MXPA06010994A - Coated abrasive products and processes for forming same - Google Patents
Coated abrasive products and processes for forming sameInfo
- Publication number
- MXPA06010994A MXPA06010994A MXPA/A/2006/010994A MXPA06010994A MXPA06010994A MX PA06010994 A MXPA06010994 A MX PA06010994A MX PA06010994 A MXPA06010994 A MX PA06010994A MX PA06010994 A MXPA06010994 A MX PA06010994A
- Authority
- MX
- Mexico
- Prior art keywords
- further characterized
- abrasive
- agglutinating
- binder
- cured
- Prior art date
Links
- 238000005296 abrasive Methods 0.000 title claims abstract description 61
- 238000000034 method Methods 0.000 title claims description 14
- 239000011230 binding agent Substances 0.000 claims abstract description 56
- 239000000203 mixture Substances 0.000 claims abstract description 54
- 239000000843 powder Substances 0.000 claims abstract description 37
- 238000009472 formulation Methods 0.000 claims abstract description 32
- 239000006061 abrasive grain Substances 0.000 claims abstract description 21
- 239000000758 substrate Substances 0.000 claims abstract description 20
- 150000001875 compounds Chemical class 0.000 claims description 25
- 230000004523 agglutinating Effects 0.000 claims description 23
- -1 epoxy acrylates Chemical class 0.000 claims description 20
- 229920000642 polymer Polymers 0.000 claims description 11
- 239000011248 coating agent Substances 0.000 claims description 10
- 238000000576 coating method Methods 0.000 claims description 10
- 239000006185 dispersion Substances 0.000 claims description 10
- WSFSSNUMVMOOMR-UHFFFAOYSA-N formaldehyde Chemical compound O=C WSFSSNUMVMOOMR-UHFFFAOYSA-N 0.000 claims description 10
- 239000004593 Epoxy Substances 0.000 claims description 7
- 239000007822 coupling agent Substances 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 7
- PNEYBMLMFCGWSK-UHFFFAOYSA-N AI2O3 Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 6
- 229920000728 polyester Polymers 0.000 claims description 6
- NIXOWILDQLNWCW-UHFFFAOYSA-M acrylate Chemical compound [O-]C(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-M 0.000 claims description 5
- 150000001252 acrylic acid derivatives Chemical class 0.000 claims description 5
- 239000004744 fabric Substances 0.000 claims description 5
- XSQUKJJJFZCRTK-UHFFFAOYSA-N urea Chemical compound NC(N)=O XSQUKJJJFZCRTK-UHFFFAOYSA-N 0.000 claims description 4
- HBMJWWWQQXIZIP-UHFFFAOYSA-N Silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 claims description 3
- OBFQBDOLCADBTP-UHFFFAOYSA-N aminosilicon Chemical compound [Si]N OBFQBDOLCADBTP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 3
- 229910052726 zirconium Inorganic materials 0.000 claims description 3
- 229910052582 BN Inorganic materials 0.000 claims description 2
- 229920000742 Cotton Polymers 0.000 claims description 2
- JDSHMPZPIAZGSV-UHFFFAOYSA-N Melamine Chemical compound NC1=NC(N)=NC(N)=N1 JDSHMPZPIAZGSV-UHFFFAOYSA-N 0.000 claims description 2
- 229920000877 Melamine resin Polymers 0.000 claims description 2
- PZNSFCLAULLKQX-UHFFFAOYSA-N N#B Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 2
- 229920002803 Thermoplastic polyurethane Polymers 0.000 claims description 2
- 239000004202 carbamide Substances 0.000 claims description 2
- 229910003460 diamond Inorganic materials 0.000 claims description 2
- 239000010432 diamond Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 claims description 2
- 239000003822 epoxy resin Substances 0.000 claims description 2
- 239000002223 garnet Substances 0.000 claims description 2
- CERQOIWHTDAKMF-UHFFFAOYSA-M methacrylate Chemical compound CC(=C)C([O-])=O CERQOIWHTDAKMF-UHFFFAOYSA-M 0.000 claims description 2
- 238000002156 mixing Methods 0.000 claims description 2
- 150000001282 organosilanes Chemical class 0.000 claims description 2
- 229920001568 phenolic resin Polymers 0.000 claims description 2
- 239000005011 phenolic resin Substances 0.000 claims description 2
- 229920000647 polyepoxide Polymers 0.000 claims description 2
- WIJVUKXVPNVPAQ-UHFFFAOYSA-N silyl 2-methylprop-2-enoate Chemical compound CC(=C)C(=O)O[SiH3] WIJVUKXVPNVPAQ-UHFFFAOYSA-N 0.000 claims description 2
- 238000010924 continuous production Methods 0.000 claims 3
- 150000002734 metacrylic acid derivatives Chemical class 0.000 claims 1
- 230000003252 repetitive Effects 0.000 claims 1
- 238000007669 thermal treatment Methods 0.000 claims 1
- 239000000047 product Substances 0.000 description 33
- 239000003082 abrasive agent Substances 0.000 description 27
- 239000010410 layer Substances 0.000 description 16
- 239000007921 spray Substances 0.000 description 10
- 241000785686 Sander Species 0.000 description 8
- 238000005520 cutting process Methods 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 6
- 229920003986 novolac Polymers 0.000 description 6
- 239000002245 particle Substances 0.000 description 6
- 229920005989 resin Polymers 0.000 description 6
- 239000011347 resin Substances 0.000 description 6
