WO2022186152A1 - Matériau résistant au feu thermo-expansible - Google Patents
Matériau résistant au feu thermo-expansible Download PDFInfo
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- WO2022186152A1 WO2022186152A1 PCT/JP2022/008347 JP2022008347W WO2022186152A1 WO 2022186152 A1 WO2022186152 A1 WO 2022186152A1 JP 2022008347 W JP2022008347 W JP 2022008347W WO 2022186152 A1 WO2022186152 A1 WO 2022186152A1
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- WO
- WIPO (PCT)
- Prior art keywords
- refractory material
- thermally expandable
- mass
- component
- ratio
- Prior art date
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- 239000000463 material Substances 0.000 title claims abstract description 27
- 230000009970 fire resistant effect Effects 0.000 title abstract description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 47
- 239000010439 graphite Substances 0.000 claims abstract description 43
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 43
- 239000011159 matrix material Substances 0.000 claims abstract description 41
- 229920005989 resin Polymers 0.000 claims abstract description 38
- 239000011347 resin Substances 0.000 claims abstract description 38
- 229920001971 elastomer Polymers 0.000 claims abstract description 19
- 239000005060 rubber Substances 0.000 claims abstract description 19
- 239000011819 refractory material Substances 0.000 claims description 115
- 229920000459 Nitrile rubber Polymers 0.000 claims description 30
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 claims description 23
- 239000005038 ethylene vinyl acetate Substances 0.000 claims description 19
- 230000001965 increasing effect Effects 0.000 claims description 16
- 239000011118 polyvinyl acetate Substances 0.000 claims description 15
- 229920002689 polyvinyl acetate Polymers 0.000 claims description 15
- XTXRWKRVRITETP-UHFFFAOYSA-N Vinyl acetate Chemical compound CC(=O)OC=C XTXRWKRVRITETP-UHFFFAOYSA-N 0.000 claims description 14
- 229920001084 poly(chloroprene) Polymers 0.000 claims description 14
- 229920003048 styrene butadiene rubber Polymers 0.000 claims description 12
- 238000010438 heat treatment Methods 0.000 claims description 11
- 150000002825 nitriles Chemical class 0.000 claims description 9
- 239000000155 melt Substances 0.000 claims description 6
- 229920002943 EPDM rubber Polymers 0.000 claims description 5
- 229920006311 Urethane elastomer Polymers 0.000 claims description 5
- 150000008360 acrylonitriles Chemical group 0.000 claims 1
- 108010094028 Prothrombin Proteins 0.000 abstract 1
- AGVAZMGAQJOSFJ-WZHZPDAFSA-M cobalt(2+);[(2r,3s,4r,5s)-5-(5,6-dimethylbenzimidazol-1-yl)-4-hydroxy-2-(hydroxymethyl)oxolan-3-yl] [(2r)-1-[3-[(1r,2r,3r,4z,7s,9z,12s,13s,14z,17s,18s,19r)-2,13,18-tris(2-amino-2-oxoethyl)-7,12,17-tris(3-amino-3-oxopropyl)-3,5,8,8,13,15,18,19-octamethyl-2 Chemical compound [Co+2].N#[C-].[N-]([C@@H]1[C@H](CC(N)=O)[C@@]2(C)CCC(=O)NC[C@@H](C)OP(O)(=O)O[C@H]3[C@H]([C@H](O[C@@H]3CO)N3C4=CC(C)=C(C)C=C4N=C3)O)\C2=C(C)/C([C@H](C\2(C)C)CCC(N)=O)=N/C/2=C\C([C@H]([C@@]/2(CC(N)=O)C)CCC(N)=O)=N\C\2=C(C)/C2=N[C@]1(C)[C@@](C)(CC(N)=O)[C@@H]2CCC(N)=O AGVAZMGAQJOSFJ-WZHZPDAFSA-M 0.000 abstract 1
- BTCSSZJGUNDROE-UHFFFAOYSA-N gamma-aminobutyric acid Chemical compound NCCCC(O)=O BTCSSZJGUNDROE-UHFFFAOYSA-N 0.000 abstract 1
- 239000003063 flame retardant Substances 0.000 description 29
