CA2099179A1 - Accelerated cycloaliphatic epoxide/aromatic amine resin systems - Google Patents
Accelerated cycloaliphatic epoxide/aromatic amine resin systemsInfo
- Publication number
- CA2099179A1 CA2099179A1 CA 2099179 CA2099179A CA2099179A1 CA 2099179 A1 CA2099179 A1 CA 2099179A1 CA 2099179 CA2099179 CA 2099179 CA 2099179 A CA2099179 A CA 2099179A CA 2099179 A1 CA2099179 A1 CA 2099179A1
- Authority
- CA
- Canada
- Prior art keywords
- bis
- composition
- ether
- epoxy
- sulfone
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 150000002118 epoxides Chemical class 0.000 title claims description 27
- 150000004982 aromatic amines Chemical class 0.000 title claims description 9
- 229920005989 resin Polymers 0.000 title abstract description 19
- 239000011347 resin Substances 0.000 title abstract description 19
- 239000004848 polyfunctional curative Substances 0.000 claims abstract description 11
- 239000000203 mixture Substances 0.000 claims description 65
- -1 polyhydroxyether Polymers 0.000 claims description 21
- GHMLBKRAJCXXBS-UHFFFAOYSA-N resorcinol Chemical compound OC1=CC=CC(O)=C1 GHMLBKRAJCXXBS-UHFFFAOYSA-N 0.000 claims description 20
- WZCQRUWWHSTZEM-UHFFFAOYSA-N 1,3-phenylenediamine Chemical compound NC1=CC=CC(N)=C1 WZCQRUWWHSTZEM-UHFFFAOYSA-N 0.000 claims description 18
- 229940018564 m-phenylenediamine Drugs 0.000 claims description 18
- 239000000835 fiber Substances 0.000 claims description 17
- ADAHGVUHKDNLEB-UHFFFAOYSA-N Bis(2,3-epoxycyclopentyl)ether Chemical group C1CC2OC2C1OC1CCC2OC21 ADAHGVUHKDNLEB-UHFFFAOYSA-N 0.000 claims description 16
- VPWNQTHUCYMVMZ-UHFFFAOYSA-N 4,4'-sulfonyldiphenol Chemical compound C1=CC(O)=CC=C1S(=O)(=O)C1=CC=C(O)C=C1 VPWNQTHUCYMVMZ-UHFFFAOYSA-N 0.000 claims description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 7
- 229910052799 carbon Inorganic materials 0.000 claims description 6
- YBRVSVVVWCFQMG-UHFFFAOYSA-N 4,4'-diaminodiphenylmethane Chemical compound C1=CC(N)=CC=C1CC1=CC=C(N)C=C1 YBRVSVVVWCFQMG-UHFFFAOYSA-N 0.000 claims description 5
- 239000011521 glass Substances 0.000 claims description 4
- 239000004760 aramid Substances 0.000 claims description 3
- 229920003235 aromatic polyamide Polymers 0.000 claims description 3
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- ZXDDPOHVAMWLBH-UHFFFAOYSA-N 2,4-Dihydroxybenzophenone Chemical compound OC1=CC(O)=CC=C1C(=O)C1=CC=CC=C1 ZXDDPOHVAMWLBH-UHFFFAOYSA-N 0.000 claims description 2
- PISLZQACAJMAIO-UHFFFAOYSA-N 2,4-diethyl-6-methylbenzene-1,3-diamine Chemical compound CCC1=CC(C)=C(N)C(CC)=C1N PISLZQACAJMAIO-UHFFFAOYSA-N 0.000 claims description 2
- CKOFBUUFHALZGK-UHFFFAOYSA-N 3-[(3-aminophenyl)methyl]aniline Chemical compound NC1=CC=CC(CC=2C=C(N)C=CC=2)=C1 CKOFBUUFHALZGK-UHFFFAOYSA-N 0.000 claims description 2
- DKKYOQYISDAQER-UHFFFAOYSA-N 3-[3-(3-aminophenoxy)phenoxy]aniline Chemical compound NC1=CC=CC(OC=2C=C(OC=3C=C(N)C=CC=3)C=CC=2)=C1 DKKYOQYISDAQER-UHFFFAOYSA-N 0.000 claims description 2
- RXNYJUSEXLAVNQ-UHFFFAOYSA-N 4,4'-Dihydroxybenzophenone Chemical compound C1=CC(O)=CC=C1C(=O)C1=CC=C(O)C=C1 RXNYJUSEXLAVNQ-UHFFFAOYSA-N 0.000 claims description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims description 2
- 239000004952 Polyamide Substances 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- 229910002804 graphite Inorganic materials 0.000 claims description 2
- 239000010439 graphite Substances 0.000 claims description 2
- 229920002647 polyamide Polymers 0.000 claims description 2
- CBCKQZAAMUWICA-UHFFFAOYSA-N 1,4-phenylenediamine Chemical compound NC1=CC=C(N)C=C1 CBCKQZAAMUWICA-UHFFFAOYSA-N 0.000 claims 1
- WCXGOVYROJJXHA-UHFFFAOYSA-N 3-[4-[4-(3-aminophenoxy)phenyl]sulfonylphenoxy]aniline Chemical compound NC1=CC=CC(OC=2C=CC(=CC=2)S(=O)(=O)C=2C=CC(OC=3C=C(N)C=CC=3)=CC=2)=C1 WCXGOVYROJJXHA-UHFFFAOYSA-N 0.000 claims 1
- ICNFHJVPAJKPHW-UHFFFAOYSA-N 4,4'-Thiodianiline Chemical compound C1=CC(N)=CC=C1SC1=CC=C(N)C=C1 ICNFHJVPAJKPHW-UHFFFAOYSA-N 0.000 claims 1
- RQCACQIALULDSK-UHFFFAOYSA-N 4-(4-hydroxyphenyl)sulfinylphenol Chemical compound C1=CC(O)=CC=C1S(=O)C1=CC=C(O)C=C1 RQCACQIALULDSK-UHFFFAOYSA-N 0.000 claims 1
- HLBLWEWZXPIGSM-UHFFFAOYSA-N 4-Aminophenyl ether Chemical compound C1=CC(N)=CC=C1OC1=CC=C(N)C=C1 HLBLWEWZXPIGSM-UHFFFAOYSA-N 0.000 claims 1
- AJYDKROUZBIMLE-UHFFFAOYSA-N 4-[2-[2-[2-(4-aminophenoxy)phenyl]propan-2-yl]phenoxy]aniline Chemical compound C=1C=CC=C(OC=2C=CC(N)=CC=2)C=1C(C)(C)C1=CC=CC=C1OC1=CC=C(N)C=C1 AJYDKROUZBIMLE-UHFFFAOYSA-N 0.000 claims 1
- WUPRYUDHUFLKFL-UHFFFAOYSA-N 4-[3-(4-aminophenoxy)phenoxy]aniline Chemical compound C1=CC(N)=CC=C1OC1=CC=CC(OC=2C=CC(N)=CC=2)=C1 WUPRYUDHUFLKFL-UHFFFAOYSA-N 0.000 claims 1
- JCRRFJIVUPSNTA-UHFFFAOYSA-N 4-[4-(4-aminophenoxy)phenoxy]aniline Chemical compound C1=CC(N)=CC=C1OC(C=C1)=CC=C1OC1=CC=C(N)C=C1 JCRRFJIVUPSNTA-UHFFFAOYSA-N 0.000 claims 1
- MQJKPEGWNLWLTK-UHFFFAOYSA-N Dapsone Chemical compound C1=CC(N)=CC=C1S(=O)(=O)C1=CC=C(N)C=C1 MQJKPEGWNLWLTK-UHFFFAOYSA-N 0.000 claims 1
- ZFVMWEVVKGLCIJ-UHFFFAOYSA-N bisphenol AF Chemical compound C1=CC(O)=CC=C1C(C(F)(F)F)(C(F)(F)F)C1=CC=C(O)C=C1 ZFVMWEVVKGLCIJ-UHFFFAOYSA-N 0.000 claims 1
- 229920002492 poly(sulfone) Polymers 0.000 claims 1
- 239000002131 composite material Substances 0.000 abstract description 7
- 239000011353 cycloaliphatic epoxy resin Substances 0.000 abstract description 3
- 125000003118 aryl group Chemical group 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 abstract 1
- IISBACLAFKSPIT-UHFFFAOYSA-N bisphenol A Chemical compound C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 IISBACLAFKSPIT-UHFFFAOYSA-N 0.000 description 19
- 239000004593 Epoxy Substances 0.000 description 18
- 238000005266 casting Methods 0.000 description 18
- 239000000243 solution Substances 0.000 description 17
- 229920000647 polyepoxide Polymers 0.000 description 13
- 150000001412 amines Chemical class 0.000 description 12
- 239000003822 epoxy resin Substances 0.000 description 11
- 229940106691 bisphenol a Drugs 0.000 description 9
- 150000001875 compounds Chemical class 0.000 description 9
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 8
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 8
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 8
- 150000003457 sulfones Chemical class 0.000 description 8
- 229910052757 nitrogen Inorganic materials 0.000 description 7
- 239000000126 substance Substances 0.000 description 7
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 6
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 5
- 239000004841 bisphenol A epoxy resin Substances 0.000 description 5
- 229920001577 copolymer Polymers 0.000 description 5
- 238000009472 formulation Methods 0.000 description 5
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 5
- 150000002500 ions Chemical class 0.000 description 5
- 229920000642 polymer Polymers 0.000 description 5
- XKZQKPRCPNGNFR-UHFFFAOYSA-N 2-(3-hydroxyphenyl)phenol Chemical compound OC1=CC=CC(C=2C(=CC=CC=2)O)=C1 XKZQKPRCPNGNFR-UHFFFAOYSA-N 0.000 description 4
- KUBDPQJOLOUJRM-UHFFFAOYSA-N 2-(chloromethyl)oxirane;4-[2-(4-hydroxyphenyl)propan-2-yl]phenol Chemical compound ClCC1CO1.C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 KUBDPQJOLOUJRM-UHFFFAOYSA-N 0.000 description 4
- QIGBRXMKCJKVMJ-UHFFFAOYSA-N Hydroquinone Chemical compound OC1=CC=C(O)C=C1 QIGBRXMKCJKVMJ-UHFFFAOYSA-N 0.000 description 4
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 4
- VCCBEIPGXKNHFW-UHFFFAOYSA-N biphenyl-4,4'-diol Chemical compound C1=CC(O)=CC=C1C1=CC=C(O)C=C1 VCCBEIPGXKNHFW-UHFFFAOYSA-N 0.000 description 4
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000003921 oil Substances 0.000 description 4
- KJFMBFZCATUALV-UHFFFAOYSA-N phenolphthalein Chemical compound C1=CC(O)=CC=C1C1(C=2C=CC(O)=CC=2)C2=CC=CC=C2C(=O)O1 KJFMBFZCATUALV-UHFFFAOYSA-N 0.000 description 4
- 230000002787 reinforcement Effects 0.000 description 4
- 229920001169 thermoplastic Polymers 0.000 description 4
- OECTYKWYRCHAKR-UHFFFAOYSA-N 4-vinylcyclohexene dioxide Chemical compound C1OC1C1CC2OC2CC1 OECTYKWYRCHAKR-UHFFFAOYSA-N 0.000 description 3
- 229920003319 Araldite® Polymers 0.000 description 3
- OWYWGLHRNBIFJP-UHFFFAOYSA-N Ipazine Chemical compound CCN(CC)C1=NC(Cl)=NC(NC(C)C)=N1 OWYWGLHRNBIFJP-UHFFFAOYSA-N 0.000 description 3
- 239000005062 Polybutadiene Substances 0.000 description 3
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 3
- 239000000654 additive Substances 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 150000004985 diamines Chemical class 0.000 description 3
- 239000003085 diluting agent Substances 0.000 description 3
- 125000003055 glycidyl group Chemical group C(C1CO1)* 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 229920003986 novolac Polymers 0.000 description 3
- 150000002989 phenols Chemical class 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 229920001187 thermosetting polymer Polymers 0.000 description 3
- VDFVNEFVBPFDSB-UHFFFAOYSA-N 1,3-dioxane Chemical compound C1COCOC1 VDFVNEFVBPFDSB-UHFFFAOYSA-N 0.000 description 2
- VWGKEVWFBOUAND-UHFFFAOYSA-N 4,4'-thiodiphenol Chemical compound C1=CC(O)=CC=C1SC1=CC=C(O)C=C1 VWGKEVWFBOUAND-UHFFFAOYSA-N 0.000 description 2
- YXALYBMHAYZKAP-UHFFFAOYSA-N 7-oxabicyclo[4.1.0]heptan-4-ylmethyl 7-oxabicyclo[4.1.0]heptane-4-carboxylate Chemical compound C1CC2OC2CC1C(=O)OCC1CC2OC2CC1 YXALYBMHAYZKAP-UHFFFAOYSA-N 0.000 description 2
- KAKZBPTYRLMSJV-UHFFFAOYSA-N Butadiene Chemical compound C=CC=C KAKZBPTYRLMSJV-UHFFFAOYSA-N 0.000 description 2
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- XDTMQSROBMDMFD-UHFFFAOYSA-N Cyclohexane Chemical compound C1CCCCC1 XDTMQSROBMDMFD-UHFFFAOYSA-N 0.000 description 2