- 238000005507 spraying Methods 0.000 description 6
- 238000004140 cleaning Methods 0.000 description 5
- 230000035876 healing Effects 0.000 description 5
- 239000000945 filler Substances 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 238000010998 test method Methods 0.000 description 4
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive Effects 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 239000003211 photoinitiator Substances 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 230000004580 weight loss Effects 0.000 description 3
- OYKPJMYWPYIXGG-UHFFFAOYSA-N 2,2-dimethylbutane;prop-2-enoic acid Chemical compound OC(=O)C=C.OC(=O)C=C.OC(=O)C=C.CCC(C)(C)C OYKPJMYWPYIXGG-UHFFFAOYSA-N 0.000 description 2
- TZCXTZWJZNENPQ-UHFFFAOYSA-L Barium sulfate Chemical compound [Ba+2].[O-]S([O-])(=O)=O TZCXTZWJZNENPQ-UHFFFAOYSA-L 0.000 description 2
- OSGAYBCDTDRGGQ-UHFFFAOYSA-L Calcium sulfate Chemical compound [Ca+2].[O-]S([O-])(=O)=O OSGAYBCDTDRGGQ-UHFFFAOYSA-L 0.000 description 2
- LXCIHXPVYQKJAG-UHFFFAOYSA-N N-[aziridin-1-yl-(2-methylaziridin-1-yl)phosphoryl]-N-prop-2-enylprop-2-en-1-amine Chemical compound CC1CN1P(=O)(N(CC=C)CC=C)N1CC1 LXCIHXPVYQKJAG-UHFFFAOYSA-N 0.000 description 2
- GHKADIDUAMVZKK-UHFFFAOYSA-N OCOC(=O)C=C.OCOC(=O)C=C.OCOC(=O)C=C Chemical compound OCOC(=O)C=C.OCOC(=O)C=C.OCOC(=O)C=C GHKADIDUAMVZKK-UHFFFAOYSA-N 0.000 description 2
- REHXRBDMVPYGJX-UHFFFAOYSA-H Sodium hexafluoroaluminate Chemical compound [Na+].[Na+].[Na+].F[Al-3](F)(F)(F)(F)F REHXRBDMVPYGJX-UHFFFAOYSA-H 0.000 description 2
- HVVWZTWDBSEWIH-UHFFFAOYSA-N [2-(hydroxymethyl)-3-prop-2-enoyloxy-2-(prop-2-enoyloxymethyl)propyl] prop-2-enoate Chemical compound C=CC(=O)OCC(CO)(COC(=O)C=C)COC(=O)C=C HVVWZTWDBSEWIH-UHFFFAOYSA-N 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 150000001412 amines Chemical class 0.000 description 2
- VTYYLEPIZMXCLO-UHFFFAOYSA-L calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 2
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium monoxide Chemical compound [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 229910001610 cryolite Inorganic materials 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- RTZKZFJDLAIYFH-UHFFFAOYSA-N diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 2
- 239000000975 dye Substances 0.000 description 2
- 239000012467 final product Substances 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229940065472 octyl acrylate Drugs 0.000 description 2
- ANISOHQJBAQUQP-UHFFFAOYSA-N octyl prop-2-enoate Chemical compound CCCCCCCCOC(=O)C=C ANISOHQJBAQUQP-UHFFFAOYSA-N 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 229920000139 polyethylene terephthalate Polymers 0.000 description 2
- 239000005020 polyethylene terephthalate Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- CDBYLPFSWZWCQE-UHFFFAOYSA-L sodium carbonate Chemical compound [Na+].[Na+].[O-]C([O-])=O CDBYLPFSWZWCQE-UHFFFAOYSA-L 0.000 description 2
- 238000001029 thermal curing Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- HPSUPGAVFFFPMQ-UHFFFAOYSA-N 1,2,3,4,6,7,10-heptachlorododecane Chemical compound CCC(Cl)CCC(Cl)C(Cl)CC(Cl)C(Cl)C(Cl)CCl HPSUPGAVFFFPMQ-UHFFFAOYSA-N 0.000 description 1
- BPXVHIRIPLPOPT-UHFFFAOYSA-N 1,3,5-tris(2-hydroxyethyl)-1,3,5-triazinane-2,4,6-trione Chemical compound OCCN1C(=O)N(CCO)C(=O)N(CCO)C1=O BPXVHIRIPLPOPT-UHFFFAOYSA-N 0.000 description 1
- ZDQNWDNMNKSMHI-UHFFFAOYSA-N 1-[2-(2-prop-2-enoyloxypropoxy)propoxy]propan-2-yl prop-2-enoate Chemical compound C=CC(=O)OC(C)COC(C)COCC(C)OC(=O)C=C ZDQNWDNMNKSMHI-UHFFFAOYSA-N 0.000 description 1
- VOBUAPTXJKMNCT-UHFFFAOYSA-N 1-prop-2-enoyloxyhexyl prop-2-enoate Chemical compound CCCCCC(OC(=O)C=C)OC(=O)C=C VOBUAPTXJKMNCT-UHFFFAOYSA-N 0.000 description 1
- 239000010963 304 stainless steel Substances 0.000 description 1
- 239000004925 Acrylic resin Substances 0.000 description 1
- 229920000178 Acrylic resin Polymers 0.000 description 1
- WNROFYMDJYEPJX-UHFFFAOYSA-K Aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 1
- DIZPMCHEQGEION-UHFFFAOYSA-H Aluminium sulfate Chemical compound [Al+3].[Al+3].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O DIZPMCHEQGEION-UHFFFAOYSA-H 0.000 description 1
- ISAOCJYIOMOJEB-UHFFFAOYSA-N Benzoin Chemical compound C=1C=CC=CC=1C(O)C(=O)C1=CC=CC=C1 ISAOCJYIOMOJEB-UHFFFAOYSA-N 0.000 description 1
- 229960002130 Benzoin Drugs 0.000 description 1
- RWCCWEUUXYIKHB-UHFFFAOYSA-N Benzophenone Chemical compound C=1C=CC=CC=1C(=O)C1=CC=CC=C1 RWCCWEUUXYIKHB-UHFFFAOYSA-N 0.000 description 1
- 229960005069 Calcium Drugs 0.000 description 1
- 229960003563 Calcium Carbonate Drugs 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- MXRIRQGCELJRSN-UHFFFAOYSA-N O.O.O.[Al] Chemical compound O.O.O.[Al] MXRIRQGCELJRSN-UHFFFAOYSA-N 0.000 description 1
- 229920001225 Polyester resin Polymers 0.000 description 1
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 1
