CN116157263B - Laminate body - Google Patents
Laminate body Download PDFInfo
- Publication number
- CN116157263B CN116157263B CN202180061035.4A CN202180061035A CN116157263B CN 116157263 B CN116157263 B CN 116157263B CN 202180061035 A CN202180061035 A CN 202180061035A CN 116157263 B CN116157263 B CN 116157263B
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- Prior art keywords
- layer
- integrated intensity
- plane
- plane diffraction
- diffraction
- Prior art date
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- 230000003373 anti-fouling effect Effects 0.000 claims abstract description 84
- 239000010702 perfluoropolyether Substances 0.000 claims abstract description 52
- 150000001875 compounds Chemical class 0.000 claims abstract description 36
- 238000012360 testing method Methods 0.000 claims abstract description 24
- 239000000463 material Substances 0.000 claims description 106
- 238000000034 method Methods 0.000 claims description 49
- 238000005259 measurement Methods 0.000 claims description 44
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 40
- 229910052751 metal Inorganic materials 0.000 claims description 19
- 239000002184 metal Substances 0.000 claims description 19
- 239000005871 repellent Substances 0.000 claims description 15
- 238000001341 grazing-angle X-ray diffraction Methods 0.000 claims description 14
- 239000000377 silicon dioxide Substances 0.000 claims description 14
- 229910044991 metal oxide Inorganic materials 0.000 claims description 8
- 150000004706 metal oxides Chemical class 0.000 claims description 8
- 230000000737 periodic effect Effects 0.000 claims description 8
- 150000004767 nitrides Chemical class 0.000 claims description 6
- 235000012239 silicon dioxide Nutrition 0.000 claims description 3
- 230000002940 repellent Effects 0.000 claims 2
- 239000010410 layer Substances 0.000 description 406
- 239000002346 layers by function Substances 0.000 description 59
- 230000003287 optical effect Effects 0.000 description 35
- 239000000758 substrate Substances 0.000 description 33
- 238000009832 plasma treatment Methods 0.000 description 27
- 239000010408 film Substances 0.000 description 25
- 238000007740 vapor deposition Methods 0.000 description 22
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 20
- 229920005989 resin Polymers 0.000 description 19
- 239000011347 resin Substances 0.000 description 19
- 239000007789 gas Substances 0.000 description 16
- 239000000203 mixture Substances 0.000 description 14
- 238000004381 surface treatment Methods 0.000 description 14
- 238000004519 manufacturing process Methods 0.000 description 12
- 238000004544 sputter deposition Methods 0.000 description 12
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 11
- 230000005484 gravity Effects 0.000 description 11
- 239000001301 oxygen Substances 0.000 description 11
- 229910052760 oxygen Inorganic materials 0.000 description 11
- 229910052786 argon Inorganic materials 0.000 description 10
- 230000015572 biosynthetic process Effects 0.000 description 9
- 230000000052 comparative effect Effects 0.000 description 7
- 238000007789 sealing Methods 0.000 description 7
- 239000012790 adhesive layer Substances 0.000 description 6
- 238000001035 drying Methods 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 150000002739 metals Chemical class 0.000 description 6
- 239000002245 particle Substances 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 238000000576 coating method Methods 0.000 description 5
- 229920001971 elastomer Polymers 0.000 description 5
- -1 polyethylene terephthalate Polymers 0.000 description 5
- 229920002284 Cellulose triacetate Polymers 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 4
- NNLVGZFZQQXQNW-ADJNRHBOSA-N [(2r,3r,4s,5r,6s)-4,5-diacetyloxy-3-[(2s,3r,4s,5r,6r)-3,4,5-triacetyloxy-6-(acetyloxymethyl)oxan-2-yl]oxy-6-[(2r,3r,4s,5r,6s)-4,5,6-triacetyloxy-2-(acetyloxymethyl)oxan-3-yl]oxyoxan-2-yl]methyl acetate Chemical compound O([C@@H]1O[C@@H]([C@H]([C@H](OC(C)=O)[C@H]1OC(C)=O)O[C@H]1[C@@H]([C@@H](OC(C)=O)[C@H](OC(C)=O)[C@@H](COC(C)=O)O1)OC(C)=O)COC(=O)C)[C@@H]1[C@@H](COC(C)=O)O[C@@H](OC(C)=O)[C@H](OC(C)=O)[C@H]1OC(C)=O NNLVGZFZQQXQNW-ADJNRHBOSA-N 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 230000003667 anti-reflective effect Effects 0.000 description 4
- 239000012461 cellulose resin Substances 0.000 description 4
- 230000007062 hydrolysis Effects 0.000 description 4
- 238000006460 hydrolysis reaction Methods 0.000 description 4
- AMGQUBHHOARCQH-UHFFFAOYSA-N indium;oxotin Chemical compound [In].[Sn]=O AMGQUBHHOARCQH-UHFFFAOYSA-N 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 229910052814 silicon oxide Inorganic materials 0.000 description 4
- 238000002834 transmittance Methods 0.000 description 4
- ILJSQTXMGCGYMG-UHFFFAOYSA-N triacetic acid Chemical compound CC(=O)CC(=O)CC(O)=O ILJSQTXMGCGYMG-UHFFFAOYSA-N 0.000 description 4
- 238000001771 vacuum deposition Methods 0.000 description 4
- 229920000178 Acrylic resin Polymers 0.000 description 3
- 239000004925 Acrylic resin Substances 0.000 description 3
- 229920000877 Melamine resin Polymers 0.000 description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 3
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 3
- 125000000217 alkyl group Chemical group 0.000 description 3
- 239000010419 fine particle Substances 0.000 description 3
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 3
- 229910052737 gold Inorganic materials 0.000 description 3
- 239000010931 gold Substances 0.000 description 3
- 229910001512 metal fluoride Inorganic materials 0.000 description 3
- URLJKFSTXLNXLG-UHFFFAOYSA-N niobium(5+);oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[Nb+5].[Nb+5] URLJKFSTXLNXLG-UHFFFAOYSA-N 0.000 description 3
- 239000012788 optical film Substances 0.000 description 3
- 229920000728 polyester Polymers 0.000 description 3
- 229920006254 polymer film Polymers 0.000 description 3
- 229920005672 polyolefin resin Polymers 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 229910052718 tin Inorganic materials 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 125000004432 carbon atom Chemical group C* 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 239000011247 coating layer Substances 0.000 description 2
- 238000006482 condensation reaction Methods 0.000 description 2
- 230000018044 dehydration Effects 0.000 description 2
- 238000006297 dehydration reaction Methods 0.000 description 2
- 125000001033 ether group Chemical group 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 125000001153 fluoro group Chemical group F* 0.000 description 2
- 125000003709 fluoroalkyl group Chemical group 0.000 description 2
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 239000011859 microparticle Substances 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 229910000484 niobium oxide Inorganic materials 0.000 description 2
- 229910052763 palladium Inorganic materials 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 229910052697 platinum Inorganic materials 0.000 description 2
- 229920003229 poly(methyl methacrylate) Polymers 0.000 description 2
- 229920001225 polyester resin Polymers 0.000 description 2
- 239000004645 polyester resin Substances 0.000 description 2
- 239000004926 polymethyl methacrylate Substances 0.000 description 2
- 229920001296 polysiloxane Polymers 0.000 description 2
- 125000005372 silanol group Chemical group 0.000 description 2
- 229910052709 silver Inorganic materials 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 239000013077 target material Substances 0.000 description 2
- 229920005992 thermoplastic resin Polymers 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- 239000011135 tin Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- GZVHEAJQGPRDLQ-UHFFFAOYSA-N 6-phenyl-1,3,5-triazine-2,4-diamine Chemical compound NC1=NC(N)=NC(C=2C=CC=CC=2)=N1 GZVHEAJQGPRDLQ-UHFFFAOYSA-N 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-M Acrylate Chemical compound [O-]C(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-M 0.000 description 1
- 229920000089 Cyclic olefin copolymer Polymers 0.000 description 1
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 241000446313 Lamella Species 0.000 description 1
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 description 1
- 239000004695 Polyether sulfone Substances 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 239000004743 Polypropylene Substances 0.000 description 1
- 239000004793 Polystyrene Substances 0.000 description 1
- 229920000180 alkyd Polymers 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 125000003368 amide group Chemical group 0.000 description 1
- 125000003277 amino group Chemical group 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910000410 antimony oxide Inorganic materials 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- CXKCTMHTOKXKQT-UHFFFAOYSA-N cadmium oxide Inorganic materials [Cd]=O CXKCTMHTOKXKQT-UHFFFAOYSA-N 0.000 description 1
- CFEAAQFZALKQPA-UHFFFAOYSA-N cadmium(2+);oxygen(2-) Chemical compound [O-2].[Cd+2] CFEAAQFZALKQPA-UHFFFAOYSA-N 0.000 description 1
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 1
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 1
- 239000000292 calcium oxide Substances 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 125000002915 carbonyl group Chemical group [*:2]C([*:1])=O 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000008199 coating composition Substances 0.000 description 1
- 229920001577 copolymer Polymers 0.000 description 1
- 238000003851 corona treatment Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 239000003085 diluting agent Substances 0.000 description 1
- 229910001882 dioxygen Inorganic materials 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 229910003437 indium oxide Inorganic materials 0.000 description 1
- PJXISJQVUVHSOJ-UHFFFAOYSA-N indium(iii) oxide Chemical compound [O-2].[O-2].[O-2].[In+3].[In+3] PJXISJQVUVHSOJ-UHFFFAOYSA-N 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 239000011256 inorganic filler Substances 0.000 description 1
- 229910003475 inorganic filler Inorganic materials 0.000 description 1
- 238000007733 ion plating Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- ORUIBWPALBXDOA-UHFFFAOYSA-L magnesium fluoride Chemical compound [F-].[F-].[Mg+2] ORUIBWPALBXDOA-UHFFFAOYSA-L 0.000 description 1
- 229910001635 magnesium fluoride Inorganic materials 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- JDSHMPZPIAZGSV-UHFFFAOYSA-N melamine Chemical compound NC1=NC(N)=NC(N)=N1 JDSHMPZPIAZGSV-UHFFFAOYSA-N 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 150000001282 organosilanes Chemical class 0.000 description 1
- VTRUBDSFZJNXHI-UHFFFAOYSA-N oxoantimony Chemical compound [Sb]=O VTRUBDSFZJNXHI-UHFFFAOYSA-N 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 125000005010 perfluoroalkyl group Chemical group 0.000 description 1
- 238000005268 plasma chemical vapour deposition Methods 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 229920003207 poly(ethylene-2,6-naphthalate) Polymers 0.000 description 1
- 229920006122 polyamide resin Polymers 0.000 description 1
- 229920001230 polyarylate Polymers 0.000 description 1
- 229920001707 polybutylene terephthalate Polymers 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920005668 polycarbonate resin Polymers 0.000 description 1
- 239000004431 polycarbonate resin Substances 0.000 description 1
- 229920006393 polyether sulfone Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 239000011112 polyethylene naphthalate Substances 0.000 description 1
