WO2014042217A1 - Feuille de protection de cellule solaire et module de cellule solaire flexible - Google Patents
Feuille de protection de cellule solaire et module de cellule solaire flexible Download PDFInfo
- Publication number
- WO2014042217A1 WO2014042217A1 PCT/JP2013/074717 JP2013074717W WO2014042217A1 WO 2014042217 A1 WO2014042217 A1 WO 2014042217A1 JP 2013074717 W JP2013074717 W JP 2013074717W WO 2014042217 A1 WO2014042217 A1 WO 2014042217A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- solar cell
- layer
- adhesive sealing
- sealing layer
- protective sheet
- Prior art date
Links
- 230000001681 protective effect Effects 0.000 title claims abstract description 71
- 239000010410 layer Substances 0.000 claims abstract description 126
- 239000000853 adhesive Substances 0.000 claims abstract description 90
- 230000001070 adhesive effect Effects 0.000 claims abstract description 90
- 238000007789 sealing Methods 0.000 claims abstract description 87
- 239000011241 protective layer Substances 0.000 claims abstract description 71
- 239000002344 surface layer Substances 0.000 claims abstract description 38
- 229920005989 resin Polymers 0.000 claims abstract description 27
- 239000011347 resin Substances 0.000 claims abstract description 27
- 239000002253 acid Substances 0.000 claims abstract description 16
- 125000004433 nitrogen atom Chemical group N* 0.000 claims abstract description 16
- 125000004018 acid anhydride group Chemical group 0.000 claims abstract description 15
- 239000004840 adhesive resin Substances 0.000 claims abstract description 11
- 229920006223 adhesive resin Polymers 0.000 claims abstract description 11
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 claims abstract description 4
- 229910052731 fluorine Inorganic materials 0.000 claims abstract description 4
- 239000011737 fluorine Substances 0.000 claims abstract description 4
- 229920002981 polyvinylidene fluoride Polymers 0.000 claims description 31
- 229920001577 copolymer Polymers 0.000 claims description 26
- 238000006243 chemical reaction Methods 0.000 claims description 23
- -1 silane compound Chemical class 0.000 claims description 21
- 238000009832 plasma treatment Methods 0.000 claims description 14
- 229910000077 silane Inorganic materials 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 12
- 229920000840 ethylene tetrafluoroethylene copolymer Polymers 0.000 claims description 11
- 125000003055 glycidyl group Chemical group C(C1CO1)* 0.000 claims description 8
- 239000002033 PVDF binder Substances 0.000 claims description 7
- 239000000203 mixture Substances 0.000 claims description 7
- 229920006226 ethylene-acrylic acid Polymers 0.000 claims description 5
- 229920000554 ionomer Polymers 0.000 claims description 5
- 229920000098 polyolefin Polymers 0.000 claims description 5
- 229920002620 polyvinyl fluoride Polymers 0.000 claims description 5
- 229920001780 ECTFE Polymers 0.000 claims description 3
- 229920002493 poly(chlorotrifluoroethylene) Polymers 0.000 claims description 3
- 229920003229 poly(methyl methacrylate) Polymers 0.000 claims description 3
- 239000005023 polychlorotrifluoroethylene (PCTFE) polymer Substances 0.000 claims description 3
- 239000004926 polymethyl methacrylate Substances 0.000 claims description 3
- CHJAYYWUZLWNSQ-UHFFFAOYSA-N 1-chloro-1,2,2-trifluoroethene;ethene Chemical group C=C.FC(F)=C(F)Cl CHJAYYWUZLWNSQ-UHFFFAOYSA-N 0.000 claims description 2
- 229920000642 polymer Polymers 0.000 claims 1
- 210000004027 cell Anatomy 0.000 description 197
- 238000000034 method Methods 0.000 description 32
- 238000004519 manufacturing process Methods 0.000 description 24
- BQCIDUSAKPWEOX-UHFFFAOYSA-N 1,1-Difluoroethene Chemical compound FC(F)=C BQCIDUSAKPWEOX-UHFFFAOYSA-N 0.000 description 23
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 18
- 229910052757 nitrogen Inorganic materials 0.000 description 12
- 238000001125 extrusion Methods 0.000 description 11
- 239000000758 substrate Substances 0.000 description 11
- 238000010586 diagram Methods 0.000 description 10
- NIXOWILDQLNWCW-UHFFFAOYSA-M Acrylate Chemical compound [O-]C(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-M 0.000 description 8
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 8
- 239000005977 Ethylene Substances 0.000 description 8
- CERQOIWHTDAKMF-UHFFFAOYSA-N Methacrylic acid Chemical compound CC(=C)C(O)=O CERQOIWHTDAKMF-UHFFFAOYSA-N 0.000 description 8
- 238000003851 corona treatment Methods 0.000 description 8
- FPYJFEHAWHCUMM-UHFFFAOYSA-N maleic anhydride Chemical group O=C1OC(=O)C=C1 FPYJFEHAWHCUMM-UHFFFAOYSA-N 0.000 description 8
- 229920005672 polyolefin resin Polymers 0.000 description 8
- 229910001873 dinitrogen Inorganic materials 0.000 description 7
- 238000004049 embossing Methods 0.000 description 7
- 238000010030 laminating Methods 0.000 description 7
- 238000002360 preparation method Methods 0.000 description 7
- 238000003825 pressing Methods 0.000 description 7
- 238000004833 X-ray photoelectron spectroscopy Methods 0.000 description 6
- 239000007772 electrode material Substances 0.000 description 6
- 239000007789 gas Substances 0.000 description 6
- 239000004065 semiconductor Substances 0.000 description 6
- BPSIOYPQMFLKFR-UHFFFAOYSA-N trimethoxy-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound CO[Si](OC)(OC)CCCOCC1CO1 BPSIOYPQMFLKFR-UHFFFAOYSA-N 0.000 description 6
- 230000037303 wrinkles Effects 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 5
- 238000001816 cooling Methods 0.000 description 5
- 230000032798 delamination Effects 0.000 description 5
- VOZRXNHHFUQHIL-UHFFFAOYSA-N glycidyl methacrylate Chemical compound CC(=C)C(=O)OCC1CO1 VOZRXNHHFUQHIL-UHFFFAOYSA-N 0.000 description 5
- 238000004898 kneading Methods 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 238000005096 rolling process Methods 0.000 description 5
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical compound COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 4
- 239000000654 additive Substances 0.000 description 4
- 239000012790 adhesive layer Substances 0.000 description 4
- 238000011156 evaluation Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- 229920001721 polyimide Polymers 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 238000000682 scanning probe acoustic microscopy Methods 0.000 description 4
- 229920002126 Acrylic acid copolymer Polymers 0.000 description 3
- JIGUQPWFLRLWPJ-UHFFFAOYSA-N Ethyl acrylate Chemical compound CCOC(=O)C=C JIGUQPWFLRLWPJ-UHFFFAOYSA-N 0.000 description 3
- 230000000996 additive effect Effects 0.000 description 3
- 229910021417 amorphous silicon Inorganic materials 0.000 description 3
- CQEYYJKEWSMYFG-UHFFFAOYSA-N butyl acrylate Chemical compound CCCCOC(=O)C=C CQEYYJKEWSMYFG-UHFFFAOYSA-N 0.000 description 3
- 150000001732 carboxylic acid derivatives Chemical class 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- WHGNXNCOTZPEEK-UHFFFAOYSA-N dimethoxy-methyl-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound CO[Si](C)(OC)CCCOCC1CO1 WHGNXNCOTZPEEK-UHFFFAOYSA-N 0.000 description 3
- 239000005038 ethylene vinyl acetate Substances 0.000 description 3
- 239000000155 melt Substances 0.000 description 3
- 239000000178 monomer Substances 0.000 description 3