- FZHAPNGMFPVSLP-UHFFFAOYSA-N Silanamine Chemical class [SiH3]N FZHAPNGMFPVSLP-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 240000008975 Styrax benzoin Species 0.000 description 1
- 235000000126 Styrax benzoin Nutrition 0.000 description 1
- 235000008411 Sumatra benzointree Nutrition 0.000 description 1
- DAKWPKUUDNSNPN-UHFFFAOYSA-N TMPTA Chemical compound C=CC(=O)OCC(CC)(COC(=O)C=C)COC(=O)C=C DAKWPKUUDNSNPN-UHFFFAOYSA-N 0.000 description 1
- VZTQQYMRXDUHDO-UHFFFAOYSA-N [2-hydroxy-3-[4-[2-[4-(2-hydroxy-3-prop-2-enoyloxypropoxy)phenyl]propan-2-yl]phenoxy]propyl] prop-2-enoate Chemical compound C=1C=C(OCC(O)COC(=O)C=C)C=CC=1C(C)(C)C1=CC=C(OCC(O)COC(=O)C=C)C=C1 VZTQQYMRXDUHDO-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 239000002216 antistatic agent Substances 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 125000001797 benzyl group Chemical group [H]C1=C([H])C([H])=C(C([H])=C1[H])C([H])([H])* 0.000 description 1
- 239000003738 black carbon Substances 0.000 description 1
- 229910001593 boehmite Inorganic materials 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- 239000000292 calcium oxide Substances 0.000 description 1
- 229910052918 calcium silicate Inorganic materials 0.000 description 1
- 235000012241 calcium silicate Nutrition 0.000 description 1
- OYACROKNLOSFPA-UHFFFAOYSA-N calcium;dioxido(oxo)silane Chemical compound [Ca+2].[O-][Si]([O-])=O OYACROKNLOSFPA-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 150000004649 carbonic acid derivatives Chemical class 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- FWLDHHJLVGRRHD-UHFFFAOYSA-N decyl prop-2-enoate Chemical compound CCCCCCCCCCOC(=O)C=C FWLDHHJLVGRRHD-UHFFFAOYSA-N 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 238000004049 embossing Methods 0.000 description 1
- 125000003700 epoxy group Chemical group 0.000 description 1
- 230000003628 erosive Effects 0.000 description 1
- JOYRKODLDBILNP-UHFFFAOYSA-N ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- 229910021485 fumed silica Inorganic materials 0.000 description 1
- 125000000524 functional group Chemical group 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 235000019382 gum benzoic Nutrition 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 150000007529 inorganic bases Chemical class 0.000 description 1
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 1
- 230000001678 irradiating Effects 0.000 description 1
- 238000011068 load Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reaction Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- KREXGRSOTUKPLX-UHFFFAOYSA-N octadecanoic acid;zinc Chemical compound [Zn].CCCCCCCCCCCCCCCCCC(O)=O.CCCCCCCCCCCCCCCCCC(O)=O KREXGRSOTUKPLX-UHFFFAOYSA-N 0.000 description 1
- 150000007530 organic bases Chemical class 0.000 description 1
- 230000036961 partial Effects 0.000 description 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- 239000004800 polyvinyl chloride Substances 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- AKEBROIVCDHVSD-UHFFFAOYSA-N potassium;tetrafluoroborate Chemical compound [K+].F[B-](F)(F)F AKEBROIVCDHVSD-UHFFFAOYSA-N 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 229910052904 quartz Inorganic materials 0.000 description 1
- 230000002829 reduced Effects 0.000 description 1
- 230000007261 regionalization Effects 0.000 description 1
- 230000001105 regulatory Effects 0.000 description 1
- 230000000717 retained Effects 0.000 description 1
- 238000000518 rheometry Methods 0.000 description 1
- BLRPTPMANUNPDV-UHFFFAOYSA-N silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 description 1
- 229910000077 silane Inorganic materials 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- KEAYESYHFKHZAL-UHFFFAOYSA-N sodium Chemical compound [Na] KEAYESYHFKHZAL-UHFFFAOYSA-N 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 239000001187 sodium carbonate Substances 0.000 description 1
- 229910000029 sodium carbonate Inorganic materials 0.000 description 1
- 239000011780 sodium chloride Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 150000003467 sulfuric acid derivatives Chemical class 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 239000000375 suspending agent Substances 0.000 description 1
- 230000002459 sustained Effects 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 239000004034 viscosity adjusting agent Substances 0.000 description 1
- 239000001993 wax Substances 0.000 description 1
- 239000000080 wetting agent Substances 0.000 description 1
- 239000008207 working material Substances 0.000 description 1
Abstract
A coated abrasive product is disclosed, which includes a substrate and an abrasive layer overlying the substrate. The abrasive layer includes abrasive grains and a binder, the binder being formed from a binder formulation having a first and second binder components mixed together uniformly with the abrasive grains, wherein the first binder component is radiation curable and the second binder component comprises a powder and is thermally curable.
