WO1995008596A1 - Flat, dark pigmented radiation curable coating compositions - Google Patents
Flat, dark pigmented radiation curable coating compositions Download PDFInfo
- Publication number
- WO1995008596A1 WO1995008596A1 PCT/US1994/007206 US9407206W WO9508596A1 WO 1995008596 A1 WO1995008596 A1 WO 1995008596A1 US 9407206 W US9407206 W US 9407206W WO 9508596 A1 WO9508596 A1 WO 9508596A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- composition
- radiation
- coating
- photoinitiator
- pigment
- Prior art date
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- 230000005855 radiation Effects 0.000 title claims abstract description 37
- 239000008199 coating composition Substances 0.000 title claims description 35
- 238000000576 coating method Methods 0.000 claims abstract description 48
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- 238000000034 method Methods 0.000 claims description 17
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- XCJYREBRNVKWGJ-UHFFFAOYSA-N copper(II) phthalocyanine Chemical compound [Cu+2].C12=CC=CC=C2C(N=C2[N-]C(C3=CC=CC=C32)=N2)=NC1=NC([C]1C=CC=CC1=1)=NC=1N=C1[C]3C=CC=CC3=C2[N-]1 XCJYREBRNVKWGJ-UHFFFAOYSA-N 0.000 description 1
- 238000007766 curtain coating Methods 0.000 description 1
- 125000000753 cycloalkyl group Chemical group 0.000 description 1
- FOTKYAAJKYLFFN-UHFFFAOYSA-N decane-1,10-diol Chemical compound OCCCCCCCCCCO FOTKYAAJKYLFFN-UHFFFAOYSA-N 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 229960002380 dibutyl phthalate Drugs 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 239000000975 dye Substances 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 230000005670 electromagnetic radiation Effects 0.000 description 1
- UNXHWFMMPAWVPI-ZXZARUISSA-N erythritol Chemical compound OC[C@H](O)[C@H](O)CO UNXHWFMMPAWVPI-ZXZARUISSA-N 0.000 description 1
- 229940009714 erythritol Drugs 0.000 description 1
- 235000019414 erythritol Nutrition 0.000 description 1
- TVFJAZCVMOXQRK-UHFFFAOYSA-N ethenyl 7,7-dimethyloctanoate Chemical compound CC(C)(C)CCCCCC(=O)OC=C TVFJAZCVMOXQRK-UHFFFAOYSA-N 0.000 description 1
- 125000001301 ethoxy group Chemical group [H]C([H])([H])C([H])([H])O* 0.000 description 1
- SUPCQIBBMFXVTL-UHFFFAOYSA-N ethyl 2-methylprop-2-enoate Chemical compound CCOC(=O)C(C)=C SUPCQIBBMFXVTL-UHFFFAOYSA-N 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N ferric oxide Chemical compound O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 230000009969 flowable effect Effects 0.000 description 1
- 239000005350 fused silica glass Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- SXCBDZAEHILGLM-UHFFFAOYSA-N heptane-1,7-diol Chemical compound OCCCCCCCO SXCBDZAEHILGLM-UHFFFAOYSA-N 0.000 description 1
- XXMIOPMDWAUFGU-UHFFFAOYSA-N hexane-1,6-diol Chemical compound OCCCCCCO XXMIOPMDWAUFGU-UHFFFAOYSA-N 0.000 description 1
- LNCPIMCVTKXXOY-UHFFFAOYSA-N hexyl 2-methylprop-2-enoate Chemical compound CCCCCCOC(=O)C(C)=C LNCPIMCVTKXXOY-UHFFFAOYSA-N 0.000 description 1
- LNMQRPPRQDGUDR-UHFFFAOYSA-N hexyl prop-2-enoate Chemical compound CCCCCCOC(=O)C=C LNMQRPPRQDGUDR-UHFFFAOYSA-N 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 235000019239 indanthrene blue RS Nutrition 0.000 description 1
- UHOKSCJSTAHBSO-UHFFFAOYSA-N indanthrone blue Chemical compound C1=CC=C2C(=O)C3=CC=C4NC5=C6C(=O)C7=CC=CC=C7C(=O)C6=CC=C5NC4=C3C(=O)C2=C1 UHOKSCJSTAHBSO-UHFFFAOYSA-N 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 235000013980 iron oxide Nutrition 0.000 description 1
- VBMVTYDPPZVILR-UHFFFAOYSA-N iron(2+);oxygen(2-) Chemical class [O-2].[Fe+2] VBMVTYDPPZVILR-UHFFFAOYSA-N 0.000 description 1
- 229940035429 isobutyl alcohol Drugs 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- HCWCAKKEBCNQJP-UHFFFAOYSA-N magnesium orthosilicate Chemical compound [Mg+2].[Mg+2].[O-][Si]([O-])([O-])[O-] HCWCAKKEBCNQJP-UHFFFAOYSA-N 0.000 description 1
- 239000000391 magnesium silicate Substances 0.000 description 1
- 229910052919 magnesium silicate Inorganic materials 0.000 description 1
