | Full-glass assembly and manufacture method thereof |
| CN102983213A (en) * | 2012-11-16 | 2013-03-20 | 中电电气（南京）光伏有限公司 | Lamination preparation process of curved-surface double-glass photovoltaic module |
| CN102991090A (en) * | 2012-11-16 | 2013-03-27 | 中电电气（南京）光伏有限公司 | Method for manufacturing curved photovoltaic component in laminating manner by utilizing high-pressure kettle |
-
2015
- 2015-10-26 CN CN201510700182.8A patent/CN105336815B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1564816A1 (en) * | 2004-02-16 | 2005-08-17 | Curvet SPA | Curved photovoltaic module and its production method |
| CN102779876A (en) * | 2012-08-01 | 2012-11-14 | 保定嘉盛光电科技有限公司 | Full-glass assembly and manufacture method thereof |
| CN102983213A (en) * | 2012-11-16 | 2013-03-20 | 中电电气（南京）光伏有限公司 | Lamination preparation process of curved-surface double-glass photovoltaic module |
| CN102991090A (en) * | 2012-11-16 | 2013-03-27 | 中电电气（南京）光伏有限公司 | Method for manufacturing curved photovoltaic component in laminating manner by utilizing high-pressure kettle |
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| CN105336815A (en) | 2016-02-17 |
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