- PNJWIWWMYCMZRO-UHFFFAOYSA-N pent‐4‐en‐2‐one Natural products CC(=O)CC=C PNJWIWWMYCMZRO-UHFFFAOYSA-N 0.000 description 3
- 229920005569 poly(vinylidene fluoride-co-hexafluoropropylene) Polymers 0.000 description 3
- 229920001897 terpolymer Polymers 0.000 description 3
- 239000010409 thin film Substances 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- SMZOUWXMTYCWNB-UHFFFAOYSA-N 2-(2-methoxy-5-methylphenyl)ethanamine Chemical compound COC1=CC=C(C)C=C1CCN SMZOUWXMTYCWNB-UHFFFAOYSA-N 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N 2-Propenoic acid Natural products OC(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- 239000004925 Acrylic resin Substances 0.000 description 2
- 229920000178 Acrylic resin Polymers 0.000 description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 239000004642 Polyimide Substances 0.000 description 2
- 150000001336 alkenes Chemical class 0.000 description 2
- 125000004429 atom Chemical group 0.000 description 2
- DQXBYHZEEUGOBF-UHFFFAOYSA-N but-3-enoic acid;ethene Chemical compound C=C.OC(=O)CC=C DQXBYHZEEUGOBF-UHFFFAOYSA-N 0.000 description 2
- 125000002843 carboxylic acid group Chemical group 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- OTARVPUIYXHRRB-UHFFFAOYSA-N diethoxy-methyl-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound CCO[Si](C)(OCC)CCCOCC1CO1 OTARVPUIYXHRRB-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 229920001038 ethylene copolymer Polymers 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 229910021645 metal ion Inorganic materials 0.000 description 2
- JRZJOMJEPLMPRA-UHFFFAOYSA-N olefin Natural products CCCCCCCC=C JRZJOMJEPLMPRA-UHFFFAOYSA-N 0.000 description 2
- XNGIFLGASWRNHJ-UHFFFAOYSA-N phthalic acid Chemical compound OC(=O)C1=CC=CC=C1C(O)=O XNGIFLGASWRNHJ-UHFFFAOYSA-N 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000004381 surface treatment Methods 0.000 description 2
- JXUKBNICSRJFAP-UHFFFAOYSA-N triethoxy-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound CCO[Si](OCC)(OCC)CCCOCC1CO1 JXUKBNICSRJFAP-UHFFFAOYSA-N 0.000 description 2
- DQZNLOXENNXVAD-UHFFFAOYSA-N trimethoxy-[2-(7-oxabicyclo[4.1.0]heptan-4-yl)ethyl]silane Chemical compound C1C(CC[Si](OC)(OC)OC)CCC2OC21 DQZNLOXENNXVAD-UHFFFAOYSA-N 0.000 description 2
- PEVRKKOYEFPFMN-UHFFFAOYSA-N 1,1,2,3,3,3-hexafluoroprop-1-ene;1,1,2,2-tetrafluoroethene Chemical group FC(F)=C(F)F.FC(F)=C(F)C(F)(F)F PEVRKKOYEFPFMN-UHFFFAOYSA-N 0.000 description 1
- VXNZUUAINFGPBY-UHFFFAOYSA-N 1-Butene Chemical compound CCC=C VXNZUUAINFGPBY-UHFFFAOYSA-N 0.000 description 1
- JAHNSTQSQJOJLO-UHFFFAOYSA-N 2-(3-fluorophenyl)-1h-imidazole Chemical compound FC1=CC=CC(C=2NC=CN=2)=C1 JAHNSTQSQJOJLO-UHFFFAOYSA-N 0.000 description 1
- CFVWNXQPGQOHRJ-UHFFFAOYSA-N 2-methylpropyl prop-2-enoate Chemical compound CC(C)COC(=O)C=C CFVWNXQPGQOHRJ-UHFFFAOYSA-N 0.000 description 1
- DAJFVZRDKCROQC-UHFFFAOYSA-N 3-(oxiran-2-ylmethoxy)propyl-tripropoxysilane Chemical compound CCCO[Si](OCCC)(OCCC)CCCOCC1CO1 DAJFVZRDKCROQC-UHFFFAOYSA-N 0.000 description 1
- WFDIJRYMOXRFFG-UHFFFAOYSA-N Acetic anhydride Chemical group CC(=O)OC(C)=O WFDIJRYMOXRFFG-UHFFFAOYSA-N 0.000 description 1
- 229910000980 Aluminium gallium arsenide Inorganic materials 0.000 description 1
- GSBRKXLSNXZYON-UHFFFAOYSA-N C1(CCCCC1)C(CC)O[Si](OCCC)(OCCC)CC Chemical compound C1(CCCCC1)C(CC)O[Si](OCCC)(OCCC)CC GSBRKXLSNXZYON-UHFFFAOYSA-N 0.000 description 1
- 229910004613 CdTe Inorganic materials 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 229910001218 Gallium arsenide Inorganic materials 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000004696 Poly ether ether ketone Substances 0.000 description 1
- 239000004695 Polyether sulfone Substances 0.000 description 1
- OFOBLEOULBTSOW-UHFFFAOYSA-N Propanedioic acid Natural products OC(=O)CC(O)=O OFOBLEOULBTSOW-UHFFFAOYSA-N 0.000 description 1
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- FKNQFGJONOIPTF-UHFFFAOYSA-N Sodium cation Chemical compound [Na+] FKNQFGJONOIPTF-UHFFFAOYSA-N 0.000 description 1
- PTFCDOFLOPIGGS-UHFFFAOYSA-N Zinc dication Chemical compound [Zn+2] PTFCDOFLOPIGGS-UHFFFAOYSA-N 0.000 description 1
- 125000005396 acrylic acid ester group Chemical group 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- 125000003277 amino group Chemical group 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- 239000002216 antistatic agent Substances 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- WPYMKLBDIGXBTP-UHFFFAOYSA-N benzoic acid Chemical group OC(=O)C1=CC=CC=C1 WPYMKLBDIGXBTP-UHFFFAOYSA-N 0.000 description 1
- CHIHQLCVLOXUJW-UHFFFAOYSA-N benzoic anhydride Chemical group C=1C=CC=CC=1C(=O)OC(=O)C1=CC=CC=C1 CHIHQLCVLOXUJW-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- IAQRGUVFOMOMEM-UHFFFAOYSA-N butene Natural products CC=CC IAQRGUVFOMOMEM-UHFFFAOYSA-N 0.000 description 1
- 125000000484 butyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- HNEGQIOMVPPMNR-IHWYPQMZSA-N citraconic acid Chemical compound OC(=O)C(/C)=C\C(O)=O HNEGQIOMVPPMNR-IHWYPQMZSA-N 0.000 description 1
- 229940018557 citraconic acid Drugs 0.000 description 1
- 229920006026 co-polymeric resin Polymers 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 239000013065 commercial product Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 125000001142 dicarboxylic acid group Chemical group 0.000 description 1
- GAURFLBIDLSLQU-UHFFFAOYSA-N diethoxy(methyl)silicon Chemical compound CCO[Si](C)OCC GAURFLBIDLSLQU-UHFFFAOYSA-N 0.000 description 1
- 238000000113 differential scanning calorimetry Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 125000001495 ethyl group Chemical group [H]C([H])([H])C([H])([H])* 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 125000000524 functional group Chemical group 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 description 1
- 230000004313 glare Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229920006015 heat resistant resin Polymers 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 150000001261 hydroxy acids Chemical group 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- VZCYOOQTPOCHFL-UPHRSURJSA-N maleic acid Chemical compound OC(=O)\C=C/C(O)=O VZCYOOQTPOCHFL-UPHRSURJSA-N 0.000 description 1
- 239000011976 maleic acid Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- ARYZCSRUUPFYMY-UHFFFAOYSA-N methoxysilane Chemical compound CO[SiH3] ARYZCSRUUPFYMY-UHFFFAOYSA-N 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- LVHBHZANLOWSRM-UHFFFAOYSA-N methylenebutanedioic acid Natural products OC(=O)CC(=C)C(O)=O LVHBHZANLOWSRM-UHFFFAOYSA-N 0.000 description 1
- 229910021424 microcrystalline silicon Inorganic materials 0.000 description 1
- 229910021421 monocrystalline silicon Inorganic materials 0.000 description 1
- 230000003472 neutralizing effect Effects 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 1
- LGRFSURHDFAFJT-UHFFFAOYSA-N phthalic anhydride Chemical group C1=CC=C2C(=O)OC(=O)C2=C1 LGRFSURHDFAFJT-UHFFFAOYSA-N 0.000 description 1
- IEQIEDJGQAUEQZ-UHFFFAOYSA-N phthalocyanine Chemical compound N1C(N=C2C3=CC=CC=C3C(N=C3C4=CC=CC=C4C(=N4)N3)=N2)=C(C=CC=C2)C2=C1N=C1C2=CC=CC=C2C4=N1 IEQIEDJGQAUEQZ-UHFFFAOYSA-N 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920001197 polyacetylene Polymers 0.000 description 1
