WO2000027771A1 - Solar control coatings and coated articles - Google Patents
Solar control coatings and coated articles Download PDFInfo
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- WO2000027771A1 WO2000027771A1 PCT/US1999/026406 US9926406W WO0027771A1 WO 2000027771 A1 WO2000027771 A1 WO 2000027771A1 US 9926406 W US9926406 W US 9926406W WO 0027771 A1 WO0027771 A1 WO 0027771A1
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- 238000000576 coating method Methods 0.000 title claims abstract description 207
- 239000010410 layer Substances 0.000 claims abstract description 155
- 239000011248 coating agent Substances 0.000 claims abstract description 149
- 239000011521 glass Substances 0.000 claims abstract description 111
- 239000011247 coating layer Substances 0.000 claims abstract description 81
- 239000000758 substrate Substances 0.000 claims abstract description 66
- 238000010521 absorption reaction Methods 0.000 claims abstract description 26
- 229910052751 metal Inorganic materials 0.000 claims abstract 8
- 239000002184 metal Substances 0.000 claims abstract 8
- 230000000007 visual effect Effects 0.000 claims abstract 5
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 74
- 230000005540 biological transmission Effects 0.000 claims description 73
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical group O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 claims description 72
- XOLBLPGZBRYERU-UHFFFAOYSA-N tin dioxide Chemical compound O=[Sn]=O XOLBLPGZBRYERU-UHFFFAOYSA-N 0.000 claims description 70
- 229910001887 tin oxide Inorganic materials 0.000 claims description 66
- 238000013461 design Methods 0.000 claims description 38
- 239000000463 material Substances 0.000 claims description 35
- 239000000377 silicon dioxide Substances 0.000 claims description 30
- 238000001228 spectrum Methods 0.000 claims description 26
- 230000003287 optical effect Effects 0.000 claims description 19
- 238000001429 visible spectrum Methods 0.000 claims description 14
- 229910052787 antimony Inorganic materials 0.000 claims description 12
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 12
- 229910000314 transition metal oxide Inorganic materials 0.000 claims description 10
- 229910052731 fluorine Inorganic materials 0.000 claims description 9
- 239000011737 fluorine Substances 0.000 claims description 9
- 230000002829 reductive effect Effects 0.000 claims description 9
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 claims description 7
- 239000003086 colorant Substances 0.000 claims description 6
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 230000000903 blocking effect Effects 0.000 claims description 4
- 239000004408 titanium dioxide Substances 0.000 claims description 4
- 230000007423 decrease Effects 0.000 claims description 3
- 238000005137 deposition process Methods 0.000 claims description 3
- 230000009977 dual effect Effects 0.000 claims description 3
- 230000004075 alteration Effects 0.000 claims description 2
- 238000002211 ultraviolet spectrum Methods 0.000 claims description 2
- 239000006117 anti-reflective coating Substances 0.000 claims 1
- 239000002019 doping agent Substances 0.000 claims 1
- 125000001153 fluoro group Chemical group F* 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 12
- 239000010409 thin film Substances 0.000 abstract description 8
- 239000002131 composite material Substances 0.000 abstract description 7
- 229910052681 coesite Inorganic materials 0.000 description 14
- 229910052906 cristobalite Inorganic materials 0.000 description 14
- 229910052682 stishovite Inorganic materials 0.000 description 14
- 229910052905 tridymite Inorganic materials 0.000 description 14
- 238000002834 transmittance Methods 0.000 description 10
- 239000000203 mixture Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 8
- 230000001629 suppression Effects 0.000 description 8
- 238000004140 cleaning Methods 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 238000013459 approach Methods 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 230000009467 reduction Effects 0.000 description 6
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 5
- 230000003247 decreasing effect Effects 0.000 description 5
- 230000005855 radiation Effects 0.000 description 5
- CJYDNDLQIIGSTH-UHFFFAOYSA-N 1-(3,5,7-trinitro-1,3,5,7-tetrazocan-1-yl)ethanone Chemical compound CC(=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)CN([N+]([O-])=O)C1 CJYDNDLQIIGSTH-UHFFFAOYSA-N 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 238000000151 deposition Methods 0.000 description 4
- 238000002310 reflectometry Methods 0.000 description 4
- 239000000654 additive Substances 0.000 description 3
- 230000002238 attenuated effect Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 230000033228 biological regulation Effects 0.000 description 3
- YMLFYGFCXGNERH-UHFFFAOYSA-K butyltin trichloride Chemical compound CCCC[Sn](Cl)(Cl)Cl YMLFYGFCXGNERH-UHFFFAOYSA-K 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 239000010408 film Substances 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 238000000985 reflectance spectrum Methods 0.000 description 3
- 238000004544 sputter deposition Methods 0.000 description 3
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 239000005329 float glass Substances 0.000 description 2
- 239000003574 free electron Substances 0.000 description 2
- 230000007935 neutral effect Effects 0.000 description 2
- NDLPOXTZKUMGOV-UHFFFAOYSA-N oxo(oxoferriooxy)iron hydrate Chemical compound O.O=[Fe]O[Fe]=O NDLPOXTZKUMGOV-UHFFFAOYSA-N 0.000 description 2
- VTRUBDSFZJNXHI-UHFFFAOYSA-N oxoantimony Chemical compound [Sb]=O VTRUBDSFZJNXHI-UHFFFAOYSA-N 0.000 description 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 2
- 108091006149 Electron carriers Proteins 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 238000006124 Pilkington process Methods 0.000 description 1
- HNZHVTZRIBKSIO-UHFFFAOYSA-N [Cs+].[Cs+].[O-][O-] Chemical compound [Cs+].[Cs+].[O-][O-] HNZHVTZRIBKSIO-UHFFFAOYSA-N 0.000 description 1
- 230000002730 additional effect Effects 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000003667 anti-reflective effect Effects 0.000 description 1
- 229910000410 antimony oxide Inorganic materials 0.000 description 1
- DAMJCWMGELCIMI-UHFFFAOYSA-N benzyl n-(2-oxopyrrolidin-3-yl)carbamate Chemical compound C=1C=CC=CC=1COC(=O)NC1CCNC1=O DAMJCWMGELCIMI-UHFFFAOYSA-N 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 239000012159 carrier gas Substances 0.000 description 1
- 238000005229 chemical vapour deposition Methods 0.000 description 1
- 239000008199 coating composition Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 229910001610 cryolite Inorganic materials 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000009501 film coating Methods 0.000 description 1
