CN108501495A - A kind of solar double-glass assemblies laminating method - Google Patents
A kind of solar double-glass assemblies laminating method Download PDFInfo
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- CN108501495A CN108501495A CN201810278951.3A CN201810278951A CN108501495A CN 108501495 A CN108501495 A CN 108501495A CN 201810278951 A CN201810278951 A CN 201810278951A CN 108501495 A CN108501495 A CN 108501495A
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- tooling
- solar double
- glass assemblies
- component
- edge
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- 239000011521 glass Substances 0.000 title claims abstract description 76
- 230000000712 assembly Effects 0.000 title claims abstract description 53
- 238000000429 assembly Methods 0.000 title claims abstract description 53
- 238000000034 method Methods 0.000 title claims abstract description 27
- 238000010030 laminating Methods 0.000 title claims abstract description 24
- 238000003475 lamination Methods 0.000 claims abstract description 30
- 239000002390 adhesive tape Substances 0.000 claims abstract description 25
- 239000012945 sealing adhesive Substances 0.000 claims abstract description 19
- 238000002407 reforming Methods 0.000 claims abstract description 8
- 230000008859 change Effects 0.000 claims abstract description 4
- 238000003825 pressing Methods 0.000 claims abstract description 4
- 238000003756 stirring Methods 0.000 claims abstract description 4
- 238000011144 upstream manufacturing Methods 0.000 claims abstract description 4
- 238000004804 winding Methods 0.000 claims abstract description 4
- 239000000463 material Substances 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
- 230000008569 process Effects 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims description 4
- 239000012790 adhesive layer Substances 0.000 claims description 3
- -1 dimercapto 2-ethyl hexyl Chemical group 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 claims description 3
- 239000000446 fuel Substances 0.000 claims description 3
- 150000001451 organic peroxides Chemical class 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
- 229920006267 polyester film Polymers 0.000 claims description 3
- 239000000758 substrate Substances 0.000 claims description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims 1
- 230000003647 oxidation Effects 0.000 claims 1
- 238000007254 oxidation reaction Methods 0.000 claims 1
- 229920005989 resin Polymers 0.000 claims 1
- 239000011347 resin Substances 0.000 claims 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 229910052726 zirconium Inorganic materials 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 13
- 238000004519 manufacturing process Methods 0.000 description 10
- 238000005516 engineering process Methods 0.000 description 4
- 239000003292 glue Substances 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000012797 qualification Methods 0.000 description 3
- 239000000741 silica gel Substances 0.000 description 3
- 229910002027 silica gel Inorganic materials 0.000 description 3
- 229920000297 Rayon Polymers 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000003670 easy-to-clean Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical class [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 230000008719 thickening Effects 0.000 description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/0007—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving treatment or provisions in order to avoid deformation or air inclusion, e.g. to improve surface quality
- B32B37/003—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding involving treatment or provisions in order to avoid deformation or air inclusion, e.g. to improve surface quality to avoid air inclusion
-
- 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
-
- 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
-
- 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)
- Physics & Mathematics (AREA)
- Microelectronics & Electronic Packaging (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Computer Hardware Design (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Power Engineering (AREA)
- Fluid Mechanics (AREA)
- Manufacturing & Machinery (AREA)
- Quality & Reliability (AREA)
- Joining Of Glass To Other Materials (AREA)
- Laminated Bodies (AREA)
- Adhesives Or Adhesive Processes (AREA)
Abstract
The invention discloses a kind of solar double-glass assemblies laminating methods, include the following steps：A, after solar double-glass assemblies change station by the inflow of upstream assembly line, the automatic function of reforming of photoelectric sensor switch triggering reforms automatically to component；B, jacking cylinder automatically jacks up solar double-glass assemblies hanging after the completion of reforming, make solar double-glass assemblies be held in can horizontal free rotation state, convenient for pasting edge sealing adhesive band to component surrounding；C, after solar double-glass assemblies jacking, it needs manually to paste edge sealing adhesive headed along component side and is fixed on module edge, then adhesive tape is taken on the other hand, the other hand stirs rotary components, both hands cooperation is by adhesive tape along one circle of component surrounding winding, adhesive tape is cut short after the completion, and pressing presses adhesive tape sturdy in the positive and negative glass edge edge of component；D, carry out installing anti-over-pressed tooling operation later, the laminating method work flow that the present invention uses is simple, it is only necessary to a people can complete independently operation, save manpower, overvoltage effect in edge when can improve solar double-glass assemblies lamination improves assembly quality.