- 235000019792 magnesium silicate Nutrition 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 125000000956 methoxy group Chemical group [H]C([H])([H])O* 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- SLCVBVWXLSEKPL-UHFFFAOYSA-N neopentyl glycol Chemical compound OCC(C)(C)CO SLCVBVWXLSEKPL-UHFFFAOYSA-N 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- IQOFOAJECLOAGR-UHFFFAOYSA-N nonane-4,5-diol Chemical compound CCCCC(O)C(O)CCC IQOFOAJECLOAGR-UHFFFAOYSA-N 0.000 description 1
- OEIJHBUUFURJLI-UHFFFAOYSA-N octane-1,8-diol Chemical compound OCCCCCCCCO OEIJHBUUFURJLI-UHFFFAOYSA-N 0.000 description 1
- NZIDBRBFGPQCRY-UHFFFAOYSA-N octyl 2-methylprop-2-enoate Chemical compound CCCCCCCCOC(=O)C(C)=C NZIDBRBFGPQCRY-UHFFFAOYSA-N 0.000 description 1
- 229940065472 octyl acrylate Drugs 0.000 description 1
- ANISOHQJBAQUQP-UHFFFAOYSA-N octyl prop-2-enoate Chemical compound CCCCCCCCOC(=O)C=C ANISOHQJBAQUQP-UHFFFAOYSA-N 0.000 description 1
- NDLPOXTZKUMGOV-UHFFFAOYSA-N oxo(oxoferriooxy)iron hydrate Chemical compound O.O=[Fe]O[Fe]=O NDLPOXTZKUMGOV-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
- 239000000123 paper Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- WXZMFSXDPGVJKK-UHFFFAOYSA-N pentaerythritol Chemical compound OCC(CO)(CO)CO WXZMFSXDPGVJKK-UHFFFAOYSA-N 0.000 description 1
- 229920001568 phenolic resin Polymers 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- FCJSHPDYVMKCHI-UHFFFAOYSA-N phenyl benzoate Chemical compound C=1C=CC=CC=1C(=O)OC1=CC=CC=C1 FCJSHPDYVMKCHI-UHFFFAOYSA-N 0.000 description 1
- 235000021317 phosphate Nutrition 0.000 description 1
- 150000003013 phosphoric acid derivatives Chemical class 0.000 description 1
- IEQIEDJGQAUEQZ-UHFFFAOYSA-N phthalocyanine Chemical compound N1C(N=C2C3=CC=CC=C3C(N=C3C4=CC=CC=C4C(=N4)N3)=N2)=C(C=CC=C2)C2=C1N=C1C2=CC=CC=C2C4=N1 IEQIEDJGQAUEQZ-UHFFFAOYSA-N 0.000 description 1
- 229920001279 poly(ester amides) Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920000570 polyether Polymers 0.000 description 1
- 229920000166 polytrimethylene carbonate Polymers 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- KCTAWXVAICEBSD-UHFFFAOYSA-N prop-2-enoyloxy prop-2-eneperoxoate Chemical class C=CC(=O)OOOC(=O)C=C KCTAWXVAICEBSD-UHFFFAOYSA-N 0.000 description 1
- PNXMTCDJUBJHQJ-UHFFFAOYSA-N propyl prop-2-enoate Chemical compound CCCOC(=O)C=C PNXMTCDJUBJHQJ-UHFFFAOYSA-N 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 238000000518 rheometry Methods 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 238000010561 standard procedure Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- YLQBMQCUIZJEEH-UHFFFAOYSA-N tetrahydrofuran Natural products C=1C=COC=1 YLQBMQCUIZJEEH-UHFFFAOYSA-N 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- ZIBGPFATKBEMQZ-UHFFFAOYSA-N triethylene glycol Chemical compound OCCOCCOCCO ZIBGPFATKBEMQZ-UHFFFAOYSA-N 0.000 description 1
- QXJQHYBHAIHNGG-UHFFFAOYSA-N trimethylolethane Chemical compound OCC(C)(CO)CO QXJQHYBHAIHNGG-UHFFFAOYSA-N 0.000 description 1
- WDRCVXGINNJWPH-UHFFFAOYSA-N tris(6-methylheptyl) benzene-1,2,4-tricarboxylate Chemical compound CC(C)CCCCCOC(=O)C1=CC=C(C(=O)OCCCCCC(C)C)C(C(=O)OCCCCCC(C)C)=C1 WDRCVXGINNJWPH-UHFFFAOYSA-N 0.000 description 1
- 235000013799 ultramarine blue Nutrition 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
- 229910052984 zinc sulfide Inorganic materials 0.000 description 1
- DRDVZXDWVBGGMH-UHFFFAOYSA-N zinc;sulfide Chemical compound [S-2].[Zn+2] DRDVZXDWVBGGMH-UHFFFAOYSA-N 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D5/00—Coating compositions, e.g. paints, varnishes or lacquers, characterised by their physical nature or the effects produced; Filling pastes
- C09D5/28—Coating compositions, e.g. paints, varnishes or lacquers, characterised by their physical nature or the effects produced; Filling pastes for wrinkle, crackle, orange-peel, or similar decorative effects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/06—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation
- B05D3/061—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation using U.V.