- 239000005357 flat glass Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000004313 glare Effects 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
- 230000003993 interaction Effects 0.000 description 1
- 239000005340 laminated glass Substances 0.000 description 1
- 239000002650 laminated plastic Substances 0.000 description 1
- 230000031700 light absorption Effects 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 230000001699 photocatalysis Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000002243 precursor Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 238000000197 pyrolysis Methods 0.000 description 1
- 238000007634 remodeling Methods 0.000 description 1
- 238000009436 residential construction Methods 0.000 description 1
- 238000010206 sensitivity analysis Methods 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- 229920005573 silicon-containing polymer Polymers 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- SKRWFPLZQAAQSU-UHFFFAOYSA-N stibanylidynetin;hydrate Chemical compound O.[Sn].[Sb] SKRWFPLZQAAQSU-UHFFFAOYSA-N 0.000 description 1
- 230000008685 targeting Effects 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- QHGNHLZPVBIIPX-UHFFFAOYSA-N tin(ii) oxide Chemical class [Sn]=O QHGNHLZPVBIIPX-UHFFFAOYSA-N 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 238000000411 transmission spectrum Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 238000001771 vacuum deposition Methods 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B5/00—Optical elements other than lenses
- G02B5/20—Filters
- G02B5/28—Interference filters
- G02B5/283—Interference filters designed for the ultraviolet
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C17/00—Surface treatment of glass, not in the form of fibres or filaments, by coating
- C03C17/34—Surface treatment of glass, not in the form of fibres or filaments, by coating with at least two coatings having different compositions
- C03C17/3411—Surface treatment of glass, not in the form of fibres or filaments, by coating with at least two coatings having different compositions with at least two coatings of inorganic materials
- C03C17/3417—Surface treatment of glass, not in the form of fibres or filaments, by coating with at least two coatings having different compositions with at least two coatings of inorganic materials all coatings being oxide coatings
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B5/00—Optical elements other than lenses
- G02B5/20—Filters
- G02B5/208—Filters for use with infrared or ultraviolet radiation, e.g. for separating visible light from infrared and/or ultraviolet radiation
Definitions
- the present invention is directed to solar control coatings for transparent articles to improve the ultraviolet reflection and/or near infrared reflection and /or to increase the visible transmission of the coated article.
- Transparent articles such as glass, certain plastics, and glass and plastic laminates used in such industries as commercial and/or residential construction and remodeling and motor vehicle and aircraft manufacturing require particular solar performance properties for these particular industries.
- designers incorporate into their designs transparencies as windows and windshields that are both functional and attractive.
- Heat that builds up in the passenger compartments of motor vehicles from exposure to solar energy can be managed with air conditioning systems.
- air conditioning systems Of course, the larger the build up of heat, the greater the demand on such systems. Reducing the build up of heat through the windows has become a concern of the designer.
- UV ultraviolet
- IR solar energy IR
- transparencies that provide lower infrared transmittance and lower total solar energy transmittance are desirable for reducing the heat gain in the vehicle interior but should also coordinate to some degree with the color of the windshield transparency. Glass with these properties would be highly desirable for not only automotive applications but for architectural use as well. It would further be desirable if the glass was also compatible with flat glass manufacturing methods for ease of production.
- glass transparencies are needed that have a UV light transmission of less than 10 percent and a total solar energy transmission (“TSET”) of less than 50 percent.
- TSET total solar energy transmission
- An attempt at serving this market involves an uncoated substrate that blocks UV light by the addition of titanium dioxide, Ti0 2 , and cesium dioxide, Ce0 2 in the glass composition. These additives substantially increase the cost of the substrate. This product is only available as a green glass.
- Organic coatings can be developed with UV and near infrared light (“NIR”) absorbing additives to attain the target specifications without the use of Ce0 2 . These organic coatings lack the durability usually obtained with uncoated glass substrate.
- NIR near infrared light
- Multi-layer coating composites on transparency or glass substrates comprise alternating layers of high and low refractive index of predominantly inorganic coatings to at least block UV light by a combination of thin film interference and absorption effects.
- the amount of UV light transmission is a function of the number of layers and the properties of the substrate. For instance the UV reduction can be obtained with as few as three layers on a solar control glass. This is possible with the alternating layers of titania and silica for rejecting ultraviolet light. In such a case the thickness of the layers is about 300 and about 550 A, for titania and silica, respectively.
- the multi-layered coating composite can have a thickness of about 1041 to 1725 A, for titania and silica layers, respectively to reject NIR.
- the TSET of the coated glass can be reduced if the thicknesses of the layers of the multi-layer are appropriately selected.
- a four layer coating on a green solar control glass can have a TSET less than 37% while simultaneously attaining a low International Standards Organization standard ("ISO") UV target.
- ISO International Standards Organization standard
- This type of coating, that reduces both the UV and NIR light transmission, is ideally suited for other substrates that do not have good solar control properties.
- the present invention can involve a four layer multilayered coating composite on the transparency or glass substrate.
- a four layer titania/silica/titania/silica coating on about a .0 mm thick green solar control glass to attain a UV transmission of less than 10%, ISO while maintaining a visible light transmission of greater than 70%.
- This coating will also reduce the visible light reflection to about 8.0% and a total solar energy transmission ("TSET") ⁇ about 45%.