Description
COATED ABRASIVE PRODUCTS AND PROCEDURES TO FORM THEMSELVES
CROSS REFERENCE TO RELATED REQUESTS
FIELD OF THE INVENTION
The present invention is directed generally to coated abrasive products, and in particular, to coated abrasive products and processes for forming them that employ a binder formulation having multiple healing paths.
BACKGROUND OF THE INVENTION
The coated abrasive products primarily include a substrate or support element that serves as a dimensionally stable component, onto which a layer containing the abrasive is deposited. In traditional coated abrasives, the abrasive grains of the abrasive layer are adhered to the support member through the use of a coating marker, which is an adhesive binder composition for anchoring the abrasive grains as they are deposited. More commonly, processing continues with the deposition of a cover of a size that allows structural integrity to the abrasive layer.
In the context of traditional coated abrasives, the abrasive grains are generally oriented in a random fashion and form a fairly uniform layer. Structured or designed abrasives have been developed to provide improved performance over traditional coated abrasive products. Structured abrasives also generally use a support element, although the abrasive layer is deposited in order to form a pre-configured pattern. Such structured abrasives generally exhibit improved spray characteristics over conventional abrasive products, such as providing a sustained cutting index, consistent surface finishing and a long life. In the context of both traditional coated abrasives and structural abrasives, thermally curable binders have been used to adhere the abrasive layer to the support element or substrate, as well as to stabilize the abrasive grains.
However, thermal curing suffers from numerous disadvantages which often include extended cure times which result in undesirable change in the position of the abrasive grains. Particularly, in the context of structured abrasives, the grain pattern can be altered during the rheological changes of the binder formulation during heating and / or during handling of the structured abrasive prior to or during heat treatment.
In an effort to orient said disadvantages, so-called agglutinating systems that can be cured by radiation have been developed, which advantageously allow to cut the healing cycles. Such binders that can be cured by radiation include binders that can be cured with UV, as well as binders that can be cured with an e-beam. However, the binders that can be cured by radiation are also free of disadvantages. For example, particularly in the case of abrasives based on silicon carbide, the penetration depth of the radiation is limited. Additionally, dyes present within the binder formulation can cause drawbacks with radiation penetration as well, resulting in incomplete cure. In an effort to orient the processing and performance characteristics associated with known coated abrasives, and in particular with structured abrasives, U.S. Pat. Nos. 5,863,306 and 5,833,724 describe various coated abrasives formed using a binder formulation that combines components that can be cured by radiation and components that can be cured in thermal form. During processing, the viscosity is modified through the use of a functional powder that is added to a coated intermediate product before curing. Functional powder intends to adjust a viscosity of the intermediate product, to retain the structural integrity during the processing, in such a way that the designed shape is maintained before and during the cure. Regardless of the advances provided in the art, as exemplified, for example, in Patents '306 and' 724, there continues to be a need for superior coated abrasives and methods to form them, and which additionally allow for manufacturing operations on a large scale.
BRIEF DESCRIPTION OF THE INVENTION
According to a first embodiment, a coated abrasive product includes a substrate, and an abrasive layer that covers the substrate. The abrasive layer includes abrasive grains and a binder, the binder being formed from a binder formulation including first and second binder compounds blended together uniformly with the abrasive grains. The first binder compound can generally be cured by radiation and the second binder compound desirably is in powder form, and can be cured in a thermal form. According to another embodiment, a method for forming a coated abrasive product includes mixing an agglutinating formulation with abrasive grains to form an abrasive dispersion, the agglutinating formulation including a mixture of first and second agglutinating compounds. The first agglutinating compound can be cured by radiation
and the second binder compound generally has a powder form, and can be cured in thermal form. The process continues with the coating of a substrate with the abrasive dispersion to form a coated intermediate, and performing the curing operations. The cure is performed by irradiating the coated intermediate to cure the first binder compound, and thermally treating the coated intermediate to cure the second binder compound.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention can be better understood, and its objects, features and numerous advantages become apparent to those skilled in the art, with reference to the accompanying drawings. Figure 1 illustrates a basic schematic design and a process flow to form a coated abrasive product structured according to one embodiment of the present invention. Figure 2 illustrates a cross-sectional view of one embodiment of the present invention. Figures 3 to 5 illustrate perspective views of various embodiments of the present invention. The use of the same reference symbols in different drawings indicates similar or identical articles.