- RNFJDJUURJAICM-UHFFFAOYSA-N 2,2,4,4,6,6-hexaphenoxy-1,3,5-triaza-2$l^{5},4$l^{5},6$l^{5}-triphosphacyclohexa-1,3,5-triene Chemical compound N=1P(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP=1(OC=1C=CC=CC=1)OC1=CC=CC=C1 RNFJDJUURJAICM-UHFFFAOYSA-N 0.000 description 21
- 239000003431 cross linking reagent Substances 0.000 description 21
- 239000004014 plasticizer Substances 0.000 description 20
- -1 aliphatic ester Chemical class 0.000 description 12
- 150000001875 compounds Chemical class 0.000 description 12
- 238000004132 cross linking Methods 0.000 description 12
- 239000011256 inorganic filler Substances 0.000 description 11
- 229910003475 inorganic filler Inorganic materials 0.000 description 11
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 10
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 10
- 239000002245 particle Substances 0.000 description 10
- 239000011593 sulfur Substances 0.000 description 10
- 229910052717 sulfur Inorganic materials 0.000 description 10
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 9
- 125000004432 carbon atom Chemical group C* 0.000 description 9
- 239000000126 substance Substances 0.000 description 8
- 239000000835 fiber Substances 0.000 description 7
- 229910044991 metal oxide Inorganic materials 0.000 description 7
- 150000004706 metal oxides Chemical class 0.000 description 7
- 239000000654 additive Substances 0.000 description 6
- 239000012790 adhesive layer Substances 0.000 description 6
- HJJOHHHEKFECQI-UHFFFAOYSA-N aluminum;phosphite Chemical compound [Al+3].[O-]P([O-])[O-] HJJOHHHEKFECQI-UHFFFAOYSA-N 0.000 description 6
- 239000011342 resin composition Substances 0.000 description 6
- 229920005992 thermoplastic resin Polymers 0.000 description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 230000000052 comparative effect Effects 0.000 description 5
- 238000011156 evaluation Methods 0.000 description 5
- 238000004898 kneading Methods 0.000 description 5
- 239000011787 zinc oxide Substances 0.000 description 5
- 235000014692 zinc oxide Nutrition 0.000 description 5
- 239000004114 Ammonium polyphosphate Substances 0.000 description 4
- 235000021355 Stearic acid Nutrition 0.000 description 4
- 235000019826 ammonium polyphosphate Nutrition 0.000 description 4
- 229920001276 ammonium polyphosphate Polymers 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 4
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 4
- 239000008117 stearic acid Substances 0.000 description 4
- 239000000758 substrate Substances 0.000 description 4
- XZZNDPSIHUTMOC-UHFFFAOYSA-N triphenyl phosphate Chemical compound C=1C=CC=CC=1OP(OC=1C=CC=CC=1)(=O)OC1=CC=CC=C1 XZZNDPSIHUTMOC-UHFFFAOYSA-N 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- XMNIXWIUMCBBBL-UHFFFAOYSA-N 2-(2-phenylpropan-2-ylperoxy)propan-2-ylbenzene Chemical compound C=1C=CC=CC=1C(C)(C)OOC(C)(C)C1=CC=CC=C1 XMNIXWIUMCBBBL-UHFFFAOYSA-N 0.000 description 3
- 239000005062 Polybutadiene Substances 0.000 description 3
- 230000000996 additive effect Effects 0.000 description 3
- 150000007933 aliphatic carboxylic acids Chemical class 0.000 description 3
- 239000002585 base Substances 0.000 description 3
- SCABKEBYDRTODC-UHFFFAOYSA-N bis[2-(2-butoxyethoxy)ethyl] hexanedioate Chemical compound CCCCOCCOCCOC(=O)CCCCC(=O)OCCOCCOCCCC SCABKEBYDRTODC-UHFFFAOYSA-N 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 3