- TSET total solar energy transmission
- Such a four layered transparency can attain an ISO UV transmission of less than 10% while maintaining a visible light transmission of greater than 70% and reducing the total solar energy transmitted to about 36%.
- This multilayered coating can also reduce the visible light reflection to ⁇ 8%.
- Such a four layer multilayered coating on solar control glass when used as a windshield can be tuned to a windshield installation angle of about 65°. This will reduce the visible light reflection to about 13%.
- Another suitable multi-layered coating composite on transparencies or glass substrates can have coatings with additional materials such as fluorine- or antimony-doped tin oxide. With these materials the coatings can impart other properties such as electrical conductivity or solar absorption.
- Antimony-doped tin oxide prepared in the appropriate manner, can absorb green light thereby altering the transmitted color of green glass like Solex ® or Solargreen 6 glass, available from PPG Industries, Inc., from green to gray. Control of possible changes to the optical properties of coatings with antimony-doped tin oxide because of heat treatment of the coated substrate like tempering or annealing is obtained by the deposition conditions and particular composition of the antimony-doped tin oxide coating.
- any of the aforediscussed multilayered coating composites on substrates can include self cleaning or easy cleaning properties imparted to the coating by depositing the titania in the anatase phase.
- the self cleaning properties can function even through a surface silica layer.
- the transmitted color of solar control coatings can be modified by substituting a transition metal oxide for all or part of a titania or high refractive index coating layer.
- a fourth coating layer can add an anti- reflection effect and aesthetic options. Also to maintain the reflected color within desired ranges, the thicknesses of these multi-layer coatings can be controlled.
- FIG. 1 is a plot of theoretical light reflectance in percent versus wavelength in nanometers ( 'nm.") of the light spectrum at curve A for a titania coating with a refractive index of 2.55 on clear glass showing the reflectance over the visible spectrum, where the illuminant was white in an air medium where the substrate is clear glass at a reference wavelength of 380 nm and 0.0 degrees with an ideal detector.
- Curve B is the reflectance versus wavelength curve for a three layer SHLH coating of titania, H (high refractive index) , and silica, L (low refractive index), on float glass.
- FIG. 2 shows plots of theoretical reflectance versus wavelength at curve A and curve B for a SHLH coating stack and SHLHLL coating stack, respectively, both on green glass available as SOLARGREEN® glass.
- the illuminant, medium detector and angle were the same as for Figure 1.
- FIG. 3 shows plots of theoretical reflectance versus wavelength at curve A and curve B for a SLHL coating stack on clear glass substrate with a design wavelength of 330 nm. With and without absorption in the Ti0 coating layer and no absorption in the Si0 2 , coating layer. Other conditions were similar to those for Figure 1.
- FIG. 4 shows plots of curves A and B of theoretical reflectance versus wavelength for an S3H3L3H3 coating stack and S3H3L3H3LL respectively.
- the last coating layer for the coating stack for Curve B is Si0 2 at a wave in the visible which is a l/8 th wave in the NIR.
- Other conditions were similar to those for Figure 1 except the design wavelength was 350 nm.
- FIG. 5 shows plots of curves A and B of theoretical reflectance versus wavelength for an S3H3L3H3 coating stack as in Fig. 4 for curve A and with fluorine doped tin oxide substituted as part of the middle third of the inner silica coating layer as curve B.
- the other conditions were the same as those for Fig 4.
- FIG. 6 shows plots of curves A and B of theoretical reflectance versus wavelength for an S3H3L3H3LL coating stack as in Fig. 4 for curve A and with fluorine doped tin oxide substituted as part of the middle third of the inner silica coating layer as curve B.
- the other conditions were the same as those for Fig 4.
- FIG. 7 shows plots of curves A and B of theoretical reflectance versus wavelength where curve A shows the NIR reflectance peak resulting from the SHLH stack where the Ti0 is the high index coating layer and the fluorine-doped tin oxide is the low index coating layer.
- Curve B is for a TCO coating layer added below the SHLH coating stack to have a SMHMH coating stack. The other conditions are the same as those for Figure 1 except the design wavelength is 1000 nm.
- FIG 8 shows plots of theoretical reflectance versus wavelength of a comparison of a coating stack without a color suppression layer to one with the stack configuration of SM/2HLH.
- the former is curve A which is curve A of Figure 7 too, and the latter is for curve B.
- the other conditions are the same as those for Figure 7.
- FIG. 9 shows plots of theoretical reflectance versus wavelength of a comparison of a coating stack without a color suppression layer, Curve A, which is Curve A of Figure 7 to one with a graded coating layer ("G") as the color suppressant of a coating stack of SGHLH for Curve B.
- G graded coating layer
- FIG. 10 shows plots of theoretical reflectance versus wavelength of a comparison of curve A of Figure 7 as curve A to a coating stack of SGLHLH for curve B.
- the other conditions are the same as those for Figure 7.
- FIG. 11 shows plots of theoretical reflectance versus wavelength of a comparison of curve A of Figure 7 as curve A to a coating stack of SMHMHL for curve B.
- the other conditions are the same as those for Figure 7.
- FIG. 12 shows plots of theoretical reflectance versus wavelength of a comparison of curve A of Figure 7 as curve A to a coating stack of SHLMLMH for curve B.
- the other conditions are the same as those for Figure 7.
- FIG. 13 shows plots of theoretical reflectance versus wavelength of a comparison of curve A of Figure 7 as curve A to a coating stack of SHLMH for curve B.
- the other conditions are the same as those for Figure 7.
- FIG. 14 shows plots of solar absorption versus wavelength for several antimony-doped tin oxide coatings indicating that as the amount of antimony increases, the electrical conductivity degrades and the coating starts to significantly absorb solar radiation.