- 229910021420 polycrystalline silicon Inorganic materials 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920006393 polyether sulfone Polymers 0.000 description 1
- 229920002530 polyetherether ketone Polymers 0.000 description 1
- 239000002861 polymer material Substances 0.000 description 1
- 238000006116 polymerization reaction Methods 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- WYVAMUWZEOHJOQ-UHFFFAOYSA-N propionic anhydride Chemical group CCC(=O)OC(=O)CC WYVAMUWZEOHJOQ-UHFFFAOYSA-N 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 150000004756 silanes Chemical class 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 229910001415 sodium ion Inorganic materials 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- RINCXYDBBGOEEQ-UHFFFAOYSA-N succinic anhydride Chemical group O=C1CCC(=O)O1 RINCXYDBBGOEEQ-UHFFFAOYSA-N 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 239000012815 thermoplastic material Substances 0.000 description 1
- VZCYOOQTPOCHFL-UHFFFAOYSA-N trans-butenedioic acid Natural products OC(=O)C=CC(O)=O VZCYOOQTPOCHFL-UHFFFAOYSA-N 0.000 description 1
- UDUKMRHNZZLJRB-UHFFFAOYSA-N triethoxy-[2-(7-oxabicyclo[4.1.0]heptan-4-yl)ethyl]silane Chemical compound C1C(CC[Si](OCC)(OCC)OCC)CCC2OC21 UDUKMRHNZZLJRB-UHFFFAOYSA-N 0.000 description 1
- 239000000326 ultraviolet stabilizing agent Substances 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 239000004711 α-olefin Substances 0.000 description 1
Images
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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
- B32B27/308—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising acrylic (co)polymers
-
- 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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/30—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
- B32B27/304—Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising vinyl halide (co)polymers, e.g. PVC, PVDC, PVF, PVDF
-
- 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
-
- 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
- H01L31/049—Protective back 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
Definitions
- the present invention relates to a highly durable solar cell protective sheet having high adhesion between a protective layer and an adhesive sealing layer, and a flexible solar cell module in which a solar cell element is protected by the solar cell protective sheet.
- a rigid solar cell module based on glass and a flexible solar cell module based on a polyimide or polyester heat-resistant polymer material or a stainless thin film are known.
- flexible solar cell modules have been attracting attention because of their ease of transportation and construction due to reduction in thickness and weight, and resistance to impact.
- Such a flexible solar cell module is a flexible solar cell element in which a photoelectric conversion layer made of a silicon semiconductor or a compound semiconductor having a function of generating a current when irradiated with light is laminated in a thin film on a flexible substrate.
- the upper and lower surfaces are sealed with an adhesive sealing layer, and a protective layer is provided as the outermost layer.
- EVA resin ethylene-vinyl acetate (EVA) resin
- Patent Document 2 ethylene-vinyl acetate (EVA) resin
- thermoplastic material has often been used for the protective layer because it has high impact resistance and is light.
- PVDF poly (vinylidene fluoride)
- PVDF poly (vinylidene fluoride)
- the adhesion between the adhesive sealing layer and the protective layer is insufficient, and the protective layer may peel off from the adhesive sealing layer when left in the environment for a long time. There was a problem in terms of durability.
- an attempt is made to improve the adhesion between layers by providing an adhesive layer made of an acrylic resin or a mixture of an acrylic resin and a fluororesin between the adhesive sealing layer and the protective layer. .
- an adhesive layer made of an acrylic resin or a mixture of an acrylic resin and a fluororesin between the adhesive sealing layer and the protective layer.
- the present invention provides a highly durable solar cell protective sheet having high adhesion between a protective layer and an adhesive sealing layer, and a flexible solar cell module in which solar cell elements are protected by the solar cell protective sheet. For the purpose.
- the present invention is a solar cell protective sheet in which a protective layer made of a fluororesin sheet and an adhesive sealing layer are laminated, wherein the protective layer has a nitrogen atom concentration of 0. 0 on the surface in contact with the adhesive sealing layer. It has a surface layer containing 2 mol% or more, and the adhesive sealing layer is a solar cell protective sheet containing a thermal adhesive resin having an acid group or an acid anhydride group.
- the present invention is described in detail below.
- the inventors of the present invention form a surface layer containing 0.2 mol% or more of nitrogen atoms on the surface of the protective layer made of a fluororesin sheet in contact with the adhesive sealing layer, and thermally bond the acid group or the acid anhydride group. It has been found that the adhesive strength between layers can be remarkably increased by combining with an adhesive sealing layer containing an adhesive resin. According to the present invention, the adhesiveness between the protective layer and the adhesive sealing layer can be improved without providing an adhesive layer as in the prior art, so there is no deterioration in weather resistance or heat resistance, and roll-to-roll method or the like. Therefore, even when the solar cell elements are continuously sealed, wrinkles and curls are hardly generated.
- the solar cell protective sheet of the present invention has a structure in which a protective layer and an adhesive sealing layer are laminated.
- FIG. 1 the longitudinal cross-section schematic diagram of an example of the solar cell protection sheet B which consists of the protective layer 1 and the adhesion sealing layer 2 is shown.
- a surface layer 12 containing 0.2 mol% or more of nitrogen atoms is formed on the surface of the protective layer 1 in contact with the adhesive sealing layer 2.
- the protective layer is the outermost layer in the obtained flexible solar cell module, and prevents external impact or corrosion of the solar cell element. It has a role to prevent.
- the protective layer is made of a fluorine resin sheet.
- the fluororesin sheet is not particularly limited as long as it is excellent in transparency, heat resistance, and flame retardancy.
- Tetrafluoroethylene-ethylene copolymer ETFE
- ECTFE ethylene chlorotrifluoroethylene resin
- PCTFE Polychlorotrifluoroethylene resin
- PVDF polyvinylidene fluoride resin
- FAP polyvinyl fluoride resin
- PVDF tetrafluoroethylene-hexafluoropropylene
- the fluororesin is more preferably a polyvinylidene fluoride resin (PVDF), a tetrafluoroethylene-ethylene copolymer (ETFE), or a polyvinyl fluoride resin (PVF) in that it is superior in heat resistance and transparency.