Description
Technical field
The present invention relates to solar double-glass assemblies lamination field, specially a kind of solar double-glass assemblies laminating method.
Background technology
With the fast development of solar power generation, that is, photovoltaic market, vast photovoltaic people develops a variety of photovoltaic module productions
Product, to adapt to varying environment condition, wherein solar double-glass assemblies become larger one of the component type of demand in recent years, still, right
For photovoltaic module manufacturer, the manufacturing process of solar double-glass assemblies is not also very ripe, especially its laminating technology, solar double-glass assemblies
Due to its special structure, there are two main problems：1）Layer glass results in the integral thickness of component relative to single layer glass
The thickness of glass component is big, and edge is pressurized larger when component lamination, generates edge overvoltage effect, and back glass is heavier, makes
It is not easy to extract out at component internal gas when lamination, easy generating assembly surrounding bubbles, fold, starved etc. are abnormal after lamination；2）Double glass
Due to not no viscoses such as protection surrounding glass edge EVA easy to stick of backboard after component lamination, cause component facade dirty serious, no
Easy to clean, above 2 points directly affect the appearance of solar double-glass assemblies, performance quality.
In the prior art, contact laminating can cause the residue glues such as the EVA of surrounding spilling to be sticky in glass after solar double-glass assemblies lamination is good
Glass edge causes component surrounding dirty serious, not easy to clean；Laminating machine upper cover is equipped with the silica gel with certain toughness
Plate, lamination pressure process is to apply pressure to silica gel plate by the upper chamber inflation to laminated resonator, then indirectly right by silica gel plate
Solar double-glass assemblies are pressurizeed, and edge stress generates edge overvoltage effect greatly compared with other positions when so easily causing component lamination
It answers, especially solar double-glass assemblies thickness is big compared with single glass component, and edge overvoltage effect is more notable, in addition solar double-glass assemblies back glass phase
For backboard weight, poor fluidity after the glued membranes such as EVA melt, gas is pressurized and is not easy to extract out when component lamination vacuumizes, and easily leads to gas
Body is gathered in component edge or marginal fold, unfilled corner phenomenon, reduces assembly quality；Someone devises a kind of special before
In " day " font or " mouth " font aluminium alloy tooling of double glass laminating technologies, i.e., complete to enter laminating machine in solar double-glass assemblies lamination
Behind feeding end, set is put in component surrounding by this tooling）, so that this tooling and component is entered in laminating machine together and is laminated, this
Method can improve solar double-glass assemblies lamination when edge overvoltage effect, reduce edge bubble, fold, unfilled corner phenomena such as；Though the method
It has some improvement, but still has the following problems to edge overvoltage effect：This Fixture Design is complex, after tooling surrounds component
Certain interval need to be reserved with module edge, the size in this gap gap is not easy to control, and the anti-over-pressed effect in excessive then edge is bad, mistake
It is small, the discharge of surrounding gas when being unfavorable for vacuumizing；Since current size of components specification is more, the double glass of various sizes need to be directed to
Component separately designs tooling, and this tooling processing cost is larger, increases production cost；Various components manufacturer is to reduce people at present
Power cost improves operating efficiency, is all made of automatic laminating technology, and this tooling specification is larger, after placing or being laminated before lamination
Two people's work compounds are needed when taking, this undoubtedly increases the human cost of solar double-glass assemblies manufacture, and reduces production efficiency；This side
Method not can relate to improve component surrounding viscose glue situation, to component facade cleannes without improvement.
For this purpose, special open is sent out a kind of solar double-glass assemblies laminating method, can significantly improve solar double-glass assemblies edge overvoltage effect, guarantee group
The cleannes of part glass edge ensure the quality of solar double-glass assemblies, improve production efficiency and qualification rate.
