CN106784158A - A kind of bonding method of solar cell - Google Patents
A kind of bonding method of solar cell Download PDFInfo
- Publication number
- CN106784158A CN106784158A CN201710015138.2A CN201710015138A CN106784158A CN 106784158 A CN106784158 A CN 106784158A CN 201710015138 A CN201710015138 A CN 201710015138A CN 106784158 A CN106784158 A CN 106784158A
- Authority
- CN
- China
- Prior art keywords
- substrate
- solar battery
- air bag
- screening glass
- battery string
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 22
- 239000011521 glass Substances 0.000 claims abstract description 36
- 238000012216 screening Methods 0.000 claims abstract description 36
- 239000000758 substrate Substances 0.000 claims abstract description 30
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000000741 silica gel Substances 0.000 claims abstract description 4
- 229910002027 silica gel Inorganic materials 0.000 claims abstract description 4
- 238000005273 aeration Methods 0.000 claims abstract description 3
- 239000000463 material Substances 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- 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
- H01L31/18—Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof
- H01L31/1876—Particular processes or apparatus for batch treatment of the devices
- H01L31/188—Apparatus specially adapted for automatic interconnection of solar cells in a module
-
- 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
- H01L31/05—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells
- H01L31/0504—Electrical interconnection means between PV cells inside the PV module, e.g. series connection of PV cells specially adapted for series or parallel connection of solar cells in a module
-
- 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
-
- 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
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Landscapes
- Engineering & Computer Science (AREA)
- Computer Hardware Design (AREA)
- Sustainable Development (AREA)
- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Sustainable Energy (AREA)
- Manufacturing & Machinery (AREA)
- Photovoltaic Devices (AREA)
Abstract
The present invention discloses a kind of bonding method of solar cell, comprises the following steps：Step one, the lower surface of screening glass is pasted onto the upper surface of solar battery string, the protruding parts alignment mutually in flakes of the through hole and solar battery string on screening glass；Step 2, is coated with silica gel on substrate, and the solar battery string for pasting screening glass is pasted onto on substrate；Step 3, the substrate that solar battery string will be pasted is placed between two pieces of fixed metallic plates, rectangular air bag is placed on substrate, makes the pressure ratio atmospheric pressure in air bag high to airbag aeration, the substrate for pasting solar battery string is pressurizeed with air bag and is kept certain hour；Step 4, to air bag deflation, then takes out air bag and substrate, removes screening glass.The method can prevent solar battery string torsional deformation or battery strings produce sliding influence regularity under pressurised conditions in taping process, due to carrying out entire pressurisation to substrate using air bag, it is ensured that the flatness that solar battery string is pasted.
Description
Technical field
The present invention relates to battery technology, more particularly to a kind of bonding method of solar cell.
Background technology
The spacecraft overwhelming majority is all powered using solar battery array, and solar battery array needs first in process of production
Solar cell piece is connected to form solar battery string, then solar battery string is pasted on substrate, at present the conventional space sun
The solar cell method of attaching of cell array, the regularity pasted for solar cell, the control effect of flatness be not good.
The content of the invention
The problem that the present invention is solved is existing space solar battery array regularity, smooth in solar cell taping process
Degree is poor.
To solve the above problems, the present invention provides a kind of bonding method of solar cell, and the method comprises the following steps：
Step one, the lower surface of screening glass is pasted onto the upper surface of solar battery string, through hole and the sun on screening glass
The protruding parts alignment mutually in flakes of battery strings；
Step 2, is coated with silica gel on substrate, and the solar battery string for pasting screening glass is pasted onto on substrate；
Step 3, the substrate that will paste solar battery string is placed between two pieces of fixed metallic plates, and length is placed on substrate
Square air bag, makes the pressure ratio atmospheric pressure in air bag high to airbag aeration, and the substrate for pasting solar battery string is entered with air bag
Row pressurization simultaneously keeps certain hour；
Step 4, to air bag deflation, then takes out air bag and substrate, removes screening glass.
Further, more than the length of solar battery string, the width of screening glass is less than solar cell for the length of the screening glass
The width of string, mutually protruding parts in flakes output through hole to screening glass correspondence, the length and width of through hole be respectively greater than the length of protruding parts,
It is wide.
Further, more than the length of solar battery string, the width of screening glass is less than solar cell for the length of the screening glass
The width of string, mutually protruding parts in flakes output through hole to screening glass correspondence, the length and width of through hole be respectively greater than the length of protruding parts,
It is wide.
Further, the screening glass is made of light basis weight material, preferably PET.
Further, during inflation the air bag pressure ratio atmospheric pressure 4~20kPa high.
Further, the time that the air bag is pressurizeed to the substrate for pasting solar battery string is more than 4 hours.
Compared with prior art, the present invention has advantages below：
1st, because solar battery string is protected using screening glass, can prevent solar battery string from being distorted in taping process
Deformation or under pressurised conditions battery strings produce sliding influence regularity.
2nd, due to carrying out entire pressurisation to substrate using air bag, it is ensured that the flatness that solar battery string is pasted.
Brief description of the drawings
Fig. 1 is the schematic top plan view of current solar battery string；
Fig. 2 is the schematic side view of current solar battery string；
Fig. 3 is the structural representation of screening glass of the invention；
Fig. 4 is the schematic diagram of entire pressurisation method of the invention.
Specific embodiment
To describe technology contents of the invention, structural feature, institute's reached purpose and effect in detail, below in conjunction with embodiment
And coordinate accompanying drawing to be described in detail.