- 229920000139 polyethylene terephthalate Polymers 0.000 description 1
- 239000005020 polyethylene terephthalate Substances 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 239000009719 polyimide resin Substances 0.000 description 1
- 229920000193 polymethacrylate Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 229920005990 polystyrene resin Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 239000011164 primary particle Substances 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007127 saponification reaction Methods 0.000 description 1
- RMAQACBXLXPBSY-UHFFFAOYSA-N silicic acid Chemical compound O[Si](O)(O)O RMAQACBXLXPBSY-UHFFFAOYSA-N 0.000 description 1
- 229920005573 silicon-containing polymer Polymers 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
- 229920002803 thermoplastic polyurethane Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 239000013008 thixotropic agent Substances 0.000 description 1
- XOLBLPGZBRYERU-UHFFFAOYSA-N tin dioxide Chemical compound O=[Sn]=O XOLBLPGZBRYERU-UHFFFAOYSA-N 0.000 description 1
- 229910001887 tin oxide Inorganic materials 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
- G02B1/10—Optical coatings produced by application to, or surface treatment of, optical elements
- G02B1/18—Coatings for keeping optical surfaces clean, e.g. hydrophobic or photo-catalytic films
-
- 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
-
- 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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/02—Physical, chemical or physicochemical properties
- B32B7/023—Optical properties
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/024—Deposition of sublayers, e.g. to promote adhesion of the coating
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/08—Oxides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/08—Oxides
- C23C14/086—Oxides of zinc, germanium, cadmium, indium, tin, thallium or bismuth
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/10—Glass or silica
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/12—Organic material
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
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- G02B1/10—Optical coatings produced by application to, or surface treatment of, optical elements
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- G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
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- G02B1/11—Anti-reflection coatings
- G02B1/113—Anti-reflection coatings using inorganic layer materials only
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- G02—OPTICS
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- G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
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- G02B1/11—Anti-reflection coatings
- G02B1/113—Anti-reflection coatings using inorganic layer materials only
- G02B1/115—Multilayers
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
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Abstract
The laminate includes a base layer and an antifouling layer in this order on one surface side in the thickness direction. The stain-proofing layer comprises an alkoxysilane compound having a perfluoropolyether group. The first integrated strength ratio of the antifouling layer measured by a predetermined first test is 0.78 or less.
Description
Technical Field
The present invention relates to a laminate, and more particularly, to a laminate provided with an antifouling layer.
Background
Conventionally, it has been known to form an antifouling layer from the viewpoint of preventing dirt such as hand scale and fingerprints from adhering to the surface of a film base material and the surface of an optical member such as an optical film.
As such an optical film having an antifouling layer, for example, an antireflection film having a film base, an antireflection layer, and an antifouling layer in this order has been proposed (for example, see patent literature 1).
Prior art literature
Patent literature
Patent document 1: japanese patent laid-open No. 2020-52221
Disclosure of Invention
Problems to be solved by the invention
On the other hand, when the dirt adhering to the dirt-repellent layer is wiped off, there is a problem that the dirt-repellent property of the dirt-repellent layer is lowered.
The present invention provides a laminate which can inhibit the pollution-proof property of the pollution-proof layer from being reduced even after wiping off the pollution adhered to the pollution-proof layer.
Solution for solving the problem
The invention [1] is a laminate comprising a base layer and an antifouling layer in this order on one surface side in the thickness direction, wherein the antifouling layer comprises an alkoxysilane compound having a perfluoropolyether group, and wherein the antifouling layer has a first integrated strength ratio of 0.78 or less as measured by the first test described below.
First test: the integrated intensity of the peak (first in-plane diffraction integrated intensity) attributed to the layered structure was measured for the antifouling layer by in-plane diffraction (in-plane) measurement in a grazing incidence X-ray diffraction method. Further, the integrated intensity of the peaks derived from the periodic arrangement of the perfluoropolyether groups in the in-plane direction (second in-plane diffraction integrated intensity) was measured for the anti-fouling layer by in-plane diffraction measurement by a grazing incidence X-ray diffraction method. From the obtained first in-plane diffraction integrated intensity and second in-plane diffraction integrated intensity, a first integrated intensity ratio (first in-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the first in-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated.
The invention [2] includes the laminate of the above [1], wherein the second integrated strength ratio of the antifouling layer measured by the second test described below is 50 or less.
Second test: the integrated intensity (out-of-plane diffraction integrated intensity) of the peak attributed to the layered structure was measured for the antifouling layer by out-of-plane diffraction (out-of-plane) measurement in a grazing incidence X-ray diffraction method. A second integrated intensity ratio (out-of-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the out-of-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated from the out-of-plane diffraction integrated intensity and the second in-plane diffraction integrated intensity.
The invention [3] includes the laminate of [1] or [2], wherein a third integrated intensity ratio (out-of-plane integrated diffraction intensity/first in-plane integrated diffraction intensity) of the out-of-plane integrated diffraction intensity to the first in-plane integrated diffraction intensity exceeds 220.
The invention [4] includes the laminate according to any one of [1] to [3], wherein a primer layer is provided on the other surface in the thickness direction of the antifouling layer.
The invention [5] includes the laminate of [4] above, wherein the primer layer is a layer containing silica.
The invention [6] includes the laminate of [5] above, wherein the antifouling layer is formed on the primer layer by a silicone bond through an alkoxysilane compound having a perfluoropolyether group.
The invention [7] includes the laminate according to any one of [1] to [3], wherein an adhesion layer and an antireflection layer are further provided between the base material layer and the antifouling layer.
The invention [8] includes the laminate of [7], wherein the antireflection layer is formed of two or more layers having refractive indices different from each other.
The invention [9] includes the laminate of [8] above, wherein the antireflection layer contains 1 kind selected from the group consisting of a metal, a metal oxide, and a metal nitride.
The invention [10] includes the laminate of [8] or [9], wherein one surface in the thickness direction of the antireflection layer is a layer containing silicon dioxide.
ADVANTAGEOUS EFFECTS OF INVENTION
The stain-proofing layer in the laminate of the present invention comprises an alkoxysilane compound having a perfluoropolyether group. In the stain-proofing layer, the first integrated intensity ratio measured by a predetermined first test is equal to or less than a predetermined value. Therefore, even after wiping off dirt adhering to the dirt-repellent layer, the dirt-repellent layer can be suppressed from deteriorating.
Drawings
Fig. 1 shows a cross-sectional view of a first embodiment of a laminate of the present invention.
Fig. 2 a to 2C show an embodiment of a method for producing a laminate according to a first embodiment of the present invention. Fig. 2 a shows a step of preparing a base material in a first step. Fig. 2B shows a step of disposing a hard coat layer (functional layer) on a substrate in the first step. Fig. 2C shows a second step of disposing an antifouling layer on the base material layer.
Fig. 3 shows a cross-sectional view of a second embodiment of the laminate of the present invention.
Fig. 4 a to 4D show an embodiment of a method for producing a laminate according to a second embodiment of the present invention. Fig. 4 a shows a step of preparing a base material in the third step. Fig. 4B shows a step of disposing a hard coat layer (functional layer) on a substrate in the third step. Fig. 4C shows a fourth step of disposing an adhesive layer and an optical functional layer (antireflection layer) in this order on the base material layer. Fig. 4D shows a fifth step of disposing an antifouling layer on the optical functional layer (antireflection layer).
Fig. 5 is a cross-sectional view showing a modification of the first embodiment of the laminate of the present invention (a laminate further comprising a primer layer and a primer adhesion layer between the base layer and the stain-proofing layer).
FIG. 6 shows the results of in-plane diffraction (in-plane) measurements of example 2.
FIG. 7 shows the results of out-of-plane diffraction (out-of-plane) measurements of example 2.
FIG. 8 shows the fitting results in an in-plane diffraction (in-plane) measurement of example 2.
FIG. 9 shows the fitting results in out-of-plane diffraction (out-of-plane) measurements of example 2.
Detailed Description
1. First embodiment
A first embodiment of the laminate of the present invention will be described with reference to fig. 1.
In fig. 1, the up-down direction of the paper surface is the up-down direction (thickness direction), the upper side of the paper surface is the upper side (one surface side in the thickness direction), and the lower side of the paper surface is the lower side (the other surface side in the thickness direction). The left-right direction and the depth direction of the paper surface are surface directions perpendicular to the up-down direction. Specifically, the directional arrows are based on the respective figures.
< laminate >
The laminate 1 has a film shape (including a sheet shape) having a predetermined thickness. The laminate 1 extends in a plane direction orthogonal to the thickness direction. The laminate 1 has a flat upper surface and a flat lower surface.
As shown in fig. 1, the laminate 1 includes a base layer 2 and an antifouling layer 3 in this order on one surface side in the thickness direction. More specifically, the laminate 1 includes a base layer 2 and an antifouling layer 3 directly disposed on the upper surface (one surface in the thickness direction) of the base layer 2.