- PVDF polyvinylidene fluoride resin
- ETFE tetrafluoroethylene-ethylene copolymer
- PVF polyvinyl fluoride resin
- the protective layer has a surface layer containing 0.2 mol% or more of nitrogen atoms on the surface in contact with the adhesive sealing layer.
- the lower limit of the nitrogen atom content in the surface layer is 0.2 mol%. If it is less than 0.2 mol%, the effect of improving the adhesion between the protective layer and the adhesive sealing layer cannot be obtained.
- the minimum with preferable content of the nitrogen atom in the surface layer of the said protective layer is 0.5 mol%, and a more preferable minimum is 1.0 mol%.
- the upper limit of the content of nitrogen atoms in the surface layer of the protective layer is not particularly limited, but technically about 20 mol% is considered to be a substantial upper limit.
- content of the nitrogen atom in a surface layer means the ratio of content of the nitrogen atom with respect to content of all the atoms contained in the said surface layer.
- the content of each atom contained in the surface layer can be measured by, for example, X-ray photoelectron spectroscopy (XPS) or Auger electron spectroscopy (AES).
- a preferable lower limit of the thickness of the surface layer is 0.05 nm. If the thickness of the surface layer is less than 0.05 nm, the effect of improving the adhesion between the protective layer and the adhesive sealing layer may not be obtained. A more preferable lower limit of the thickness of the surface layer is 0.1 nm.
- the upper limit of the thickness of the surface layer is not particularly limited, but technically about 10 nm is considered to be a substantial upper limit. Note that the thickness of the surface layer is measured from a cross-sectional plot of the surface layer specific element by etching the surface layer using, for example, X-ray photoelectron spectroscopy (XPS) or Auger electron spectroscopy (AES). Can do.
- Examples of the method for forming the surface layer on the surface of the protective layer in contact with the adhesive sealing layer include a method in which the surface of the protective layer is subjected to plasma treatment and a method in which corona discharge treatment is performed in a nitrogen atmosphere.
- the adhesive strength with the adhesive sealing layer containing an acid group or an acid anhydride group is remarkably increased, and when left in the environment for a long time. It is possible to prevent the protective layer from being peeled off from the adhesive sealing layer.
- the method of performing plasma treatment is preferable because the generation of wrinkles is reduced and the adhesive strength after high temperature and high humidity conditions can be maintained high.
- the plasma treatment to the protective layer can be performed by a conventionally known method.
- Specific examples include nitrogen gas plasma, nitrogen / methane mixed gas plasma, nitrogen / carbon dioxide mixed gas plasma, and nitrogen / argon mixed gas plasma.
- nitrogen gas plasma under conditions of a processing speed of 25 m / min or less and a processing intensity of 0.8 kW or more. It is preferable to process.
- the corona discharge treatment to the protective layer can be performed by a conventionally known method.
- Specific examples include nitrogen gas corona, nitrogen / hydrogen mixed gas corona, nitrogen / amine mixed gas corona, and nitrogen / methane mixed gas corona.
- nitrogen gas corona discharge treatment under the condition of a treatment amount of 20 W / m 2 or more.
- the protective layer preferably has an embossed shape on the surface in contact with the adhesive sealing layer.
- the adhesive force between the protective layer and the adhesive sealing layer can be further increased.
- the emboss shape on the surface of the protective layer may be a regular uneven shape or a random uneven shape.
- the protective layer has an embossed shape on the surface opposite to the surface in contact with the adhesive sealing layer, that is, the surface that seals the solar cell element and becomes the outermost layer of the flexible solar cell module. It is preferable.
- the outermost layer has an embossed shape, it is possible to reduce the reflection loss of sunlight, prevent glare, and improve the appearance.
- the embossed shape is a method of performing embossing at the same time when the molten resin is cooled by using an embossed roll as a cooling roll when the fluororesin sheet constituting the protective layer is extruded by a melt extrusion method. Or the like.
- the embossing may be performed after the plasma treatment or the corona discharge treatment first, but the embossed shape is determined by a method using an embossing roll in the melt extrusion method.
- a method of performing plasma treatment or corona discharge treatment on the embossed surface of the applied fluororesin sheet by the above method is preferable.
- the preferable lower limit of the thickness of the protective layer is 10 ⁇ m, and the preferable upper limit is 100 ⁇ m. If the thickness of the protective layer is less than 10 ⁇ m, insulation may not be ensured or flame retardancy may be impaired. If the thickness of the protective layer exceeds 100 ⁇ m, the weight of the flexible solar cell module may be increased, which is economically disadvantageous.
- the minimum with more preferable thickness of the said protective layer is 15 micrometers, and a more preferable upper limit is 80 micrometers.
- the solar cell protective sheet of the present invention has an adhesive sealing layer.
- the said adhesive sealing layer has a role which seals a solar cell element.
- the adhesive sealing layer contains a heat-adhesive resin having an acid group or an acid anhydride group.
- a high interlayer adhesion can be achieved by combining such an adhesive sealing layer with a protective layer having a surface layer containing 0.2 mol% or more of the nitrogen atoms.
- Examples of the acid group include a carboxyl group, an unsaturated carboxylic acid group, a hydroxy acid group, an aromatic carboxylic acid group, and a dicarboxylic acid group.
- Examples of the acid anhydride group include a maleic anhydride group, an acetic anhydride group, a propionic anhydride group, a succinic anhydride group, a phthalic anhydride group, and a benzoic anhydride group.
- heat-adhesive resin having an acid group or an acid anhydride group examples include an acid-modified polyolefin, an acid-modified ethylene-glycidyl methacrylate copolymer, an ionomer, and an ethylene-acrylic acid ester-anhydride group copolymer. It is done.
- thermal adhesive resins having an acid group or an acid anhydride group may be used alone or in combination of two or more.
- the acid-modified polyolefin can prevent the generation of wrinkles and curls when a solar cell element is sealed using the solar cell protective sheet of the present invention to produce a flexible solar cell module, and the adhesion to the solar cell surface is improved.
- it is preferably a maleic anhydride-modified polyolefin.
- the maleic anhydride-modified polyolefin is a resin in which an ⁇ -olefin-ethylene copolymer having an ⁇ -olefin content of 1 to 25% by weight is graft-modified with maleic anhydride, and the total content of maleic anhydride The amount is preferably 0.1 to 3% by weight.
- the ionomer is preferably one obtained by neutralizing part or all of the unsaturated carboxylic acid group of the ethylene-unsaturated carboxylic acid copolymer with a metal ion.
- the ethylene-unsaturated carboxylic acid copolymer include a copolymer comprising at least a copolymer component of ethylene and an unsaturated carboxylic acid.
- the ionomer can be produced by a known method.
- the unsaturated carboxylic acid examples include acrylic acid, methacrylic acid, maleic acid, phthalic acid, citraconic acid, itaconic acid, and the like, among which acrylic acid and methacrylic acid are preferable.
- acrylic acid and methacrylic acid are preferable.
- metal ion a sodium ion and a zinc ion are preferable.
- the minimum with preferable content of the said unsaturated carboxylic acid component is 15 weight%, and a preferable upper limit is 25 weight%.
- the ethylene-unsaturated carboxylic acid copolymer may further contain a (meth) acrylic acid ester component as a third component.
- the (meth) acrylic acid ester is at least one selected from the group consisting of methyl (meth) acrylate, ethyl (meth) acrylate and butyl (meth) acrylate from the viewpoint of cost and polymerizability. Is preferred. Among these, from the viewpoint of the melting point, an acrylate ester is preferable, and specifically, n-butyl acrylate, isobutyl acrylate, and ethyl acrylate are more preferable.
- the content of the (meth) acrylic acid ester component is preferably 25% by weight or less. If the content of the (meth) acrylic acid ester component exceeds 25% by weight, the melting point may be too low.