- FIG. 15 shows plots of theoretical transmission in percent versus wavelength of a comparison of that for curve A of Figure 7 as curve A to a coating stack of a single coating layer of antimony tin oxide for curve B.
- the other conditions are the same as those for Figure 7.
- FIG. 16 shows the theoretical light transmission curves from a coating stack of G and antimony-doped tin oxide and fluorine- doped tin oxide through a plot of transmission versus wavelength as curve B versus one for curve A of Figure 7 as curve A.
- the other conditions are the same as those for Figure 15.
- FIG. 17 shows the theoretical light transmission curves from a coating stack similar to that of Curve B of Figure 16 but with a thicker antimony-doped tin oxide layer as Curve A and with an outer coating layer of Ti0 for curve B.
- the other conditions are the same as those for Figure 15.
- FIG. 18 shows the theoretical light transmission curves of that for curve A of Figure 17 and that of curve B for a coating stack with the fluorine-doped tin oxide removed to have a coating stack of graded layer, antimony-doped tin oxide,, and Ti0 2 .
- the other conditions are the same as those for Figure 15.
- FIG. 19 shows the theoretical light transmission curves of that for curve A which is a single antimony-doped tin oxide coating on the clear glass substrate similar to curve B of Figure 15 to that for curve B of a coating stack of antimony- doped tin oxide with a reduced thickness to 1800 angstroms with a over coat of titanium dioxide.
- the latter is a quarter wave optical thickness at 1000 nm.
- the other conditions are the same as those for Figure 15.
- Figure 20 shows the theoretical light transmission for two curves.
- Curve A is for a five layer coating with a configuration of SHLHLH where H is Ti0 and L is silica.
- B is for a coating stack of the same configuration where fluorine doped tin oxide is L.
- the other conditions are the same as those for Figure 15.
- the transmission of light through a transparent substrate can be modified by the application of inorganic coatings.
- the inorganic coatings can absorb light and, through thin film physics, can reject light by reflection as well as absorption.
- thin film means a film thickness of 1 micron or less .
- the automotive and architectural markets often require different levels of light transmission depending on the wavelength of light. For instance, it is important in an automobile to have a relatively high transmission of visible light so that the driver can see out of the vehicle, but simultaneously reject the solar radiation that is not in the visible spectrum.
- the substrate would act as a band pass filter, ideally transmitting all visible light equally, but fully rejecting the UV and NIR parts of the solar spectrum. The occupant would feel more comfortable in a vehicle with this glass and the vehicle would have better fuel efficiency because it could use a smaller air conditioner.
- a solar control glass is one that reflects or absorbs rather than transmitting a portion of the liqht spectrum, for instance reflecting and/or absorbing some portion of the ultraviolet light spectrum and/or infrared light spectrum and/or visible light spectrum thereby decreasing the transmission of that particular portion of the light spectrum.
- tinted products are solar control glasses where the amount of total iron in the finished product generally can be within the range of around 0.5 to around 2 by weight %. Usually at least 20%, preferably in the range 30 to 45% by weight of this total iron content of the finished glass is comprised of ferrous iron.
- solar control glasses include those which reduce direct solar heat transmittance (DSHT) and/or reduce ultraviolet radiation transmittance while permitting some degree of desirable visible light transmittance.
- DSHT direct solar heat transmittance
- solar control glasses can be privacy glazings.
- the solar control glasses can reduce problems associated with excessive heating on sunny days while permitting a desirable amount of visible light to pass. Also it is possible that these glasses can maintain a private setting with regards to the interior of the vehicle.
- the glass used as the substrate of the present invention is one that has some degree of visible transmittance or the glass has at least some degree of transparency so that one can see through the glass to discern an object on the other side. This transparency is less with the privacy glazings of the glass.
- Three types of solar control glass have gained in popularity, due as much for solar performance as from aesthetic concerns. They are SOLARGREEN® glass and SOLEXTRA® glass, which are green and blue, respectively.
- SOLARGREEN glass substrate is a, solar control glass available from PPG Industries, Inc. having an LTA level of 71%, a TSET of 42.9%, and a performance ratio of 1.65.
- Solargreen ® and Solextra ® glass have focused on minimizing total, solar energy transmitted (TSET) , rather than targeting a specific part of the spectrum such as UV light.
- TSET total, solar energy transmitted
- Recently, the automotive market in Japan has started to shift toward a glazing requirement that has a UV light transmission less than 10% while maintaining the TSET level comparable to Solargreen ® glass.
- a commercial version of this glass is known as
- the low UV light transmission is due to high levels of an expensive additive, Ce0 2 .
- the application of a coating in accordance with the present invention can attain the UV transmission target and has the possibility of adding features while simultaneously giving a cost advantage compared to the uncoated substrate, which can be essentially free of Ce0 .
- the various thin film coatings with a degree of transparency of the present invention will reduce the transmission of UV light while optionally imparting additional properties such as anti-reflection, lower TSET, and/or self cleaning attributes and different reflected or transmitted colors.
- the combination of the various coatings provides several properties together in one coated glass product which can give a cost as well as a performance advantage.
- the thin film structures described below have one to five layers made up of several preferably one to four materials. The materials are selected for different characteristics. In order to capitalize on the physics of thin films, materials with different refractive indices (RI) are used. In addition, the materials should be physically and chemically durable and, if possible, contribute other properties such as absorption of light in different parts of the solar spectrum.
- a high .refractive index is merely one that is higher than a low refractive index and vice versa for a low refractive index.
- a high refractive index is greater than 1.9 and a low refractive index is less than 1.6 and a medium refractive index is between 1.6 and 1.9.
- the dividing lines for these ranges is not a stark line and the RI at the extremes of adjoining ranges may cross over between the adjacent regions to a .degree .
- Non-exclusive examples of suitable materials for the high and low refractive index coatings layers include various metal oxides, nitrides, and their alloys and mixtures.