The total light transmittance (JIS K7375-2008) of the laminate 1 is, for example, 80% or more, preferably 85% or more.
The thickness of the laminate 1 is, for example, 300 μm or less, preferably 200 μm or less, and is, for example, 10 μm or more, preferably 30 μm or more.
< substrate layer >
The base material layer 2 is a base material for securing mechanical strength of the laminate 1.
The base material layer 2 has a film shape. The base material layer 2 is disposed on the entire lower surface of the antifouling layer 3 so as to contact the lower surface of the antifouling layer 3.
The base material layer 2 includes a base material 4 and a functional layer 5. Specifically, the base material layer 2 includes a base material 4 and a functional layer 5 in this order on one surface side in the thickness direction.
The total light transmittance of the base material layer 2 (JIS K7375-2008) is, for example, 80% or more, preferably 85% or more.
< substrate >
The substrate 4 is a treatment object to which stain resistance is imparted by the stain-proofing layer 3.
The substrate 4 has a film shape. The base material 4 preferably has flexibility. The base material 4 is disposed on the entire lower surface of the functional layer 5 so as to contact the lower surface of the functional layer 5.
The substrate 4 is, for example, a polymer film. Examples of the material of the polymer film include polyester resins, (meth) acrylic resins, olefin resins, polycarbonate resins, polyethersulfone resins, polyarylate resins, melamine resins, polyamide resins, polyimide resins, cellulose resins, and polystyrene resins. Examples of the polyester resin include polyethylene terephthalate, polybutylene terephthalate, and polyethylene naphthalate. The (meth) acrylic resin may be, for example, polymethacrylate. Examples of the olefin resin include polyethylene, polypropylene and cycloolefin polymer. As the cellulose resin, for example, cellulose triacetate is cited. The material of the polymer film is preferably a cellulose resin, more preferably cellulose triacetate.
The thickness of the base material 4 is, for example, 1 μm or more, preferably 5 μm or more, more preferably 10 μm or more, and is, for example, 200 μm or less, preferably 150 μm or less, more preferably 100 μm or less.
The thickness of the substrate 4 can be measured by using a micrometer (manufactured by PEACOCK Co., ltd., "DG-205").
< functional layer >
The functional layer 5 has a thin film shape. The functional layer 5 is disposed on one surface in the thickness direction of the base material 4.
The functional layer 5 may be, for example, a hard coat layer.
In this case, the base material layer 2 includes the base material 4 and the hard coat layer in this order on one surface side in the thickness direction.
In the following description, the case where the functional layer 5 is a hard coat layer will be described.
The hard coat layer is a protective layer for inhibiting the damage to the substrate 4.
The hard coat layer is formed of, for example, a hard coat composition.
The hard coat composition contains a resin and, if necessary, particles. In other words, the hard coat layer contains a resin and particles as needed.
Examples of the resin include thermoplastic resins and curable resins. Examples of the thermoplastic resin include polyolefin resins.
Examples of the curable resin include an active energy ray curable resin cured by irradiation with active energy rays (for example, ultraviolet rays and electron rays) and a thermosetting resin cured by heating. The curable resin may preferably be an active energy ray curable resin.
Examples of the active energy ray-curable resin include (meth) acrylic ultraviolet-curable resins, urethane resins, melamine resins, alkyd resins, silicone polymers, and organosilane condensates. The active energy ray-curable resin may preferably be a (meth) acrylic ultraviolet-curable resin.
The resin may contain a reactive diluent described in, for example, japanese patent application laid-open No. 2008-88309. Specifically, the resin may contain a multifunctional (meth) acrylate.
The resin may be used alone or in combination of 2 or more.
Examples of the particles include metal oxide microparticles and organic microparticles. Examples of the material of the metal oxide fine particles include silica, alumina, titania, zirconia, calcium oxide, tin oxide, indium oxide, cadmium oxide, and antimony oxide. Examples of the material of the organic fine particles include polymethyl methacrylate, silicone, polystyrene, polyurethane, acrylic-styrene copolymer, benzoguanamine, melamine, and polycarbonate. The organic fine particles are preferably polymethyl methacrylate.
The purpose of the particles contained in the hard coat layer is, for example, to impart antiglare properties, improve adhesion, improve hardness, adjust refractive index, and the like.
The particles may be used alone or in combination of 2 or more.
In addition, a thixotropic agent (e.g., organoclay), a photopolymerization initiator, a filler, and a leveling agent may be blended into the hard coat composition in an appropriate ratio, as needed. The hard coat composition may be diluted with a known solvent.
In order to form the hard coat layer, a diluted solution of the hard coat composition is applied to one surface of the base material 4 in the thickness direction, and heated and dried as necessary, as will be described later. After drying, the hard coat composition is cured by, for example, irradiation with active energy rays or heating.
Thereby, a hard coat layer is formed.
The thickness of the hard coat layer is 1 μm or more and 10 μm or less, preferably 5 μm or less.
< antifouling layer >
The stain-proofing layer 3 is a layer for preventing stains such as dirt and fingerprints from adhering to one surface side in the thickness direction of the base material layer 2.
The stain-proofing layer 3 has a film shape. The stain-proofing layer 3 is disposed on the entire upper surface of the base material layer 2 so as to contact the upper surface of the base material layer 2.
The stain-proofing layer 3 is formed of an alkoxysilane compound having a perfluoropolyether group. In other words, the stain-proofing layer 3 contains an alkoxysilane compound having a perfluoropolyether group, and is preferably formed of an alkoxysilane compound having a perfluoropolyether group.
Examples of the alkoxysilane compound having a perfluoropolyether group include compounds represented by the following general formula (1).
R 1 -R 2 -X-(CH 2 ) m -Si(OR 3 ) 3 (1)
In the general formula (1), R 1 A linear or branched fluoroalkyl group (having 1 to 20 carbon atoms, for example) in which one or more hydrogen atoms of the alkyl group are replaced with fluorine atoms is preferable, and a perfluoroalkyl group in which all hydrogen atoms of the alkyl group are replaced with fluorine atoms is preferable.
R 2 Represents a structure comprising at least one repeating structure of a perfluoropolyether (PFPE) group, preferably a structure comprising two repeating structures of a PFPE group. Examples of the repeating structure of the PFPE group include a repeating structure of a linear PFPE group and a repeating structure of a branched PFPE group. Examples of the repeating structure of the linear PFPE group include- (OC) n F 2n ) p The structure shown (n represents an integer from 1 to 20, p represents an integer from 1 to 50, and the same applies hereinafter). Examples of the repeating structure of the branched PFPE group include- (OC (CF) 3 ) 2 ) p -the structure shown and- (OCF) 2 CF(CF 3 )CF 2 ) p -the structure shown. The repeating structure of the PFPE group is preferably a linear PFPE group, more preferably- (OCF) 2 ) p -and- (OC) 2 F 4 ) p -。
R 3 An alkyl group having 1 to 4 carbon atoms is preferably methyl.
X represents an ether group, a carbonyl group, an amino group or an amide group, preferably an ether group.
m represents an integer of 1 or more. M is preferably an integer of 20 or less, more preferably 10 or less, and still more preferably 5 or less.
Among such alkoxysilane compounds having a perfluoropolyether group, a compound represented by the following general formula (2) is preferably used.
CF 3 -(OCF 2 ) q -(OC 2 F 4 ) r -O-(CH 2 ) 3 -Si(OCH 3 ) 3 (2)
In the general formula (2), q represents an integer of 1 to 50 inclusive, and r represents an integer of 1 to 50 inclusive.
As the alkoxysilane compound having a perfluoropolyether group, commercially available products can be used, and specifically, optool UD509 (an alkoxysilane compound having a perfluoropolyether group represented by the above general formula (2) and manufactured by Dain industries, ltd.), optool UD120 (manufactured by Dain industries, ltd.) and KY1903-1 (manufactured by Xin Yue chemical Co., ltd.) can be cited.
The alkoxysilane compound having a perfluoropolyether group may be used alone or in combination of 2 or more.
The stain-proofing layer 3 is formed by a method described later.
The thickness of the stain-proofing layer 3 is, for example, 1nm or more, preferably 5nm or more, and is, for example, 30nm or less, preferably 20nm or less, more preferably 15nm or less, and still more preferably 10nm or less.
The thickness of the antifouling layer 3 can be measured by fluorescent X-rays (ZXS PrimusII, manufactured by phys).
The first integrated strength ratio of the stain-proofing layer 3 measured by a first test described later is 0.78 or less, preferably 0.60 or less, more preferably 0.50 or less, still more preferably 0.40 or less, particularly preferably 0.35 or less, and most preferably 0.30 or less.
In addition, it is preferable that: the second integrated strength ratio of the stain-proofing layer 3 measured by a second test described later is 50 or less, preferably 30 or less, more preferably 28 or less.
The first integrated intensity ratio and the second integrated intensity ratio can be adjusted to a predetermined value or less by adjusting the type of the alkoxysilane compound having a perfluoropolyether group, the method of performing the surface treatment (in the case where the surface treatment method is plasma treatment, the type of gas used in the plasma treatment) on the substrate layer 2 in the second step described later, and the output power of the plasma treatment when the surface treatment method is plasma treatment.
The measurement methods of the in-plane diffraction (in-plane diffraction integrated intensity) measurement and the out-of-plane diffraction (out-of-plane diffraction integrated intensity) measurement are described in detail in examples described later.
The water contact angle of the antifouling layer 3 is, for example, 100 ° or more, preferably 105 ° or more, and 120 ° or less.
If the water contact angle of the antifouling layer 3 is not less than the lower limit, the antifouling property of the antifouling layer 3 can be improved.
The method for measuring the water contact angle of the antifouling layer 3 is described in detail in examples described later.
< method for producing laminate >
A method of manufacturing the laminate 1 will be described with reference to fig. 2.