Invention content
The purpose of the present invention is to provide a kind of solar double-glass assemblies laminating methods, to solve mentioned above in the background art ask
Topic.
To achieve the above object, the present invention provides the following technical solutions：A kind of solar double-glass assemblies laminating method, including walk as follows
Suddenly：
A, after solar double-glass assemblies change station by the inflow of upstream assembly line, the automatic function of reforming of photoelectric sensor switch triggering, to group
Part is reformed automatically；
B, jacking cylinder automatically jacks up solar double-glass assemblies hanging after the completion of reforming, make solar double-glass assemblies be held in can level rotate freely
State, convenient for pasting edge sealing adhesive band to component surrounding；
C, it after solar double-glass assemblies jacking, needs manually to paste edge sealing adhesive headed along component side and is fixed on module edge, then one
Hand takes adhesive tape, the other hand to stir rotary components, and adhesive tape along one circle of component surrounding winding, is cut short adhesive tape by both hands cooperation after the completion,
Pressing presses adhesive tape sturdy in the positive and negative glass edge edge of component；
D, it carries out that anti-over-pressed tooling operation is installed later.
Preferably, anti-over-pressed tooling is installed to be as follows in the step D：
1）, anti-over-pressed tooling need when using to paste high temperature gummed tape in one side in advance, tape width can be had by oneself according to adhesive tape viscosity with
Until firm pasting；
2）, this time glass component be in jacking state, and face down, back side state upward, lamination employee need to take tooling, make
Adhesive tape has viscosity one side upward, by tape-stripping in component front, so that tooling is pasted and fixes, and anti-overvoltage tooling need to make when pasting
Closely two right-angle side of component corner on the inside of two right-angle sides；
3）And then high temperature gummed tape is pasted on module backside, that is, tooling, so that tooling and two surface glass fixation of component；
4）, after the completion rotary components press step 2）、3）Method pastes the tooling for fixing its excess-three corner successively；
5）, after the completion of four corners tooling pastes, click assembly line completing button, PLC will control turntable it is automatic advise just and under
Drop, makes the sturdy assembly line belt of component, component that will flow out to lamination process automatically；
6）, after the completion of lamination, station can be examined in appearance and collect tooling, remove edge sealing adhesive band.
Preferably, the jacking cylinder in the step B includes cylinder barrel, and inner casing is equipped in the cylinder barrel, is set in the inner casing
There are plunger rod, the cylinder barrel and inner casing side wall to be equipped with fuel feed hole, the side wall and bottom of the cylinder barrel and inner casing are equipped with oil groove,
It is equipped with sealing ring between the plunger rod and inner casing and between cylinder barrel and inner casing.
Preferably, the edge sealing adhesive band in the step B is made of base material and adhesive layer, and the base material is by comprising following heavy
The group of amount part is grouped as：40-50 parts of polyester films, 10-20 parts of dimercapto 2-ethyl hexyl ethanoate dioctyltins, 8-18 parts of thickening trees
Fat, 4-12 part organic peroxide, 3-9 parts of zirconium oxides；The substrate surface is uniformly arranged multiple through-holes.
Preferably, the anti-over-pressed tooling in the step D is made of aluminium alloy or epoxy resin board, the anti-over-pressed work
Dress is right-angle structure, including two right-angle sides, and two right angle edge lengths are 50-80mm；Width is 15-30mm；It is described anti-
Over-pressed tooling thickness is 5-10mm.
Preferably, the edge sealing tape thickness is 1mm-1.5mm.
Compared with prior art, the beneficial effects of the invention are as follows：
（1）The laminating method work flow that the present invention uses is simple, it is only necessary to a people can complete independently operation, save manpower, energy
Phenomena such as enough improving overvoltage effect in edge when solar double-glass assemblies are laminated, avoiding solar double-glass assemblies lamination back edge bubble, fold, starved,
Improve assembly quality；Additionally it is possible to improve the cleannes of solar double-glass assemblies, cleaning operation flow is more eliminated, improves operation effect
Rate reduces production cost.