- the upper limit with more preferable content of the said (meth) acrylic acid ester component is 20 weight%.
- the ethylene- (meth) acrylic acid copolymer is preferably an ethylene-acrylic acid ester-maleic anhydride terpolymer.
- the ethylene-acrylic acid ester-maleic anhydride terpolymer is a copolymer composed of at least three components of ethylene, acrylic acid ester and maleic anhydride.
- the acrylic ester is preferably at least one selected from the group consisting of methyl acrylate, ethyl acrylate, and butyl acrylate from the viewpoint of cost and polymerizability.
- the ethylene- (meth) acrylic acid copolymer has an ethylene component content of 71 to 93% by weight, an acrylic ester component content of 5 to 28% by weight, and a maleic anhydride component content. Is preferably 0.1 to 4% by weight.
- the ethylene- (meth) acrylic acid copolymer is preferably an ethylene-glycidyl methacrylate copolymer.
- the ethylene-glycidyl methacrylate copolymer is a copolymer composed of at least two components of ethylene and glycidyl methacrylate.
- the content of the glycidyl methacrylate component in the ethylene-glycidyl methacrylate copolymer is preferably 7% by weight and preferably 9% by weight from the viewpoint of the melting point.
- the ethylene-glycidyl methacrylate copolymer can be produced using a conventionally known polymerization method.
- the ethylene-glycidyl methacrylate copolymer may further contain components derived from other monomers in addition to the ethylene component and the glycidyl methacrylate component.
- the other monomer is not particularly limited as long as it is a monomer copolymerizable with ethylene and glycidyl methacrylate as long as the physical properties necessary for the present invention are not impaired.
- (meth) acrylate is preferred from the viewpoint of melting point, polymerizability, and cost.
- the (meth) acrylate is preferably an acrylate, and methyl acrylate, ethyl acrylate or butyl acrylate is particularly preferable.
- the preferable upper limit of the content of the (meth) acrylate component is 15% by weight, and the more preferable upper limit is 10% by weight.
- the lower limit is not particularly limited as long as the copolymer resin can be obtained.
- the adhesive sealing layer preferably further contains a silane compound having a glycidyl group.
- a silane compound having a glycidyl group By containing such a silane compound having a glycidyl group, the adhesive force between the protective layer and the adhesive sealing layer can be further improved. Moreover, since almost no foreign substances such as gel are generated when the solar cell protective sheet is manufactured, it can be manufactured continuously. Moreover, when a solar cell element is continuously sealed by a roll-to-roll method or the like, the resin hardly protrudes from the end portion of the protective layer of the obtained flexible solar cell module. Furthermore, the adhesive force between the adhesive sealing layer and the surface of the solar cell element can also be improved.
- silane compound having a glycidyl group examples include 3-glycidoxypropylmethyldimethoxysilane, 3-glycidoxypropylmethyldiethoxysilane, 3-glycidoxypropyltrimethoxysilane, and 3-glycidoxypropyltriethoxy.
- 3-glycidoxypropyltrimethoxysilane, 2- (3,4-epoxycyclohexyl) ethyltrimethoxysilane, 3-glycidoxypropyltriethoxysilane, 3-glycidoxypropylmethyldimethoxysilane, 3- Glycidoxypropylmethyldiethoxysilane is preferred.
- silane compounds having a glycidyl group are Z-6040 (3-glycidoxypropyltrimethoxysilane), Z-6043 (2- (3,4-epoxycyclohexyl) ethyltril) manufactured by Toray Dow Corning. Methoxysilane), KBE-403 (3-glycidoxypropyltriethoxysilane), KBM-402 (3-glycidoxypropylmethyldimethoxysilane), KBE-402 (3-glycidoxypropyl) manufactured by Shin-Etsu Silicone Methyldiethoxysilane) and the like.
- the content of the silane compound having a glycidyl group in the adhesive sealing layer is 0.05 to 5 parts by weight with respect to 100 parts by weight of the thermoadhesive resin having an acid group or an acid anhydride group. preferable.
- the adhesive force between the protective layer and the adhesive sealing layer and the adhesive force between the adhesive sealing layer and the solar cell element may be reduced.
- the content of the silane compound is more preferably 0.07 parts by weight with respect to 100 parts by weight of the thermoadhesive resin having the acid group or acid anhydride group, and the upper limit is 1.5 parts by weight. It is more preferable that
- the said adhesive sealing layer may further contain the other additive in the range which does not impair the physical property.
- the other additives include, for example, an ultraviolet stabilizer, an antioxidant, a light resistance stabilizer, a plasticizer, a filler, a colorant, a pigment, an antistatic agent, a surfactant, a toning liquid, and a refractive index matching additive. Agents and dispersion aids.
- the minimum with the preferable thickness of the said adhesive sealing layer is 80 micrometers, and a preferable upper limit is 700 micrometers. If the thickness of the adhesive sealing layer is less than 80 ⁇ m, the insulating property of the flexible solar cell module may not be maintained. If it exceeds 700 ⁇ m, the flame resistance of the flexible solar cell module may be adversely affected, or the flexible solar cell The module may become heavy.
- the minimum with more preferable thickness of the said adhesive sealing layer is 150 micrometers, and a more preferable upper limit is 400 micrometers.
- the method for forming the adhesive sealing layer includes, for example, a predetermined weight ratio of a silane compound having a glycidyl group and an additive added as necessary to the thermal adhesive resin having an acid group or an acid anhydride group. And a method of forming an adhesive sealing layer by feeding into an extruder and melting and kneading, and extruding into a sheet form from the extruder.
- a single screw extruder or a twin screw extruder may be used as the extruder.
- the solar cell protective sheet of the present invention is obtained by laminating the protective layer and the adhesive sealing layer.
- the lamination method for example, a conventionally known method such as a vacuum laminating method, a roll laminating method, or an extrusion laminating method can be used.
- the solar cell protective sheet of the present invention is for manufacturing a flexible solar cell module by sealing solar cell elements.
- the flexible solar cell module in which the solar cell protective sheet of the present invention and the solar cell element in which the photoelectric conversion layer is disposed on the flexible base material are laminated and integrated are also one aspect of the present invention.
- the solar cell element is generally composed of a photoelectric conversion layer in which electrons are generated by receiving light, an electrode layer for taking out the generated electrons, and a flexible substrate.
- FIG. 3 the longitudinal cross-sectional schematic diagram of an example of the solar cell element C by which the photoelectric converting layer 3 is arrange
- the flexible substrate is not particularly limited as long as it is flexible and can be used for a flexible solar cell element.
- heat-resistant resin such as polyimide, polyetheretherketone, polyethersulfone, etc.
- the base material which consists of can be mentioned.
- the preferable lower limit of the thickness of the flexible substrate is 10 ⁇ m, and the preferable upper limit is 80 ⁇ m.
- the photoelectric conversion layer examples include crystal semiconductors such as single crystal silicon, single crystal germanium, polycrystalline silicon, and microcrystalline silicon, amorphous semiconductors such as amorphous silicon, GaAs, InP, AlGaAs, Cds, CdTe, and Cu 2. Examples thereof include compounds formed from compound semiconductors such as S, CuInSe 2 and CuInS 2 , and organic semiconductors such as phthalocyanine and polyacetylene.
- the photoelectric conversion layer may be a single layer or a multilayer. The minimum with the preferable thickness of the said photoelectric converting layer is 0.5 micrometer, and a preferable upper limit is 10 micrometers.
- the electrode layer is a layer made of an electrode material.
- the electrode layer may be on the photoelectric conversion layer, between the photoelectric conversion layer and the flexible base, or on the surface of the flexible base, as necessary.