- KWYHDKDOAIKMQN-UHFFFAOYSA-N N,N,N',N'-tetramethylethylenediamine Chemical compound CN(C)CCN(C)C KWYHDKDOAIKMQN-UHFFFAOYSA-N 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- KKEYFWRCBNTPAC-UHFFFAOYSA-N Terephthalic acid Chemical compound OC(=O)C1=CC=C(C(O)=O)C=C1 KKEYFWRCBNTPAC-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 125000000217 alkyl group Chemical group 0.000 description 2
- 150000001414 amino alcohols Chemical class 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000009734 composite fabrication Methods 0.000 description 2
- KZTYYGOKRVBIMI-UHFFFAOYSA-N diphenyl sulfone Chemical compound C=1C=CC=CC=1S(=O)(=O)C1=CC=CC=C1 KZTYYGOKRVBIMI-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 235000011187 glycerol Nutrition 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 150000002483 hydrogen compounds Chemical class 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- OIPPWFOQEKKFEE-UHFFFAOYSA-N orcinol Chemical compound CC1=CC(O)=CC(O)=C1 OIPPWFOQEKKFEE-UHFFFAOYSA-N 0.000 description 2
- QQVIHTHCMHWDBS-UHFFFAOYSA-N perisophthalic acid Natural products OC(=O)C1=CC=CC(C(O)=O)=C1 QQVIHTHCMHWDBS-UHFFFAOYSA-N 0.000 description 2
- 229920000090 poly(aryl ether) Polymers 0.000 description 2
- 229920002857 polybutadiene Polymers 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000001294 propane Substances 0.000 description 2
- YPFDHNVEDLHUCE-UHFFFAOYSA-N propane-1,3-diol Chemical compound OCCCO YPFDHNVEDLHUCE-UHFFFAOYSA-N 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 125000000020 sulfo group Chemical group O=S(=O)([*])O[H] 0.000 description 2
- 238000004046 wet winding Methods 0.000 description 2
- GHPYJLCQYMAXGG-WCCKRBBISA-N (2R)-2-amino-3-(2-boronoethylsulfanyl)propanoic acid hydrochloride Chemical compound Cl.N[C@@H](CSCCB(O)O)C(O)=O GHPYJLCQYMAXGG-WCCKRBBISA-N 0.000 description 1
- RDEIXVOBVLKYNT-VQBXQJRRSA-N (2r,3r,4r,5r)-2-[(1s,2s,3r,4s,6r)-4,6-diamino-3-[(2r,3r,6s)-3-amino-6-(1-aminoethyl)oxan-2-yl]oxy-2-hydroxycyclohexyl]oxy-5-methyl-4-(methylamino)oxane-3,5-diol;(2r,3r,4r,5r)-2-[(1s,2s,3r,4s,6r)-4,6-diamino-3-[(2r,3r,6s)-3-amino-6-(aminomethyl)oxan-2-yl]o Chemical compound OS(O)(=O)=O.O1C[C@@](O)(C)[C@H](NC)[C@@H](O)[C@H]1O[C@@H]1[C@@H](O)[C@H](O[C@@H]2[C@@H](CC[C@@H](CN)O2)N)[C@@H](N)C[C@H]1N.O1C[C@@](O)(C)[C@H](NC)[C@@H](O)[C@H]1O[C@@H]1[C@@H](O)[C@H](O[C@@H]2[C@@H](CC[C@H](O2)C(C)N)N)[C@@H](N)C[C@H]1N.O1[C@H](C(C)NC)CC[C@@H](N)[C@H]1O[C@H]1[C@H](O)[C@@H](O[C@@H]2[C@@H]([C@@H](NC)[C@@](C)(O)CO2)O)[C@H](N)C[C@@H]1N RDEIXVOBVLKYNT-VQBXQJRRSA-N 0.000 description 1
- NSGXIBWMJZWTPY-UHFFFAOYSA-N 1,1,1,3,3,3-hexafluoropropane Chemical compound FC(F)(F)CC(F)(F)F NSGXIBWMJZWTPY-UHFFFAOYSA-N 0.000 description 1
- BCMCBBGGLRIHSE-UHFFFAOYSA-N 1,3-benzoxazole Chemical compound C1=CC=C2OC=NC2=C1 BCMCBBGGLRIHSE-UHFFFAOYSA-N 0.000 description 1
- HYZJCKYKOHLVJF-UHFFFAOYSA-N 1H-benzimidazole Chemical compound C1=CC=C2NC=NC2=C1 HYZJCKYKOHLVJF-UHFFFAOYSA-N 0.000 description 1
- VILCJCGEZXAXTO-UHFFFAOYSA-N 2,2,2-tetramine Chemical compound NCCNCCNCCN VILCJCGEZXAXTO-UHFFFAOYSA-N 0.000 description 1
- JHOPNNNTBHXSHY-UHFFFAOYSA-N 2-(4-hydroxyphenyl)phenol Chemical compound C1=CC(O)=CC=C1C1=CC=CC=C1O JHOPNNNTBHXSHY-UHFFFAOYSA-N 0.000 description 1
- HHRACYLRBOUBKM-UHFFFAOYSA-N 2-[(4-tert-butylphenoxy)methyl]oxirane Chemical compound C1=CC(C(C)(C)C)=CC=C1OCC1OC1 HHRACYLRBOUBKM-UHFFFAOYSA-N 0.000 description 1
- TZLVUWBGUNVFES-UHFFFAOYSA-N 2-ethyl-5-methylpyrazol-3-amine Chemical compound CCN1N=C(C)C=C1N TZLVUWBGUNVFES-UHFFFAOYSA-N 0.000 description 1
- GRWFFFOEIHGUBG-UHFFFAOYSA-N 3,4-Epoxy-6-methylcyclohexylmethyl-3,4-epoxy-6-methylcyclo-hexanecarboxylate Chemical compound C1C2OC2CC(C)C1C(=O)OCC1CC2OC2CC1C GRWFFFOEIHGUBG-UHFFFAOYSA-N 0.000 description 1
- ISPWSRVEMSGMKS-UHFFFAOYSA-N 3-[[3-hydroxypropyl(dimethyl)silyl]oxy-dimethylsilyl]propan-1-ol Chemical compound OCCC[Si](C)(C)O[Si](C)(C)CCCO ISPWSRVEMSGMKS-UHFFFAOYSA-N 0.000 description 1
- 229940018563 3-aminophenol Drugs 0.000 description 1
- ZRYCRPNCXLQHPN-UHFFFAOYSA-N 3-hydroxy-2-methylbenzaldehyde Chemical compound CC1=C(O)C=CC=C1C=O ZRYCRPNCXLQHPN-UHFFFAOYSA-N 0.000 description 1
- GPAPPPVRLPGFEQ-UHFFFAOYSA-N 4,4'-dichlorodiphenyl sulfone Chemical compound C1=CC(Cl)=CC=C1S(=O)(=O)C1=CC=C(Cl)C=C1 GPAPPPVRLPGFEQ-UHFFFAOYSA-N 0.000 description 1
- ODJUOZPKKHIEOZ-UHFFFAOYSA-N 4-[2-(4-hydroxy-3,5-dimethylphenyl)propan-2-yl]-2,6-dimethylphenol Chemical compound CC1=C(O)C(C)=CC(C(C)(C)C=2C=C(C)C(O)=C(C)C=2)=C1 ODJUOZPKKHIEOZ-UHFFFAOYSA-N 0.000 description 1
- WFCQTAXSWSWIHS-UHFFFAOYSA-N 4-[bis(4-hydroxyphenyl)methyl]phenol Chemical compound C1=CC(O)=CC=C1C(C=1C=CC(O)=CC=1)C1=CC=C(O)C=C1 WFCQTAXSWSWIHS-UHFFFAOYSA-N 0.000 description 1
- RZJKZTPKSRPUFJ-UHFFFAOYSA-N 5,5-dimethyl-1,3-bis(oxiran-2-ylmethyl)imidazolidine-2,4-dione Chemical compound O=C1N(CC2OC2)C(=O)C(C)(C)N1CC1CO1 RZJKZTPKSRPUFJ-UHFFFAOYSA-N 0.000 description 1
- RBHIUNHSNSQJNG-UHFFFAOYSA-N 6-methyl-3-(2-methyloxiran-2-yl)-7-oxabicyclo[4.1.0]heptane Chemical compound C1CC2(C)OC2CC1C1(C)CO1 RBHIUNHSNSQJNG-UHFFFAOYSA-N 0.000 description 1
- NHJIDZUQMHKGRE-UHFFFAOYSA-N 7-oxabicyclo[4.1.0]heptan-4-yl 2-(7-oxabicyclo[4.1.0]heptan-4-yl)acetate Chemical compound C1CC2OC2CC1OC(=O)CC1CC2OC2CC1 NHJIDZUQMHKGRE-UHFFFAOYSA-N 0.000 description 1
- OXQXGKNECHBVMO-UHFFFAOYSA-N 7-oxabicyclo[4.1.0]heptane-4-carboxylic acid Chemical compound C1C(C(=O)O)CCC2OC21 OXQXGKNECHBVMO-UHFFFAOYSA-N 0.000 description 1
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical compound C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 1
- 229920001342 Bakelite® Polymers 0.000 description 1
- 229930185605 Bisphenol Natural products 0.000 description 1
- 229920013683 Celanese Polymers 0.000 description 1
- 241000736839 Chara Species 0.000 description 1
- OPFTUNCRGUEPRZ-QLFBSQMISA-N Cyclohexane Natural products CC(=C)[C@@H]1CC[C@@](C)(C=C)[C@H](C(C)=C)C1 OPFTUNCRGUEPRZ-QLFBSQMISA-N 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- JIGUQPWFLRLWPJ-UHFFFAOYSA-N Ethyl acrylate Chemical compound CCOC(=O)C=C JIGUQPWFLRLWPJ-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-M Methacrylate Chemical compound CC(=C)C([O-])=O CERQOIWHTDAKMF-UHFFFAOYSA-M 0.000 description 1
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 229920002292 Nylon 6 Polymers 0.000 description 1
- 229920002302 Nylon 6,6 Polymers 0.000 description 1
- FQYUMYWMJTYZTK-UHFFFAOYSA-N Phenyl glycidyl ether Chemical compound C1OC1COC1=CC=CC=C1 FQYUMYWMJTYZTK-UHFFFAOYSA-N 0.000 description 1
- 239000004734 Polyphenylene sulfide Substances 0.000 description 1
- 239000004793 Polystyrene Substances 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 239000004963 Torlon Substances 0.000 description 1
- 229920003997 Torlon® Polymers 0.000 description 1
- ZJCCRDAZUWHFQH-UHFFFAOYSA-N Trimethylolpropane Chemical compound CCC(CO)(CO)CO ZJCCRDAZUWHFQH-UHFFFAOYSA-N 0.000 description 1
- 239000004955 Trogamid T Substances 0.000 description 1
- 229920004738 ULTEM® Polymers 0.000 description 1
- NIYNIOYNNFXGFN-UHFFFAOYSA-N [4-(hydroxymethyl)cyclohexyl]methanol;7-oxabicyclo[4.1.0]heptane-4-carboxylic acid Chemical compound OCC1CCC(CO)CC1.C1C(C(=O)O)CCC2OC21.C1C(C(=O)O)CCC2OC21 NIYNIOYNNFXGFN-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- WNLRTRBMVRJNCN-UHFFFAOYSA-L adipate(2-) Chemical compound [O-]C(=O)CCCCC([O-])=O WNLRTRBMVRJNCN-UHFFFAOYSA-L 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- RREGISFBPQOLTM-UHFFFAOYSA-N alumane;trihydrate Chemical compound O.O.O.[AlH3] RREGISFBPQOLTM-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 239000004637 bakelite Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- HFACYLZERDEVSX-UHFFFAOYSA-N benzidine Chemical group C1=CC(N)=CC=C1C1=CC=C(N)C=C1 HFACYLZERDEVSX-UHFFFAOYSA-N 0.000 description 1
- JRPRCOLKIYRSNH-UHFFFAOYSA-N bis(oxiran-2-ylmethyl) benzene-1,2-dicarboxylate Chemical compound C=1C=CC=C(C(=O)OCC2OC2)C=1C(=O)OCC1CO1 JRPRCOLKIYRSNH-UHFFFAOYSA-N 0.000 description 1
- ZXOATMQSUNJNNG-UHFFFAOYSA-N bis(oxiran-2-ylmethyl) benzene-1,3-dicarboxylate Chemical compound C=1C=CC(C(=O)OCC2OC2)=CC=1C(=O)OCC1CO1 ZXOATMQSUNJNNG-UHFFFAOYSA-N 0.000 description 1
- KBWLNCUTNDKMPN-UHFFFAOYSA-N bis(oxiran-2-ylmethyl) hexanedioate Chemical compound C1OC1COC(=O)CCCCC(=O)OCC1CO1 KBWLNCUTNDKMPN-UHFFFAOYSA-N 0.000 description 1
- CDQSJQSWAWPGKG-UHFFFAOYSA-N butane-1,1-diol Chemical compound CCCC(O)O CDQSJQSWAWPGKG-UHFFFAOYSA-N 0.000 description 1
- 125000000484 butyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 150000001735 carboxylic acids Chemical class 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 229920006026 co-polymeric resin Polymers 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000006482 condensation reaction Methods 0.000 description 1
- 229920006037 cross link polymer Polymers 0.000 description 1
- 150000007973 cyanuric acids Chemical class 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 150000001991 dicarboxylic acids Chemical class 0.000 description 1
- 150000001993 dienes Chemical class 0.000 description 1
- HPNMFZURTQLUMO-UHFFFAOYSA-N diethylamine Chemical compound CCNCC HPNMFZURTQLUMO-UHFFFAOYSA-N 0.000 description 1
- GYZLOYUZLJXAJU-UHFFFAOYSA-N diglycidyl ether Chemical compound C1OC1COCC1CO1 GYZLOYUZLJXAJU-UHFFFAOYSA-N 0.000 description 1
- IJRJBQGVWNVZSA-UHFFFAOYSA-N dilC18(3)(1+) Chemical compound CC1(C)C2=CC=CC=C2N(CCCCCCCCCCCCCCCCCC)C1=CC=CC1=[N+](CCCCCCCCCCCCCCCCCC)C2=CC=CC=C2C1(C)C IJRJBQGVWNVZSA-UHFFFAOYSA-N 0.000 description 1
- MCWXGJITAZMZEV-UHFFFAOYSA-N dimethoate Chemical compound CNC(=O)CSP(=S)(OC)OC MCWXGJITAZMZEV-UHFFFAOYSA-N 0.000 description 1
- 150000002009 diols Chemical class 0.000 description 1
- 238000005485 electric heating Methods 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 238000006735 epoxidation reaction Methods 0.000 description 1
- 125000003700 epoxy group Chemical group 0.000 description 1
- 150000002148 esters Chemical class 0.000 description 1