DESCRIPTION OF THE PREFERRED MODALITIES
In accordance with one aspect of the present invention, a coated abrasive product is provided, generally including a substrate and an abrasive layer covering the substrate. The abrasive layer includes abrasive grains and a binder, the binder being formed from an agglutinating formulation. In a particular embodiment, the binder formulation includes first and second binder compounds that are blended together uniformly with the abrasive grains. Normally, the first binder can be cured by radiation, and the second binder is formed of a powder that can be cured in thermal form. Each of the first and second agglutinators can have only a single cure path. That is, each binder can be mono-curable, such that only a single cure methodology can be used to cure the particular binder compound. For example, as noted above, the first binder can be mono-curable in such a way that it can only be cured by irradiation, while the second binder is mono-curable, which can be cured only by a heat treatment. Returning to the particularities of the agglutinating formulation, as noted above, one of the agglutinating compounds, can generally be cured by radiation, such that it can be cured by UV, cured by e-beam, or can be heal by
microwave. A particularly useful UV binder composition contains the constituents chosen from the group of acrylate and methacrylate oligomers and monomers. Useful oligomers include epoxy acrylates, aliphatic urethane acrylates, aromatic urethane acrylates, polyester acrylates, aromatic acid acrylates, epoxy methacrylates, and aromatic methacrylates. The monomers include mono, di, tri, tetra and pentafunctional acrylates, such as trimethylpropane triacrylate, trimethylolpropane triacrylate, tris (2-hydroxyethyl) isocyanurate triacrylate, tripropylene glycol diacrylate, hexanediol diacrylate, octyl acrylate, octyl acrylate and decyl acrylate. . The binder formulation may include substantial amounts of acrylate monomers containing 3 or more acrylate groups per molecule. Typically, commercial products include trimethylpropane triacrylate, (TMPTA) as noted above, as well as pentaerythritol triacrylate (PETA). The relative amounts of di and tri-functional acrylates, as well as higher molecular weight acrylate oligomers can be adjusted together with the other components to provide the rheological properties suitable for processing and the appropriate hardness and cut characteristics of the final product. after the healing. Additionally, the coupling agents can be used to improve the bond between the adhesive grains and the abrasives. Typical coupling agents include organosilanes, for example A-174 and A1100 available from Osi Specialties, Inc., and organotitanates and
zircoaluminates. A particular group of coupling agents include aminosilanes and methacryloxy silanes. The fillers can be incorporated into the dispersion to modify the rheology of the dispersion and the hardening and hardness of the cured agglutinators. Examples of useful fillers include: metal carbonates such as calcium carbonate, sodium carbonate, silicas, such as quartz, glass beads, glass bubbles; silicates such as calcium, clays, calcium metasilicate; metal sulfates such as barium sulfate, calcium sulfate, aluminum sulfate; metal oxides such as calcium oxide, aluminum oxide (such as in the form of boehmite and / or pseudos boehmites); and aluminum trihydrate. The dispersion may comprise a spray aid to increase the spray efficiency and the cutting index. Useful spraying aids may be of inorganic base, such as halide salts, for example, sodium cryolite, tetrafluous potassium steal, etc .; or with an organic base, such as chlorinated waxes, for example, polyvinyl chloride. A particular embodiment includes cryolite and potassium tetrafluoroborate with a particle size that varies within the range of 1 to 80 microns, and more preferably 5 to 30 microns. The percentage by weight of the spray aid varies from 0 to 50%, and more preferably from 10 to 30% of the complete formulation (including the abrasive components). In addition to the above constituents, other components can also be added: usually a photoinitiator such as an ether
benzoin, ketal benzyl, α-alkoxy-acetophenone, α-hydroxy-alkylphenone, α-amino alkylphenone, acylphosphine oxide, benzophenone / amine, toxanthone / amine, or other free radical generator; anti-static agents, such as graphite, black carbon and the like, suspending agents, such as fumed silica, anti-loading agents, such as zinc stearate, lubricants such as wax, wetting agents; dyes; fillers, viscosity modifiers; dispersants; and defoamers. Returning to the second binder compound, various polymers can be used which can be cured in thermal form. Although thermoplastic and thermoadjustable polymers, thermoadjustable polymers are often preferred because of their stable nature, particularly in the context of cutting and finishing operations that generate excessive heat. According to a particular development, the second agglutinating compound is comprised of a powder, normally formed mainly of a powder or even essentially powder in its entirety. In general, polymers that can be cured in liquid thermal form are excluded in favor of the powders. The powder forms thermally curable agglutinators that are particularly advantageous, so that they can be incorporated into a process flow to form coated abrasives rather easily. In fact, the use of a thermally curable binder in powder form is particularly advantageous for the creation of abrasive dispersions used to form structured abrasives. Additionally, it has been discovered that the use of components
that can be cured in powder form have been shown to provide improved abrasive performance in the final product, as well as provide abrasive dispersions that have improved processing capacity due at least in part to beneficial changes in the viscosity of the dispersions. Examples of curable thermal polymers include epoxy resins, urethane resins, phenolic resins, urea / formaldehyde, melamine / formaldehyde, acrylic resins, polyester resins, vinyl, and mixtures thereof, provided said resins are used in powder form instead of liquid form. It should be understood that such resins are available in any form and that the powder or particle form is hereby preferably used. The abrasive grains can be formed from any or a combination of the known abrasive grains, including alumina (fused or sintered), zirconium, zirconium / alumina oxides, silicon carbide, garnet, diamond, cubic boron nitride and combinations of the same. The particular modalities have been created by the use of dense abrasive grains comprised primarily of alpha-alumina. The abrasive particles generally have an average particle size of 1 to 150 microns, and more typically of 1 to 80 microns. However, in general, the amount of abrasive present provides from about 10 to about 90%, such as from about 30 to about 80% of the weight of the formulation.