- B05D3/065—After-treatment
- B05D3/067—Curing or cross-linking the coating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/06—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation
- B05D3/068—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to radiation using ionising radiations (gamma, X, electrons)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D5/00—Processes for applying liquids or other fluent materials to surfaces to obtain special surface effects, finishes or structures
- B05D5/06—Processes for applying liquids or other fluent materials to surfaces to obtain special surface effects, finishes or structures to obtain multicolour or other optical effects
- B05D5/061—Special surface effect
- B05D5/062—Wrinkled, cracked or ancient-looking effect
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D4/00—Coating compositions, e.g. paints, varnishes or lacquers, based on organic non-macromolecular compounds having at least one polymerisable carbon-to-carbon unsaturated bond ; Coating compositions, based on monomers of macromolecular compounds of groups C09D183/00 - C09D183/16
- C09D4/06—Organic non-macromolecular compounds having at least one polymerisable carbon-to-carbon unsaturated bond in combination with a macromolecular compound other than an unsaturated polymer of groups C09D159/00 - C09D187/00
Definitions
- Another method heretofore employed to produce low gloss films from radiation curable compositions utilized a two step curing process wherein polymerization of certain coating compositions was inhibited in surface portions in the first step by the presence of oxygen (air) , and curing of the coating was completed in the second step in an inert atmosphere. Shrinkage of underlying layers during the first step caused pigment particles to be driven into the surface portions, whereby the surface contained a larger amount of pigment than the body of the film which reduced the gloss of the film without sacrificing film strength or rheology properties of the coating composition.
- U.S. Patent Nos. 3,918,393 (Hahn) and 4,048,036 (Prucnal) illustrate this approach.
- a drawback to the approach of concentrating flatting pigments at the surface of the film is that the surface is subject to physical damage that causes unattractive marking of the surface.
- One potential form of damage to which these types of low gloss coatings are susceptible is metal marking, whereby contact of certain metals with the surface causes dark markings. It would be desirable to avoid these problems with radiation curable, low gloss coatings as well as to be able to produce coatings of even lower gloss than prior art methods.
- Multi-step radiation curing techniques have also been proposed for producing textured finishes. These techniques are disclosed in U.S. Patent Nos. 4,421,784 (Troue) , 3,840,448 (Osborne et al. ) , and 4,411,931 (Duong). The methods of these patents do not appear to be intended to produce the type of flat, low gloss finishes that are the subject of this invention, but are directed to the production of relatively gross, visibly perceivable, surface wrinkle patterns. These patented methods do not involve the use of electron beam radiation. Prior art techniques for producing low gloss or textured radiation cured coatings, including the patents set forth above, have generally been limited to non-pigmented coatings.
- the low gloss or textured coating is a clear coating that is applied over a pigmented base coat. This has generally been considered necessary in order to assure adequate penetration of radiation during the curing step. It would be highly desirable to produce low gloss coatings by radiation curing directly from pigmented coating compositions.
- This invention provides a dark (particularly black) pigmented, radiation curable coating composition adapted to produce a low gloss film, i.e., at gloss levels below 30%.
- the composition comprises: a resin binder curable by radiation exposure in the presence of a photoinitiator compound, photoinitiator compound, and black silica pigment.