- the solar cell element may have a plurality of the electrode layers.
- the electrode material is preferably a general transparent electrode material such as a metal oxide. Although it does not specifically limit as said transparent electrode material, ITO or ZnO etc. are used suitably.
- the bus electrode and the finger electrode attached thereto may be patterned with a metal such as silver.
- the electrode layer on the back side (back side) does not need to be transparent and may be made of a general electrode material, but silver is preferably used as the electrode material.
- the solar cell element does not specifically limit as a method of manufacturing the said solar cell element, For example, it can manufacture by well-known methods, such as arrange
- the solar cell element may have a long shape wound in a roll shape or a rectangular sheet shape.
- the flexible solar cell module of the present invention has an adhesive sealing layer 2 and a protective layer 1 on the side of the photoelectric conversion layer 3 of the solar cell element C.
- the adhesive sealing layer and the protective layer may also be provided on the side surface of the flexible substrate.
- FIG. 4 is a schematic longitudinal sectional view of a flexible solar cell module F of the present invention comprising a protective layer 1, an adhesive sealing layer 2, a photoelectric conversion layer 3, a flexible substrate 4, an adhesive sealing layer 2 and a protective layer 1 in this order. Indicates.
- the solar cell protective sheet comprising the adhesive sealing layer and the protective layer is formed on at least the light receiving surface of the solar cell element by using a pair of heat rolls.
- a method of constricting and thermocompression bonding can be mentioned.
- the light receiving surface of the solar cell element is a surface that can receive light and is a surface on which the photoelectric conversion layer of the solar cell element is disposed.
- the solar cell element and the solar cell element are arranged in a state where the surface on which the photoelectric conversion layer of the solar cell element is disposed and the side surface of the adhesive sealing layer of the solar cell protection sheet are opposed to each other.
- a method of laminating solar cell protective sheets, constricting them using a pair of heat rolls, and thermocompression bonding is preferable.
- the preferable lower limit of the temperature of the heat roll when constricting using the pair of heat rolls is 70 ° C., and the preferable upper limit is 160 ° C. If the temperature of the heat roll is less than 70 ° C., adhesion failure may occur. If the temperature of the heat roll exceeds 160 ° C., wrinkles are likely to occur during thermocompression bonding.
- a more preferable lower limit of the temperature of the heat roll is 80 ° C., and a more preferable upper limit is 110 ° C.
- a preferable lower limit of the rotation speed of the heat roll is 0.1 m / min, and a preferable upper limit is 10 m / min. If the rotational speed of the heat roll is less than 0.1 m / min, wrinkles may easily occur after thermocompression bonding. When the rotation speed of the heat roll exceeds 10 m / min, there is a possibility that adhesion failure may occur.
- a more preferable lower limit of the rotation speed of the heat roll is 0.3 m / min, and a more preferable upper limit is 5 m / min.
- FIG. 5 An example of the method for producing the flexible solar cell module of the present invention will be specifically described with reference to FIG.
- a long solar cell protective sheet B composed of the protective layer and the adhesive sealing layer and wound in a roll shape, and a solar cell element C are prepared.
- the roll of the solar cell protection sheet B and the solar cell element C is unwound, and the light receiving surface of the photoelectric conversion layer of the solar cell element C and the adhesive sealing layer surface of the solar cell protection sheet B are arranged to face each other. Both are laminated to obtain a laminated sheet D.
- the laminated sheet D is supplied between a pair of rolls E and E heated to a predetermined temperature, and the laminated sheet D is heated and thermocompression bonded while pressing in the thickness direction, so that the solar cell element C and the solar cell.
- the protective sheet B is bonded and integrated. Thereby, a photoelectric converting layer is sealed by the adhesive sealing layer, and the flexible solar cell module A can be obtained.
- the solar cell protective sheet of the present invention is applied to the side surface of the flexible substrate of the solar cell, and the adhesive sealing layer is a flexible substrate.
- a method of thermocompression bonding by narrowing them using a pair of heat rolls may be performed on the light receiving surface of the solar cell element described above before the step of thermocompression bonding the solar cell protective sheet, It may be done at the same time or later.
- the solar cell protective sheet of the present invention for example, an example of a method for producing the flexible solar cell module of the present invention by simultaneously sealing the photoelectric conversion layer side surface and the flexible substrate side surface of the solar cell element, This will be described with reference to FIG. Specifically, while preparing a long solar cell element C wound in a roll shape, two long solar cell protective sheets wound in a roll shape are prepared. And as shown in FIG. 6, while unwinding the elongate solar cell protection sheets B and B, respectively, unwind the elongate solar cell element C, and the adhesive sealing layer of two solar cell protection sheets is In a state of facing each other, the solar cell protective sheets B and B are overlapped with each other through the solar cell element C to obtain a laminated sheet D.
- the solar cell protective sheets B, B are brought together.
- the solar cell element C is sealed with the solar cell protective sheets B and B, and the flexible solar cell module F is continuously manufactured.
- the solar cell protective sheets B and B are overlapped with each other via the solar cell element C to form the laminated sheet D, and at the same time, the laminated sheet D is heated while being pressed in the thickness direction. May be.
- FIG. 7 an example of the manufacturing point of the flexible solar cell module of this invention at the time of using a rectangular sheet-like thing as the solar cell element C is shown in FIG. Specifically, instead of the long solar cell element C wound in a roll shape, a rectangular sheet-like solar cell element C having a predetermined size is prepared. And as shown in FIG. 7, the solar cell protection sheet which unwinded the elongate solar cell protection sheet B and B currently wound by roll shape, and made each adhesive sealing layer face each other. A solar cell element C is supplied between B and B at predetermined time intervals, and the solar cell protective sheets B and B are overlapped with each other via the solar cell element C to obtain a laminated sheet D.
- the solar cell protective sheets B, B are brought together.
- the solar cell element C is sealed with the solar cell protective sheets B and B, and the flexible solar cell module F is continuously manufactured.
- the laminated sheet D may be heated while being pressed in the thickness direction simultaneously with the formation of the laminated sheet D.
- the flexible solar cell module of the present invention can be suitably manufactured by applying such a roll-to-roll method.
- the solar cell protective sheet and the solar cell element of the present invention cut into a desired shape are prepared, and the adhesive sealing layer of the solar cell protective sheet;
- the solar cell protective sheet and the solar cell element are laminated in a state where the photoelectric conversion layer side surface or both surfaces of the solar cell element are opposed to each other, and the obtained laminate is stationary under reduced pressure.
- the method may be such that the solar cell element is sealed with the solar cell protective sheet by heating while applying a pressing force in the thickness direction.
- the step of heating the laminate while applying a pressing force in the thickness direction under reduced pressure can be performed using a conventionally known apparatus such as a vacuum laminator.
- the flexible solar cell module by which the solar cell element was protected by the solar cell protective sheet excellent in durability with the high adhesiveness of a protective layer and an adhesive sealing layer, and this solar cell protective sheet. can be provided.
- Example 1 Preparation of PVDF sheet having surface layer Polyvinylidene fluoride (PVDF, manufactured by Arkema Corp., Kyner 720) is used as a fluororesin using a single screw extruder at 250 ° C., 180 rotations / minute, extrusion rate of 12 kg / hour. After melt-kneading under the above conditions, melt extrusion was performed, and an embossing roll was used as a cooling roll, thereby obtaining a PVDF sheet having a thickness of 50 ⁇ m having an embossed shape on one surface.
- PVDF Polyvinylidene fluoride
- a plasma processing apparatus (AP / T04-R1540 apparatus and product lineup made by Sekisui Chemical Co., Ltd.) on the surface of the obtained PVDF sheet having an embossed shape, 1 head, sheet processing speed of 5 m / min, processing strength of 1
- a nitrogen gas plasma treatment was performed under a condition of 3 kW to obtain a PVDF sheet having a surface layer.