- 150000002170 ethers Chemical class 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 238000009730 filament winding Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- SLGWESQGEUXWJQ-UHFFFAOYSA-N formaldehyde;phenol Chemical class O=C.OC1=CC=CC=C1 SLGWESQGEUXWJQ-UHFFFAOYSA-N 0.000 description 1
- 229910021485 fumed silica Inorganic materials 0.000 description 1
- 238000001879 gelation Methods 0.000 description 1
- VOZRXNHHFUQHIL-UHFFFAOYSA-N glycidyl methacrylate Chemical compound CC(=C)C(=O)OCC1CO1 VOZRXNHHFUQHIL-UHFFFAOYSA-N 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 150000001469 hydantoins Chemical class 0.000 description 1
- WGCNASOHLSPBMP-UHFFFAOYSA-N hydroxyacetaldehyde Natural products OCC=O WGCNASOHLSPBMP-UHFFFAOYSA-N 0.000 description 1
- RGXCTRIQQODGIZ-UHFFFAOYSA-O isodesmosine Chemical compound OC(=O)C(N)CCCC[N+]1=CC(CCC(N)C(O)=O)=CC(CCC(N)C(O)=O)=C1CCCC(N)C(O)=O RGXCTRIQQODGIZ-UHFFFAOYSA-O 0.000 description 1
- 238000004811 liquid chromatography Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 229910052751 metal Chemical class 0.000 description 1
- 239000002184 metal Chemical class 0.000 description 1
- KOARAHKGQSHYGJ-UHFFFAOYSA-N methyl 2-methylprop-2-enoate;oxiran-2-ylmethyl prop-2-enoate Chemical compound COC(=O)C(C)=C.C=CC(=O)OCC1CO1 KOARAHKGQSHYGJ-UHFFFAOYSA-N 0.000 description 1
- 125000000250 methylamino group Chemical group [H]N(*)C([H])([H])[H] 0.000 description 1
- 239000010445 mica Substances 0.000 description 1
- 229910052618 mica group Inorganic materials 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- QYYJKPCROQHRJJ-UHFFFAOYSA-N n',n'-bis(oxiran-2-ylmethyl)oxamide Chemical class C1OC1CN(C(=O)C(=O)N)CC1CO1 QYYJKPCROQHRJJ-UHFFFAOYSA-N 0.000 description 1
- JAYXSROKFZAHRQ-UHFFFAOYSA-N n,n-bis(oxiran-2-ylmethyl)aniline Chemical compound C1OC1CN(C=1C=CC=CC=1)CC1CO1 JAYXSROKFZAHRQ-UHFFFAOYSA-N 0.000 description 1
- UMRZSTCPUPJPOJ-KNVOCYPGSA-N norbornane Chemical compound C1C[C@H]2CC[C@@H]1C2 UMRZSTCPUPJPOJ-KNVOCYPGSA-N 0.000 description 1
- 238000007339 nucleophilic aromatic substitution reaction Methods 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000002674 ointment Substances 0.000 description 1
- YPNZYYWORCABPU-UHFFFAOYSA-N oxiran-2-ylmethyl 2-methylprop-2-enoate;styrene Chemical compound C=CC1=CC=CC=C1.CC(=C)C(=O)OCC1CO1 YPNZYYWORCABPU-UHFFFAOYSA-N 0.000 description 1
- RPQRDASANLAFCM-UHFFFAOYSA-N oxiran-2-ylmethyl prop-2-enoate Chemical compound C=CC(=O)OCC1CO1 RPQRDASANLAFCM-UHFFFAOYSA-N 0.000 description 1
- WXZMFSXDPGVJKK-UHFFFAOYSA-N pentaerythritol Chemical compound OCC(CO)(CO)CO WXZMFSXDPGVJKK-UHFFFAOYSA-N 0.000 description 1
- PNJWIWWMYCMZRO-UHFFFAOYSA-N pent‐4‐en‐2‐one Natural products CC(=O)CC=C PNJWIWWMYCMZRO-UHFFFAOYSA-N 0.000 description 1
- 229920002863 poly(1,4-phenylene oxide) polymer Polymers 0.000 description 1
- 229920002239 polyacrylonitrile Polymers 0.000 description 1
- 229920001230 polyarylate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 150000004291 polyenes Chemical class 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920001601 polyetherimide Polymers 0.000 description 1
- 229920005862 polyol Polymers 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 150000003077 polyols Chemical class 0.000 description 1
- 229920006324 polyoxymethylene Polymers 0.000 description 1
- 229920000069 polyphenylene sulfide Polymers 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 239000004800 polyvinyl chloride Substances 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 238000004382 potting Methods 0.000 description 1
- 125000001436 propyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000000565 sealant Substances 0.000 description 1
- 229920002050 silicone resin Polymers 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 150000005846 sugar alcohols Polymers 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- KKEYFWRCBNTPAC-UHFFFAOYSA-L terephthalate(2-) Chemical compound [O-]C(=O)C1=CC=C(C([O-])=O)C=C1 KKEYFWRCBNTPAC-UHFFFAOYSA-L 0.000 description 1
- 229920001897 terpolymer Polymers 0.000 description 1
- 125000000383 tetramethylene group Chemical group [H]C([H])([*:1])C([H])([H])C([H])([H])C([H])([H])[*:2] 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 150000003568 thioethers Chemical class 0.000 description 1
- 239000013008 thixotropic agent Substances 0.000 description 1
- 150000004992 toluidines Chemical class 0.000 description 1
- 238000001721 transfer moulding Methods 0.000 description 1
- 238000009756 wet lay-up Methods 0.000 description 1
Landscapes
- Compositions Of Macromolecular Compounds (AREA)
- Epoxy Resins (AREA)
Abstract
ABSTRACT
High modulus matrix resins for composites comprising a cycloaliphatic epoxy resin, an aromatic diamirle hardener and a particular cure accelerator.
94, 342
High modulus matrix resins for composites comprising a cycloaliphatic epoxy resin, an aromatic diamirle hardener and a particular cure accelerator.
94, 342
Description
9~79 ACCELERATED CYCLOAL I PHAT I C
EPOXIDE~AF~OMATIC AMINE RESIN SYSTEMS
B~CKGROIJND OF THE INVENTION
~ mine curable epoxy resin formulations are widely used as coatings, adhesi~es, sealants, and matrices for fiber-reinforced composites. For many applications, a ~ast rate of cure is desira~le.
Many additives have been tested as cure accelerators for epoxy/amine mixtures. Several references teach that additives with phenolic hydroxyl groups are efEective with epoxy resins derived from epihalohydrins and active hydrogen compounds, such as bisphenol A epoxy resins. For example, Shechter et al in Industrial and Engineering Chemistry, Volume g~, No. 1, pages 94 to 97, 1956, disclosed that phenol was more effectiv0 than aliphatic alcohols in accelerating the reaction of phenyl glycidyl ether with diethylamine. ~owen et al in the American Che~ical Society Advances in Chemistry Series, Volume 92, pages 48 to 59, 1970, disclosed that a variety of hydroxyl containing compounds decreased ~he gel time of a bisphenol A
epoxy~triethylenetetramine mixture. ~owen et al disclosed tha~ 4,4'-dihydroxydiphenyl sulfone, glycerin, phenol, ~etrabromobisphenol A, and bisphenol A a~celerated the cure with a similar degree of effectiveness.
Epoxy compositions containing resorcinol are described in the prior art. For example, Gough et al lin ~he Journ~l of Oil and Color Chemists 2099~79 Association, volume 43, pages 409 to 418, 1961), Nagy (in Adhesive~ Age, pages 20 to 27, April, 1967), and Parten~ky (in the American Chemical Society Advances in Chemistry S~ries, Volume 92, pages 29 to 47, 1970~ disclo~ed that resorcinol and many other phenolic compounds accelerate the cure of glycidyl epoxy/amine mixture~. Markovitz in "Chemical Properties of Crosslinked Polymers,"
American Chemical Society 5ympo~ium 1976, S.S.
Labana, Ed., page~ 49 to 58 described curable compositions containing cycloaliphatic epoxides, resorcinol and metal salts as coaccelerator~. No reference was found to cycloaliphatic epoxide/aromatic amine mixtures containing resorcinol as an accelerator.
In many epoxy/amine formulations, cycloaliphatic epoxides ar~ used as the epoxy component ~ince they impart improved mechanical and thermal properties to the cured compositions. For example, unreinforced castings of bis(2,3-epoxy-cyclopentyl) ether cured with m-phenylenediamine have tensile strengths and tensile ~oduli which are among ~he highes~ of any ~hermosetting material.
Similarly, as described by McLean et. al. in Report No. 14450 of the National Research Council o ~9917~
Canada, November, 1974, high mechanical properties can be achieve~ in unreinforced castings made by curing 3,4-epoxycyclohexylmethyl 3,4-epoxycyclohexane carboxylate with methylene dianiline. ~owever, resin systems containing bis(2,3-epoxycyclopentyl) ether or 3,4-epoxycyclohexylmethyl 3,~-epoxycyclohexane carboxylate cure more slowly with aromatic amines than ~imilar compositions containing bisphenol A
epoxy resins. This characteristic limit~ their utility in composite fabrication processe6 such as filament winding and reaction injection moldi~g.
Thus ~here i~ a need for cure accelerators for cycloaliphatic epoxide/amine re~in systems2 Moreover~ in commercial practîce it is desirable that the mixture of the accelerator and epoxy resin have good storage stability in the absence of the amine hardener. Thi~ chara~,teri~tic fa~ ta~es handling in a production environment.
It has now been found that a select group of phenolic compounds are highly effec~ive cure accelera~ors for cycloaliphatic/aromatic amine resin sy~tems. Under a fixed cure schedule, the accelerated compositions afford improved properties compared to compositions which do not contain the accelerator, ~uch as higher mechanical propereies and/or increased heat deflection temperature~ in unreinforced ca6tings.
~ urther~ a method for accelerating the cure of cycloaliphatic epoxide/aromatic amine mixture6 at low temperatures has been found which comprises adding a 601id solution of a high melting 20~9~7C3 _ 4 accelerator in a low melting solid cycloaliphatic epoxy resin.
THE INVENTION
This invention is directed to a compo~ition comprising:
ta) a cycloaliphatic epoxy resin containing two or more epoxide groups, (b) an aromatic amine hardener, and (c) a cure accelerator selected from (i) HO ~ ~ ~ ~ and/or HO OH
(ii) Ra ~
wherein ~ is selected from SO2, SO, OH O O
C(CF3)2, CN, C, CO, R i~ selected from haloyen O ;.
or alkyl of 1 to 4 carb~n at.om~, or ~ C.-and a i~ O
to ~.
The composition may optionally contain a thermoplastic polymer and/or a s~ructural ~iber.
The preferred cure accelerator~ are one or more of the following: 4,4'-dihydroxydiphenyl sulfone, re~orcinol, 2,2-bis(~-hydroxyphenyl~
hexafluoropropane, 4,4~-dihydroxydiphenyl sulfo~ide, 2,4 dihydroxybenzophenone, 4,4'-dihydroxybenzophenone, and 4,4'-dihydroxy-3,3-dichlorodiphenyl sulone.