- Low gloss is achieved in the present invention at least in part by means of a uniform, microscopic surface wrinkling of the film that is produced from the coating composition when the coating is cured by a two step radiation curing process, wherein the first step involves ionizing radiation (e.g., electron beam) and the second step involves actinic radiation (e.g., ultraviolet light).
- ionizing radiation e.g., electron beam
- actinic radiation e.g., ultraviolet light
- a resin binder that has been found effective in preferred embodiments comprises polyacrylate functional resin.
- the resin binders of the present invention are characterized as being radiation cure inhibited by the presence of oxygen, it has been found advantageous in producing flat, dark colors to employ a photoinitiator that has relatively less oxygen inhibition. For this reason a preferred class of photoinitiator constitutes the alkoxy substituted acetophenones.
- the mottling problem was found to be further alleviated by the inclusion of a selected viscosity control resin in addition to the primary radiation curable binder resin.
- the viscosity control resin is reactive with the binder resin and is of relatively high molecular weight.
- the binder resin is an acrylic resin, it is preferred that the viscosity control resin be an acrylate functional acrylic polymer for the sake of compatibility.
- the coating composition is pigmented, whereby the desired low gloss finish can be attained with one coat rather than requiring a base coat and clear top coat as required by some prior art methods.
- Another aspect of the invention is the method of using the novel coating composition described above wherein the coating composition is cured in a subsurface portion in a first step by electron beam radiation in the presence of oxygen whereby curing at the surface is partially inhibited. In a subsequent step the curing is completed by means of ultraviolet radiation in a substantially inert atmosphere (less than 1000 ppm oxygen, preferably less than 500 ppm oxygen) .
- the present invention involves a coating composition containing a photoinitiators.
- Photoinitiators absorb radiation and thereby obtain energy to form free radicals that initiate polymerization of the binder resin.
- the photoinitiator is one which forms free radicals upon exposure to actinic radiation, viz., ultraviolet light.
- a particularly suitable class of photoinitiators for this purpose are acetophenone derivatives. Many acetophenone derivatives are known as photoinitiators, a large number of which are disclosed in U.S. Patent No. 4,229,274 (Carlblom) .
- Acetophenone derivative photoinitiators may be generally characterized by the formula:
- Ri, R 2 , and R3 may, for example, include independently hydrogen, alkyl usually having from 1 to 6 carbon atoms (preferably 1 to 4 carbon atoms) , alkoxy, cycloalkyl, or substituted or unsubstituted phenyl groups, and d is a phenyl group.
- a particularly useful family of acetophenone derivatives for use in the present invention are those in which at least one (preferably two) of Ri, R 2 , and/or R3 is an alkoxy group, for example, methoxy or ethoxy.
- the photoinitiator may be present in an amount in the range of from 0.01 percent to 4 percent by weight based on total solids content of the coating composition, preferably at least 0.1 percent to 2 percent.
- the primary binder or vehicle in the coating composition of the present invention comprises at least one resin (monomer, oligomer, or polymer) including at least one resin which is curable by exposure to radiation in the presence of one or more of the photoinitiators disclosed above. Binder may constitute 20 to 80, preferably 30 to 70, percent by weight of the total coating composition. Many such resins are known in the art and may be used in the present invention.
- the resins suitable for use in the present invention are characterized by inhibition of curing by the presence of oxygen (such as in air) . Oxygen inhibition permits maintaining a partially uncured surface layer during the initial curing step, which is important for attaining the wrinkle effect of the present invention.
- radiation curable resins that are adapted to be curable in the presence of oxygen, such as those containing substantial amounts of epoxy acrylate derivatives or allyl groups, are not appropriate for use in the present invention.
- a particular category of useful radiation curable compounds are characterized by a plurality of acrylyloxy groups and the ability to be free radically addition polymerized by initiation f om the photoinitiators. These are numerous and include difunctional, trifunctional, tetrafunctional and higher polyfunctional organic radicals whose bonds are satisfied with unsubstituted acrylyloxy or a-substituted acrylyloxy groups.
- the polyvalent radical may be aliphatic, cycloaliphatic, aromatic or other.
- acrylyloxy is used in its broad sense to mean unsubstituted acrylyloxy or a-substituted acrylyloxy groups such as methacrylyloxy, ethacrylyloxy and a-chloroacrylyloxy.