- About the PVDF sheet which has the obtained surface layer when nitrogen atom content of the surface layer was measured by X-ray photoelectron spectroscopy (XPS), it was 2.02 mol%.
- Modified olefin resin 100 obtained by graft-modifying a butene-ethylene copolymer having an ethylene component content of 75% by weight and a butene component content of 25% by weight with maleic anhydride
- a composition for an adhesive sealing layer comprising, by weight, 0.5 part by weight of 3-glycidoxypropyltrimethoxysilane (trade name “Z-6040”, manufactured by Dow Corning Toray) as a silane compound having a glycidyl group
- Z-6040 3-glycidoxypropyltrimethoxysilane
- the adhesive sealing layer composition is laminated while being extruded on the surface layer of the PVDF sheet having the surface layer obtained above to form an adhesive sealing layer, and contains a modified olefin resin and a silane compound.
- a solar cell protective sheet having a long and constant width was obtained by laminating and integrating an adhesive sealing layer having a thickness of 300 ⁇ m and a protective layer having a thickness of 50 ⁇ m.
- the modified olefin resin used had a melt flow rate (MFR) of 3 g / 10 min and a maximum peak temperature (Tm) of an endothermic curve measured by differential scanning calorimetry of 80 ° C.
- the total content of maleic anhydride in the modified olefin resin was 0.3% by weight.
- a photoelectric conversion layer made of thin amorphous silicon is formed on a flexible base material made of a flexible polyimide film, and A solar cell element wound in a roll shape and a solar cell protection sheet in which the solar cell protection sheet obtained above was wound in a roll shape were prepared.
- the solar cell element C and the solar cell protection sheet B are unwound, the solar cell protection sheet B is placed on the photoelectric conversion layer of the solar cell element C, and the adhesive sealing layer is the photoelectric conversion layer.
- Laminated sheets D were laminated so as to face the layers.
- the laminated sheet D is supplied between a pair of rolls E and E heated to the temperatures shown in Table 1, and the laminated sheet D is heated while pressing the laminated sheet D in the thickness direction, and the solar cell protective sheet
- the photoelectric conversion layer was sealed by bonding and integrating B with the solar cell element C, and the flexible solar cell module A was continuously manufactured, and wound around a winding shaft (not shown).
- (3-2) Manufacture of flexible solar cell module by vacuum laminating method
- a solar cell element in which a photoelectric conversion layer made of amorphous silicon in the form of a thin film is formed on a flexible base material made of a polyimide film having flexibility.
- the solar cell protective sheet obtained above was prepared by cutting it into a predetermined shape.
- the solar cell protective sheet and the solar cell element were laminated in a state where the adhesive sealing layer of the solar cell protective sheet and the photoelectric conversion layer side surface of the solar cell element were opposed to each other.
- the obtained laminate is heated using a vacuum laminator under a reduced pressure atmosphere of 1000 Pa or less while applying a pressing force in the thickness direction under the conditions shown in Table 1, and the solar cell element is sealed with a solar cell protective sheet. Stopped.
- Examples 2 to 4, 7 to 9, 13, 15 and Comparative Examples 1 to 4, 6 In the preparation of PVDF sheet, the presence or absence of embossed shape, the plasma treatment conditions were changed as shown in Tables 1 to 4, and the composition of modified olefin resin and the presence or absence of silane compound in the production of solar cell protective sheet A solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 1 except that the values were changed as shown in Tables 1 to 4.
- Examples 5 and 14 A vinylidene fluoride-hexafluoropropylene copolymer (trade name “Kyner Flex 2800” manufactured by Arkema Co., Ltd.) as a fluororesin is used at 250 ° C., 180 rotations / minute, and an extrusion rate of 12 kg / hour using a single screw extruder. After melt kneading under the conditions, melt extrusion was performed, and an embossing roll was used as a cooling roll to obtain a 50 ⁇ m thick PVDF-HFP copolymer sheet having an embossed shape on one surface.
- the surface of the obtained PVDF-HFP copolymer sheet having an embossed shape is subjected to plasma surface treatment using a plasma treatment device (AP / T04-R1540 device and product lineup manufactured by Sekisui Chemical Co., Ltd.)
- a PVDF sheet was obtained. Except for changing the plasma treatment conditions as shown in Tables 1 and 2 or changing the composition of the modified olefin resin and the presence or absence of the silane compound in the production of the solar cell protective sheet as shown in Tables 1 and 2.
- a solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 1.
- Tetrafluoroethylene-ethylene copolymer (trade name “Neofluon ETFE”, manufactured by Daikin Industries, Ltd.) is used as a fluororesin under the conditions of 310 ° C., 180 rotations / minute, extrusion rate of 12 kg / hour using a single screw extruder. After melt kneading, melt extrusion was performed, and an embossing roll was used as a cooling roll to obtain an ETFE sheet having an embossed shape on one surface and a thickness of 50 ⁇ m.
- a nitrogen gas plasma treatment was performed under a condition of .3 kW to obtain an ETFE sheet having a surface layer.
- a solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 1 except that the ETFE sheet having the obtained surface layer was used.
- Example 10 Comparative Example 7
- the plasma treatment conditions were as shown in Tables 2 and 4.
- a commercial product of ionomer resin (trade name: Himiran 1705, Zn ion type, manufactured by Mitsui DuPont Polychemical Co., Ltd.) was used in place of the modified olefin-based resin.
- a solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 1.
- Example 11 Comparative Example 8
- the plasma treatment conditions were as shown in Tables 2 and 4.
- an ethylene-acrylic acid ester-maleic anhydride terpolymer containing a predetermined amount of components described in Tables 2 and 4 was used, as described in Tables 2 and 4.
- a solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 1.
- Example 12 Comparative Example 9
- the plasma treatment conditions were as shown in Tables 2 and 4.
- a resin obtained by modifying an ethylene-glycidyl methacrylate copolymer containing a predetermined amount of ethylene component and glycidyl methacrylate component described in Tables 2 and 4 with maleic anhydride was used.
- a solar cell protective sheet and a flexible solar cell module were obtained by the same method as in Example 1.
- PVDF sheet having surface layer Polyvinylidene fluoride (PVDF, manufactured by Arkema Corp., Kyner 720) is used as a fluororesin using a single screw extruder at 250 ° C., 180 rotations / minute, extrusion rate of 12 kg / hour. After melt-kneading under the above conditions, melt extrusion was performed, and an embossing roll was used as a cooling roll, thereby obtaining a PVDF sheet having a thickness of 50 ⁇ m having an embossed shape on one surface.
- PVDF Polyvinylidene fluoride
- the surface having the embossed shape of the obtained PVDF sheet is subjected to a nitrogen gas corona discharge treatment using a corona discharge treatment device (manufactured by Kasuga Denki Co., Ltd., high frequency power supply device and treatment station) under conditions of a treatment amount of 20 W / m 2.
- a PVDF sheet having a surface layer was obtained.
- a solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 1 except that the obtained PVDF sheet having the surface layer was used.
- Examples 17 and 18, Comparative Example 5 Except for changing the corona discharge treatment conditions as shown in Tables 2 and 3 in the preparation of the PVDF sheet, and changing the presence or absence of the silane compound as shown in Tables 2 and 3 in the production of the solar cell protective sheet.
- a solar cell protective sheet and a flexible solar cell module were obtained in the same manner as in Example 16.
- the initial delamination strength between the protective layer and the adhesive sealing layer is generally required to be 10 N / cm or more, preferably 20 N / cm or more, and more preferably 30 N / cm or more.