The support element can be formed of flexible though mechanically stable materials, including various polymer films, paper or other cellulosic materials and fabrics including cotton and polyester with various polymeric saturators. A particular type of support element or substrate is the polyethylene terephthalate film. Other polymeric films include polycarbonate films. The support elements can be primed or pretreated to promote adhesion between the abrasive layer and the support element. The details of the radiation-curable binding component, the additives with respect thereto, the support element and the abrasive grains can be found in the U.S. Pat. 5,014,468 commonly owned by the present Beneficiary, incorporated herein by reference. Returning to a particular aspect of the present invention, the following description focuses on structured abrasives, which generally have a high pattern of the abrasive material, as well as the methods for making the same. Figure 1 illustrates a basic process flow for the continuous manufacture of a coated abrasive product 10, and in particular, a structured or designed coated abrasive product. At this point, a support member 12 is extracted from a roller 42 provided on a non-shrouded platform. The non-wrapped platform is adjusted with a brake, in accordance with the usual practice to provide a desired resistance for
unroll the support element. The support member 12 is moved from the non-shrouded area around one or more suitable rolls designated by the reference numerals 44, 46, 48 and 50, and to the coating area generally denoted by the reference numeral 52, in FIG. where it is passed between the biter formed by the roller 53 and the patterned roller 56, which rotates in the directions indicated by the arrows. The pattern roller is a type of tool for imparting three-dimensional structures that can be used in accordance with the embodiments of the present invention. The support element 12 with the abrasive coating 14 coated thereon is passed around one or more rollers 58, 60 to a cutting station 62 having a radiation source, such as and an e-beam source or source. of actinic light, that is, a source of ultraviolet (UV) light, to cure a portion of the agglutinating formulation. The curing station 62 may additionally include a downstream thermal source of the UV light source, to complete the curing of the product. Alternatively, the thermal source may be provided off-line. For example, following a partial cure using only radiation, the product partially cured in this way can be rolled and cured in a coiled form in a heat curing oven (cured by volume), or it can be routed through another coil process to coil that contains a thermal curing station (linear or non-linear curing). According to one aspect, the use of a first binding compound that allows to cure in line, fast, the last stage of healing
it may occur off-line from a curing operation by volume, while maintaining the desired structural characteristics of the adhesive layer. The rollers 64, 66, route the coated abrasive material 10 to move horizontally through the healing zone. From the curing zone, the coated abrasive material 10 is moved over the roller 68 for a conventional removable assembly generally denoted by the reference number 70 and which includes a roller 72, a roller covered with plastic 74 and compressed air that drives the removable roll 76 to provide a roll wrapped with coated abrasive material. The radiant energy of the actinic light source can be supplied by any conventional UV source. For example, in the practice of the present invention, the coatings were exposed to UV light generated from bulbs V, D, H, or H +, or a combination thereof at an energy output that varies from 39 watts per centimeter wide at 236 watts per centimeter wide. The pattern formed in the support member through contact with the patterned roller may comprise islands of isolated formulation, or a pattern of folds separated by valleys. The patterns are generally designed to provide an abrasive product with a plurality of spraying surfaces equidistant from the support with the area of the spray surface increasing the erosion of the layer. Between
Spray surfaces are often provided with channels that allow the circulation of spray fluids and the removal of chips generated by spraying. In addition, the tool used to make the pattern and deposit the abrasive composition, can be heated or cooled, in such a way that it contributes to the elevation of the viscosity to produce the plastic surface of the formulation but not the fluid. However, the heating may not be of a level such that the binder is cured while in contact with the tool. By adjusting the viscosity of the resin formulation or the surface layer, the pattern is retained substantially to allow cure and handling, such as for at least about 30 seconds and preferably at least 60 seconds. Although the above embodiment has been described specifically in relation to the use of a pattern roller, other pattern formation techniques can be used. In a relatively simple form, a suitable substrate can be coated with an abrasive formulation, and then the pattern formed by contact with a embossing tool, such as a pattern forming seal or a nodular steel roll. According to a particular development, the dispersion or abrasive composition makes use of a thermal cure polymer in powder form, combined with the radiation curative polymer with a
abrasive component and additional components as detailed above. Typically, the particle size of the thermal cure polymer can vary from sub-microns to 500 microns. The change of particles can be used to modify the rheological properties of the coating, as well as the final mechanical properties. The incorporation of an agglutinating resin in the form of a powder also allows the processing of pastes with auxiliary content of abrasion, filler and low pulverization, which could not be processed when they are made only with a binder in liquid form. Returning to Figure 2, a cross-sectional view of a structured abrasive embodiment is illustrated. In particular, structured abrasive product 200 includes a substrate or support element 205 on which a layer of abrasive 208 is provided. Abrasive layer 208 includes, in cross section, elevated characteristics 210. The profile of the features Elevations 210 may vary considerably based on the intended end use. In the modality shown, the features 210 have a generally inclined and triangular cross section, ending in a sharp peak 214 that forms a cutting surface, and / or a flat cutting surface 216. The various features can be related through an underlying matrix 121. or they can be separated from each other by the empty spaces in the abrasive material as illustrated in portion 225, which generally exposes a portion of the support element 205. As can be seen in a perspective view, the
Structured abrasive has a contiguous polygonal pattern that is usually repeated. It should be noted that the portions of the pattern can be broken, forming only the localized patterns of contiguous elevated characteristics. Returning to Figures 3 to 5, various embodiments of structured abrasives are described. These figures represent the graphic representations of the real SEM photos that show, in an example form, different geometric patterns. Figure 3 shows surface features with a hexagonal shape arranged in an ordered group. Figure 4 shows generally linear surface features that have a substantially complete aspect ratio, defined as the ratio of the length of the surface feature to the next longest dimension, at this point, the width. The aspect ratios of 10, 100 or even greater are typical. Figure 5 shows a group of square surface characteristics (in horizontal cross section). As shown, each surface feature forms a pyramid, which has four larger lateral surfaces that end in a peak. The valleys between the surface features may be completely devoid of abrasive material, although in the embodiments shown, the valleys generally contain a comparatively thinner portion of the abrasive layer.
EXAMPLES
EXAMPLE 1 Off-center wet spraying of stainless steel
Tested products: Novolac Varbum 94-345 heat-adjustable powder from OxiChem was added in a designed formulation of control abrasives to evaluate the effect of heat-adjustable powder, providing thermal cure functionality to the binder formulation, in spraying performance in spray application Decentered wet. The modified and control formulations were coated on a polyester cloth substrate and processed under the same conditions to produce the designed abrasive product, which included exposure to UV radiation in a UV fusion unit. The product containing Novolac was further cured thermally at a temperature of 121 ° C for 3.5 hours. The formulations are related in Table 1.