- acrylate unsaturation is used in its broad sense to mean the unsaturation provided by unsubstituted acrylyl groups or a-substituted acrylyl groups such as ethacrylyl, ethacrylyl and a-chloroacrylyl.
- Examples of these compounds are the diacrylates and dimethacrylates of ethylene glycol, 1,3-propanediol, propylene glycol, 2,3-butanediol, 1,4-butanediol, 2-ethylbutane-l,4-diol, 1,5- pentanediol, 1,6-hexanediol, 1,7-heptanediol, 1, 8-octanediol, 1,9- nonanediol, 1, 10-decanediol, 2,10-decanediol, 1,4-cyclohexanediol, 1,4-dimethylolcyclohexane, 2,2-diethylpropane-l,3-diol, 2,2- dimethylpropane-l,3-diol, 3-methylpentane-l,4-diol, 2,2- diethylbutane-1,3-di
- the acrylyloxy groups in each of the molecules are usually the same, but they may be different as exemplified by the compound 2,2-dimethyl-1-acrylyloxy-3- ** methacrylyloxypropane.
- Further examples of satisfactory polyacrylyloxy compounds that may be included in the radiation curable resin include polyacrylyloxy functional polyesters, polamides, polyacrylates, polyethers, polycarbonates or polyurethanes as well as polyacrylyloxy functional compounds of mixed functionality such as polyacrylyloxy functional poly(ester-urethanes) , poly(ester-amides) and polyfether- urethanes) . Mixtures of compounds having a plurality of acrylyloxy groups may be used, if desired.
- the second polymer reactive with the primary binder resin that is less sensitive to oxygen inhibition than the primary binder resin.
- the primary binder resin is an acrylate functional material
- the second polymer is preferably also acrylate functional. It is also advantageous for the second polymer to have relatively high molecular weight to serve as a viscosity control agent, whereby fluidity of the uncured coating is decreased. This is believed to contribute to the avoidance of mottling attainable by the present invention.
- Viscosity of the viscosity control resin is preferably greater than 3000 centipoise at 60°C.
- a class of materials that have been found to be particularly compatible with the preferred acrylate binder resins are acrylate functional acrylic polymers such as "Ebecryl 1701" from Radcure, Inc., Louisville, KY.
- the amount of the viscosity control polymer to be included will vary substantially, depending upon the particular polymer used and its viscosity. For the preferred class of acrylated acrylic polymers, the amount may range from 5 to 40 percent by weight on the solids basis.
- Monomers having monoacrylate functionality which crosslinks with the compound having polyacrylyloxy functionality may optionally be present in the coating composition.
- monoacrylate functional monomers which may be used are methyl acrylate, methyl methacrylate, ethyl acrylate, ethyl methacrylate, propyl acrylate, propyl methacrylate, butyl acrylate, butyl methacrylate, hexyl acrylate, hexyl methacrylate, hexyl ethyl acrylate, hexyl butyl acrylate, 2-ethyl hydroxy acrylate, octyl acrylate, octyl methacrylate, hydroxy ethyl acrylate, hydroxy butyl acrylate, caprolactone-hydroxyl alkyl acrylate reaction products, and 2-ethyl hydroxy acrylate.
- the preferred monoacrylate functional monomers are liquid compounds miscible with the polyacrylyloxy compound.
- a benefit from the use of one or more monoacrylate functional monomers is that the monoacrylate functional monomer may act as a reactive solvent for the polyacrylyloxy functional compound, thereby providing coating compositions having a satisfactory low viscosity without using relatively small amounts or no volatile, nonreactive solvent.
- the monoacrylate functional monomer, or mixtures of monoacrylate functional monomers may be employed over a broad range, although none is required. The amount of such monomer when used should be sufficient to provide a liquid, flowable, interpolymerizable mixture.
- the monomer When used, the monomer will ordinarily be present in the coating composition in the range of from about 0 to about 80 percent by weight of the binder of the coating composition. Typically, the monoacrylate functional monomer will be present in the range of from about 0 to about 30 percent by weight of the binder.
- Other monovalent functional monomers may be employed as known in the radiation curing art, including N-vinyl-2-pyrolidone, vinyl neodecanoate, and other ethylenic unsaturated monomers known to be suitable for radiation curable coatings.
- the pigment portion of the compositions of the present invention includes black silica.
- black silica describes a naturally occuring mineral substance that includes silica as a major component, and in which the black color is imparted by a small amount of carbon. Other mineral oxides are also usually present, particularly aluminum oxide.