- the flexible solar cell module by which the solar cell element was protected by the solar cell protective sheet excellent in durability with the high adhesiveness of a protective layer and an adhesive sealing layer, and this solar cell protective sheet. can be provided.
Landscapes
- 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)
- Laminated Bodies (AREA)
Abstract
La présente invention concerne la fourniture d'une feuille de protection de cellule solaire, qui présente une forte adhésivité entre une couche de protection et une couche d'étanchéité adhésive, ainsi qu'une excellente durabilité et un module de cellule solaire flexible, dans lequel des éléments de cellule solaire sont protégés par ladite feuille de protection de cellule solaire. Cette feuille de protection de cellule solaire est un stratifié d'une couche de protection, qui comprend une feuille de résine à base de fluor, et d'une couche d'étanchéité adhésive, la couche de protection ayant une couche de surface avec 0,2 % en moles ou plus d'atomes d'azote sur la surface, en contact avec la couche d'étanchéité adhésive et la couche d'étanchéité adhésive contenant une résine adhésive à la chaleur ayant un groupe acide ou un groupe anhydride d'acide.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2014535590A JPWO2014042217A1 (ja) | 2012-09-13 | 2013-09-12 | 太陽電池保護シート及びフレキシブル太陽電池モジュール |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2012-201695 | 2012-09-13 | ||
JP2012201695 | 2012-09-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2014042217A1 true WO2014042217A1 (fr) | 2014-03-20 |
Family
ID=50278326
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2013/074717 WO2014042217A1 (fr) | 2012-09-13 | 2013-09-12 | Feuille de protection de cellule solaire et module de cellule solaire flexible |
Country Status (2)
Country | Link |
---|---|
JP (1) | JPWO2014042217A1 (fr) |
WO (1) | WO2014042217A1 (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2019053832A (ja) * | 2017-09-12 | 2019-04-04 | トヨタ自動車株式会社 | 電極の製造方法 |
JP7535235B2 (ja) | 2020-03-19 | 2024-08-16 | 大日本印刷株式会社 | 表面改質フッ素系樹脂フィルム、積層体、及び複合ゴム成形体の製造方法、並びに表面改質フッ素系樹脂フィルム、積層体、及び複合ゴム成形体 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114211844B (zh) * | 2021-11-26 | 2023-05-16 | 常州斯威克光伏新材料有限公司 | 一种光伏用透明背板及其制备方法 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004031445A (ja) * | 2002-06-21 | 2004-01-29 | Du Pont Mitsui Polychem Co Ltd | 太陽電池モジュールの表層構造 |
JP2004055970A (ja) * | 2002-07-23 | 2004-02-19 | Fuji Electric Holdings Co Ltd | 太陽電池モジュールとその製造方法 |
JP2012074419A (ja) * | 2010-09-27 | 2012-04-12 | Dainippon Printing Co Ltd | 太陽電池モジュール用裏面保護シート、太陽電池モジュール用裏面一体化シート及び太陽電池モジュール |
WO2012056941A1 (fr) * | 2010-10-28 | 2012-05-03 | 富士フイルム株式会社 | Module de cellules solaires et son procédé de fabrication |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102725865A (zh) * | 2010-01-26 | 2012-10-10 | 积水化学工业株式会社 | 太阳能电池用密封材料、太阳能电池保护片以及太阳能电池组件的制造方法 |
-
2013
- 2013-09-12 JP JP2014535590A patent/JPWO2014042217A1/ja active Pending
- 2013-09-12 WO PCT/JP2013/074717 patent/WO2014042217A1/fr active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004031445A (ja) * | 2002-06-21 | 2004-01-29 | Du Pont Mitsui Polychem Co Ltd | 太陽電池モジュールの表層構造 |
JP2004055970A (ja) * | 2002-07-23 | 2004-02-19 | Fuji Electric Holdings Co Ltd | 太陽電池モジュールとその製造方法 |
JP2012074419A (ja) * | 2010-09-27 | 2012-04-12 | Dainippon Printing Co Ltd | 太陽電池モジュール用裏面保護シート、太陽電池モジュール用裏面一体化シート及び太陽電池モジュール |
WO2012056941A1 (fr) * | 2010-10-28 | 2012-05-03 | 富士フイルム株式会社 | Module de cellules solaires et son procédé de fabrication |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2019053832A (ja) * | 2017-09-12 | 2019-04-04 | トヨタ自動車株式会社 | 電極の製造方法 |
JP7535235B2 (ja) | 2020-03-19 | 2024-08-16 | 大日本印刷株式会社 | 表面改質フッ素系樹脂フィルム、積層体、及び複合ゴム成形体の製造方法、並びに表面改質フッ素系樹脂フィルム、積層体、及び複合ゴム成形体 |
Also Published As
Publication number | Publication date |
---|---|
JPWO2014042217A1 (ja) | 2016-08-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
TWI479006B (zh) | Solar battery seal and flexible solar module | |
WO2012066848A1 (fr) | Procédé de fabrication d'un module de cellule solaire flexible | |
JP5714959B2 (ja) | 太陽電池用保護シートおよびその製造方法、ならびに太陽電池モジュール | |
JP2012216805A (ja) | 太陽電池モジュール用充填材シート | |
WO2012043304A1 (fr) | Procédé de fabrication de modules de cellules solaires flexibles | |
JP4889828B2 (ja) | 太陽電池用封止材、太陽電池保護シート及び太陽電池モジュールの製造方法 | |
WO2012039389A1 (fr) | Procédé de fabrication d'un module de pile solaire souple | |
JPWO2012053475A1 (ja) | 太陽電池用保護シートおよびその製造方法、ならびに太陽電池モジュール | |
WO2014042217A1 (fr) | Feuille de protection de cellule solaire et module de cellule solaire flexible | |
JP2012099803A (ja) | 太陽電池封止シート、その製造方法、及び、フレキシブル太陽電池モジュールの製造方法 | |
WO2013121838A1 (fr) | Feuille protectrice pour cellule solaire, son procédé de fabrication et module de cellule solaire | |
JP2015073048A (ja) | 太陽電池保護シート、及び、太陽電池モジュール | |
WO2014049778A1 (fr) | Feuille de matériau de remplissage pour module de cellules solaires, feuille de scellement de cellules solaires, et procédé de fabrication de module de cellules solaires | |
JP2013199030A (ja) | 太陽電池保護シート及びフレキシブル太陽電池モジュール | |
JP2014027018A (ja) | フレキシブル太陽電池モジュールの製造方法 | |
JP2011176273A (ja) | 太陽電池用封止材、太陽電池保護シート及び太陽電池モジュールの製造方法 | |
JP2012079884A (ja) | フレキシブル太陽電池モジュールの製造方法 | |
WO2012046565A1 (fr) | Procédé pour produire un module de photopile souple | |
JP2013065619A (ja) | 太陽電池封止シート及びフレキシブル太陽電池モジュール | |
JP2013214544A (ja) | フレキシブル太陽電池モジュールの製造方法 | |
JP2014027017A (ja) | フレキシブル太陽電池モジュールの製造方法及び太陽電池封止シート | |
JP2015065340A (ja) | 太陽電池保護シート及びフレキシブル太陽電池モジュール | |
JP2012227280A (ja) | 太陽電池封止シート及びフレキシブル太陽電池モジュール | |
JP2013235874A (ja) | フレキシブル太陽電池モジュールの製造方法 | |
JP2012222147A (ja) | フレキシブル太陽電池モジュール |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 13837420 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2014535590 Country of ref document: JP Kind code of ref document: A |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 13837420 Country of ref document: EP Kind code of ref document: A1 |