（2）In the present invention, edge sealing adhesive 150 DEG C of high temperature resistant of band of use or more；Its adhesive tape viscosity is strong, tensile strength is good；And
And the small pore of special construction distribution is designed on adhesive tape, it is ensured that gas is extracted out when lamination vacuumizes.
（3）In the present invention, the anti-over-pressed tooling of use can significantly improve the anti-over-pressed effect in edge, improve solar double-glass assemblies manufacture
Qualification rate, while this tooling is small need to only be pasted when use fixed with component four in lamination station high temperature gummed tape
Right angle, special messenger places when without being laminated, and improves operating efficiency, reduces human cost.
Description of the drawings
Fig. 1 is present device structural schematic diagram；
Fig. 2 is structural schematic diagram after present invention lamination；
Fig. 3 is edge sealing adhesive of the present invention band vertical view；
Fig. 4 is jacking cylinder structural schematic diagram of the present invention.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
- 4 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of solar double-glass assemblies laminating method, includes the following steps：
A, after solar double-glass assemblies change station by the inflow of upstream assembly line, the automatic function of reforming of photoelectric sensor switch triggering, to group
Part is reformed automatically；
B, jacking cylinder 1 automatically jacks up solar double-glass assemblies 2 vacantly after the completion of reforming, and so that solar double-glass assemblies 2 is held in can be horizontal free
Rotation status, convenient for pasting edge sealing adhesive band 3 to component surrounding；
C, it after solar double-glass assemblies 2 jack, needs manually to paste on 3 head of edge sealing adhesive band along component side and is fixed on module edge, then
Adhesive tape, the other hand is taken to stir rotary components 4 on the other hand, adhesive tape along one circle of component surrounding winding, is cut short glue by both hands cooperation after the completion
Band, pressing press adhesive tape sturdy in the positive and negative glass edge edge of component；
D, it carries out that 5 operation of anti-over-pressed tooling is installed later.
In the present invention, anti-over-pressed tooling is installed in step D and is as follows：
1）, anti-over-pressed tooling 5 need when using to paste high temperature gummed tape in one side in advance, tape width can be had by oneself according to adhesive tape viscosity with
Until firm pasting；
2）, this time glass component be in jacking state, and face down, back side state upward, lamination employee need to take tooling, make
Adhesive tape has viscosity one side upward, by tape-stripping in component front, so that tooling is pasted and fixes, and anti-overvoltage tooling need to make when pasting
Closely two right-angle side of component corner on the inside of two right-angle sides；
3）And then high temperature gummed tape is pasted on module backside, that is, tooling, so that tooling and two surface glass fixation of component；
4）, after the completion rotary components press step 2）、3）Method pastes the tooling for fixing its excess-three corner successively；
5）, after the completion of four corners tooling pastes, click assembly line completing button, PLC will control turntable it is automatic advise just and under
Drop, makes the sturdy assembly line belt of component, component that will flow out to lamination process automatically；
6）, after the completion of lamination, station can be examined in appearance and collect tooling, remove edge sealing adhesive band.
In the present invention, jacking cylinder 1 in step B includes cylinder barrel 6, is equipped with inner casing 7 in the cylinder barrel 6, in the inner casing 7
Equipped with plunger rod 8, the cylinder barrel 6 and 7 side wall of inner casing are equipped with fuel feed hole 8, and the side wall and bottom of the cylinder barrel 6 and inner casing 7 are equal
Equipped with oil groove 10, sealing ring 11 is equipped between the plunger rod 8 and inner casing 7 and between cylinder barrel 6 and inner casing 7.The present invention uses
Jacking cylinder stretching speed it is fast, it is efficient, working efficiency can be improved.
In the present invention, the edge sealing adhesive band 3 in step B is made of base material and adhesive layer, and the base material is by comprising following heavy
The group of amount part is grouped as：40-50 parts of polyester films, 10-20 parts of dimercapto 2-ethyl hexyl ethanoate dioctyltins, 8-18 parts of thickening trees
Fat, 4-12 part organic peroxide, 3-9 parts of zirconium oxides；The substrate surface is uniformly arranged multiple through-holes；3 thickness of edge sealing adhesive band
For 1mm-1.5mm.In the present invention, edge sealing adhesive 150 DEG C of high temperature resistant of band of use or more；Its adhesive tape viscosity is strong, tensile strength is good；And
And the small pore of special construction distribution is designed on adhesive tape, it is ensured that gas is extracted out when lamination vacuumizes.