- the doped oxides have a very low refractive index in the near infrared region due to the free electrons in the material.
- the fluorine and/or indium doped tin oxides has a higher refractive index than that of antimony doped tin oxide.
- Nonexclusive examples of the materials for the low index coating layers may include silicon dioxide, Si02 (about 1.45), A1203 (about 1.65), B203 (about 1.60), silicone polymer, magnesium oxide, and cryolite.
- the preferred coatings discussed below are made up of four different coatings.
- the first layer can be titania or
- Ti0 2 This material has a very high refractive index, absorbs UV light, is chemically inert and durable and, when deposited in the antatase form, is photocatalytic.
- the second material is silica or Si0 2 . This material is also chemically inert and durable and it has a very low refractive index.
- the first is fluorine-doped tin oxide.
- This material is electrically conductive and has a high refractive index in the UV and visible part of the spectrum and a low refractive index in the NIR part of the spectrum. This property allows unique features to be designed into various coatings.
- the fourth material is antimony-doped tin oxide. This material absorbs light across the entire solar spectrum and more importantly, control of the relative absorption at different wavelengths is achieved by altering the deposition process. It is possible to tune the coating to absorb relatively more visible light or UV light or NIR light. A very unique property of this material is that it can have a very high absorption of green light. By placing this coating on a green glass we can change it to a gray glass, thus creating a high performance solar control glass with neutral aesthetics .
- All of these basic coatings can generally be applied in a manner similar to the electroconductive coatings on windshields as described in U.S. Patent 4,610,771 hereby incorporated by reference. This on-line effort can utilize similar equipment to produce these novel coatings on a solar control glass substrate. Any other known method in the art for deposition of any of these coating layers can be utilized, for instance by sputtering under vacuum at a radio-frequency can be employed. Also other techniques can be used such as cathodic sputtering, particularly by CVD plasma from an appropriate siliceous precursor or by a gas phase pyrolysis under ambient pressure.
- the UV blocking coating is the simplest of the solar control coatings discussed herein, and the physics behind it is common to many of the other designs. .
- the interaction of light with any substrate, coated or not, must conform to the following formula.
- the percentage of light absorbed (A) plus the percentage of light reflected (R) plus the percentage of light transmitted (T) must add up to 100 percent. If more light is reflected by a coating then less will be absorbed and/or transmitted.
- the function of the UV reflection coating is to reflect as much UV light as needed to meet a transmission target of less than 10% for the coated glass article. Some UV light will be absorbed by the coating and glass substrate, but most of the transmission loss is due to a high reflection attained through appropriate selection of layer materials and thicknesses. More or less layers may be needed depending on the UV absorption properties of the substrate. Specific examples will be discussed below.
- the maximum reflection attained by a single high index layer on a substrate is easily calculated and this type of layer is known as a quarter wave layer.
- the thickness of the quarter wave layer is calculated with the following formula: O 00/27771 - 14 -
- h is the thickness of the layer
- lambda is the wavelength that maximum reflection occurs (design wavelength)
- ni is the refractive index of the coating at the design wavelength
- the layer is designated with an "H” and if the refractive index is low it is designated with a "L” and medium or in-between an “M” .
- a coating stack can be easily abbreviated with this terminology. For instance, an anti-reflection coating with a quarter wave of a medium index material next to the glass and a half wave (two quarter waves) of a high index material next and a quarter wave of a low index material on top would be designated as SMHHL, where S indicates the substrate. It should be noted that each layer is a quarter wave only at the ' wavelength for maximum reflectivity in the desired portion of the light spectrum. The intensity of the reflection is calculated using equation 3.
- R is the reflectance
- n s is the refractive index of the substrate and n 0 is the refractive index of the incident medium and ⁇ i is the refractive index of the coating.
- the incident medium in the environment in which the substrate exists, i.e., air or otherwise for laminate structures.
- the quarter wave thickness of the titania layer would be 372A and the reflectance would be 26.5%. This reflectance is from the coated surface only. Absorption in the coating is neglected for the next several examples but absorption will be noted when included.
- the reflectance over the visible spectrum is shown in Figure 1 at Curve A. One can see from Curve A of Figure 1 that the maximum reflectance occurs at the design wavelength, 380 nm, and that the reflectance is decreased at all other wavelengths across the solar spectrum.
- Equation 5 Equation 5
- Equation 6 is equivalent to equation 4 above.
- a three layer SHLH coating of titania, H, and silica, L, on float glass would have an equivalent refractive index of:
- Table 1 summarizes the performance for some illustrative examples and predictive examples of a one, three and five layer coating on clear, and solar control glasses of SOLEX ® and
- UV REFLECTION WITH ANTI-REFLECTION A feature of the simple SHLH configuration described above is the relatively high visible reflectance.
- the high reflectance can limit the utility of this approach when applied to solar control glasses with uncoated visible transmission near the 65 to 70 percent range.
- the high reflectance will reduce the visible transmission below the 70% limit, for instance, when applied to SOLARGREEN glass for a windshield application.
- a half wave layer at the design wavelength is an absentee layer since it is optically invisible at the design wavelength. Therefore, at the design wavelength the substrate and coating stack of SHLHLL behaves the same as the stack SHLH and there is no alteration of the UV rejection performance.
- the top half wave of silica LL is a quarterwave in the visible spectrum. This layer then acts a visible spectrum reflectance reducing layer.
- the design wavelength and/or layer thicknesses can then be optimized for the desired UV reflectance and visible light transmission requirements.
- the SHLH and SHLHLL coatings are shown in Figure 2. These coatings have a design wavelength of
- Curve B is the stack SHLHLL and curve A is the stack SHLH.
- the reflectance of both coatings remains the same at the design wavelength (330nm) and the reflectance curve is substantially modified throughout the rest of the spectrum.