The method for producing the laminate 1 comprises: a first step of preparing a base material layer 2; and a second step of disposing the antifouling layer 3 on the base material layer 2. In this manufacturing method, for example, each layer is arranged in sequence by a roll-to-roll (roll-to-roll) method.
< first step >
In the first step, as shown in fig. 2 a, the base material 4 is first prepared.
Next, as shown in fig. 2B, a diluted solution of the hard coat composition is applied to one surface of the base material 4 in the thickness direction, and after drying, the hard coat composition is cured by irradiation of ultraviolet rays or heating.
Thus, the hard coat layer (functional layer 5) is disposed (formed) on one surface of the base material 4 in the thickness direction. Thereby, the base material layer 2 is prepared.
< second step >
In the second step, as shown in fig. 2C, the antifouling layer 3 is disposed on the base material layer 2. Specifically, the antifouling layer 3 is disposed on one surface in the thickness direction of the base material layer 2.
In order to dispose the stain-proofing layer 3 on the base material layer 2, first, the surface of the base material layer 2 is subjected to, for example, a surface treatment from the viewpoint of improving the adhesion between the base material layer 2 and the stain-proofing layer 3. The surface treatment may be, for example, corona treatment, plasma treatment, flame treatment, ozone treatment, primer treatment, glow treatment, or saponification treatment, and plasma treatment is preferable.
Examples of the plasma treatment include an argon-based plasma treatment and an oxygen-based plasma treatment, and oxygen-based plasma treatment is preferable. The output power of the plasma treatment is, for example, 80W or more and 150W or less.
The method of disposing the antifouling layer 3 on the base layer 2 includes, for example, a dry coating method and a wet coating method, and from the viewpoint of adjusting the first integrated strength ratio to a predetermined value or less, a dry coating method is preferable. Examples of the dry coating method include a vacuum deposition method, a sputtering method, and CVD, and a vacuum deposition method is preferable.
In the vacuum vapor deposition method, a vapor deposition source (alkoxysilane compound having a perfluoropolyether group) and a substrate layer 2 (functional layer 5) are disposed in a vacuum chamber, and the vapor deposition source is heated to evaporate or sublimate the vapor deposition source, so that the evaporated or sublimated vapor deposition source is deposited on the surface of the substrate layer 2 (functional layer 5).
In the vacuum vapor deposition method, the temperature of the vapor deposition source (crucible) is, for example, 200 ℃ or higher, preferably 250 ℃ or higher, and 300 ℃ or lower.
Thus, the antifouling layer 3 is disposed on one surface in the thickness direction of the base material layer 2, and the laminate 1 including the base material layer 2 and the antifouling layer 3 in this order on one surface side in the thickness direction is manufactured.
< Effect >
In the laminate 1, the first integrated strength ratio of the stain-proofing layer 3 measured by a first test described later is 0.78 or less.
Specifically, in the first test, the integrated intensity (first in-plane diffraction integrated intensity) of the peak attributed to the layered structure (structure in which the flakes (lamella) are oriented parallel to the base material layer 2) was measured by in-plane diffraction (in-plane) measurement by the grazing incidence X-ray diffraction method for the anti-fouling layer 3. The integrated intensity of the peaks derived from the periodic arrangement of the perfluoropolyether groups in the in-plane direction (second in-plane diffraction integrated intensity) was measured separately for the anti-fouling layer by in-plane diffraction measurement by the grazing incidence X-ray diffraction method. From the obtained first in-plane diffraction integrated intensity and second in-plane diffraction integrated intensity, a first integrated intensity ratio (first in-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the first in-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated.
The first integrated strength ratio is an index of the amount (hereinafter, sometimes referred to as the alignment amount) by which fluoroalkyl groups of the alkoxysilane compound having a perfluoropolyether group in the stain-proofing layer 3 are periodically aligned in the in-plane direction. If the first integrated intensity ratio becomes smaller, this means that the arrangement amount becomes larger.
As described above, the first integrated intensity ratio is calculated by dividing the first in-plane diffraction integrated intensity by the second in-plane diffraction integrated intensity.
The second in-plane diffraction integrated intensity is an integrated intensity of peaks derived from the periodic arrangement of the perfluoropolyether groups of the alkoxysilane compound having a perfluoropolyether group in the in-plane direction. When the second in-plane diffraction integrated intensity becomes large, this means that the alignment amount becomes large. Thus, it has also been studied to use such second in-plane diffraction integrated intensity directly as an index of the alignment amount.
However, in the grazing incidence X-ray diffraction measurement, the background value of each measurement is changed by a slight difference in the sample, and therefore, the integrated intensity of diffraction in the second plane of each measurement is also changed. Therefore, if the absolute value of the second in-plane diffraction integrated intensity is directly used as an index, the arrangement amount cannot be uniformly obtained.
Thus, the first in-plane diffraction integrated intensity is divided by the second in-plane diffraction integrated intensity, whereby the second in-plane diffraction integrated intensity is shown in the form of a relative value to the first in-plane diffraction integrated intensity, i.e., a first integrated intensity ratio. This allows the arrangement amount to be uniformly obtained.
If the first integrated intensity ratio is equal to or less than the upper limit, the arrangement amount becomes large. In this way, even after wiping off dirt adhering to the dirt-repellent layer 3, the dirt-repellent layer 3 can be suppressed from decreasing in dirt-repellent performance (excellent dirt-repellent durability).
In the laminate 1, the second integrated strength ratio of the stain-proofing layer 3 measured by a second test described later is preferably 50 or less.
Specifically, in the second test, the integrated intensity (integrated intensity of out-of-plane diffraction) of the peak attributed to the layered structure (structure in which the sheet is oriented vertically with respect to the base material layer 2) was measured on the anti-fouling layer 3 by out-of-plane diffraction (out-of-plane) measurement in the grazing incidence X-ray diffraction method. From the out-of-plane diffraction integrated intensity and the second in-plane diffraction integrated intensity, a second integrated intensity ratio (out-of-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the out-of-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated.
The second integrated intensity ratio is an index of the arrangement amount in the stain-proofing layer 3. When the second integrated intensity ratio is smaller, this means that the arrangement amount in the stain-proofing layer 3 is increased.
The second integrated intensity ratio is not an absolute value, but a relative value, as in the first integrated intensity ratio described above. In detail, the second integrated intensity ratio is a relative value of the second in-plane diffraction integrated intensity with respect to the out-of-plane diffraction integrated intensity. This allows the arrangement amount to be uniformly obtained.
If the second integrated intensity ratio is equal to or less than the upper limit, the arrangement amount becomes large. In this way, even after wiping off the dirt adhering to the dirt-repellent layer 3, the dirt-repellent layer 3 can be further suppressed from being lowered in dirt-repellent performance (more excellent in dirt-repellent durability).
In addition, in the laminate 1, the third integrated strength ratio of the stain-proofing layer 3 is preferably more than 220.
The third integrated intensity ratio is the ratio of the out-of-plane integrated diffraction intensity to the first in-plane integrated diffraction intensity (out-of-plane integrated diffraction intensity/first in-plane integrated diffraction intensity).
As described above, the out-of-plane diffraction integrated intensity is the integrated intensity of the diffraction peak due to the structure in which the flakes are oriented vertically with respect to the base material layer 2. If the sheet is oriented vertically with respect to the substrate layer 2, the alkoxysilane compound having a perfluoropolyether group is also oriented vertically with respect to the substrate layer 2, and thus the alkoxysilane at the terminal thereof is likely to contact the substrate layer 2.
The in-plane diffraction integrated intensity is the integrated intensity of diffraction peaks due to a structure in which the flakes are aligned parallel to the base layer 2. If the sheet is oriented parallel to the substrate layer 2, the alkoxysilane compound having a perfluoropolyether group is also oriented parallel to the substrate layer 2, and thus the alkoxysilane at the terminal thereof is less likely to contact the substrate layer 2.
Accordingly, as the third integrated intensity ratio is larger, the structure in which the flakes are oriented vertically to the substrate layer 2 is relatively larger than the structure in which the flakes are oriented parallel to the substrate layer 2, and therefore, the proportion of alkoxysilane at the end of the alkoxysilane compound having a perfluoropolyether group in contact with the substrate layer 2 increases.
Specifically, if the third integrated intensity ratio exceeds 220, the deterioration of the antifouling property of the antifouling layer 3 (more excellent antifouling durability) can be further suppressed even after wiping off the dirt adhering to the antifouling layer 3.
The peaks (peak A1 and peak B1 (detailed in examples described later)) belonging to the layered structure are the wave numbersThe observed peak (peak A4 (detailed in the examples described below)) derived from the periodic arrangement of the perfluoropolyether groups in the in-plane direction was at wave number +.>Observed in between.
The antifouling durability can be evaluated by an antifouling durability test described in detail in examples described later. Specifically, the antifouling durability of the antifouling layer 3 is excellent if the amount of change in the contact angle obtained by the antifouling durability test is, for example, 30 ° or less, preferably 23 ° or less, and more preferably 15 ° or less.
2. Second embodiment
A second embodiment of the laminate of the present invention will be described with reference to fig. 3.
In the second embodiment, the same members and steps as those in the first embodiment are denoted by the same reference numerals, and detailed description thereof is omitted. The second embodiment can exhibit the same operational effects as the first embodiment unless specifically described. Further, the first embodiment and the second embodiment can be appropriately combined.
< laminate >
As shown in fig. 3, the laminate 1 includes a base material layer 2, an adhesive layer 6, an optical functional layer 7, and an antifouling layer 3 in this order on one surface side in the thickness direction. More specifically, the laminate 1 includes the base layer 2, the adhesion layer 6 directly disposed on the upper surface (one surface in the thickness direction) of the base layer 2, the optical functional layer 7 directly disposed on the upper surface (one surface in the thickness direction) of the adhesion layer 6, and the stain-proofing layer 3 directly disposed on the upper surface (one surface in the thickness direction) of the optical functional layer 7.