2 ~ 7 ~
~ 5 --The cycloaliphatic epoxide~ of ~his invention are prepared by epoxidation of dienes or polyenes. Resin~ of this type include bi~(2,3-epoxycyclopentyl) ~her, I, ~~ ~
I II
reaction products of I with e~hylene glycol which are described in U.S. Patent 3,398,102, 5(6)-glycidyl-2-(1,2-epoxyethyl)bicyclo[2.2.1]
heptane, II, and dicyclopentadiene diepoxide~
Commercial examples o these epoxides include vinyl cyclohexene diepoxide. e.g., "ERL-4206" (obtained from Union Carbide Corp.), 3,g-epoxycyclohexylmethyl 3,4-epoxycyclohexane carboxylate, e.g., "ERL-4221 (obtained from Union Carbide Corp.) t 3,4-epoxy-6-methylcyclohexylmethyl 3,4-epoxy-6-methyl-cyclohexane carboxylate, e.g., ~'ER~-4201" (obtained from Union Carbide Corp.), bis(3,4-epoxycyclo-hexylme~yl)adipa~e, e.g., "ERL-4299" ~obtained from Union Carbide Corp.), dipentene dioxide, e.g., "ERL-4269~' (obtained from Union Carbide Corp.~
2-(3,q-epoxycyclohexyl-5,5-spiro-3,4-epoxy)cyclo-hexane meta-dioxane, e.g., "ERL-4234" (obtained from Union Carbide Corp.) and epoxidized poly-butadiene, e.g., "Oxiron 2001" (obtained from FMC Corp.) Other 6uitable cycloaliphatic epoxides include those described in U.S. Patents Z,750,395;
2,890,194; and 3,318,822 ~hich are incorporated ~erein by referenoe, and ~he following:
--"` 2~9~179 , ~al~ , ~p ~\o\~
~C--o~ ~
~c ..o L}
Other suitable epoxide6 include:
O
~ ~ b ~ J b whers b is 1 to 4, m is ~5-b), and Rl is H, halogen, or Cl to C4 alkyl.
Coepoxides may be used with the cycloaliphatic epoxide of this invention. These coepoxides are called polyglycidyl compounds. They contain a plurality of l,2-epoxide groups derived from the reaction of a polyfunctional active hydrogen coneaining compound with an excess of an epihalohydrin under basic conditions. ~hen the active hydrogen compound i~ a polyhydric alcohol or phenol, the r~sulting e~oxide resin con~ains glycidyl ~ther groups~ A preferred group of polyglycidyl compounds are made via condensation reactions ~i~h 2,~-bis(4-hydroxyphenyl)propane~ also 2~99179 .
_ 7 known as bisphenol A, and have structure~ such as H C - CH - CH - O ~ C ~ ~ CH2 l 'H - CH - O ~ C ~ O ~ CH2- CH - H2 OH C~3 III
where c has a value from about 0 to about 15. These epoxides are bisphenol-A epoxy r0sins. They are available commercially under the trade name~ such as "Epon 828," "Epon 1001", and "Epon 1009" from Shell Chemical Co., and as ~DER 331", and "DER 334" from Dow Chemical Co. The most preferred bisphenol A
epoxy resins have an "c" value between O and 10.
Polyepoxides which are polyglycidyl ethers of q,g'-dihydroxydiphenyl methane~
EPOXIDE~AF~OMATIC AMINE RESIN SYSTEMS
B~CKGROIJND OF THE INVENTION
~ mine curable epoxy resin formulations are widely used as coatings, adhesi~es, sealants, and matrices for fiber-reinforced composites. For many applications, a ~ast rate of cure is desira~le.
Many additives have been tested as cure accelerators for epoxy/amine mixtures. Several references teach that additives with phenolic hydroxyl groups are efEective with epoxy resins derived from epihalohydrins and active hydrogen compounds, such as bisphenol A epoxy resins. For example, Shechter et al in Industrial and Engineering Chemistry, Volume g~, No. 1, pages 94 to 97, 1956, disclosed that phenol was more effectiv0 than aliphatic alcohols in accelerating the reaction of phenyl glycidyl ether with diethylamine. ~owen et al in the American Che~ical Society Advances in Chemistry Series, Volume 92, pages 48 to 59, 1970, disclosed that a variety of hydroxyl containing compounds decreased ~he gel time of a bisphenol A
epoxy~triethylenetetramine mixture. ~owen et al disclosed tha~ 4,4'-dihydroxydiphenyl sulfone, glycerin, phenol, ~etrabromobisphenol A, and bisphenol A a~celerated the cure with a similar degree of effectiveness.
Epoxy compositions containing resorcinol are described in the prior art. For example, Gough et al lin ~he Journ~l of Oil and Color Chemists 2099~79 Association, volume 43, pages 409 to 418, 1961), Nagy (in Adhesive~ Age, pages 20 to 27, April, 1967), and Parten~ky (in the American Chemical Society Advances in Chemistry S~ries, Volume 92, pages 29 to 47, 1970~ disclo~ed that resorcinol and many other phenolic compounds accelerate the cure of glycidyl epoxy/amine mixture~. Markovitz in "Chemical Properties of Crosslinked Polymers,"
American Chemical Society 5ympo~ium 1976, S.S.
Labana, Ed., page~ 49 to 58 described curable compositions containing cycloaliphatic epoxides, resorcinol and metal salts as coaccelerator~. No reference was found to cycloaliphatic epoxide/aromatic amine mixtures containing resorcinol as an accelerator.
In many epoxy/amine formulations, cycloaliphatic epoxides ar~ used as the epoxy component ~ince they impart improved mechanical and thermal properties to the cured compositions. For example, unreinforced castings of bis(2,3-epoxy-cyclopentyl) ether cured with m-phenylenediamine have tensile strengths and tensile ~oduli which are among ~he highes~ of any ~hermosetting material.
Similarly, as described by McLean et. al. in Report No. 14450 of the National Research Council o ~9917~
Canada, November, 1974, high mechanical properties can be achieve~ in unreinforced castings made by curing 3,4-epoxycyclohexylmethyl 3,4-epoxycyclohexane carboxylate with methylene dianiline. ~owever, resin systems containing bis(2,3-epoxycyclopentyl) ether or 3,4-epoxycyclohexylmethyl 3,~-epoxycyclohexane carboxylate cure more slowly with aromatic amines than ~imilar compositions containing bisphenol A
epoxy resins. This characteristic limit~ their utility in composite fabrication processe6 such as filament winding and reaction injection moldi~g.
Thus ~here i~ a need for cure accelerators for cycloaliphatic epoxide/amine re~in systems2 Moreover~ in commercial practîce it is desirable that the mixture of the accelerator and epoxy resin have good storage stability in the absence of the amine hardener. Thi~ chara~,teri~tic fa~ ta~es handling in a production environment.
It has now been found that a select group of phenolic compounds are highly effec~ive cure accelera~ors for cycloaliphatic/aromatic amine resin sy~tems. Under a fixed cure schedule, the accelerated compositions afford improved properties compared to compositions which do not contain the accelerator, ~uch as higher mechanical propereies and/or increased heat deflection temperature~ in unreinforced ca6tings.
~ urther~ a method for accelerating the cure of cycloaliphatic epoxide/aromatic amine mixture6 at low temperatures has been found which comprises adding a 601id solution of a high melting 20~9~7C3 _ 4 accelerator in a low melting solid cycloaliphatic epoxy resin.
THE INVENTION
This invention is directed to a compo~ition comprising:
ta) a cycloaliphatic epoxy resin containing two or more epoxide groups, (b) an aromatic amine hardener, and (c) a cure accelerator selected from (i) HO ~ ~ ~ ~ and/or HO OH
(ii) Ra ~
wherein ~ is selected from SO2, SO, OH O O
C(CF3)2, CN, C, CO, R i~ selected from haloyen O ;.
or alkyl of 1 to 4 carb~n at.om~, or ~ C.-and a i~ O
to ~.
The composition may optionally contain a thermoplastic polymer and/or a s~ructural ~iber.
The preferred cure accelerator~ are one or more of the following: 4,4'-dihydroxydiphenyl sulfone, re~orcinol, 2,2-bis(~-hydroxyphenyl~
hexafluoropropane, 4,4~-dihydroxydiphenyl sulfo~ide, 2,4 dihydroxybenzophenone, 4,4'-dihydroxybenzophenone, and 4,4'-dihydroxy-3,3-dichlorodiphenyl sulone.
2 ~ 7 ~
~ 5 --The cycloaliphatic epoxide~ of ~his invention are prepared by epoxidation of dienes or polyenes. Resin~ of this type include bi~(2,3-epoxycyclopentyl) ~her, I, ~~ ~
I II
reaction products of I with e~hylene glycol which are described in U.S. Patent 3,398,102, 5(6)-glycidyl-2-(1,2-epoxyethyl)bicyclo[2.2.1]
heptane, II, and dicyclopentadiene diepoxide~
Commercial examples o these epoxides include vinyl cyclohexene diepoxide. e.g., "ERL-4206" (obtained from Union Carbide Corp.), 3,g-epoxycyclohexylmethyl 3,4-epoxycyclohexane carboxylate, e.g., "ERL-4221 (obtained from Union Carbide Corp.) t 3,4-epoxy-6-methylcyclohexylmethyl 3,4-epoxy-6-methyl-cyclohexane carboxylate, e.g., ~'ER~-4201" (obtained from Union Carbide Corp.), bis(3,4-epoxycyclo-hexylme~yl)adipa~e, e.g., "ERL-4299" ~obtained from Union Carbide Corp.), dipentene dioxide, e.g., "ERL-4269~' (obtained from Union Carbide Corp.~
2-(3,q-epoxycyclohexyl-5,5-spiro-3,4-epoxy)cyclo-hexane meta-dioxane, e.g., "ERL-4234" (obtained from Union Carbide Corp.) and epoxidized poly-butadiene, e.g., "Oxiron 2001" (obtained from FMC Corp.) Other 6uitable cycloaliphatic epoxides include those described in U.S. Patents Z,750,395;
2,890,194; and 3,318,822 ~hich are incorporated ~erein by referenoe, and ~he following:
--"` 2~9~179 , ~al~ , ~p ~\o\~
~C--o~ ~
~c ..o L}
Other suitable epoxide6 include:
O
~ ~ b ~ J b whers b is 1 to 4, m is ~5-b), and Rl is H, halogen, or Cl to C4 alkyl.
Coepoxides may be used with the cycloaliphatic epoxide of this invention. These coepoxides are called polyglycidyl compounds. They contain a plurality of l,2-epoxide groups derived from the reaction of a polyfunctional active hydrogen coneaining compound with an excess of an epihalohydrin under basic conditions. ~hen the active hydrogen compound i~ a polyhydric alcohol or phenol, the r~sulting e~oxide resin con~ains glycidyl ~ther groups~ A preferred group of polyglycidyl compounds are made via condensation reactions ~i~h 2,~-bis(4-hydroxyphenyl)propane~ also 2~99179 .
_ 7 known as bisphenol A, and have structure~ such as H C - CH - CH - O ~ C ~ ~ CH2 l 'H - CH - O ~ C ~ O ~ CH2- CH - H2 OH C~3 III
where c has a value from about 0 to about 15. These epoxides are bisphenol-A epoxy r0sins. They are available commercially under the trade name~ such as "Epon 828," "Epon 1001", and "Epon 1009" from Shell Chemical Co., and as ~DER 331", and "DER 334" from Dow Chemical Co. The most preferred bisphenol A
epoxy resins have an "c" value between O and 10.
Polyepoxides which are polyglycidyl ethers of q,g'-dihydroxydiphenyl methane~
4,4'-dihydroxydiphenyl sulfone, 4,q'-biphenol, 4,4'-dihydroxydiphenyl sulfide, phenolphthalein, resorcinol, 4,2'-biphenol, or tris(4-hydroxyphenyl) methane and the like, are useful in this invention.
In addition, EPON 1031 (a tetraglycidyl derivative of 1,1,2,Z-~etraki6(hydroxyphenyl)ethane from Shell Chemical Company), and Apogen 101, (a methylolated bisphenol A resin fro~ Schaefer Chemical Co.) may also be used. Halogenated poly~lycidyl compounds such a~ D.E.R. 580 (a bromina~ed bisp~eno~ A epoxy resin from Dow Chemical Company) are also useful.
---`` 209~ 79 Other suitable epoxy resin~ incl~de pslyepoxide~
-prepar~d fro~ polyols such as pentaerythritol, glycerol, butanediol or trimethylolpropane and an epihalohydrin.
Polyglycidyl derivatives of phenol-formaldehyde novolaks ~uch a~ IV where d =
0.1 to 8 and cresol-formaldehyde novolak~ such as V
where d = O.l to ~ are al~o useable.