- the halfwave of silica since it acts as an anti-reflective ("AR") layer, maintains, or increases, the visible light transmission, thereby improving the utility of this UV rejection coating for more substrates. If the transmission of light through the coated substrate is increased, then the substrate could be modified to absorb more solar radiation while simultaneously maintaining its visible light transmission requirements.
- the glass composition of the solar control glass can be modified to reduce the TSET to about 40% and the visible transmission increases from an average performing AR coating.
- the examples listed above were made using optical constants for coatings without absorption coefficients to easily demonstrate the effects of interference coatings on the optical properties of glasses.
- coatings absorb some light and therefore have non-zero absorption coefficients.
- coatings that have different optical constants to demonstrate the effect of absorption on the transmission spectrum of the coatings.
- Figure 3 shows the transmission curves for a SLHL stack with and without absorption in the Ti02 layer. There is no absorption in the Si02 layer. Curve B is without absorption and curve A is with absorption.
- the previous two embodiments were directed to a three layer coating that reflected light in both the UV and NIR parts of the spectrum. Earlier it was indicated that the intensity of the reflected light is a function of the number of alternating high and low refractive index layers. More layers means higher reflectance. But as more layers are added to a dual reflectance coating the overall thickness becomes a problem. The cost increases and more coaters are needed to produce the coating in a float line environment.
- the intensity of the UV reflectance can be increased without increasing the total thickness of the stack or sacrificing the intensity of the NIR reflectance. This is accomplished by substituting part of the middle third of the inner silica layer with fluorine-doped tin oxide. Put another way the middle layer becomes a combination of several layers.
- the fluorine-doped Sn02 like most transparent conducting oxides, has the unique property of having a high refractive index in the UV and visible spectrum but has a low refractive index in the NIR.
- the coating then in the UV is S3HLHL3H and in the NIR is SHLH.
- the coating is effectively a five layer coating in the UV and visible but reduces to a three layer coating in the NIR.
- TCO TRANSPARENT CONDUCTING OXIDES
- Transparent conducting oxides can be used in HLH stacks to increase the reflectivity of light in the near IR with a high refractive index material as shown above because they have a low refractive index in the NIR region believed to result from the free electrons and their mobility in the crystal lattice. They therefore have utility beyond the example cited above for a combination UV/NIR blocking design.
- Curve A of Figure 7 shows the NIR reflectance peak resulting from a SHLH stack where Ti02 is the high index layer and fluorine-doped tin oxide is the low index layer.
- the coating stack will reflect about 58% at the design wavelength of 1 micron.
- the refractive indices in the visible region are different also " and this results in interference peaks and reflected color.
- This trait is considered objectionable and a means to maintain the reflectance peak while minimizing the reflected can be attained by either of two methods i.e., coatings above or below the stack.
- the key is to add layers that will alter the visible light reflection properties without significantly attenuating the NIR peak.
- One way to do this is to add a coating that is optically active in the visible region and optically inactive in the NIR region.
- a conductive transparent oxide (“TCD”) is good for this purpose.
- the refractive index of a TCO is low in the NIR and moderate in the visible spectrum, relative to Ti02.
- SMHMH the refractive index of a TCO
- the designation SMHMH for this coating is not used because the layers are not quarter wave optical thickness in the visible region.
- the L/3 layer is optically inactive as shown in Figure 7 at curve B where the plot of this stack is compared to the stack of curve A. Curve A is the normal line and curve B is the bold line for the L/3 containing stack.
- This stack would have a TSET of about 57% and a visible transmission of about 76%.
- This coating would also have a low emissivity due to long wavelength reflection of light by the transparent conducting oxide.
- the reflectance peak can be increased as mentioned previously by additional LH pairs of layers.
- graded index layer beneath the coating stack.
- This layer generally has an increasing (or decreasing) refractive index with increasing film thickness through the film layer.
- This type of color suppression is well known for suppressing the color of a single coating (see U.S. Patents 5,356,718; 5,599,387, hereby incorporated by reference) .
- This type of color suppression has not been examined for use in suppressing the color of a stack of coatings and more importantly, its effect on the NIR reflection from such a stack has been unexamined.
- the graded index coating can both suppress color and in some cases improve performance in a HLH stack.
- the gradient layer used in these examples is modeled as a ten layer coating, which I will designate with a G, with each layer being lOnm thick and whose indices vary from 1.55 the glass interface to 2.0 at the top of the graded layer.
- the reflectance curve again compared to the SHLH stack of curve A of Figure 7, is shown in Figure 9. Our stack is now SGHLH. For curve B with the graded layer the peak reflectance is only slightly reduced and shifted in wavelength and the visible reflectance is substantially dampened.
- the reflectance peak can now be further increased because the gradient layer creates a higher interface than that of the glass and the addition of another fluorine-doped tin oxide layer median the graded index layer and the first high index layer will now be optically active and will result in a increase in the reflectance peak.
- the stack is SGLHLH. The color is still dampened but the performance is increased. This stack would be very good when lower emissivity is needed.
- the reflectance spectrum, compared to curve A from Figure 7, is shown below in Figure 10.
- the fluorine-doped tin oxide coatings also absorb some NIR light and are therefore, ideally suited for solar control applications. They contribute to reductions in NIR light transmission through both reflection and absorption. Also, unexpectedly, a pair of high/low index layers much less than a quarter wave optical thickness can be used to dampen the reflected color. They also do not effect the NIR reflection substantially.
- Adding a layer above the stack will result in a reduction of reflection as described above and this method is suitable here also.
- the stack would have a moderate refractive index, high, moderate, high and then low (MHMHL) .
- MHMHL moderate refractive index
- the resultant coating stack compared to curve A from Figure 7 is shown in Figure 11.
- the visible intensity is substantially dampened and the color is neutral. There is some shift in the intensity of the reflectance peak, but this can be corrected for by adjusting the thicknesses of the HLH layers.