The total light transmittance (JIS K7375-2008) of the laminate 1 is, for example, 80% or more, preferably 85% or more.
The thickness of the laminate 1 is, for example, 250 μm or less, preferably 200 μm or less, and is, for example, 10 μm or more, preferably 20 μm or more.
< substrate layer >
The base material layer 2 is a base material for securing mechanical strength of the laminate 1.
The base material layer 2 has a film shape. The base material layer 2 is disposed on the entire lower surface of the optical functional layer 7 so as to contact the lower surface of the optical functional layer 7.
The base material layer 2 includes a base material 4 and a functional layer 5, similar to the base material layer 2 in the first embodiment.
The total light transmittance of the base material layer 2 (JIS K7375-2008) is, for example, 80% or more, preferably 85% or more.
< substrate >
The substrate 4 has a film shape. The base material 4 preferably has flexibility. The base material 4 is disposed on the entire lower surface of the functional layer 5 so as to contact the lower surface of the functional layer 5.
The substrate 4 is the same as the substrate 4 in the first embodiment, and preferably includes a cellulose resin, and more preferably includes cellulose triacetate.
The thickness of the base material 4 is the same as that of the base material 4 in the first embodiment.
< functional layer >
The functional layer 5 has a thin film shape. The functional layer 5 is disposed on one surface of the substrate 4 in the thickness direction.
The functional layer 5 is, for example, a hard coat layer similar to that of the first embodiment.
In this case, the base material layer 2 includes the base material 4 and the hard coat layer in this order on one surface side in the thickness direction.
The thickness of the hard coat layer is the same as that in the first embodiment.
< sealing layer >
The adhesion layer 6 is a layer for securing adhesion between the base material layer 2 and the optical functional layer 7.
The sealing layer 6 has a film shape. The adhesion layer 6 is disposed on the entire upper surface of the base material layer 2 (functional layer 5) so as to contact the upper surface of the base material layer 2 (functional layer 5).
As a material of the sealing layer 6, for example, a metal is cited. Examples of the metal include indium, silicon, nickel, chromium, aluminum, tin, gold, silver, platinum, zinc, titanium, tungsten, zirconium, and palladium. The material of the adhesion layer 6 may be an alloy of two or more of the above metals or an oxide of the above metals.
As a material of the adhesion layer 6, silicon oxide (SiOx) and Indium Tin Oxide (ITO) are preferable from the viewpoints of adhesion and transparency. When silicon oxide is used as the material of the adhesion layer 6, siOx having a smaller oxygen content than the stoichiometric composition is preferably used, and SiOx having x of 1.2 or more and 1.9 or less is more preferably used. As a material of the adhesion layer 6, indium Tin Oxide (ITO) is more preferable.
The thickness of the adhesion layer 6 is, for example, 1nm or more and, in addition, 10nm or less, from the viewpoint of securing adhesion between the substrate layer 2 and the optical functional layer 7 and also considering transparency of the adhesion layer 6.
< optical functional layer >
In the second embodiment, the optical functional layer 7 is an antireflection layer for suppressing the reflection intensity of external light.
In the following description, the case where the optical functional layer 7 is an antireflection layer will be described in detail.
The antireflection layer includes two or more layers having refractive indices different from each other. Specifically, the antireflection layer alternately has a high refractive index layer having a relatively large refractive index and a low refractive index layer having a relatively small refractive index in the thickness direction. In the antireflection layer, substantial reflected light intensity is attenuated by interference between reflected light at a plurality of interfaces of a plurality of thin layers (high refractive index layer, low refractive index layer) contained therein. In addition, in the antireflection layer, by adjusting the optical film thickness (product of refractive index and thickness) of each thin layer, interference effect of attenuating the intensity of reflected light can be exhibited. The antireflection layer includes, in order on one surface side in the thickness direction, a first high refractive index layer 11, a first low refractive index layer 12, a second high refractive index layer 13, and a second low refractive index layer 14.
The antireflection layer (specifically, the high refractive index layer and the low refractive index layer) preferably contains 1 selected from the group consisting of a metal, an alloy, a metal oxide, a metal nitride, and a metal fluoride, more preferably contains 1 selected from the group consisting of a metal, a metal oxide, and a metal nitride. Thus, the antireflection layer can suppress the reflection intensity of external light.
Examples of the metal include silicon, nickel, chromium, aluminum, tin, gold, silver, platinum, zinc, titanium, tungsten, zirconium, niobium, and palladium. As the alloy, for example, an alloy of the above metals can be cited. Examples of the metal oxide include metal oxides of the above metals. Examples of the metal nitride include metal nitrides of the above metals. Examples of the metal fluoride include metal fluorides of the above metals.
In particular, the material used in the anti-reflection layer is selected according to the desired refractive index.
Specifically, the first high refractive index layer 11 and the second high refractive index layer 13 are each formed of a high refractive index material having a refractive index of preferably 1.9 or more at a wavelength of 550 nm. From the viewpoint of both high refractive index and low absorptivity of visible light, examples of the high refractive index material include niobium oxide (Nb 2 O 5 ) Titanium oxide, zirconium oxide, indium Tin Oxide (ITO) and antimony doped tin oxideAs The (ATO), niobium oxide is preferably used. In other words, it is preferable that the material of the first low refractive index layer 12 and the material of the second low refractive index layer 14 are both niobium oxide.
The first low refractive index layer 12 and the second low refractive index layer 14 are each formed of a low refractive index material having a refractive index of preferably 1.6 or less at a wavelength of 550 nm. From the viewpoint of both low refractive index and low absorptivity of visible light, examples of the low refractive index material include silica (SiO 2 ) And magnesium fluoride, silica is preferably exemplified. In other words, it is preferable that the material of the first low refractive index layer 12 and the material of the second low refractive index layer 14 are both silicon dioxide.
In particular, if the material of the second low refractive index layer 14 is silica (in other words, if one surface in the thickness direction of the antireflection layer is a layer containing silica), the adhesion between the second low refractive index layer 14 and the stain-proofing layer 3 is excellent.
In the antireflection layer, the thickness of the first high refractive index layer 11 is, for example, 1nm or more, preferably 5nm or more, and is, for example, 30nm or less, preferably 20nm or less. The thickness of the first low refractive index layer 12 is, for example, 10nm or more, preferably 20nm or more, and is, for example, 50nm or less, preferably 30nm or less. The thickness of the second high refractive index layer 13 is, for example, 50nm or more, preferably 80nm or more, and is, for example, 200nm or less, preferably 150nm or less. The thickness of the second low refractive index layer 14 is, for example, 60nm or more, preferably 80nm or more, and 150nm or less, preferably 100nm or less.
The ratio of the thickness of the second low refractive index layer 14 to the thickness of the second high refractive index layer 13 (the thickness of the second low refractive index layer 14/the thickness of the second high refractive index layer 13) is, for example, 0.5 or more, preferably 0.7 or more, and, for example, 0.9 or less.
The ratio of the thickness of the second high refractive index layer 13 to the thickness of the first high refractive index layer 11 (the thickness of the second high refractive index layer 13/the thickness of the first high refractive index layer 11) is, for example, 5 or more, preferably 7 or more, and is, for example, 15 or less, preferably 10 or less.
The ratio of the thickness of the second low refractive index layer 14 to the thickness of the first low refractive index layer 12 (the thickness of the second low refractive index layer 14/the thickness of the first low refractive index layer 12) is, for example, 1 or more, preferably 3 or more, and is, for example, 10 or less, preferably 8 or less.
The antireflection layer is formed by a method described later.
The thickness of the antireflection layer is, for example, 100nm or more, preferably 150nm or more, and 300nm or less, preferably 250nm or less.
The thickness of the anti-reflection layer can be measured by cross-sectional TEM observation.
< antifouling layer >
The stain-proofing layer 3 has a film shape. The antifouling layer 3 is disposed on the entire upper surface of the optical functional layer 7 (antireflection layer) so as to contact the upper surface of the optical functional layer 7 (antireflection layer).
The stain-proofing layer 3 is formed of the above alkoxysilane compound having a perfluoropolyether group (preferably, the alkoxysilane compound having a perfluoropolyether group represented by the above general formula (2)). In other words, the stain-proofing layer 3 contains an alkoxysilane compound having a perfluoropolyether group, and is preferably formed of an alkoxysilane compound having a perfluoropolyether group.
The stain-proofing layer 3 is formed by a method described later.
The thickness, the first integrated intensity ratio, the second integrated intensity ratio, and the water contact angle of the stain-proofing layer 3 are the same as those of the stain-proofing layer 3 in the first embodiment.
The first integrated intensity ratio and the second integrated intensity ratio can be adjusted to a predetermined value or less by adjusting the type of alkoxysilane compound having a perfluoropolyether group, a method of surface-treating the optical functional layer 7 (antireflection layer) in the fifth step described later (in the case where the surface-treating method is plasma treatment, the type of gas used in plasma treatment), and the output power of plasma treatment when the surface-treating method is plasma treatment.
< method for producing laminate >
Referring to fig. 4, a method of manufacturing the laminate 1 will be described.
The method for producing the laminate 1 comprises: a third step of preparing a base material layer 2; a fourth step of disposing an adhesive layer 6 and an optical functional layer 7 (antireflection layer) in this order on the base layer 2; and a fifth step of disposing the antifouling layer 3 on the optical functional layer 7 (antireflection layer). In this manufacturing method, the layers are arranged in sequence by, for example, a roll-to-roll method.
< third step >
In the third step, as shown in a of fig. 4, the base material 4 is first prepared.
Next, as shown in B of fig. 4, a diluted solution of the hard coat composition is applied to one surface of the base material 4 in the thickness direction, and after drying, the hard coat composition is cured by irradiation of ultraviolet rays or heating.
Thus, the hard coat layer (functional layer 5) is disposed (formed) on one surface of the base material 4 in the thickness direction. Thereby, the base material layer 2 is prepared.