In addition, in the present invention, the anti-over-pressed tooling 5 in step D is made of aluminium alloy or epoxy resin board, the anti-mistake
Pressure tooling is right-angle structure, including two right-angle sides, and two right angle edge lengths are 50-80mm；Width is 15-30mm；Institute
It is 5-10mm to state anti-over-pressed tooling thickness.In the present invention, the anti-over-pressed tooling of use can significantly improve the anti-over-pressed effect in edge, carry
High solar double-glass assemblies manufacture qualification rate, while this tooling is small, and when use need to only be pasted in lamination station with high temperature gummed tape
Fixed and four right angles of component, special messenger places when without being laminated, and improves operating efficiency, reduces human cost.
In conclusion the laminating method work flow that the present invention uses is simple, it is only necessary to a people can complete independently operation, section
Human-saving, overvoltage effect in edge when can improve solar double-glass assemblies lamination avoid solar double-glass assemblies lamination back edge bubble, fold, lack
Phenomena such as glue, improves assembly quality；Additionally it is possible to improve the cleannes of solar double-glass assemblies, cleaning operation flow is more eliminated, is carried
High operating efficiency reduces production cost.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of solar double-glass assemblies laminating method, it is characterised in that：Include the following steps：
A, after solar double-glass assemblies change station by the inflow of upstream assembly line, the automatic function of reforming of photoelectric sensor switch triggering, to group
Part is reformed automatically；
B, jacking cylinder after the completion of reforming（1）Automatically by solar double-glass assemblies（2）It jacks up vacantly, makes solar double-glass assemblies（2）Being held in can water
Flat free rotation state, convenient for pasting edge sealing adhesive band to component surrounding（3）；
C, solar double-glass assemblies（2）After jacking, need manually by edge sealing adhesive band（3）Head is pasted along component side is fixed on module edge,
Then adhesive tape, the other hand is taken to stir rotary components on the other hand（4）, both hands, which coordinate, encloses adhesive tape along component surrounding winding one, after the completion
Adhesive tape is cut short, pressing presses adhesive tape sturdy in the positive and negative glass edge edge of component；
D, it carries out that anti-over-pressed tooling is installed later（5）Operation.
2. a kind of solar double-glass assemblies laminating method according to claim 1, it is characterised in that：Anti- mistake is installed in the step D
Pressure tooling is as follows：
1）, anti-over-pressed tooling（5）It needs to paste high temperature gummed tape in one side in advance when use, tape width can have viscosity by oneself according to adhesive tape
Until firm pasting；
2）, this time glass component be in jacking state, and face down, back side state upward, lamination employee need to take tooling, make
Adhesive tape has viscosity one side upward, by tape-stripping in component front, so that tooling is pasted and fixes, and anti-overvoltage tooling need to make when pasting
Closely two right-angle side of component corner on the inside of two right-angle sides；
3）And then high temperature gummed tape is pasted on module backside, that is, tooling, so that tooling and two surface glass fixation of component；
4）, after the completion rotary components press step 2）、3）Method pastes the tooling for fixing its excess-three corner successively；
5）, after the completion of four corners tooling pastes, click assembly line completing button, PLC will control turntable it is automatic advise just and under
Drop, makes the sturdy assembly line belt of component, component that will flow out to lamination process automatically；
6）, after the completion of lamination, station can be examined in appearance and collect tooling, remove edge sealing adhesive band.
3. a kind of solar double-glass assemblies laminating method according to claim 1, it is characterised in that：Jacking gas in the step B
Cylinder（1）Including cylinder barrel（6）, the cylinder barrel（6）It is interior to be equipped with inner casing（7）, the inner casing（7）It is interior to be equipped with plunger rod（8）, the cylinder barrel
（6）And inner casing（7）Side wall is equipped with fuel feed hole（8）, the cylinder barrel（6）And inner casing（7）Side wall and bottom be equipped with oil groove
（10）, the plunger rod（8）With inner casing（7）Between and cylinder barrel（6）With inner casing（7）Between be equipped with sealing ring（11）.