- a commercial source of black silica is “Ebony Novacite” from Malvern Minerals Company, Hot Springs National Park, Arkansas.
- a typical chemical analysis of this product is as follows:
- Black silica has low oil absorption, and therefore it can be included in the coating compositions of the present invention in relatively large amounts without having a detrimental effect on coating properties.
- the relatively high pigment content raises the viscosity of the uncured coatings, which is believed to account at least in part to the avoidance of the mottling problem that was associated with prior art black coatings that employed carbon black, for example.
- Black silica may be present in amounts of 5 to 20 percent by weight of solids of the coating compositions of the present invention.
- the pigment portion may optionally contain other coloring or opacifying agents, flatting agents, fillers, and extenders, including titanium dioxide (rutile or anatase) , zinc oxide, zirconium oxide, zinc sulfide and lithopone.
- coloring pigments include iron oxides, cadmium sulfide, carbon black, phthalocyanine blue, phthalocyanine green, indanthrone blue, ultramarine blue, chromium oxide, burnt umber, benzidine yellow, tolluidine red, aluminum power and aluminum flakes.
- extender pigments examples include silica, barytes, calcium carbonate, barium sulfate, talc, aluminum silicates, sodium aluminum silicates, potassium aluminum silicates and magnesium silicate.
- the pigment When the pigment is ultraviolet light absorbing, it should be used in amounts which do not preclude curing of the interior of the coating. The maximum amount is therefore related to the thickness of the coating to be cured. Thin coatings may tolerate more ultraviolet light absorbing pigment than thick coatings. When the pigment does not significantly absorb ultraviolet light, there is usually greater latitude in the amounts which may be employed.
- Total pigment content, including the black silica may range from 10 to 70 percent by weight of solids of the coating composition, preferably 10 to 50 percent. Dyes and tints may be included in the coating composition as replacements for all or some of the optional pigment content.
- resinous pigment dispersant e.g., cellulose acetate butyrate
- viscosity control agent e.g., cellulose acetate butyrate
- grinding vehicle e.g., cellulose acetate butyrate
- resinous dispersants which.are commercially available which may be used for that purpose. These dispersants are used in the manner and in amounts known to the art, such as 0 to 20 weight percent of the total composition.
- plasticizers such as dibutyl phthalate, butyl benzyl phthalate, diisooctyl phthalate, decyl butyl phthalate, diisooctyl adipate, dibutyl sebacate, butyl benzoate, triisooctyl trimellitate, n-octyl n-decyl trimellitate, and tricresyl phosphates and flow promoters such as phenyl benzoate, dibenzyl ketone, benzyl methyl ketone and the like may also be optionally included in amounts customary in the art, although they are not considered necessary for the present invention. If any plasticizer is included, it is usually present in amounts no greater than 5 weight percent of the total composition.
- non-reactive, volatile organic solvent Another ingredient which is often included in coating compositions of this type is a non-reactive, volatile organic solvent.
- solvent may be present, but in lesser amounts than conventional. It is generally advantageous to minimize the amount of organic solvent, but if reduction of viscosity is desired for a particular application, the present invention does not preclude adding larger amounts of a non-reactive solvent or mixtures of several solvents.
- non-reactive organic solvents examples include acetone, methyl ethyl ketone, methyl isobutyl ketone, methyl alcohol, ethyl alcohol, propyl alcohol, isopropyl alcohol, butyl alcohol, secutyl alcohol, isobutyl alcohol, tert-butyl alcohol, amyl alcohol, hexyl alcohol, 2-ethylhexyl alcohol, cellosolve, ethyl cellosolve, cellosolve acetate, 2-ethylhexyl acetate, tetrahydrofuran, and aliphatic naphtha.
- solvent of this type it is ordinarily present in the coating composition in the range of from about 0.1 to about 40 percent by weight of the vehicle of the coating composition. From about 0 to about 15 percent is typical.
- the preferred compositions are solvent-free.
- a small amount of wax may be included in the composition as it conventional in the art.
- the coating compositions of the invention are usually prepared by simply admixing the various ingredients.
- the compounds comprising the photoinitiator system may be premixed and then admixed with the other ingredients of the coating composition, or they may be added separately. Although mixing is usually accomplished at room temperature, elevated temperatures are sometimes used. The maximum temperature which is usable depends upon the heat stability of the ingredients. Temperatures above about 200°F (93°C) are only rarely employed.
- the radiation curable coating compositions of the invention are generally used to form cured, adherent coatings on substrates.