< fourth step >
In the fourth step, as shown in fig. 4C, the adhesion layer 6 and the optical functional layer 7 (antireflection layer) are sequentially disposed on the base material layer 2. Specifically, the adhesive layer 6 and the optical functional layer 7 (antireflection layer) are disposed in this order on one surface in the thickness direction of the base material layer 2.
More specifically, the sealing layer 6, the first high refractive index layer 11, the first low refractive index layer 12, the second high refractive index layer 13, and the second low refractive index layer 14 are disposed in this order on one surface side in the thickness direction on the base material layer 2.
In other words, in this method, the fourth step includes: an adhesion layer disposing step of disposing an adhesion layer 6 on the base material layer 2; a first high refractive index layer arrangement step of arranging a first high refractive index layer 11 on the sealing layer 6; a first low refractive index layer arrangement step of arranging a first low refractive index layer 12 on the first high refractive index layer 11; a second high refractive index layer arrangement step of arranging a second high refractive index layer 13 on the first low refractive index layer 12; and a second low refractive index layer arrangement step of arranging a second low refractive index layer 14 on the second high refractive index layer 13. In this production method, for example, vacuum deposition, sputtering, lamination, plating, and ion plating are used, and it is preferable to dispose the layers sequentially by sputtering.
The method of sequentially disposing the layers by the sputtering method will be described in detail below.
In this method, first, from the viewpoint of improving the adhesion between the substrate layer 2 and the adhesion layer 6, the surface of the substrate layer 2 is subjected to, for example, a surface treatment. The surface treatment may be a surface treatment as described in the second step, and plasma treatment is preferable.
In the sputtering method, the target (the material of each layer (the sealing layer 6, the first high refractive index layer 11, the first low refractive index layer 12, the second high refractive index layer 13, and the second low refractive index layer 14)) and the base material layer 2 are disposed in the vacuum chamber, and a gas is supplied thereto, and a voltage is applied thereto by a power supply, whereby the gas ions are accelerated and irradiated to the target, a target material is ejected from the target surface, and the target material is sequentially deposited on the surface of the base material layer 2.
As the gas, for example, an inert gas (for example, argon) is cited. In addition, a reactive gas such as oxygen may be used in combination as necessary. In the case of using the reactive gas in combination, the flow rate ratio (sccm) of the reactive gas is not particularly limited, and is, for example, 0.1 to 100% by flow rate with respect to the total flow rate ratio of the sputtering gas and the reactive gas.
The air pressure during sputtering is, for example, 0.1Pa or more, and is, for example, 1.0Pa or less, preferably 0.7Pa or less.
The power source may be any of, for example, a DC power source, an AC power source, an MF power source, and an RF power source, and may be a combination thereof.
Thus, the adhesive layer 6 and the optical functional layer 7 (antireflection layer) are disposed in this order on one surface of the base layer 2 in the thickness direction.
< fifth step >
In the fifth step, as shown in D of fig. 4, the antifouling layer 3 is disposed on the optical functional layer 7 (antireflection layer). Specifically, the antifouling layer 3 is disposed on one surface of the optical functional layer 7 (antireflection layer) in the thickness direction.
In this method, first, from the viewpoint of improving the adhesion between the optical functional layer 7 (anti-reflection layer) and the stain-proofing layer 3, the surface of the optical functional layer 7 (anti-reflection layer) is subjected to, for example, a surface treatment. The surface treatment may be the surface treatment in the second step, and preferably the surface treatment may be a plasma treatment, and more preferably an oxygen-based plasma treatment.
The method of disposing the antifouling layer 3 on the optical functional layer 7 (antireflection layer) may be the same as the method of disposing the antifouling layer 3 on the base layer 2 in the second step, and from the viewpoint of adjusting the integrated intensity ratio to a predetermined value or less, a dry coating method may be preferable, and a vacuum vapor deposition method may be more preferable.
In the vacuum vapor deposition method, a vapor deposition source (alkoxysilane compound having a perfluoropolyether group) and an optical functional layer 7 (antireflection layer) are disposed in a vacuum chamber, and the vapor deposition source is heated to evaporate or sublimate the vapor deposition source, and the evaporated or sublimated vapor deposition source is deposited on the surface of the optical functional layer 7 (antireflection layer).
In the vacuum vapor deposition method, the temperature of the vapor deposition source (crucible) is, for example, 200 ℃ or higher, preferably 250 ℃ or higher, and 300 ℃ or lower.
Thus, the antifouling layer 3 is disposed on one surface in the thickness direction of the optical functional layer 7 (antireflection layer), and the laminate 1 including the base material layer 2, the adhesive layer 6, the optical functional layer 7 (antireflection layer), and the antifouling layer 3 in this order on one surface in the thickness direction is manufactured.
< Effect >
The laminate 1 has an optical functional layer 7 (antireflection layer) between the base layer 2 and the stain-proofing layer 3.
Therefore, reflection of external light can be suppressed.
In the case where one surface in the thickness direction of the optical functional layer 7 (antireflection layer) is a layer containing silica, in other words, in the case where a layer containing silica (for example, the second low refractive index layer 14 made of silica) is directly disposed on the lower surface of the antifouling layer 3, the hydrolysis group in the alkoxysilane compound having a perfluoropolyether group in the antifouling layer 3 (formula (1) In- (OR) 3 ) Silanol groups generated during the hydrolysis process and silicon in the silica undergo dehydration condensation reaction. In other words, the stain-proofing layer 3 is formed on the optical functional layer 7 (antireflection layer) by a siloxane bond through an alkoxysilane compound having a perfluoropolyether group. This can further improve the stain resistance.
3. Modification examples
In the modification, the same members and steps as those in the first and second embodiments are denoted by the same reference numerals, and detailed description thereof is omitted. The modified example can exhibit the same operational effects as those of the first embodiment and the second embodiment unless otherwise described. Further, the first embodiment, the second embodiment, and modifications thereof can be appropriately combined.
In the first embodiment, the laminate 1 includes the base layer 2 and the stain-proofing layer 3, but as shown in fig. 5, a primer layer 15 may be further provided between the base layer 2 and the stain-proofing layer 3. Specifically, the laminate 1 may include the primer layer 15 on the other surface in the thickness direction of the stain-proofing layer 3.
In other words, in this case, the laminate 1 includes the base material layer 2, the primer layer 15, and the stain-proofing layer 3 in this order on one surface side in the thickness direction.
The primer layer 15 is a layer that adheres to the stain-proofing layer 3.
As a material of the primer layer 15, silica (SiO 2 ). Primer layer 15 is more preferably composed of silica (SiO 2 ) And (5) forming.
If the material of the primer layer 15 is silica (SiO 2 ) The hydrolysis group in the alkoxysilane compound having a perfluoropolyether group in the stain-proofing layer 3 (- (OR) in the above formula (1) 3 ) Silanol groups generated during the hydrolysis process and silicon in the silica undergo dehydration condensation reaction. In other words, the stain-proofing layer 3 is formed on the primer layer 15 via a siloxane bond by an alkoxysilane compound having a perfluoropolyether group. This can further improve the stain resistance.
The primer layer 15 is formed by, for example, a sputtering method, a plasma CVD method, a vacuum deposition method, or the like.
In the first and second embodiments, the base material layer 2 includes the base material 4 and the functional layer 5 in this order on one surface side in the thickness direction. However, the base material layer 2 may be formed of the base material 4 without the functional layer 5.
In the second embodiment, the antireflection layer includes two high refractive index layers having relatively high refractive index, and two low refractive index layers having relatively low refractive index. However, the number of the high refractive index layers and the low refractive index layers is not particularly limited.
Examples
Hereinafter, the present invention will be described more specifically by way of examples and comparative examples. The present invention is not limited to examples and comparative examples. Specific numerical values such as the blending ratio (content ratio), physical property value, and parameter used in the following description may be replaced with the upper limit value (numerical value defined in the form of "below", "less than") or the lower limit value (numerical value defined in the form of "above", "exceeding") described in the above "specific embodiment" in correspondence with the blending ratio (content ratio), physical property value, parameter, and the like.
1. Manufacture of laminate
Example 1
< third step >
As a substrate, a cellulose Triacetate (TAC) film (thickness 80 μm) was prepared.
Next, a hard coat layer is disposed on one surface of the base material (TAC film) in the thickness direction. Specifically, first, an organic silica sol (MEK-ST-L, manufactured by Nissan chemical Co., ltd., silica particles (inorganic filler) having an average primary particle diameter of 50nm, a particle diameter distribution of silica particles of 30nm to 130nm, and a solid content of 30 wt%) was added to an ultraviolet-curable acrylic resin composition (trade name "GRANDIC PC-1070", manufactured by DIC Co., ltd., refractive index at 405 nm: 1.55) so that the amount of silica particles was 25 parts by mass relative to 100 parts by mass of the resin component, and the mixture was mixed to prepare a hard coat composition. The hard coating composition was applied to the substrate (TAC film) in the thickness direction so that the thickness after drying became 6. Mu.m Is dried at 80℃for 3 minutes. Thereafter, an accumulated light amount of 200mJ/cm was irradiated using a high-pressure mercury lamp 2 The coating layer is cured by ultraviolet rays to form a hard coating layer. Thereby, a base material layer is prepared.
< fourth step >
One surface of the base material layer (hard coat layer) in the thickness direction was subjected to plasma treatment in a vacuum atmosphere of 1.0Pa by a roll-to-roll type plasma treatment apparatus. In this plasma treatment, argon gas was used as an inert gas, and the discharge power was set to 100W.
Next, an adhesion layer and an antireflection layer (optical functional layer) are sequentially arranged (formed) on one surface in the thickness direction of the base material layer.
Specifically, by using a roll-to-roll type sputter film forming apparatus, an Indium Tin Oxide (ITO) layer having a thickness of 2.0nm as an adhesion layer and Nb having a thickness of 12nm as a first high refractive index layer were sequentially disposed (formed) on the HC layer of the TAC film having the HC layer after plasma treatment 2 O 5 Layer, siO with thickness of 28nm as first low refractive index layer 2 Layer, nb with thickness of 100nm as second high refractive index layer 2 O 5 Layer, siO 85nm thick as second low refractive index layer 2 A layer.