- Combinations of Si02 and a TCO can be used in combination for the low index layer as described above for the dual NIR/UV rejection coating.
- a stack having, the substrate, Ti02, Si02, Fluorine-doped tin oxide, Si02, Fluorine-doped tin oxide, and Ti02 with the Si02 and Fluorine-doped tin oxide (SHLMLMH) having a combined optical thickness in the NIR of a quarter wavelength is shown in Figure 12 along with the curve A from Figure 7 for comparison.
- the reflectance peak is enhanced with this multi-layer low index quarter wave approach. Also note that the visible reflectance peaks are attenuated somewhat.
- the new ability to attenuate the visible reflectance spectrum with this multi-layer approach for a low index layer can be used regarding the visible reflectance spectrum for reduced reflected color while maintaining the ' NIR reflectance peak.
- a stack having a substrate, Ti02, Si02, Sn02:F and Ti02 will have no reflected color and an enhanced reflection peak as shown in Figure 13. Again the reflectance curve A from Figure 7 is included for comparison.
- the inclusion of layers that are optically active in the visible and combine to be of low index in the NIR spectrum can be used to attain any desired visible optical effect desired by the designer and is not limited simply to color suppression .
- antimony to tin oxide in doping levels will impart electrical conductivity. As the amount of antimony increases, the electrical conductivity degrades and the coating starts to significantly absorb solar radiation.
- Figure 14 shows the solar absorption of several antimony-doped tin oxide coatings.
- the chemical vapor deposition (“CVD") process parameters that produced these coatings are listed in Table 3.
- CVD chemical vapor deposition
- other known deposition processes can be used such as pyrolytic coating techniques and sputter coating techniques like MSVD magnetron sputtered vacuum deposition.
- the spray coating was made as a 5 weight percent mixture. 00/27771 25 -
- the mixture was of antimony trichloride in monobutyl- tintrichloride (MBTC) and the mixture was hand sprayed onto a clear glass substrate heated to about 1150 degrees F.
- the antimony was fed into the CVD experiments 1 to 11 at a constant 20 weight % relative to the MBTC.
- the coater had a central inlet slot with upstream and downstream exhaust slots. The width of the coating zone was four inches and the contact length between exhausts was five inches. Air was used as the carrier gas .
- coatings 4 and 8 absorb more NIR light than visible light, making the coatings good for solar control when high visible light transmission is needed.
- Coatings 2 and 6 have peak absorption at about 550nm. These coatings are well suited for muting the green color of Solex ® glass and
- Coating 10 absorbs more visible light than NIR light
- coating 1 absorbs a relatively constant amount across the solar spectrum
- coatings 9 and 11 absorb appreciable UV light.
- a significant issue for coatings that will be glazed in the annealed and tempered states is color fastness, or color that does not change when the coated glass is heated.
- the appearance and performance is preferably the same before and after heat treating.
- the antimony doped tin oxide coatings studied for this project may or may not change upon heating, depending on deposition parameters.
- the properties of various samples and how certain properties change with heat treating are listed in table 4. The sample numbers with an H after them indicate the samples after heat treating. Table 4 (Part A)
- the NIR reflectors shown above are to help control the solar light transmittance through a window.
- the amount of solar light rejection is a function of many layers with a large total thickness. Many layers are needed to further reduce the transmission of light through the glass.
- the application of a coating that selectively or preferentially absorbs NIR solar light as opposed to visible light would be helpful in making a good solar control stack.
- a single layer of antimony doped tin oxide, with the optical properties listed above, that is 800 angstroms thick will have about a 69% visible transmission and a 58% TSET.
- the transmission curve is compared to curve A from Figure 7 above and is shown in Figure 15.
- the coating does not have as high a transmittance in the visible but the TSET is comparable.
- the addition of an antimony layer to the stack is a good one.
- the antimony doped tin oxide layer can be combined with a fluorine doped tin oxide or other TCO to get both low emissivity and transmission reduction.
- Figure 16 shows the theoretical light transmission from a graded layer, antimony-doped tin oxide and fluorine- doped tin oxide coating.
- the TSET drops to 51% and the visible light transmission stays at about 69%.
- the TSET and visible light transmission can be altered with this design by varying the thickness of the antimony-doped tin oxide layer or by changing the antimony concentration in the coating.
- This coating has a visible light transmission of about 52% and a TSET of about 37%.
- the fluorine-doped tin oxide coating as the top layer will give this coating an emissivity less than about 0.35.
- the graded layer thickness is 800 angstroms
- the antimony-doped tin oxide is 1800 angstroms
- the fluorine-doped tin oxide is 1800 angstroms.
- the TSET of this coating can be further reduced by the application of a quarter wave high index layer such as Ti02 onto the top of the graded, antimony-doped tin oxide, fluorine-doped tin oxide discussed above.
- the TSET drops to 32.5% but the visible transmission only drops to 51%.
- the transmission curve of these stacks, with and without the Ti02 layer are shown in Figure 17 as curves B and A respectively below.
- the fluorine-doped tin oxide, or other suitable transparent conducting oxide can be removed leaving the graded layer, antimony-doped tin oxide and Ti02.
- the transmission curve for this coating is compared to the coating with fluorine-doped tin oxide in Figure 18.
- a antimony-doped tin oxide coating, 2100 angstroms thick, on clear glass will have a visible transmission of 49% and a TSET of about 37%.
- the antimony-doped tin oxide thickness can be decreased to 1800 angstroms with the addition of a Ti02 layer that is a quarter wave optical thickness at lOOOnm.
- the TSET remains the same but the visible light transmission increased to 54%.
- the two curves are shown in Figure 19, The bold curve is the antimony-doped tin oxide with the Ti02 layer.
- the position of the Ti02 or high index layer, relative to a graded color suppression layer and antimony-doped tin oxide and fluorine-doped tin oxide layer was studied.
- the graded index layer was first on the glass in all cases.