R 2 ~ ]
IV R2 = H
V R2 = C~3 The former are commercially available as D.E.N 931, D.E.N. 438, and D.E.N. 485 from Dow Chemical Company. The latter are available a~, for example, ECN 1235, ECN 1273, and ECN 1299 (obtained ~rom Ciba-Geigy Corporation, Ardsley, NY). Other epoxidized novolaks such as SU-8 (ob~ained ~rom Celanese Polymer 5pecialties Company, ~ouisville, KY) are also suitable.
Other poly~unctional active hydrogen compounds besides phenols and alcohols may be used to prepare the polyqlycidyl adduc~s oE t~is invention. They include amines, aminoalcohols and polycarboxylic acids.
Adducts derived from amines include N,N-diglycidyl aniline, N,N-diglycidyl toluidine, N~N,N',N'-tetraglycidylxylylene diamine, (i.e.~ VI) N,N,N',N'-~etraglycidyl-bis (methylamino) ~-- 2099179 _ 9 _ cyclohexdne (i.e. VII) , N,N,M',N'-tetraglycidyl-4,4`-diaminodiphenyl methane, (i.e. VIII) N,N,N',N'-tetraglycidyl-3,3'-diaminodiphenyl sulfone, and N,N' dimethyl-N,N'-diglycidyl-4,q'-diaminodiphenyl methane. Commercially available resins of this type include Glyamins 135 and Glyamine 125 (obtained fro~ F.I.C. Corporation, San Francisco, CA.), Araldite MY-720 (obtained from Ciba Geigy Corporation) and PGA-~ and PGA-C
(obtained from The Sherwin-Williams Co., Chica~o, Illinois).
~0 /CH2 rH_CHZ
T CH2 CH\ ~CH2 CH
~CH~H2 CH - N
2 ~ CH2 - ~ ~ ~ CH2 Vl CH - ~ ~ ~ C~2 ~H - ~
~ ~CEI2 C~ 2 CH ~ ~2 CH2~
~C~2 SH~ ~ H2 VII
-- - 2~99179 - 10 ~
" 0 - / C~2-CH-C~2 CH2 ~\ f ~A2 N~
CH2 -CH~H2 O~
VIII
Suitable polyglycidyl adduc~s derived from amino alcohols include O,N,N-triglycidyl-4-amino-phenol, availa~le as Araldite 0500 or Araldite 0510 (obtained from Ciba Geigy Corporation) and O,N,N-triglycidyl-3-aminophenol (available as Glyamine 115 from F.I.C. Corporation).
Also sui~able for use herein are the glycidyl esters of carboxylic acids. Such glycidyl ester~ include, for example, diglycidyl phthalate, diglycidyl terephthala~e, diglycidyl isophthalate, and diglycidyl adipate. There may also be used polyepoxides such as triglycidyl cyanurates and isocyanurates, N,N-diglycidyl oxamides, N,N'-diglycidyl derivatives of hydantoins such as "XB 2793" tobtained f~om Ciba Geigy Corporation), diglycidyl esters of cycloaliphatic dicarboxylic acids, and polyglycidyl thioethers of pslythiols.
Other epoxy-containing materials are copolymers oP acrylic dCi~ es~er~ of glyridol such as glycidyl acrylate and glycldyl methacrylate with ~ 2~9~17~
one or more copolymerizable ~inyl compounds.
-Examples of such copolymers are lul styrene-glycidyl methacrylate, 1:1 methyl methacrylate-glycidyl acrylate and 62.5:24:13.5 methyl methacrylate:ethyl acrylate:glycidyl methacrylate.
Silicone resins containing epoxy functionality, e.g., 2,4,6,~,10-pentakis [3-(2,3-epoxypropoxy)propyl]-2,4,6,fl,10-pentamethyl-cyclopen~asiloxane and the diglycidyl ether of 1,3-bis-(3-hydroxypropyl)tetramethyldisiloxane are also useable.
Reactive diluents containinq one epoxide group such as t-butylphenyl glycidyl ether, may also be used. The reactive diluent may comprise up to 25 percent by weight of the epoxide component.
The reactive diluent dnd coepoxide are used in amounts of up to 40, preferably 30 percent by weight.
The preferred epoxy resins are bis~2,3-epoxycyclopentyl)ether, vinyl cyclohexene diepoxide, 2-(3,9-expoxycyclohexyl-5,5-spiro-3~4 epoxy)cyclohexane meta-dioxane, the diepoxides of allyl cyclopentenyl ether, l,q-cyclohexadiene diepoxide, 3,4-epoxycyclohexylmeehyl 3,4-epoxycyclohexane carboxylate, and bis~3,4-epoxycyclohexylmethyl~adipate.
Th~ hardeners which may be used in the composition of this invention are selected ~rom one or more of the following: 4,~'-diaminodiphenyl ether, 4,4'-diaminodiphenyl methane, 3,3'-diaminodiphenyl methane, 4,4'-diaminodlphenyl sulfone, m-phenylenediamine, p-phenylenediami~e, 4,4'-diaminodiphenylpropane, 4,4'-diaminodiphenyl 209~7~
sulfide, l,9-bis(p-aminophenoxy)benzene, alkylated derivatives of 4,4'-diaminodiphenyl methane su~h as 3,3'-dii~opropyl-4,4;-diaminodiphenyl methane, 1,3-bis(m-aminophenoxy)benzene, diethyltoluenediamine, l,3-bis(p-aminophenoxy) benzene, adducts of epoxy re~ins with the above diamines, such as the adduce formed by reacing one mole of a liquid bisphenol-A epoxy resin with 2 to 4 moles of m-phenylenediamine by itself or in combination with 4,4'-diaminodiphenyl methane or the adducts of a bisphenol-A epoxy resin with a molar excess of g,q-diaminodiphenyl sulfone, as described in U.S. Patent 4,330,659, 9,4'-bis(3-aminophenoxy)diphenyl sulfone, 2,2-bis(~-aminophenoxyphenyl) propane and trimethylene glycol di-para-aminobenzoate.
The pre~erred hardeners are m-phenylene-diamine, 4,4'-~iamino~iphenyl met.hane, low mel~ing mixtures o~ m-phenylenediamine and 4.~-diamino-diphenyl methane, 2,2-bis(4-aminophenoxyphenyl~
propane and the adduc~ formed by reac~ing one mole of a liquid bisphenol-A epoxy with 2 to 4 moles of m-phenylenediamine.
The compositions of this invention may optionally contain a thermoplastic polymer~ These materials have beneficial effec~ on the viscosity and film strength characteristics of the epoxy~ardener/accelerator mixture.
The thermopla~tic polymers used in ~his inven~ion i~clude polyarylethers of formula I~ wh;ch are described in U.S. Paten~s 4,lO8,B37 and 4,175,175, `` 209~179 ~ -O-R3-0-R4-~e . IX
wherein R3 is a residuum of a dihydric phenol such as bisphenol A, hydroquinone. resorcinol, 4,9-biphenol, q,4'-dihydroxydiphenyl sulfone, 4,4'-dihydroxy-3,3' 5,5'-t.etramethyldiphenyl sulfide, 4,4'-dihydroxy-3,3',5.5'-tetramethyldiphenyl sulfone and the like. R4 is a residuum of a benzenoid compound susceptible to nucleophilic aromatic substitution reactions such as 4,4'-dichlorodiphenyl sulfone, ~,~'-difluorobenæophenone, and the like. The average value of e is from about 8 to about 120.
These polymers may have terminal groups which react with epoxy resins, such as hydroxyl or carboxyl, or terminal groups which do not react.
Other suitable polyarylethers are described in U,S, Patent 3,332,209.
Also suitable are polyhydroxyethers of formula X.
-~0 - R3 0 - CHz CH -CH
OH
X
where R3 has the same meaning as for Formula I~
and the average value of f is between about 8 and about 300; and polycarbonates such as those based on bisphenol A, tetramethyl bisphenol A, 4,4'-dihydroxydiphenyl sulfone, 4,4l-dibydroxy-3,3',5,5'tetramethyldiphenyl sulfo~e, hydroquinone, resorcinol, 4,4l-dihydroxy-3,3l,5,5~-tetramethyldiphenyl -. :
.
' -- 2~99179 sulfide, 4,4'biphenol, 4,4'-dihydroxydiphenyl sulfide, phenolphthalein, 2,2,4,4-tetramethyl-1,3-cyclobutan~ diol. and the like. Other suitable thermoplastic6 include poly (~-caprolactone);
polybutadiene: polybutadiene/acrylonitrile copolymers, including those optionally con~aining amine, carboxyl, hydroxyl, or -SH groups;
polyesters, such as poly(butylene terepht~alate);
poly(e~hylene terephthalate); polyetherimides such as the Ultem resins (obtained from the General Electric Company); acrylonitrile~ butadiene~styrene terpolymers, polyamides such as nylon 6, nylon 6,6, nylon 6,12, and Trogamid T (obtained from Dynamit Nobel Corporation); poly(amide imides) such as Torlon poly(amide imide) (obtained from Amoco Chemical Corporation, Napierville, IL); polyolefins:
polyethylene oxid~; poly(butyl me~hacrylate);
impact-modified polystyrene; sulfonated polyethylene: polyarylates such as those derived from bisphenol A and isophthalic and terephthalic acid; poly(2,6- dimethyl phenylene oxide); polyvinyl chloride and its copolymers; polyacetals;
polyphenylene sulfide and ~he like.
The compositions of this inv~ntion may include a structural fiber. The structural fibers which are useful in this invention include carbon, graphite, glass, silicon carbide, poly(benzothiazole), poly(benzimidazole~, poly(benzoxazole~, alumina, titania, boron, and aromatic polyamide fibers. These fibers are characterized by a tensile strengt~ of greater than 100,000 psi, a tensile modulus of g~eater than two million psi, and a decomposition temperature of ` -` 2~93~7~
- 15 ~
greater than 200C. The fiber~ may be used in the form of contin~ous tows ~1000 to 400,000 filaments each), woven cloth, whiskers, chopped fiber or random mat. The preferred fibers are carbon fiber6, aromatic polyamide fibers, such as Kevldr 49 fiber (ohtained from E.I. duPont de Nemour~, Inc., Wilmingeon~ DE), and silicon carbide fibers.
The composition contain6 from about 20 to about 90 percent by weight of cycloaliphatic epoxide, fro~ about 15 to about 80, preferably fro~
about 20 to about 70 percent by weight of hardener.
The composition also contains from 0.1 to about 10, prefer~bly from 0.1 to about 8 percent by weight of the accelerator. The thermoplastic polymer may be used in amounts up to Z0 percent by weight of the total composition. The structural fiber may be u~ed in amounts of up to 90, preferably between about 20 and about 85 percènt by we~ht o~ the total composite.
In the compositions of this invention, the molar ratio of amine NH groups to epoxy groups i5 0.5 to 2.0, preferably 0.6 to 1.7.
Preimpregnated reinforcement may be made from the compositions of this invention by combining epoxy resins, hardener, accelerator, and optionally ~hermoplastic polymer with the structural fiber.
Preimpregnated reinforcement ~ay be prepared by ~everal techniques known in the art, such as wet winding or hot melt. In wet winding, a continuous tow of reinPorcement is passed through a resin bath cvntaining a mix~ure of the cycloaliphatic epoxide, the amine hardener, accelerator and optionally, the thermoplastic .
--~ 2~9~79 polymer. After the tow is impregnated with the resin, i~ i8 p~ssed through squeeze rolls to remove excess resin. Preferably, because of the fast curing characteristics of these compositions. the preimpregnated reinPorcement is used to make a composite article soon after it is prepared.
Composites may be preparea by curing preimpregnated reinforcement using heat and pressure. Vacuum bag~autoclave cures work well with these compositions. Laminates may also be prepared via wet layup followed by compression molding, resin transfer molding, or by resin injection, as described in European Patent Application 0019149 published November 26, 1980. Typical cure temperatures are from about 100F to about 500F, preferably from about 180F to about 450F. Cure times may be as short as from about 1 to about 2 minutes depending on the composition utilized.
The compositions of this inventisn are well suited for filament windin~. In this composite fabrication process, continuous reinforcement in the form of tape or tow--either previously impregnated with resin or impregnated during winding--is placed over a rotating and removable form or mandrel i~ a previou~ly determined pattern. Generally the shape is a surface of revolution and contain~ end clo~ure~. ~hen the proper number of layers are applied, the wound form is cured in an oYen or autoclave and the mandrel removed.
The composition of this inven~ion may be used as aircraft parts such as wing skins, wing-to-bsdy fairingE, flo~r panels, ~laps, radomes;
., .
1 7 ~
as au~omotive parts such as driveshaft~, bumpers, and spring~: and as pressure vessels, tanks and pipes. ~hey are also suitable or sporeing go~ds applications such as golf shafts, tennis rackets, and fishing rods.
In addition to structural fibers~ the composi~ion may also ccntain particulate fillers such as talc, mica, calcium carbonate, aluminum trihydrate, glass microballoons, phenolic thermospheres, and carbon black. Up to hal~ of the weight struct~ral fibers in the composition may be replaced by filler. Thixotropic agents such as fumed silica may also be used.
Further, the compositions may be used in adhesives, potting and encapsulation compounds, and in coating applications.