In the formation of the adhesion layer, an ITO target was used, and an oxygen gas as a reactive gas was used in an amount of 10 parts by volume relative to 100 parts by volume of argon gas and argon gas, the discharge voltage was set to 350V, and the gas pressure in the film forming chamber (film forming gas pressure) was set to 0.4Pa, whereby an ITO layer was formed by MFAC sputtering.
In the formation of the first high refractive index layer, an Nb target is used. In addition, 100 parts by volume of argon and 5 parts by volume of oxygen were used. Further, nb was formed by MFAC sputtering with a discharge voltage of 415V and a film formation air pressure of 0.42Pa 2 O 5 A layer.
In the formation of the first low refractive index layer, a Si target is used. In addition, 100 parts by volume of argon and 30 parts by volume of oxygen were used. Further, the discharge voltage was set to 350V, the film formation air pressure was set to 0.3Pa, and S was formed by MFAC sputteringiO 2 A layer.
In the formation of the second high refractive index layer, an Nb target is used. In addition, 100 parts by volume of argon and 13 parts by volume of oxygen were used. Further, nb was formed by MFAC sputtering with a discharge voltage of 460V and a film formation air pressure of 0.5Pa 2 O 5 A layer.
In the formation of the second low refractive index layer, a Si target is used. In addition, 100 parts by volume of argon and 30 parts by volume of oxygen were used. Further, siO was formed by MFAC sputtering with a discharge voltage of 340V and a film formation air pressure of 0.25Pa 2 A layer.
In this way, the adhesion layer and the antireflection layer are sequentially disposed (formed) on one surface of the base material layer in the thickness direction.
< fifth step >
An anti-fouling layer is arranged on one surface of the anti-reflection layer in the thickness direction.
Specifically, first, plasma treatment is performed with oxygen as a surface treatment on one surface of the antireflective layer in the thickness direction. The output power of the plasma treatment was 100W. Next, an anti-fouling layer having a thickness of 7nm was disposed on one surface in the thickness direction of the anti-reflective layer by a vacuum vapor deposition method using an alkoxysilane compound containing a perfluoropolyether group as a vapor deposition source.
The vapor deposition source is a solid component obtained by drying Optool UD509 (alkoxysilane compound containing a perfluoropolyether group represented by the above general formula (2), having a solid component concentration of 20% by mass, and manufactured by large-size gold industry). The heating temperature of the vapor deposition source (crucible) in the vacuum vapor deposition method was set to 260 ℃. Thus, a laminate was obtained.
Example 2
A laminate was produced according to the same procedure as in example 1.
In the fifth step, the surface treatment of one surface of the antireflective layer in the thickness direction is changed from the oxygen-based plasma treatment to the argon-based plasma treatment.
In the fifth step, the vapor deposition source was changed to an Optool UD120 (manufactured by dajinshi corporation).
Example 3
A laminate was produced according to the same procedure as in example 1.
In the fifth step, the vapor deposition source was changed to KY1903-1 (manufactured by Xinyue chemical Co., ltd.).
Comparative example 1
A laminate was produced according to the same procedure as in example 1.
The fifth step is modified as follows.
< fifth step >
Using a gravure coater, the Optool UD509 was applied to one surface of the antireflective layer in the thickness direction so that the applied thickness became 8 μm. Thereafter, a heating treatment was performed at a drying temperature of 60℃for 60 seconds. Thus, an anti-fouling layer having a thickness of 7nm was disposed on one surface in the thickness direction of the anti-reflection layer.
Comparative example 2
A laminate was produced according to the same procedure as in example 2.
In the fifth step, the output power of the plasma treatment was changed to 4500W.
2. Evaluation
(grazing incidence X-ray diffraction measurement)
For the antifouling layers of the laminates of each example and each comparative example, in-plane diffraction (in-plane) measurement and out-of-plane diffraction (out-of-plane) measurement were performed by a grazing incidence X-ray diffraction method according to the following conditions.
The results of the in-plane diffraction (in-plane) measurement of example 2 are shown in FIG. 6. The results of the out-of-plane diffraction (out-of-plane) measurement of example 2 are shown in FIG. 7.
< measurement conditions >
Experiment place: japanese love synchronous accelerator optical center
Experiment station: BL8S1
Incident energy: 14.4keV
Beam size: 500 μm (width). Times.40 μm (longitudinal)
Sample angle: at 0.1 degree relative to incident light
A detector: two-dimensional detector PILATAS
The sample setting method comprises the following steps: fixed on a flat sample table by using thin Bao Tubu grease
The in-plane diffraction integrated intensity (first in-plane diffraction integrated intensity and second in-plane diffraction integrated intensity) and the out-of-plane diffraction integrated intensity are calculated from the results of the in-plane diffraction (in-plane) measurement and the out-of-plane diffraction (out-of-plane) measurement. The calculation method uses a fitting method from the viewpoint of uniformly calculating the in-plane diffraction integrated intensity and the out-of-plane diffraction integrated intensity. The method will be described in detail by taking example 2 as an example.
First, fitting was performed according to the following formula (3) on the results obtained in the in-plane diffraction (in-plane) measurement (hereinafter referred to as actual measurement data (in-plane diffraction measurement)). Specifically, the actual measurement data (in-plane diffraction) is assumed to be the sum of the background and the peaks A1 to A4 (see fig. 8), and fitting is performed. The wavelength of the light was 24nm at a high wavelength between all samples -1 Is standardized in a manner consistent with the background of the figure.
(in the formula (3), q represents a scattering vector (wave number) (=4πsin Θ/λ)/nm) -1 (Θ represents the Bragg angle. Lambda. Represents the wavelength of X-rays). An represents the peak intensity (n is An integer of 1 to 4. A) 1 The peak intensity of the peak A1 is shown. A is that 2 The peak intensity of peak A2 is shown. A is that 3 The peak intensity of the peak A3 is shown. A is that 4 Representing the peak intensity of peak A4). q An Represents the position of the center of gravity (q A1 The center of gravity position of the peak A1 is shown. q A2 The center of gravity position of the peak A2 is shown. q A3 The center of gravity position of the peak A3 is shown. q A4 Representing the position of the center of gravity of peak A4). Δq An Representing the full width at half maximum (Δq A1 Representing the full width at half maximum of peak A1. Δq A2 Representing the full width at half maximum of peak A2. Δq A3 Representing the full width at half maximum of peak A3. Δq A4 Representing the full width half maximum of peak A4).
In addition, the peak A1 and the peak B1 show layered laminationPeak of structure, gravity center position isAbove and->The following is given. In addition, the peak A4 is a peak derived from the periodic arrangement of the perfluoropolyether groups in the in-plane direction, and the center of gravity is +.>Above and->The following is given.
The fitting result is shown in fig. 8 (example 2).
The fitting result is shown in FIG. 6 together with measured data (in-plane diffraction measurement).
As can be seen from fig. 6: the measured data (in-plane diffraction (in-plane) measurements) are sufficiently consistent with the fitting results.
From this, it can be seen that: the measured data (in-plane diffraction (in-plane) measurements) can be shown as a sum of background and peaks A1 to A4 as assumed.
Then, the integrated intensity (first in-plane diffraction integrated intensity) of the diffraction peak A1 belonging to the structure in which the sheet is aligned parallel to the base material layer was calculated according to the following formula (4). The results are shown in Table 1.
First in-plane diffraction integrated intensity=peak intensity (a 1 ) Full width at half maximum (. DELTA.q) A1 ) (4)
Further, the integrated intensity (second in-plane diffraction integrated intensity) of the peak A4 derived from the periodic arrangement of the perfluoropolyether group in the in-plane direction was calculated according to the following formula (5). The results are shown in Table 1.
Second in-plane diffraction integrated intensity=peak intensity (a 4 ) Full width at half maximum (. DELTA.q) A4 )(5)
Next, the results obtained in the out-of-plane diffraction (out-of-plane) measurement (hereinafter, referred to as actual measurement data (out-of-plane)Measurement), fitting was performed according to the following equation (6). Specifically, the actual measurement data (out-of-plane measurement) is assumed to be the sum of the background and peaks B1 to B3 (see fig. 9), and fitting is performed. The wavelength of the light was 24nm at a high wavelength between all samples -1 Is standardized in a manner consistent with the background of the figure.
(in the formula (6), q represents a scattering vector (=4pi.sin. Theta./lambda.)/nm -1 (Θ represents a Bragg angle, λ represents a wavelength of X-rays), bn represents a peak intensity (n is an integer of 1 to 3, B) 1 The peak intensity of the peak B1 is shown. B (B) 2 The peak intensity of the peak B2 is shown. B (B) 3 Representing the peak intensity of peak B3). q Bn Represents the position of the center of gravity (q B1 The center of gravity position of the peak B1 is shown. q B2 The center of gravity position of the peak B2 is shown. q B3 Representing the position of the center of gravity of peak B3). Δq Bn Representing the full width at half maximum (Δq B1 Representing the full width at half maximum of peak B1. Δq B2 Representing the full width at half maximum of peak B2. Δq B3 Representing the full width half maximum of peak B3).
The fitting result is shown in fig. 9 (example 2).
The fitting result is shown in FIG. 7 together with measured data (out-of-plane measurement).
As can be seen from fig. 7: the measured data (out-of-plane measurement) are sufficiently consistent with the fitting results.
From this, it can be seen that: the measured data (out-of-plane measurement) can be shown as a sum of background and peaks B1 to B3 as assumed.
Then, the integrated intensity (out-of-plane diffraction integrated intensity) of the diffraction peak B1 due to the structure in which the flakes are oriented vertically with respect to the base material layer was calculated according to the following formula (7). The results are shown in Table 1.