TABLE 1
The process flow to form the embodiments herein are described in detail in the U.S. Patent. No. 5,863,306, incorporated herein by reference. Key: Ebecryl 3700: epoxy acrylate from UCB Chemicals. TMPTA: trimethylol triacrylate from UCB chemicals. Irgacure 819: phosphine oxide photoinitiator from Ciba Geiby. Varcum 29-345: Novolac powder from OxyChem. ATC- ALCOA aluminum trihydroxide with silane surface treatment A1100. A1100: aminosilane A1100 from Osi. Test machine tool: An off-center sprayer, constant feed ACME Model 47 was used for the complete test procedure. The machine consists of four main components that include the adjusting wheel, the work support blade, the contact wheel and the abrasive belt.
Work material: a group of 304 stainless steel work pieces, cylindrical 29, each measuring 3.67 centimeters x 24.5 centimeters at the start of the test. Test procedure: The products were flexed and converted into bands of 10.16 centimeters x 137.16 centimeters to test in the off-center spray. Prior to spraying any work pieces, the following parameters were checked in the machine tool: Wheel angle adjustment was adjusted to 5 °. The axes of the adjustment and contact wheel were confirmed parallel to each other. The regulating wheel and the contact wheel were coated. The rest of the working nylon was ground clean. The work guides were adjusted to allow the cleaning of suitable parts. The test procedure followed the sequence of steps indicated below: The work pieces were previously ground to remove surface defects. The weight of each piece of work was recorded. The machine was adjusted for the desired feed by 0.015 centimeters and the speed of the adjusting wheel was adjusted to 53 RPM. Two bars were passed through the machine, this was counted as a step. During the grinding of a coolant fluid containing a rust inhibitor, it is sprayed onto the abrasive belt. The weight of each piece of work was recorded to calculate the metal removed. The thickness of the band and the elongation of
the band were measured. Feeding was additionally increased by an additional 0.015 centimeters, two more rods were sent through the machine and measurements of weight, thickness, and elongation were taken again. These steps were repeated until the product was worn to the support. Test results: the formulation with the addition of the Novolac powder exhibited improved wear resistance over the control formulation. This lasted 5 steps compared to 4 for the control formulation. Even with a lower abrasive grain content than in the control, the product with Novolac powder (or similar to phenol / formaldehyde-based powders) achieved a greater stock removal. Additionally, the cutting to wear ratio for the Novolac powder product is significantly better than the control product.
TABLE 2
EXAMPLE 2: Compound sanding discs
Test products: products were tested in impurities of two sizes: 9 micras and 30 micras. For each size of impurity, a control formulation was made with a binder consisting only of resin that can be cured with UV, and a modified formulation containing a thermoadjustable powder based on acrylic was elaborated in addition to the resin that can be cured with UV. The modified and control formulations were coated on a polyethylene terephthalate film substrate and processed under the same conditions to produce the designed abrasive product, which includes exposure to UV radiation in a UV Fusion unit. The products with the thermo-adjustable powder received an additional thermal cure at a temperature of 121 ° C for 4 hours.
TABLE 3
TABLE 4 9 microns with thermo-adjustable powder
TABLE 5 control formulation of 30 microns
TABLE 6 30 microns with thermo-adjustable powder
Key: Ebecryl 3720: epoxy acrylate from UCB chemicals.
TMPTA: trimethylol triacrylate from UCB chemicals. Irgacure 819: phosphine oxide photoinitiator from Ciba-Geigy. BYK A501: BYK defoamer
Chemie A1100: aminosilane A1100 from Osi. Thermoadjustable acrylic powder: 158C121 of Ferro VEDOC powder coatings. Working materials: composite panels of 15.24 centimeters x 60.96 centimeters x 1.27 centimeters were used for the test. Equipment: the products were tested on an automated sander machine designed for test discs for random orbital sanders. The machine consists of a random orbital sander of Dynbrade mounted on an arm that alternates in a group of striking length. The machine works by starting the disc, lowering the arm to place the sander against the work piece, moving the sander back and forth on the workpiece at a set pressure and for an established amount of time, and subsequently, raising the sander away from the work piece. A scale is used to measure your weight; A surface analyzer is used to measure the surface finish; and a brightness meter is used to measure the brightness. Test procedure: it was cleaned and a dry cloth was passed to the composite panel, and its weight was recorded. The stroke length of the machine was adjusted to 50.8 centimeters and the downward force on the abrasive disk was adjusted to 453 grams. The panel was placed on the sanding machine and the machine was turned on for 1 minute. The transverse speed of the sander through
of the workpiece was approximately 10.16 cm / sec. Water is sprayed onto the surface of the solid surface panel using a spray bottle during the sanding test. After a minute of sanding on the machine, the panel was removed from the machine, cleaned with water and wiped dry. The panel was weighed and the weight loss recorded. A surface analyzer was used to register Ra, Ry and Rmax. A brightness meter was used to record the brightness reading at 20, 60 and 85 degrees. The panel was placed back on the sander, sanded for one minute, cleaned and measured. This procedure was repeated until 12 minutes of sanding was achieved on the panel.