- the substrate is coated with the coating composition using substantially any technique known to the art. These include spraying, curtain coating, dipping, roller application, printing, brushing, drawing and extrusion.
- Substrates which may be coated with the compositions of this invention may vary widely in their properties.
- Organic substrates such as wood, fiberboard, particle board, composition board, paper, cardboard and various polymers such as polyesters, polyamides, cured phenolic resins, cured aminoplasts, acrylics, polyurethanes and rubber may be used.
- Inorganic substrates are exemplified by glass, quartz and ceramic materials.
- Many metallic substrates may be coated. Exemplary metallic substrates are iron, steel, stainless steel, copper, brass, bronze, aluminum, magnesium, titanium, nickel, chromium, zinc and alloys.
- the method of curing the coating composition of the present invention involves a two step radiation exposure wherein the applied coating layer is cured in a subsurface portion in a first step by exposure to ionizing radiation (e.g., electron beam radiation or laser) in the presence of oxygen whereby curing at the surface is at least partially inhibited.
- ionizing radiation e.g., electron beam radiation or laser
- the curing is completed throughout the remainder of the coating thickness by means of ultraviolet radiation in a substantially inert atmosphere.
- Suitable electron beam radiation for use in the first curing step may constitute a dose of 2 to 10 megarads, preferably 2 to 5 megarads, at 150 to 300 kiloelectron volts, preferably 170 to 250 kiloelectron volts.
- the exposure in the first step is chosen so as to substantially cure the portion of the coating closest to the substrate. A portion of the coating thickness nearest to the surface will remain at least partially uncured due to oxygen inhibition.
- Any suitable source which emits ultraviolet light viz., electromagnetic radiation having a wavelength in the range of from about 180 to about 400 nanometers, may be used in the practice of the second curing step.
- Suitable sources are mercury arcs, carbon arcs, low pressure mercury lamps, medium pressure mercury lamps, high pressure mercury lamps, swirl-flow plasma arc, ultraviolet light- emitting diodes and ultraviolet light emitting lasers.
- Particularly preferred are ultraviolet light emitting lamps of the medium or high pressure mercury vapor type. Such lamps usually have fused quartz envelopes to withstand the heat and transmit the ultraviolet radiation and are ordinarily in the form of long tubes having an electrode at either end.
- the time of exposure to ultraviolet light and the intensity of the ultraviolet light to which the coating composition is exposed may vary greatly. Generally the exposure to ultraviolet light should continue until either the film is thermoset throughout or at least cured to the point where subsequent reactions cause the film to become thermoset throughout. Exposure of the coating to ultraviolet light may be accomplished in the presence of an inert atmosphere, viz., an atmosphere either containing no oxygen or only a concentration of oxygen which insignificantly inhibits polymerization of the coating surface (less than 1000 parts per million, preferably less than 500 parts per million oxygen) . Gases such as nitrogen, argon, carbon dioxide or mixtures thereof are typically the major components of inert atmospheres, although other unreactive gases may be used. Nitrogen is generally employed for this purpose.
- Coatings produced in accordance with the present invention exhibit a surface with very fine wrinkles, which are generally smaller than can be seen with the unaided eye. When viewed under magnification, the wrinkles can be seen to be uniformly distributed over the surface in a substantially regular pattern as shown in the drawing. This finely wrinkled surface appears to be responsible for the low gloss attained by the present invention without total reliance on flatting agents. Gloss may conveniently be determined by the Standard Method of Test for Specular Gloss, ASTM Designation D- 523-67 (Reapproval 1971) . Using a Gardner 60 ⁇ glossmeter, the gloss of cured coatings of the present invention can be less than 30 percent reflected light, preferably less than 25 percent reflected light. Although not precluded from the present invention, black coatings having less than about 10-15 percent reflected light are generally not considered attractive.
- Example 1 is a specific embodiment of the invention, which is compared in Table I to a typical prior art commercial composition, Comparative Example A, which had been suggested for flat black, radiation cured coatings prior to the present invention.
- Example 1 and Comparative Example A were each applied by a curtain coater at a thickness of 2.2 mils onto pre- filled substrate (flat stock medium density fiberboard) and cured via electronbeam energy at the following conditions: 250 kilovolts potential (220KV - 275KV) , total dose of 5 megarads achieved at a production line speed of 120 ft./min. in a partially inerted atmosphere by use of nitrogen to 14% oxygen content (10% - 15%) .