4. a kind of solar double-glass assemblies laminating method according to claim 1, it is characterised in that：Edge sealing adhesive in the step B
Band（3）It is made of base material and adhesive layer, the base material is grouped as by the group comprising following parts by weight：40-50 parts of polyester films,
10-20 parts of dimercapto 2-ethyl hexyl ethanoate dioctyltins, 8-18 parts of tackifying resins, 4-12 parts of organic peroxides, 3-9 parts of oxidations
Zirconium；The substrate surface is uniformly arranged multiple through-holes.
5. a kind of solar double-glass assemblies laminating method according to claim 1, it is characterised in that：Anti- overvoltage in the step D
Tooling（5）It being made of aluminium alloy or epoxy resin board, the anti-over-pressed tooling is right-angle structure, including two right-angle sides, two
Right angle edge lengths are 50-80mm；Width is 15-30mm；The anti-over-pressed tooling thickness is 5-10mm.
6. a kind of solar double-glass assemblies laminating method according to claim 4, it is characterised in that：The edge sealing adhesive band（3）Thickness
For 1mm-1.5mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810278951.3A CN108501495A (en) | 2018-03-31 | 2018-03-31 | A kind of solar double-glass assemblies laminating method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810278951.3A CN108501495A (en) | 2018-03-31 | 2018-03-31 | A kind of solar double-glass assemblies laminating method |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114326176A (en) * | 2021-12-29 | 2022-04-12 | 芜湖长信新型显示器件有限公司 | Tool for sticking edge sealing adhesive tape of LCD display module |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010114196A1 (en) * | 2009-04-03 | 2010-10-07 | (주) 엘지하우시스 | Solar cell module with layers of design for integration into buildings |
| CN103848373A (en) * | 2012-12-06 | 2014-06-11 | 苏州宏瑞达新能源装备有限公司 | Jack-up rotating mechanism |
| CN104119814A (en) * | 2014-07-07 | 2014-10-29 | 苏州世优佳电子科技有限公司 | High-temperature-resistant adhesive tape |
| CN204977721U (en) * | 2015-05-26 | 2016-01-20 | 连云港神舟新能源有限公司 | Dual glass assembly is angle bead frock for lamination |
| CN105845762A (en) * | 2016-03-31 | 2016-08-10 | 太仓海润太阳能有限公司 | Novel double-glass solar module and edge sealing method thereof |
| CN107634116A (en) * | 2017-09-26 | 2018-01-26 | 苏州英达瑞机器人科技有限公司 | A kind of photovoltaic double-glass battery component full automatic edge bander |
-
2018
- 2018-03-31 CN CN201810278951.3A patent/CN108501495A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010114196A1 (en) * | 2009-04-03 | 2010-10-07 | (주) 엘지하우시스 | Solar cell module with layers of design for integration into buildings |
| CN103848373A (en) * | 2012-12-06 | 2014-06-11 | 苏州宏瑞达新能源装备有限公司 | Jack-up rotating mechanism |
| CN104119814A (en) * | 2014-07-07 | 2014-10-29 | 苏州世优佳电子科技有限公司 | High-temperature-resistant adhesive tape |
| CN204977721U (en) * | 2015-05-26 | 2016-01-20 | 连云港神舟新能源有限公司 | Dual glass assembly is angle bead frock for lamination |
| CN105845762A (en) * | 2016-03-31 | 2016-08-10 | 太仓海润太阳能有限公司 | Novel double-glass solar module and edge sealing method thereof |
| CN107634116A (en) * | 2017-09-26 | 2018-01-26 | 苏州英达瑞机器人科技有限公司 | A kind of photovoltaic double-glass battery component full automatic edge bander |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114326176A (en) * | 2021-12-29 | 2022-04-12 | 芜湖长信新型显示器件有限公司 | Tool for sticking edge sealing adhesive tape of LCD display module |
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Application publication date: 20180907 |