EXAMPLES
The following examples serve to give specific illustrations of the practice of this invention but they are not intended in any way to limit the scope of this invention.
In the Exameles which follow, the epoxy equivalent weight (EEW) is defined as the grams of epoxy resin per mole of 1,2 epoxide ~roup.
Examples 1 through ~ and Controls A through H describe effects of accelerators on the viscosity of cycloaliphatic epoxide/aromatic amine mixtures.
ExamPle 1 A 250 ml, three necked flask equipped with a paddle stirrer, thermometer with a Therm-0-~atch Controller, an inlet and outlet for nitrogen9 and an electric heating mantle was charged with 190 g o-f bis(2,3-epoxycyclopentyl) ether and 10 g of 4,4'-aihydroxyaiphenyl sulfone. The mixture was heated and s~irred at a temperature of 100C for 1 hour to dissolve the bisphenol.
A lO0 g portion of the dihydroxydiphenyl sulfone/bis(2,3-epoxycyclopentyl ether solution was placed in a 4 ounce jar in an oil ba~h maintained a~
a temperature of 66C. Then 30.7 g sf m-phenylenediamine (MPDA) was added. The mixture was stirred for about five minutes uneil the diamine dissolYed. The viscosity of the solution was measured with a Brookfield viscometer (obtained from Brookfield ~ngineering Laboratories, Stoughton, MA) at fixed intervals. The viscosity was 25 centipoises after Q.5 hours and 35 centipoises after l.0 hour. After 1.5 hours, the mixture gelled and increased in temperature.
ExamPle 2 A flask equipped as in Example l was charged with lO g of resorcinol and 190 g of bis(2,3-epoxycyclop0ntyl~ ether. ~he mixture was stirred and heated at a tempera~ure of ~0C ~or 1 hour to dissolve the resorcinol. Then a lO0 g portion of ~he solution wa~ transferred to a 4 ounce jar in an oil bath at a tempera~ure of 66C and treated with 30.7 g of MPDA. The viscosity of the mixture at various times is shown in Table I.
F.xamPle 3 A flask equipped as in Example l was charged with lO g of 4,4l-dihydroxybenzophenone and l90 g o bis(2,3-epoxycyclopentyl~ether. ~he mixture was heated at a temperature of 120~C for l hour to dissolve the diphenol. T~en a lO0 g poreion 2099~79 of the solution was tran~ferred ~o a 9 ounce jar in an oil bat~ at a temperature of 66C and treated with 30.7 9 of MPDA. The viscosity of the mixture at various times i~ shown in Table I.
Control~ A throuqh F
A series of other hydroxyl compounds were screened as accelerators for bis(2,3-epoxycyclo-pentyl) ether/MPD~ mixtures using the procedure descr;bed in Example 1. As shown by the data i~
Table I, none of these additives caused the mixture to gel in 1.5 hours. To determine if additional heating would cause gelation, samples which had been held at 66C for 1.5 hours were removed from the bath and allowed to stand for 16 hours at room temperature (23C). They were then replaced in the 66C bath. After an additional hour, the viscosity of each mixture was measured. None had gelled.
2~9~179 U U~; o o o o E
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20~9179 Example ~ and Control G describe vi6c06ity versus time behavior of 3,4-epoxycyclohexylmethyl 3 J 4-epoxycyclohexane carboxylate/MPDA mixtures.
Viscosity measurements were made on samples in the chamber of a Brookfield Thermosel viscometer (obtained from Brookfield Engineering Laboratories) maintained a~ a temperature of 66C. The accelera~ing effect of 4,4'-dihydroxydiphenyl sulfone on the cure of this epoxy formulation wa~
demonstrated by adding this compound in an ea~ily dissolvable form. A ~olution containing 20 percent by weight of 4,4'-dihydroxydiphenyl sulfone was prepared by heating the diphenol in Bakelite ERRA-0300 epoxy resin for 1 hour at a temperature of 120C. ERRA-0~00, obtained from Union Carbide, was a mixture of the solid isomers of bis(2,3-epoxycyclopentyl) ether. The solution was allowed to cool to room temperature and solidify.
This compo~ition had good stability a~ room ~emperature and was a convenient means for adding 4,4'-dihydroxydiphenyl sulfone to epoxy/amine mix~ures at moderate temperatures.
Exam~le 4 An accelerated thermosetting epoxy composition was prepared by combining:
14.0 g of 3,4-epoxycyclohexylmethyl 3,4-epoxycyclohexane carboxylate, 3.0 g of the solid solut;on of 4,4'-dihydroxydiphenyl ~ulfone in bis~
(2,3-epoxycyclopentyl) ether described above, and 3.79 9 o~ m-phenylenediamine.
at a temperature o 66C. This mixture had an NH~epoxide ~toichiometry of 1.10. Its viscosity wa~
measured as a ~unction of time. The results as shown in Table II.
Control G
A thermosetting mixture wa~ prepared by combining 19.0 g of 3,4-epoxycyclohexylmethyl 3,9-epoxycyclohexane carboxylate.
and 4.2 g of m-~henylenediamine.
The NH/epoxide stoichiometry of this mixture was 1.10. Its viscosity at a temperature of 66C was measured periodically as described in Example 4. The results are ~hown in Table II.
- 23 - 2~99~79 o r~
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Comparison of the viscosity versus ~ime data for ~xample ~ with that of Control G and Control A ~i.e., a bis(2,3-epoxycyclopentyl) ether/MPDA mixture~ shows that 4,4'-dihydroxydiphenyl sulfone is an effective accelerator when added a8 a solid solution in bis(2,3-epoxycyclopentyl) ether~
Example 5 demonstrates the storage stabili~y of bis (2,3-epoxycyclopentyl) ether/g,4'-dihydroxydiphenyl sulfone solutions.
ExamPle 5 A 100 g portion of the solution of 4,q'-dihydroxydiphenyl sulfone in bis-(2,3-epoxycyclopentyl) ether prepared a~ in Example 1 was maintained at a temperature of 66C for 96 hours. At the end of that period, the solution was a clear low viscosity fluid. Analysis of the final solution by liquid chromatography showed ~hat le~s than 2 percent of the epoxide had reacted with the diphenol.
Examples 6 through 11 and Controls M
through K describe the preparation and properties of unreinforced castings. Casting dimensions were 1/8 x 8 x 4 to 8 inches. Typically they weighed 80 to 160 g.
The general procedure for making castings was the following: The epoxy resin and accelera~or ~ere charged ~o a 3-necked flask equipped wi~h a paddle stirrer. The contents of the flask were s~irred and heated at a temperature of 85 to 100C
~til t~e accelerator aissolved. The solution was - ` 20~9~79 then cooled to a temperature of 70C. The amine hardener was a~ded to this solution. It dissolved in about 2 eo 5 minute~. The resulting solution wa~
subjected to a vacuum of about 28 inches of mercury to remove air bubbles for about 3 minutes. It was then poured into a preheated glass mold with a cavity of dimensions of 1/8 x 8 x ~ inches.
Casting~ were tested to determine tensile properties and heat deflection temperature. Ten ile properties were measured a~cordinq to AST~ D-63~
using a Type I dogbone specimen. Heat deflection tempera~ure was measured according eO ASTM D-648 (264 psi stress).
Examples 6 through 8 and Control H describe unreinforced castings made with the following cure schedule: 2 hours at 85C; 85~ to 150C at 1C~minute: 1 hour at 150C.
ExamPle 6 A solution containing 190 g of bis-(2,3-epoxycyclopentyl) ether and 10 9 of ~,4'-dihydroxydiphenyl sulfone was prepared as described in Example 1. A 60 g por~ion of this solution was blended with 18.4 9 of MPDA, poured into a mold, and cured as described above. The tensile properties and heat deflection temperature of the cured casting are given in Table III.
ExamPle 7 The pxocedure in Example 6 was repeated excep~ that the amount of 4,4'-dihydroxydiphenyl sulrone was reduced by one half. The data on this casting are sho~n in Ta~le III.
. .
2~99179 .
Control H
A thermosetting composition was prepared by blending 60 g of bis(2,3-epoxycyclopentyl) ether with 18.g g of MPDA. A casting was then prepared by the procedure as de~cribed above. The propertie~
of the casting made from this composition are shown in Table III.
ExamDle 8 A copolymer of bis(2,3-epoxycyclopentyl) ether and ethylene glycol (i.e. ERLA-~617 obtained from Union Carbide Corporation), 93.7 g, and 6.4 g of 4,4'-dihydroxydiphenyl sulfone were heated at a temperature of 100C for 0.5 hours with stirring ~o dissolve the diphenol. This solution was cooled to a temperature of 80~C and treated with 21.2 g of MPDA. This solution was poured into a mold and cured. The properties of the casting are shown in Table III.
---`"` 2~179 _I
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`` 2~9~179 Examples 9 through 11 and Control I
describe other unreinforced castings. Resin formulations, casting properties, and cure sch~dul0s are shown in Table IV.
The data in Tables III and IV show that the cure accelerators of this invention may be used with a wide variety of epoxides and aromatic amines.
In Table III, higher heat deflection temperatures are obtained in bis-(2,3-epoxycyclopentyl) ether~MPDA castings containing 4,4'-dihydroxydiphenyl sul~one than in the Con~rol. In Example 8, a high level of properties are also ob~ained with the ethylene glycol~bi~2,3-epoxycyclopentyl) ether copolymer resin. Note that the tensile strengths of all castings in Table III are very high. Other accelerators such as borontri~loride:
~onoethyla~ine complexes do not produce unrein~orcad castings wit~ such high mechanical propertie~.
Tensile strength and elongation measurements are sensitive to defects in the sample so that small difEersnces between sample6 (e.g., tensile streng~h6 of 14,000 psi versus l6,000 psi) do no~ serve as a basis of diPferen~iation. In contra6t, hea~
deflection temperature is a bulk property of the material and is much less affected by d~fects.
In Table IV, the cas~ing in Control I was so severely undercured that it could no~ be ~ested.
In contrast, the aceelerated composition of Exam21e 9 afforded a casting with good mechanical propertie~. Example 10 shows ~hat mix~ures of cycloaliphatic epoxides and glycidyl epoxides can be cured wi~h the accelerators of ~hi~ inven~ion.
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--" 2~9~179 . - .
_ 30 -ExamPle 12 - Example 12 describes the preparation of a unidirectional carbon fi~er composite using the composition o~ this invention. The prepreg is made using a polyacrylonitrile-based carbon fiber with a tensile strength of 6.6 x 10 psi and a tensile modulus of 36 X 106 pci.
A tow of carbon ~iber containing 6000 filaments is drawn through a resin bath contain;ng the resin formulation shown in E~ample 6. The impregnated fiber i6 wound on an 8 inch square frame to a thickness of approximately lJ8 inch. The impregnated fiber in the frame contains approximately 35 percent by weight of resin. The resin is cured by placing the frame in an oven and heating wieh a programmed cure cycle. The cure cycle is 2 hours at 85C to 160C at 1C/minute, hold 2 hours at 160C. The frame is removed from the oven and the cured carbon fiber composite is removed erom the frame. The composite has a high level of longitudinal and transverse tensile properties.
In addition, EPON 1031 (a tetraglycidyl derivative of 1,1,2,Z-~etraki6(hydroxyphenyl)ethane from Shell Chemical Company), and Apogen 101, (a methylolated bisphenol A resin fro~ Schaefer Chemical Co.) may also be used. Halogenated poly~lycidyl compounds such a~ D.E.R. 580 (a bromina~ed bisp~eno~ A epoxy resin from Dow Chemical Company) are also useful.
---`` 209~ 79 Other suitable epoxy resin~ incl~de pslyepoxide~
-prepar~d fro~ polyols such as pentaerythritol, glycerol, butanediol or trimethylolpropane and an epihalohydrin.
Polyglycidyl derivatives of phenol-formaldehyde novolaks ~uch a~ IV where d =
0.1 to 8 and cresol-formaldehyde novolak~ such as V
where d = O.l to ~ are al~o useable.
R 2 ~ ]
IV R2 = H
V R2 = C~3 The former are commercially available as D.E.N 931, D.E.N. 438, and D.E.N. 485 from Dow Chemical Company. The latter are available a~, for example, ECN 1235, ECN 1273, and ECN 1299 (obtained ~rom Ciba-Geigy Corporation, Ardsley, NY). Other epoxidized novolaks such as SU-8 (ob~ained ~rom Celanese Polymer 5pecialties Company, ~ouisville, KY) are also suitable.
Other poly~unctional active hydrogen compounds besides phenols and alcohols may be used to prepare the polyqlycidyl adduc~s oE t~is invention. They include amines, aminoalcohols and polycarboxylic acids.