Results of the test The results of the grind are summarized in Table 7. The formulations with the thermo-adjustable powder had significantly better wear resistance over the control formulations. The weight loss of the formulations, both 9 microns and 30 microns with the heat-adjustable powder after 12 minutes of wet sanding was only 0.1 gram compared to 7.4 and 10.6 grams respectively, for the control counterparts. The proportion G, defined as the proportion of the removal of the stocks to produce the weight loss, was also substantially improved for the formulations with the thermo-adjustable powder (125 and 43 against 0.54 and 0.77). Additionally, the products with thermoadjustable powders achieved final brightness values much
greater than the control formulations on polished solid surfaces, which is a critical performance criterion for this application. In summary, the addition of plastic powder improved the wear resistance, the G-ratio and the final gloss values of the polished solid surfaces by a surprisingly considerable amount. TABLE 7
According to the embodiments described above, the coated abrasives, and in particular, the structured or designed coated abrasives, are described having a particular binder formulation, which not only improves the processability, but also manifests itself in performance characteristics. notable as summarized above. In addition, the use of a first and second different agglutinating compounds as described in connection with the various embodiments described above, allows a better flexibility arrangement in the choice of agglutinating composition. In contrast, before the use of Vd.-functional compounds that have functional groups designed
different in a single binder compound that suffers from a reduced process flexibility and are significantly more difficult to design and implement. The subject matter of the material described above will be considered illustrative, and not restrictive, and the appended claims are intended to embrace all such modifications, improvements and other embodiments, which are within the scope of the present invention. Accordingly, to the maximum extent permitted by law, the scope of the present invention will be determined by its broader permissible interpretation of the following Claims and their equivalents, and should not be restricted or limited by the foregoing detailed description. For example, although the above makes specific reference to different agglutinating compounds that can respectively be cured by radiation or in thermal form, the binder that can be cured by relatively rapid radiation can be replaced with alternative binders. For example, a catalyst coated with fast curing epoxy that is cured rapidly by heat treatment can be used. Alternatively, a fast / blocked urethane curing catalyst that is cured rapidly by heat treatment can be used. In this regard, the first binding compound generally desirably maintains its fast curing properties, combined with the relatively slower, more robust second cure binder compound.
Claims (1)
1- A method for forming a coated abrasive product, characterized in that it comprises: mixing an agglutinating formulation with abrasive grains to form an abrasive paste, wherein the agglutinating formulation comprises a mixture of first and second agglutinating components, wherein the first binder component is it can be cured by radiation and the second binder component can be cured in thermal form and comprises a powder that functions to modify the rheological properties of the abrasive paste; coating a substrate with the abrasive paste to form a coated intermediate having an abrasive layer; irradiate the coated intermediate to cure the first binder compound; and heat treating the coated intermediate to cure the second binder compound. 2. The method according to claim 1, further characterized in that the first agglutinating component can be cured by at least one UV, microwave and e-beam radiation. 3. The method according to claim 1, further characterized in that the first agglutinating component comprises a mixture of agglutinating compounds that can be cured by UV. 4. The method according to claim 1, further characterized in that the abrasive grains comprise at least one material from the group consisting of alumina, zirconium, silicon carbide, garnet, diamond, cubic boron nitride, and combinations thereof. 5. The method according to claim 4, further characterized in that the abrasive grains comprise alpha alumina. 6. The method according to claim 1, further characterized in that the agglutinating formulation further comprises a coupling agent. 7. The method according to claim 6, further characterized in that the abrasive grains are treated with the coupling agent before being mixed with the rest of the agglutinating formulation. 8. The method according to claim 6, further characterized in that the coupling agent comprises an organosilane or an organotitanate. 9. The method according to claim 8, further characterized in that the coupling agent comprises an amino silane or methacryloxy silane. 10. The method according to claim 1, further characterized in that the substrate comprises a component of the group consisting of polymeric films, cellulosic materials and fabrics. 11. - The method according to claim 10, further characterized in that the cellulosic materials include paper, and the fabrics include cotton and polyester substrates having polymeric saturators. 12. The method according to claim 1, further characterized in that the first agglutinator is mono-curable, and the second agglutinator is mono-curable. 13. The method according to claim 1, further characterized in that the second agglutinating compound consists essentially of powder. 14. The method according to claim 1, further characterized in that the coating and irradiation are carried out in a continuous process. 15. The method according to claim 14, further characterized in that the treatment in thermal form is carried out in the continuous process. 16. The method according to claim 14, further characterized in that the continuous process is a cylinder-by-cylinder process, in which the substrate is moved during at least the coating and irradiation steps. 17. The method according to claim 14, further characterized in that the coating is performed using a tool to form the pattern of the abrasive dispersion on the substrate. 18. - The method according to claim 14, further characterized in that the thermal treatment is performed offline, the coated intermediate is in the wrapped form, and the volume is heated to effect the curing of the second binding component. 19. The method according to claim 1, further characterized in that the coating is performed in such a way that the abrasive layer has a pattern, the coated abrasive product is a structured abrasive product. 20. The method according to claim 1, further characterized in that the first binder component is a binder component that can be cured with UV. 21. The method according to claim 1, further characterized in that the UV-curable binder component is selected from the group consisting of acrylate and methacrylate oligomers and monomers which include epoxy acrylates, aliphatic urethane acrylates, aromatic urethane acrylates, polyester acrylates, aromatic acid acrylates, epoxy methacrylates, aromatic acid methacrylates, and mono, di, tri, black and pentafunctional acrylates and methacrylates. 22. The method according to claim 1, further characterized in that the second binder component comprises a thermoadjusted polymer. 23. The method according to claim 22, further characterized in that the thermoadjusted polymer comprises an epoxy resin, urethane resin, phenolic resin, urea / formaldehyde, melamine / formaldehyde, acrylic, polyester or a mixture thereof. 24. The method according to claim 19, further characterized in that the pattern comprises high surface characteristics. 25. The method according to claim 24, further characterized in that the high surface characteristics form a contiguous pattern. 26. The method according to claim 24, further characterized in that the high surface characteristics are discrete protuberances. 27. The method according to claim 17, further characterized in that the tool has a repetitive polygonal pattern, leaving a high polygonal pattern of surface characteristics on the substrate.
Applications Claiming Priority (1)
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US10809197 | 2004-03-25 |
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MXPA06010994A true MXPA06010994A (en) | 2007-04-20 |
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