As depicted in figs. 1 and 2, solar battery string 1 is by solar cell piece 11 and mutually 12 constitutes in flakes, in solar battery string
Mutually the front welding of 12 one end and solar cell piece 11 in flakes, the back side weldering of the other end and solar cell piece 11 of 1 centre
Connect, mutually 12 there are protruding parts 121 in the front of solar battery string 1 in flakes.
As shown in figure 3, screening glass 2 is made of light basis weight material, such as PET, the length of screening glass 2 is more than solar battery string 1
Length, less than the width of solar battery string 1, the correspondence of screening glass 1 mutually open in flakes by 12 protruding parts 121 for the width of screening glass 2
Go out through hole 21, the length and width of through hole 21 is respectively greater than the length and width of protruding parts 121.
Further, the lower surface of screening glass 2 scribbles adhesive sticker.
The bonding method of solar battery of the invention is as follows：
Step one, the lower surface of screening glass 2 is pasted onto the upper surface of solar battery string 1, the He of through hole 21 on screening glass 2
Solar battery string 1 mutually in flakes 12 protruding parts 121 be aligned.
Step 2, is coated with silica gel on the substrate 3, and the solar battery string 1 for pasting screening glass 2 is pasted on the substrate 3.
Step 3, as shown in figure 4, the substrate 3 that will paste solar battery string 1 is placed between two pieces of fixed metallic plates 4,
Rectangular air bag 5 is placed on substrate 3, the pressure ratio atmospheric pressure 4~20kPa high made in air bag is inflated to air bag 5, with air bag 5
Substrate 3 to pasting solar battery string 1 is pressurizeed and is kept for more than 4 hours.
Step 4, deflates to air bag 5, then takes out air bag 5 and substrate 3, removes screening glass 2.
Because solar battery string 1 is protected using screening glass 2, can prevent solar battery string 1 from being turned round in taping process
Song deformation or the under pressurised conditions generation of battery strings 1 sliding influence regularity, due to carrying out overall adding to substrate 3 using air bag 5
Pressure, it is ensured that the flatness that solar battery string 1 is pasted.
Claims (6)
1. a kind of bonding method of solar cell, it is characterized in that：The method comprises the following steps：
Step one, the lower surface of screening glass is pasted onto the upper surface of solar battery string, through hole and solar cell on screening glass
The protruding parts alignment mutually in flakes of string；
Step 2, is coated with silica gel on substrate, and the solar battery string for pasting screening glass is pasted onto on substrate；
Step 3, the substrate that will paste solar battery string is placed between two pieces of fixed metallic plates, and rectangle is placed on substrate
Air bag, make the pressure ratio atmospheric pressure in air bag high to airbag aeration, with air bag to paste solar battery string substrate added
Press and keep certain hour；
Step 4, to air bag deflation, then takes out air bag and substrate, removes screening glass.
2. the bonding method of solar cell as claimed in claim 1, it is characterized in that：The length of the screening glass is more than sun electricity
The length of pond string, the width of the width less than solar battery string of screening glass, screening glass correspondence protruding parts mutually in flakes are outputed logical
Hole, the length and width of through hole is respectively greater than the length and width of protruding parts.
3. the bonding method of solar cell as claimed in claim 1, it is characterized in that：The screening glass uses light basis weight material system
Into.
4. the bonding method of solar cell as claimed in claim 1, it is characterized in that：The screening glass uses PET.
5. the bonding method of solar cell as claimed in claim 1, it is characterized in that：The pressure ratio air of air bag during inflation
Press 4~20kPa high.
6. the bonding method of solar cell as claimed in claim 1, it is characterized in that：The air bag is to pasting solar battery string
The time that substrate is pressurizeed is more than 4 hours.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710015138.2A CN106784158B (en) | 2017-01-10 | 2017-01-10 | A kind of bonding method of solar cell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710015138.2A CN106784158B (en) | 2017-01-10 | 2017-01-10 | A kind of bonding method of solar cell |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106784158A true CN106784158A (en) | 2017-05-31 |
| CN106784158B CN106784158B (en) | 2018-04-17 |
Family
ID=58948607
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710015138.2A Active CN106784158B (en) | 2017-01-10 | 2017-01-10 | A kind of bonding method of solar cell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106784158B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109041448A (en) * | 2018-09-26 | 2018-12-18 | 深圳市致竑光电有限公司 | A kind of adhering method of the FPC of fluorescent glass |
| CN109686815A (en) * | 2018-11-15 | 2019-04-26 | 上海空间电源研究所 | The production method that space is pasted with flexible battle array solar battery module positioning and upper plate |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090220794A1 (en) * | 2005-05-12 | 2009-09-03 | O'neill Liam | Bonding An Adherent To A Substrate Via A Primer |
| CN101916788A (en) * | 2010-04-23 | 2010-12-15 | 杭州索乐光电有限公司 | Solar panel and encapsulation process |
-
2017
- 2017-01-10 CN CN201710015138.2A patent/CN106784158B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090220794A1 (en) * | 2005-05-12 | 2009-09-03 | O'neill Liam | Bonding An Adherent To A Substrate Via A Primer |
| CN101916788A (en) * | 2010-04-23 | 2010-12-15 | 杭州索乐光电有限公司 | Solar panel and encapsulation process |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109041448A (en) * | 2018-09-26 | 2018-12-18 | 深圳市致竑光电有限公司 | A kind of adhering method of the FPC of fluorescent glass |
| CN109686815A (en) * | 2018-11-15 | 2019-04-26 | 上海空间电源研究所 | The production method that space is pasted with flexible battle array solar battery module positioning and upper plate |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106784158B (en) | 2018-04-17 |
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