Adducts derived from amines include N,N-diglycidyl aniline, N,N-diglycidyl toluidine, N~N,N',N'-tetraglycidylxylylene diamine, (i.e.~ VI) N,N,N',N'-~etraglycidyl-bis (methylamino) ~-- 2099179 _ 9 _ cyclohexdne (i.e. VII) , N,N,M',N'-tetraglycidyl-4,4`-diaminodiphenyl methane, (i.e. VIII) N,N,N',N'-tetraglycidyl-3,3'-diaminodiphenyl sulfone, and N,N' dimethyl-N,N'-diglycidyl-4,q'-diaminodiphenyl methane. Commercially available resins of this type include Glyamins 135 and Glyamine 125 (obtained fro~ F.I.C. Corporation, San Francisco, CA.), Araldite MY-720 (obtained from Ciba Geigy Corporation) and PGA-~ and PGA-C
(obtained from The Sherwin-Williams Co., Chica~o, Illinois).
~0 /CH2 rH_CHZ
T CH2 CH\ ~CH2 CH
~CH~H2 CH - N
2 ~ CH2 - ~ ~ ~ CH2 Vl CH - ~ ~ ~ C~2 ~H - ~
~ ~CEI2 C~ 2 CH ~ ~2 CH2~
~C~2 SH~ ~ H2 VII
-- - 2~99179 - 10 ~
" 0 - / C~2-CH-C~2 CH2 ~\ f ~A2 N~
CH2 -CH~H2 O~
VIII
Suitable polyglycidyl adduc~s derived from amino alcohols include O,N,N-triglycidyl-4-amino-phenol, availa~le as Araldite 0500 or Araldite 0510 (obtained from Ciba Geigy Corporation) and O,N,N-triglycidyl-3-aminophenol (available as Glyamine 115 from F.I.C. Corporation).
Also sui~able for use herein are the glycidyl esters of carboxylic acids. Such glycidyl ester~ include, for example, diglycidyl phthalate, diglycidyl terephthala~e, diglycidyl isophthalate, and diglycidyl adipate. There may also be used polyepoxides such as triglycidyl cyanurates and isocyanurates, N,N-diglycidyl oxamides, N,N'-diglycidyl derivatives of hydantoins such as "XB 2793" tobtained f~om Ciba Geigy Corporation), diglycidyl esters of cycloaliphatic dicarboxylic acids, and polyglycidyl thioethers of pslythiols.
Other epoxy-containing materials are copolymers oP acrylic dCi~ es~er~ of glyridol such as glycidyl acrylate and glycldyl methacrylate with ~ 2~9~17~
one or more copolymerizable ~inyl compounds.
-Examples of such copolymers are lul styrene-glycidyl methacrylate, 1:1 methyl methacrylate-glycidyl acrylate and 62.5:24:13.5 methyl methacrylate:ethyl acrylate:glycidyl methacrylate.
Silicone resins containing epoxy functionality, e.g., 2,4,6,~,10-pentakis [3-(2,3-epoxypropoxy)propyl]-2,4,6,fl,10-pentamethyl-cyclopen~asiloxane and the diglycidyl ether of 1,3-bis-(3-hydroxypropyl)tetramethyldisiloxane are also useable.
Reactive diluents containinq one epoxide group such as t-butylphenyl glycidyl ether, may also be used. The reactive diluent may comprise up to 25 percent by weight of the epoxide component.
The reactive diluent dnd coepoxide are used in amounts of up to 40, preferably 30 percent by weight.
The preferred epoxy resins are bis~2,3-epoxycyclopentyl)ether, vinyl cyclohexene diepoxide, 2-(3,9-expoxycyclohexyl-5,5-spiro-3~4 epoxy)cyclohexane meta-dioxane, the diepoxides of allyl cyclopentenyl ether, l,q-cyclohexadiene diepoxide, 3,4-epoxycyclohexylmeehyl 3,4-epoxycyclohexane carboxylate, and bis~3,4-epoxycyclohexylmethyl~adipate.
Th~ hardeners which may be used in the composition of this invention are selected ~rom one or more of the following: 4,~'-diaminodiphenyl ether, 4,4'-diaminodiphenyl methane, 3,3'-diaminodiphenyl methane, 4,4'-diaminodlphenyl sulfone, m-phenylenediamine, p-phenylenediami~e, 4,4'-diaminodiphenylpropane, 4,4'-diaminodiphenyl 209~7~
sulfide, l,9-bis(p-aminophenoxy)benzene, alkylated derivatives of 4,4'-diaminodiphenyl methane su~h as 3,3'-dii~opropyl-4,4;-diaminodiphenyl methane, 1,3-bis(m-aminophenoxy)benzene, diethyltoluenediamine, l,3-bis(p-aminophenoxy) benzene, adducts of epoxy re~ins with the above diamines, such as the adduce formed by reacing one mole of a liquid bisphenol-A epoxy resin with 2 to 4 moles of m-phenylenediamine by itself or in combination with 4,4'-diaminodiphenyl methane or the adducts of a bisphenol-A epoxy resin with a molar excess of g,q-diaminodiphenyl sulfone, as described in U.S. Patent 4,330,659, 9,4'-bis(3-aminophenoxy)diphenyl sulfone, 2,2-bis(~-aminophenoxyphenyl) propane and trimethylene glycol di-para-aminobenzoate.
The pre~erred hardeners are m-phenylene-diamine, 4,4'-~iamino~iphenyl met.hane, low mel~ing mixtures o~ m-phenylenediamine and 4.~-diamino-diphenyl methane, 2,2-bis(4-aminophenoxyphenyl~
propane and the adduc~ formed by reac~ing one mole of a liquid bisphenol-A epoxy with 2 to 4 moles of m-phenylenediamine.
The compositions of this invention may optionally contain a thermoplastic polymer~ These materials have beneficial effec~ on the viscosity and film strength characteristics of the epoxy~ardener/accelerator mixture.
The thermopla~tic polymers used in ~his inven~ion i~clude polyarylethers of formula I~ wh;ch are described in U.S. Paten~s 4,lO8,B37 and 4,175,175, `` 209~179 ~ -O-R3-0-R4-~e . IX
wherein R3 is a residuum of a dihydric phenol such as bisphenol A, hydroquinone. resorcinol, 4,9-biphenol, q,4'-dihydroxydiphenyl sulfone, 4,4'-dihydroxy-3,3' 5,5'-t.etramethyldiphenyl sulfide, 4,4'-dihydroxy-3,3',5.5'-tetramethyldiphenyl sulfone and the like. R4 is a residuum of a benzenoid compound susceptible to nucleophilic aromatic substitution reactions such as 4,4'-dichlorodiphenyl sulfone, ~,~'-difluorobenæophenone, and the like. The average value of e is from about 8 to about 120.
These polymers may have terminal groups which react with epoxy resins, such as hydroxyl or carboxyl, or terminal groups which do not react.
Other suitable polyarylethers are described in U,S, Patent 3,332,209.
Also suitable are polyhydroxyethers of formula X.
-~0 - R3 0 - CHz CH -CH
OH
X
where R3 has the same meaning as for Formula I~
and the average value of f is between about 8 and about 300; and polycarbonates such as those based on bisphenol A, tetramethyl bisphenol A, 4,4'-dihydroxydiphenyl sulfone, 4,4l-dibydroxy-3,3',5,5'tetramethyldiphenyl sulfo~e, hydroquinone, resorcinol, 4,4l-dihydroxy-3,3l,5,5~-tetramethyldiphenyl -. :
.
' -- 2~99179 sulfide, 4,4'biphenol, 4,4'-dihydroxydiphenyl sulfide, phenolphthalein, 2,2,4,4-tetramethyl-1,3-cyclobutan~ diol. and the like. Other suitable thermoplastic6 include poly (~-caprolactone);
polybutadiene: polybutadiene/acrylonitrile copolymers, including those optionally con~aining amine, carboxyl, hydroxyl, or -SH groups;
polyesters, such as poly(butylene terepht~alate);
poly(e~hylene terephthalate); polyetherimides such as the Ultem resins (obtained from the General Electric Company); acrylonitrile~ butadiene~styrene terpolymers, polyamides such as nylon 6, nylon 6,6, nylon 6,12, and Trogamid T (obtained from Dynamit Nobel Corporation); poly(amide imides) such as Torlon poly(amide imide) (obtained from Amoco Chemical Corporation, Napierville, IL); polyolefins:
polyethylene oxid~; poly(butyl me~hacrylate);
impact-modified polystyrene; sulfonated polyethylene: polyarylates such as those derived from bisphenol A and isophthalic and terephthalic acid; poly(2,6- dimethyl phenylene oxide); polyvinyl chloride and its copolymers; polyacetals;
polyphenylene sulfide and ~he like.
The compositions of this inv~ntion may include a structural fiber. The structural fibers which are useful in this invention include carbon, graphite, glass, silicon carbide, poly(benzothiazole), poly(benzimidazole~, poly(benzoxazole~, alumina, titania, boron, and aromatic polyamide fibers. These fibers are characterized by a tensile strengt~ of greater than 100,000 psi, a tensile modulus of g~eater than two million psi, and a decomposition temperature of ` -` 2~93~7~
- 15 ~
greater than 200C. The fiber~ may be used in the form of contin~ous tows ~1000 to 400,000 filaments each), woven cloth, whiskers, chopped fiber or random mat. The preferred fibers are carbon fiber6, aromatic polyamide fibers, such as Kevldr 49 fiber (ohtained from E.I. duPont de Nemour~, Inc., Wilmingeon~ DE), and silicon carbide fibers.
The composition contain6 from about 20 to about 90 percent by weight of cycloaliphatic epoxide, fro~ about 15 to about 80, preferably fro~
about 20 to about 70 percent by weight of hardener.
The composition also contains from 0.1 to about 10, prefer~bly from 0.1 to about 8 percent by weight of the accelerator. The thermoplastic polymer may be used in amounts up to Z0 percent by weight of the total composition. The structural fiber may be u~ed in amounts of up to 90, preferably between about 20 and about 85 percènt by we~ht o~ the total composite.
In the compositions of this invention, the molar ratio of amine NH groups to epoxy groups i5 0.5 to 2.0, preferably 0.6 to 1.7.
Preimpregnated reinforcement may be made from the compositions of this invention by combining epoxy resins, hardener, accelerator, and optionally ~hermoplastic polymer with the structural fiber.
Preimpregnated reinforcement ~ay be prepared by ~everal techniques known in the art, such as wet winding or hot melt. In wet winding, a continuous tow of reinPorcement is passed through a resin bath cvntaining a mix~ure of the cycloaliphatic epoxide, the amine hardener, accelerator and optionally, the thermoplastic .
--~ 2~9~79 polymer. After the tow is impregnated with the resin, i~ i8 p~ssed through squeeze rolls to remove excess resin. Preferably, because of the fast curing characteristics of these compositions. the preimpregnated reinPorcement is used to make a composite article soon after it is prepared.
Composites may be preparea by curing preimpregnated reinforcement using heat and pressure. Vacuum bag~autoclave cures work well with these compositions. Laminates may also be prepared via wet layup followed by compression molding, resin transfer molding, or by resin injection, as described in European Patent Application 0019149 published November 26, 1980. Typical cure temperatures are from about 100F to about 500F, preferably from about 180F to about 450F. Cure times may be as short as from about 1 to about 2 minutes depending on the composition utilized.
The compositions of this inventisn are well suited for filament windin~. In this composite fabrication process, continuous reinforcement in the form of tape or tow--either previously impregnated with resin or impregnated during winding--is placed over a rotating and removable form or mandrel i~ a previou~ly determined pattern. Generally the shape is a surface of revolution and contain~ end clo~ure~. ~hen the proper number of layers are applied, the wound form is cured in an oYen or autoclave and the mandrel removed.
The composition of this inven~ion may be used as aircraft parts such as wing skins, wing-to-bsdy fairingE, flo~r panels, ~laps, radomes;
., .
1 7 ~
as au~omotive parts such as driveshaft~, bumpers, and spring~: and as pressure vessels, tanks and pipes. ~hey are also suitable or sporeing go~ds applications such as golf shafts, tennis rackets, and fishing rods.
In addition to structural fibers~ the composi~ion may also ccntain particulate fillers such as talc, mica, calcium carbonate, aluminum trihydrate, glass microballoons, phenolic thermospheres, and carbon black. Up to hal~ of the weight struct~ral fibers in the composition may be replaced by filler. Thixotropic agents such as fumed silica may also be used.
Further, the compositions may be used in adhesives, potting and encapsulation compounds, and in coating applications.
EXAMPLES
The following examples serve to give specific illustrations of the practice of this invention but they are not intended in any way to limit the scope of this invention.
In the Exameles which follow, the epoxy equivalent weight (EEW) is defined as the grams of epoxy resin per mole of 1,2 epoxide ~roup.
Examples 1 through ~ and Controls A through H describe effects of accelerators on the viscosity of cycloaliphatic epoxide/aromatic amine mixtures.
ExamPle 1 A 250 ml, three necked flask equipped with a paddle stirrer, thermometer with a Therm-0-~atch Controller, an inlet and outlet for nitrogen9 and an electric heating mantle was charged with 190 g o-f bis(2,3-epoxycyclopentyl) ether and 10 g of 4,4'-aihydroxyaiphenyl sulfone. The mixture was heated and s~irred at a temperature of 100C for 1 hour to dissolve the bisphenol.