- the second stage cure employed ultraviolet light exposure with 200 watt/in. medium pressure mercury vapor lamps at a speed of 10 ft./min. per lamp in a totally inerted atmosphere by use of nitrogen to 500 ppm of oxygen (0 - 1000 ppm) .
- Table I The results are set forth in Table I.
- Example 1 Example A Gloss (60° glossmeter) 15 26
- Comparative Example B had the following composition:
- Tripropylene glycol diacrylate 76.0 Celluose acetate butyrate 1 3.0 Lampblack 2 3.0 Polyethylene wax 3 1.0 Silica flatting pigment 4 1.8
- Comparative Example C constituted 87.5 percent by weight of the composition of Comparative Example A with the addition of 10 percent by weight hexanediol diacrylate, 1.5 percent additional Irgacure photoinitiator, and 1..0 percent benzophenone photoinitiator.
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- Materials Engineering (AREA)
- Wood Science & Technology (AREA)
- Organic Chemistry (AREA)
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU75126/94A AU7512694A (en) | 1993-09-20 | 1994-06-27 | Flat, dark pigmented radiation curable coating compositions |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12354493A | 1993-09-20 | 1993-09-20 | |
US08/123,544 | 1993-09-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1995008596A1 true WO1995008596A1 (en) | 1995-03-30 |
Family
ID=22409292
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1994/007206 WO1995008596A1 (en) | 1993-09-20 | 1994-06-27 | Flat, dark pigmented radiation curable coating compositions |
Country Status (4)
Country | Link |
---|---|
AU (1) | AU7512694A (enrdf_load_html_response) |
TR (1) | TR27853A (enrdf_load_html_response) |
TW (1) | TW287193B (enrdf_load_html_response) |
WO (1) | WO1995008596A1 (enrdf_load_html_response) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998027171A1 (en) * | 1996-12-17 | 1998-06-25 | Minnesota Mining And Manufacturing Company | Curable ink composition |
US6410147B1 (en) | 2000-08-24 | 2002-06-25 | E. I. Du Pont De Nemours And Company | Low gloss crosslinkable coating compositions |
WO2024197004A3 (en) * | 2023-03-20 | 2024-10-31 | Miltec UV International, LLC | Actinic or electron beam radiation curable binder for ceramic materials |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3840448A (en) * | 1972-06-26 | 1974-10-08 | Union Carbide Corp | Surface curing of acrylyl or methacrylyl compounds using radiation of 2,537 angstroms |
US4048036A (en) * | 1974-10-24 | 1977-09-13 | Ppg Industries, Inc. | Process for producing films of low gloss by exposure to ultraviolet light |
-
1994
- 1994-06-27 AU AU75126/94A patent/AU7512694A/en not_active Abandoned
- 1994-06-27 WO PCT/US1994/007206 patent/WO1995008596A1/en active Application Filing
- 1994-07-28 TW TW83106905A patent/TW287193B/zh active
- 1994-08-26 TR TR84994A patent/TR27853A/xx unknown
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3840448A (en) * | 1972-06-26 | 1974-10-08 | Union Carbide Corp | Surface curing of acrylyl or methacrylyl compounds using radiation of 2,537 angstroms |
US4048036A (en) * | 1974-10-24 | 1977-09-13 | Ppg Industries, Inc. | Process for producing films of low gloss by exposure to ultraviolet light |
Non-Patent Citations (1)
Title |
---|
DATABASE WPI Derwent World Patents Index; * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998027171A1 (en) * | 1996-12-17 | 1998-06-25 | Minnesota Mining And Manufacturing Company | Curable ink composition |
US5981113A (en) * | 1996-12-17 | 1999-11-09 | 3M Innovative Properties Company | Curable ink composition and imaged retroreflective article therefrom |
US6232359B1 (en) | 1996-12-17 | 2001-05-15 | 3M Innovative Properties Company | Curable ink composition |
CN1088731C (zh) * | 1996-12-17 | 2002-08-07 | 美国3M公司 | 可固化的油墨组合物 |
US6410147B1 (en) | 2000-08-24 | 2002-06-25 | E. I. Du Pont De Nemours And Company | Low gloss crosslinkable coating compositions |
WO2024197004A3 (en) * | 2023-03-20 | 2024-10-31 | Miltec UV International, LLC | Actinic or electron beam radiation curable binder for ceramic materials |
Also Published As
Publication number | Publication date |
---|---|
TR27853A (tr) | 1995-09-04 |
TW287193B (enrdf_load_html_response) | 1996-10-01 |
AU7512694A (en) | 1995-04-10 |
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