Out-of-plane diffraction integral intensity=peak intensity (B 1 ) Full width at half maximum (. DELTA.q) B1 )(7)
In summary, from the first in-plane diffraction integrated intensity, the second in-plane diffraction integrated intensity, and the out-of-plane diffraction integrated intensity, a first integrated intensity ratio of the first in-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity (first in-plane diffraction integrated intensity/second in-plane diffraction integrated intensity), a second integrated intensity ratio of the out-of-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity (out-of-plane diffraction integrated intensity/second in-plane diffraction integrated intensity), and a third integrated intensity ratio of the first in-plane diffraction integrated intensity to the out-of-plane diffraction integrated intensity (first in-plane diffraction integrated intensity/out-of-plane diffraction integrated intensity) are calculated. The results are shown in Table 1.
(antifouling durability)
For the antifouling layer of the laminate of each example and each comparative example, the contact angle (sometimes referred to as initial contact angle) of the antifouling layer with pure water was measured under the following conditions using DMo-501 manufactured by the company of interfacial science. The results are shown in Table 1.
< measurement conditions >
Drop amount: 2 μl
Temperature: 25 DEG C
Humidity: 40 percent of
Next, after the rubber slip test was performed on the antifouling layer of the laminate of each example and each comparative example under the following conditions, the water contact angle (sometimes referred to as the contact angle after the rubber slip test) was measured in the same manner as described above. The results are shown in Table 1.
Then, the amount of change in the contact angle was calculated according to the following formula (8). The results are shown in Table 1.
The smaller the amount of change in contact angle, the more excellent the antifouling durability was evaluated.
Variation of contact angle = initial contact angle-contact angle after rubber slip test (8)
(rubber slip test)
Rubber (phi 6 mm) made by Minoan company
Sliding distance: single pass 100mm sliding speed: 100 mm/sec load: number of sliding of 1kg/6mm phi: 3000 times
TABLE 1
The above-described invention is provided as an exemplary embodiment of the present invention, and is merely illustrative, and not restrictive. Variations of the present invention that are obvious to a practitioner of skill in the art are included in the foregoing claims.
Industrial applicability
The laminate of the present invention can be suitably used in, for example, an antireflection film with an antifouling layer, a transparent conductive film with an antifouling layer, and an electromagnetic wave-shielding film with an antifouling layer.
Description of the reference numerals
1 laminate
2 substrate layer
3 antifouling layer
6 sealing layer
15 primer layer
Claims (7)
1. A laminate comprising a base layer and an antifouling layer in this order on one side in the thickness direction,
the stain repellent layer comprises an alkoxysilane compound having a perfluoropolyether group,
the laminate has a first integrated strength ratio of the antifouling layer of 0.78 or less as measured by a first test described below,
a primer layer is provided on the other surface of the antifouling layer in the thickness direction,
the primer layer is a layer comprising silica,
first test: for the antifouling layer, the integrated intensity of the peak attributed to the layered structure (first in-plane diffraction integrated intensity) was measured by in-plane diffraction (in-plane) measurement in a grazing incidence X-ray diffraction method; further, the integrated intensity of the peaks derived from the periodic arrangement of the perfluoropolyether groups in the in-plane direction (second in-plane diffraction integrated intensity) was measured for the anti-fouling layer by in-plane diffraction measurement by a grazing incidence X-ray diffraction method; from the obtained first in-plane diffraction integrated intensity and second in-plane diffraction integrated intensity, a first integrated intensity ratio (first in-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the first in-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated.
2. A laminate comprising a base layer and an antifouling layer in this order on one side in the thickness direction,
the stain repellent layer comprises an alkoxysilane compound having a perfluoropolyether group,
the laminate has a first integrated strength ratio of the antifouling layer of 0.78 or less as measured by a first test described below,
an adhesion layer and an antireflection layer are further provided between the base material layer and the stain-proofing layer,
one surface of the anti-reflection layer in the thickness direction is a layer containing silicon dioxide,
first test: for the antifouling layer, the integrated intensity of the peak attributed to the layered structure (first in-plane diffraction integrated intensity) was measured by in-plane diffraction (in-plane) measurement in a grazing incidence X-ray diffraction method; further, the integrated intensity of the peaks derived from the periodic arrangement of the perfluoropolyether groups in the in-plane direction (second in-plane diffraction integrated intensity) was measured for the anti-fouling layer by in-plane diffraction measurement by a grazing incidence X-ray diffraction method; from the obtained first in-plane diffraction integrated intensity and second in-plane diffraction integrated intensity, a first integrated intensity ratio (first in-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the first in-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated.
3. The laminate according to claim 1 or 2, wherein the second integrated strength ratio of the antifouling layer measured by the second test described below is 50 or less,
second test: for the antifouling layer, the integrated intensity of the peak attributed to the layered structure (integrated intensity of out-of-plane diffraction) was measured by out-of-plane diffraction (out-of-plane) measurement in a grazing incidence X-ray diffraction method; a second integrated intensity ratio (out-of-plane diffraction integrated intensity/second in-plane diffraction integrated intensity) of the out-of-plane diffraction integrated intensity to the second in-plane diffraction integrated intensity is calculated from the out-of-plane diffraction integrated intensity and the second in-plane diffraction integrated intensity.
4. The laminate of claim 1 or 2, wherein a third integrated intensity ratio (out-of-plane integrated diffraction intensity/first in-plane integrated diffraction intensity) of the out-of-plane integrated diffraction intensity to the first in-plane integrated diffraction intensity exceeds 220.
5. The laminate according to claim 1, wherein the anti-fouling layer is formed on the primer layer by a siloxane bond through an alkoxysilane compound having a perfluoropolyether group.
6. The laminate according to claim 2, wherein the antireflection layer is formed of two or more layers having refractive indices different from each other.
7. The laminate according to claim 6, wherein the antireflection layer comprises 1 kind selected from the group consisting of a metal, a metal oxide, and a metal nitride.
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| JP2020-120131 | 2020-07-13 | ||
| JP2020120131 | 2020-07-13 | ||
| JP2020146144 | 2020-08-31 | ||
| JP2020-146144 | 2020-08-31 | ||
| JP2020-166847 | 2020-10-01 | ||
| JP2020-166844 | 2020-10-01 | ||
| JP2020166844 | 2020-10-01 | ||
| JP2020166847 | 2020-10-01 | ||
| JP2020-190465 | 2020-11-16 | ||
| JP2020-190466 | 2020-11-16 | ||
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| JP2020190465 | 2020-11-16 | ||
| JP2020190466 | 2020-11-16 | ||
| JP2020-190468 | 2020-11-16 | ||
| JP2020-191680 | 2020-11-18 | ||
| JP2020191680 | 2020-11-18 | ||
| JP2021-015315 | 2021-02-02 | ||
| JP2021015315 | 2021-02-02 | ||
| PCT/JP2021/026253 WO2022014575A1 (en) | 2020-07-13 | 2021-07-13 | Laminate |
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| KR (1) | KR102522232B1 (en) |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5922787A (en) * | 1996-03-21 | 1999-07-13 | Sony Corporation | Composition for forming antifouling antifouling film, optical component, and display device |
| JP2005301208A (en) * | 2004-03-17 | 2005-10-27 | Seiko Epson Corp | Method for manufacturing stain proof optical article |
| JP2017170827A (en) * | 2016-03-25 | 2017-09-28 | 大日本印刷株式会社 | Laminate, touch panel, touch panel display device, and production method of laminate |
| CN110997587A (en) * | 2017-05-08 | 2020-04-10 | 康宁股份有限公司 | Glass, glass-ceramic and ceramic articles having durable lubricious anti-fingerprint coatings on optical and scratch-resistant coatings and methods of making same |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4289935B2 (en) * | 2003-06-19 | 2009-07-01 | 三井化学株式会社 | Composite multilayer film, self-organized manufacturing method thereof, and electronic component |
| US8945684B2 (en) * | 2005-11-04 | 2015-02-03 | Essilor International (Compagnie Generale D'optique) | Process for coating an article with an anti-fouling surface coating by vacuum evaporation |
| JP2009139530A (en) * | 2007-12-05 | 2009-06-25 | Seiko Epson Corp | Method for manufacturing optical article |
| JP2009251008A (en) * | 2008-04-01 | 2009-10-29 | Seiko Epson Corp | Optical product and method for producing the same |
| JP5387096B2 (en) * | 2008-08-27 | 2014-01-15 | 株式会社リコー | Liquid discharge head, image forming apparatus, and method of manufacturing liquid discharge head |
| JP5628491B2 (en) * | 2009-07-15 | 2014-11-19 | 日本ゼオン株式会社 | Resin surface modification method and surface modified resin substrate |
| JP2018004921A (en) * | 2016-06-30 | 2018-01-11 | ホヤ レンズ タイランド リミテッドＨＯＹＡ Ｌｅｎｓ Ｔｈａｉｌａｎｄ Ｌｔｄ | Spectacle lens, and manufacturing method for the same |
| JP7217118B2 (en) | 2018-09-26 | 2023-02-02 | 日東電工株式会社 | Optical film with protective film |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5922787A (en) * | 1996-03-21 | 1999-07-13 | Sony Corporation | Composition for forming antifouling antifouling film, optical component, and display device |
| JP2005301208A (en) * | 2004-03-17 | 2005-10-27 | Seiko Epson Corp | Method for manufacturing stain proof optical article |
| JP2017170827A (en) * | 2016-03-25 | 2017-09-28 | 大日本印刷株式会社 | Laminate, touch panel, touch panel display device, and production method of laminate |
| CN110997587A (en) * | 2017-05-08 | 2020-04-10 | 康宁股份有限公司 | Glass, glass-ceramic and ceramic articles having durable lubricious anti-fingerprint coatings on optical and scratch-resistant coatings and methods of making same |
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| JPWO2022014575A1 (en) | 2022-01-20 |
| WO2022014575A1 (en) | 2022-01-20 |
| TW202212138A (en) | 2022-04-01 |
| KR102522232B1 (en) | 2023-04-14 |
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