A lO0 g portion of the dihydroxydiphenyl sulfone/bis(2,3-epoxycyclopentyl ether solution was placed in a 4 ounce jar in an oil ba~h maintained a~
a temperature of 66C. Then 30.7 g sf m-phenylenediamine (MPDA) was added. The mixture was stirred for about five minutes uneil the diamine dissolYed. The viscosity of the solution was measured with a Brookfield viscometer (obtained from Brookfield ~ngineering Laboratories, Stoughton, MA) at fixed intervals. The viscosity was 25 centipoises after Q.5 hours and 35 centipoises after l.0 hour. After 1.5 hours, the mixture gelled and increased in temperature.
ExamPle 2 A flask equipped as in Example l was charged with lO g of resorcinol and 190 g of bis(2,3-epoxycyclop0ntyl~ ether. ~he mixture was stirred and heated at a tempera~ure of ~0C ~or 1 hour to dissolve the resorcinol. Then a lO0 g portion of ~he solution wa~ transferred to a 4 ounce jar in an oil bath at a tempera~ure of 66C and treated with 30.7 g of MPDA. The viscosity of the mixture at various times is shown in Table I.
F.xamPle 3 A flask equipped as in Example l was charged with lO g of 4,4l-dihydroxybenzophenone and l90 g o bis(2,3-epoxycyclopentyl~ether. ~he mixture was heated at a temperature of 120~C for l hour to dissolve the diphenol. T~en a lO0 g poreion 2099~79 of the solution was tran~ferred ~o a 9 ounce jar in an oil bat~ at a temperature of 66C and treated with 30.7 9 of MPDA. The viscosity of the mixture at various times i~ shown in Table I.
Control~ A throuqh F
A series of other hydroxyl compounds were screened as accelerators for bis(2,3-epoxycyclo-pentyl) ether/MPD~ mixtures using the procedure descr;bed in Example 1. As shown by the data i~
Table I, none of these additives caused the mixture to gel in 1.5 hours. To determine if additional heating would cause gelation, samples which had been held at 66C for 1.5 hours were removed from the bath and allowed to stand for 16 hours at room temperature (23C). They were then replaced in the 66C bath. After an additional hour, the viscosity of each mixture was measured. None had gelled.
2~9~179 U U~; o o o o E
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20~9179 Example ~ and Control G describe vi6c06ity versus time behavior of 3,4-epoxycyclohexylmethyl 3 J 4-epoxycyclohexane carboxylate/MPDA mixtures.
Viscosity measurements were made on samples in the chamber of a Brookfield Thermosel viscometer (obtained from Brookfield Engineering Laboratories) maintained a~ a temperature of 66C. The accelera~ing effect of 4,4'-dihydroxydiphenyl sulfone on the cure of this epoxy formulation wa~
demonstrated by adding this compound in an ea~ily dissolvable form. A ~olution containing 20 percent by weight of 4,4'-dihydroxydiphenyl sulfone was prepared by heating the diphenol in Bakelite ERRA-0300 epoxy resin for 1 hour at a temperature of 120C. ERRA-0~00, obtained from Union Carbide, was a mixture of the solid isomers of bis(2,3-epoxycyclopentyl) ether. The solution was allowed to cool to room temperature and solidify.
This compo~ition had good stability a~ room ~emperature and was a convenient means for adding 4,4'-dihydroxydiphenyl sulfone to epoxy/amine mix~ures at moderate temperatures.
Exam~le 4 An accelerated thermosetting epoxy composition was prepared by combining:
14.0 g of 3,4-epoxycyclohexylmethyl 3,4-epoxycyclohexane carboxylate, 3.0 g of the solid solut;on of 4,4'-dihydroxydiphenyl ~ulfone in bis~
(2,3-epoxycyclopentyl) ether described above, and 3.79 9 o~ m-phenylenediamine.
at a temperature o 66C. This mixture had an NH~epoxide ~toichiometry of 1.10. Its viscosity wa~
measured as a ~unction of time. The results as shown in Table II.
Control G
A thermosetting mixture wa~ prepared by combining 19.0 g of 3,4-epoxycyclohexylmethyl 3,9-epoxycyclohexane carboxylate.
and 4.2 g of m-~henylenediamine.
The NH/epoxide stoichiometry of this mixture was 1.10. Its viscosity at a temperature of 66C was measured periodically as described in Example 4. The results are ~hown in Table II.
- 23 - 2~99~79 o r~
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Comparison of the viscosity versus ~ime data for ~xample ~ with that of Control G and Control A ~i.e., a bis(2,3-epoxycyclopentyl) ether/MPDA mixture~ shows that 4,4'-dihydroxydiphenyl sulfone is an effective accelerator when added a8 a solid solution in bis(2,3-epoxycyclopentyl) ether~
Example 5 demonstrates the storage stabili~y of bis (2,3-epoxycyclopentyl) ether/g,4'-dihydroxydiphenyl sulfone solutions.
ExamPle 5 A 100 g portion of the solution of 4,q'-dihydroxydiphenyl sulfone in bis-(2,3-epoxycyclopentyl) ether prepared a~ in Example 1 was maintained at a temperature of 66C for 96 hours. At the end of that period, the solution was a clear low viscosity fluid. Analysis of the final solution by liquid chromatography showed ~hat le~s than 2 percent of the epoxide had reacted with the diphenol.
Examples 6 through 11 and Controls M
through K describe the preparation and properties of unreinforced castings. Casting dimensions were 1/8 x 8 x 4 to 8 inches. Typically they weighed 80 to 160 g.
The general procedure for making castings was the following: The epoxy resin and accelera~or ~ere charged ~o a 3-necked flask equipped wi~h a paddle stirrer. The contents of the flask were s~irred and heated at a temperature of 85 to 100C
~til t~e accelerator aissolved. The solution was - ` 20~9~79 then cooled to a temperature of 70C. The amine hardener was a~ded to this solution. It dissolved in about 2 eo 5 minute~. The resulting solution wa~
subjected to a vacuum of about 28 inches of mercury to remove air bubbles for about 3 minutes. It was then poured into a preheated glass mold with a cavity of dimensions of 1/8 x 8 x ~ inches.
Casting~ were tested to determine tensile properties and heat deflection temperature. Ten ile properties were measured a~cordinq to AST~ D-63~
using a Type I dogbone specimen. Heat deflection tempera~ure was measured according eO ASTM D-648 (264 psi stress).
Examples 6 through 8 and Control H describe unreinforced castings made with the following cure schedule: 2 hours at 85C; 85~ to 150C at 1C~minute: 1 hour at 150C.
ExamPle 6 A solution containing 190 g of bis-(2,3-epoxycyclopentyl) ether and 10 9 of ~,4'-dihydroxydiphenyl sulfone was prepared as described in Example 1. A 60 g por~ion of this solution was blended with 18.4 9 of MPDA, poured into a mold, and cured as described above. The tensile properties and heat deflection temperature of the cured casting are given in Table III.
ExamPle 7 The pxocedure in Example 6 was repeated excep~ that the amount of 4,4'-dihydroxydiphenyl sulrone was reduced by one half. The data on this casting are sho~n in Ta~le III.
. .
2~99179 .
Control H
A thermosetting composition was prepared by blending 60 g of bis(2,3-epoxycyclopentyl) ether with 18.g g of MPDA. A casting was then prepared by the procedure as de~cribed above. The propertie~
of the casting made from this composition are shown in Table III.
ExamDle 8 A copolymer of bis(2,3-epoxycyclopentyl) ether and ethylene glycol (i.e. ERLA-~617 obtained from Union Carbide Corporation), 93.7 g, and 6.4 g of 4,4'-dihydroxydiphenyl sulfone were heated at a temperature of 100C for 0.5 hours with stirring ~o dissolve the diphenol. This solution was cooled to a temperature of 80~C and treated with 21.2 g of MPDA. This solution was poured into a mold and cured. The properties of the casting are shown in Table III.
---`"` 2~179 _I
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`` 2~9~179 Examples 9 through 11 and Control I
describe other unreinforced castings. Resin formulations, casting properties, and cure sch~dul0s are shown in Table IV.
The data in Tables III and IV show that the cure accelerators of this invention may be used with a wide variety of epoxides and aromatic amines.
In Table III, higher heat deflection temperatures are obtained in bis-(2,3-epoxycyclopentyl) ether~MPDA castings containing 4,4'-dihydroxydiphenyl sul~one than in the Con~rol. In Example 8, a high level of properties are also ob~ained with the ethylene glycol~bi~2,3-epoxycyclopentyl) ether copolymer resin. Note that the tensile strengths of all castings in Table III are very high. Other accelerators such as borontri~loride:
~onoethyla~ine complexes do not produce unrein~orcad castings wit~ such high mechanical propertie~.
Tensile strength and elongation measurements are sensitive to defects in the sample so that small difEersnces between sample6 (e.g., tensile streng~h6 of 14,000 psi versus l6,000 psi) do no~ serve as a basis of diPferen~iation. In contra6t, hea~
deflection temperature is a bulk property of the material and is much less affected by d~fects.
In Table IV, the cas~ing in Control I was so severely undercured that it could no~ be ~ested.
In contrast, the aceelerated composition of Exam21e 9 afforded a casting with good mechanical propertie~. Example 10 shows ~hat mix~ures of cycloaliphatic epoxides and glycidyl epoxides can be cured wi~h the accelerators of ~hi~ inven~ion.
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--" 2~9~179 . - .
_ 30 -ExamPle 12 - Example 12 describes the preparation of a unidirectional carbon fi~er composite using the composition o~ this invention. The prepreg is made using a polyacrylonitrile-based carbon fiber with a tensile strength of 6.6 x 10 psi and a tensile modulus of 36 X 106 pci.
A tow of carbon ~iber containing 6000 filaments is drawn through a resin bath contain;ng the resin formulation shown in E~ample 6. The impregnated fiber i6 wound on an 8 inch square frame to a thickness of approximately lJ8 inch. The impregnated fiber in the frame contains approximately 35 percent by weight of resin. The resin is cured by placing the frame in an oven and heating wieh a programmed cure cycle. The cure cycle is 2 hours at 85C to 160C at 1C/minute, hold 2 hours at 160C. The frame is removed from the oven and the cured carbon fiber composite is removed erom the frame. The composite has a high level of longitudinal and transverse tensile properties.
Claims (6)
1. A composition comprising a cycloaliphatic epoxide containing two or more epoxide groups, an aromatic amine hardener and a cure accelerator selected from:resorcinol, 4,4'-dihydroxydiphenyl sulfone, 4,4'-dihydroxydiphenyl sulfoxide,
2,2-bis(4-hydroxyphenyl) hexafluoropropane, 2,4-dihydroxybenzophenone, 4,4'-dihydroxybenzophenone, and 4,4'-dihydroxy-3,3'-dichlorodiphenyl sulfone.
2. The composition of Claim 1 wherein said hardener is selected from one or moreof the following: 4,4'-diaminodiphenyl ether, 4,4'-diaminodiphenyl methane,
2. The composition of Claim 1 wherein said hardener is selected from one or moreof the following: 4,4'-diaminodiphenyl ether, 4,4'-diaminodiphenyl methane,
3,3'-diaminodiphenyl methane, 4,4'-diaminodiphenyl sulfone, m-phenylenediamine, p-phenylenediamine, 4,4'-diaminodiphenylpropane, 4,4'-diaminodiphenyl sulfide, 1,4-bis(p-aminophenoxy) benzene, 1,3-bis(m-aminophenoxy) benzene, 1,3-bis(p-aminophenoxy) benzene, 4,4'-bis(3-aminophenoxy) diphenyl sulfone,2,2-bis(4-aminophenoxyphenyl) propane, and diethyltoluene diamine.
3. The composition of Claims 1 or 2 wherein said cycloaliphatic epoxide is bis(2,3-epoxycyclopentyl) ether.
3. The composition of Claims 1 or 2 wherein said cycloaliphatic epoxide is bis(2,3-epoxycyclopentyl) ether.
4. The composition of Claims 1-3 further comprising a structural fiber selected from the group consisting of carbon, graphite, glass boron, silicon carbide and aromatic polyamides.
5. The composition of Claim 4 in the form of a prepreg.
6. The composition of Claims 1 or 4 further comprising a therrnoplastic selectedfrom the group consisting of polysulfone, polyhydroxyether, and polyamide.
94, 342
94, 342
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA 2099179 CA2099179A1 (en) | 1993-06-25 | 1993-06-25 | Accelerated cycloaliphatic epoxide/aromatic amine resin systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA 2099179 CA2099179A1 (en) | 1993-06-25 | 1993-06-25 | Accelerated cycloaliphatic epoxide/aromatic amine resin systems |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2099179A1 true CA2099179A1 (en) | 1993-07-25 |
Family
ID=4151838
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA 2099179 Abandoned CA2099179A1 (en) | 1993-06-25 | 1993-06-25 | Accelerated cycloaliphatic epoxide/aromatic amine resin systems |
Country Status (1)
Country | Link |
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CA (1) | CA2099179A1 (en) |
-
1993
- 1993-06-25 CA CA 2099179 patent/CA2099179A1/en not_active Abandoned
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