- the stack configuration is abbreviated as follows: S-substrate, G-graded index color suppression layer 800 angstroms thick, Sn-fluorine doped tin oxide 1600 angstroms thick, Ti - Ti02 layer 1100 angstroms thick and Sb-antimony-doped tin oxide layer 1800 angstroms thick.
- the results are shown in Table 6.
- the addition of the Ti02 or high index layer improves the TSET in all cases. TABLE 6
- Curve A is a five layer coating of the configuration SHLHLH with Ti02 as the high index layer and silica as the low index layer.
- Curve B is the same configuration but with F:Sn02 as the low index layer.
- the design that contains Si02 is a total of around 6747 preferably 6747 angstroms thick, has a TSET of around but preferably 60% and a visible light transmission of around but preferably 85%.
- the design with fluorine-doped tin oxide has a total thickness of around but preferably 6461 angstroms, has a TSET of around but preferably 50% and a visible light transmission of around but preferably 71.1 percent.
- TSET of around but preferably 50%
- visible light transmission of around but preferably 71.1 percent.
- the first case is a coating to mask the green color of Solex ® glass or Solargreen ® glass and turn the glass gray.
- a thin layer of an antimony-doped tin oxide containing coating is applied to the glass or coated glass.
- the transmitted color will shift from green to gray and if the coating is increased enough the transmitted color will shift to magenta. Based on the heat treated coatings, the transmitted and reflected color will shift to a degree.
- Anti-reflection (AR) coatings will reduce the reflectance from 18% for Solargreen ® glass to about 12-13% at an installation angle of about 65°. These traditional AR coatings do not impart any additional solar control properties but the increases in visible transmission due to the AR properties can be used to darken the substrate and lower the TSET.
- An alternate approach to AR can be used to further reduce the TSET while imparting comparable AR performance to the traditional designs. This alternate approach does not require the modifications of the substrate composition to attain the lower TSET.
- the UV/NIR coating with a top quarter wave of silica described above is used as the basis for this application (SHLHL/2 tuned for NIR) . As the installation angle is increased the optical thickness of the coating decreases. The physical thickness of the layers can be increased to compensate for this effect. The reflectance is reduced to 13% and the TSET is calculated to be about 37%.
- these solar control coatings provide a unique opportunity to further reduce the TSET of a windshield. If an AR coating is not necessary, the solar reflection can be placed between the lites of the windshield. Conceivably two coatings, one on each lite, tuned to reflect different wavelengths, could reduce the TSET below 37% all while maintaining the target visible light transmission.
- the AR coating could also be applied to the inner lite of the Sungate ® windshield as disclosed in U.S. Patent.
- the NIR reflector properties of this coating could further improve the properties of this product while imparting anti-reflection properties as well.
- Titania When titania is deposited in the anatase phase and exposed to UV light it becomes self-cleaning. Titania can be used as the high index layers in such designs. This will impart self-cleaning properties to the designs as well as the advanced solar control properties. These self cleaning coatings can be applied as disclosed in Patent Cooperation
- NIR WITH COLORED COATINGS Transition metal oxides can be used to alter the reflected and transmitted color of glass for automotive use.
- the coatings provide a broad palette of colors, but the TSET of the coated glass can be improved. This is accomplished by combining transition metal oxides with the designs described above to attain both solar control with the broad palette of colors .
- the transition metal oxides have a high refractive index can be used as the high index layer in these designs. If the color is too intense using exclusively the transition metal oxides, then the transition metal oxides can be used as only one high index layer, or even as part of a high index layer. Alternately, the colored transition metal oxide can be combined with a non-colored oxide to mute the color of the coating. Using either of these techniques, one can attain both solar control with a variety of colors. One could even have different colored materials for the various high index layers, giving the designer even more choices for controlling the color of the coated glass.
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AU16128/00A AU758267B2 (en) | 1998-11-09 | 1999-11-08 | Solar control coatings and coated articles |
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NZ511302A NZ511302A (en) | 1998-11-09 | 1999-11-08 | Solar control coatings and coated articles |
CA002348597A CA2348597A1 (en) | 1998-11-09 | 1999-11-08 | Solar control coatings and coated articles |
EP99958844A EP1137608A1 (en) | 1998-11-09 | 1999-11-08 | Solar control coatings and coated articles |
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- 1999-11-08 JP JP2000580955A patent/JP2002529356A/en active Pending
- 1999-11-08 NZ NZ511302A patent/NZ511302A/en unknown
- 1999-11-08 WO PCT/US1999/026406 patent/WO2000027771A1/en active IP Right Grant
- 1999-11-08 KR KR1020017005809A patent/KR100700800B1/en not_active IP Right Cessation
- 1999-11-08 EP EP99958844A patent/EP1137608A1/en not_active Withdrawn
- 1999-11-08 CA CA002348597A patent/CA2348597A1/en not_active Abandoned
- 1999-11-08 AU AU16128/00A patent/AU758267B2/en not_active Ceased
- 1999-11-08 CN CNB998141984A patent/CN1160273C/en not_active Expired - Fee Related
- 1999-11-08 CZ CZ20011442A patent/CZ20011442A3/en unknown
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Also Published As
Publication number | Publication date |
---|---|
JP2002529356A (en) | 2002-09-10 |
EP1137608A1 (en) | 2001-10-04 |
CN1329579A (en) | 2002-01-02 |
CN1160273C (en) | 2004-08-04 |
KR20010080401A (en) | 2001-08-22 |
AU758267B2 (en) | 2003-03-20 |
AU1612800A (en) | 2000-05-29 |
CA2348597A1 (en) | 2000-05-18 |
CZ20011442A3 (en) | 2001-12-12 |
KR100700800B1 (en) | 2007-03-27 |
NZ511302A (en) | 2004-01-30 |
WO2000027771A9 (en) | 2000-11-09 |
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