- RTZKZFJDLAIYFH-UHFFFAOYSA-N ether Substances CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 3
- 229910000000 metal hydroxide Inorganic materials 0.000 description 3
- 150000004692 metal hydroxides Chemical class 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000007800 oxidant agent Substances 0.000 description 3
- VLTRZXGMWDSKGL-UHFFFAOYSA-N perchloric acid Chemical compound OCl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-N 0.000 description 3
- 229920002857 polybutadiene Polymers 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- UWNADWZGEHDQAB-UHFFFAOYSA-N 2,5-dimethylhexane Chemical compound CC(C)CCC(C)C UWNADWZGEHDQAB-UHFFFAOYSA-N 0.000 description 2
- OZAIFHULBGXAKX-UHFFFAOYSA-N 2-(2-cyanopropan-2-yldiazenyl)-2-methylpropanenitrile Chemical compound N#CC(C)(C)N=NC(C)(C)C#N OZAIFHULBGXAKX-UHFFFAOYSA-N 0.000 description 2
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-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
- MQIUGAXCHLFZKX-UHFFFAOYSA-N Di-n-octyl phthalate Chemical compound CCCCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCCC MQIUGAXCHLFZKX-UHFFFAOYSA-N 0.000 description 2
- XTJFFFGAUHQWII-UHFFFAOYSA-N Dibutyl adipate Chemical compound CCCCOC(=O)CCCCC(=O)OCCCC XTJFFFGAUHQWII-UHFFFAOYSA-N 0.000 description 2
- RDOFJDLLWVCMRU-UHFFFAOYSA-N Diisobutyl adipate Chemical compound CC(C)COC(=O)CCCCC(=O)OCC(C)C RDOFJDLLWVCMRU-UHFFFAOYSA-N 0.000 description 2
- ZVFDTKUVRCTHQE-UHFFFAOYSA-N Diisodecyl phthalate Chemical compound CC(C)CCCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCCC(C)C ZVFDTKUVRCTHQE-UHFFFAOYSA-N 0.000 description 2
- ZRALSGWEFCBTJO-UHFFFAOYSA-N Guanidine Chemical compound NC(N)=N ZRALSGWEFCBTJO-UHFFFAOYSA-N 0.000 description 2
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 description 2
- CSNNHWWHGAXBCP-UHFFFAOYSA-L Magnesium sulfate Chemical compound [Mg+2].[O-][S+2]([O-])([O-])[O-] CSNNHWWHGAXBCP-UHFFFAOYSA-L 0.000 description 2
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- 239000004820 Pressure-sensitive adhesive Substances 0.000 description 2
- 229920004411 Skyprene® Polymers 0.000 description 2
- 239000002174 Styrene-butadiene Substances 0.000 description 2
- FZWLAAWBMGSTSO-UHFFFAOYSA-N Thiazole Chemical compound C1=CSC=N1 FZWLAAWBMGSTSO-UHFFFAOYSA-N 0.000 description 2
- 239000001361 adipic acid Substances 0.000 description 2
- 235000011037 adipic acid Nutrition 0.000 description 2
- 150000001298 alcohols Chemical class 0.000 description 2
- 125000000217 alkyl group Chemical group 0.000 description 2
- 125000003118 aryl group Chemical group 0.000 description 2
- TZCXTZWJZNENPQ-UHFFFAOYSA-L barium sulfate Chemical compound [Ba+2].[O-]S([O-])(=O)=O TZCXTZWJZNENPQ-UHFFFAOYSA-L 0.000 description 2
- IOJUPLGTWVMSFF-UHFFFAOYSA-N benzothiazole Chemical compound C1=CC=C2SC=NC2=C1 IOJUPLGTWVMSFF-UHFFFAOYSA-N 0.000 description 2
- SAOKZLXYCUGLFA-UHFFFAOYSA-N bis(2-ethylhexyl) adipate Chemical compound CCCCC(CC)COC(=O)CCCCC(=O)OCC(CC)CCCC SAOKZLXYCUGLFA-UHFFFAOYSA-N 0.000 description 2
- BJQHLKABXJIVAM-UHFFFAOYSA-N bis(2-ethylhexyl) phthalate Chemical compound CCCCC(CC)COC(=O)C1=CC=CC=C1C(=O)OCC(CC)CCCC BJQHLKABXJIVAM-UHFFFAOYSA-N 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 239000004927 clay Substances 0.000 description 2
- 229940100539 dibutyl adipate Drugs 0.000 description 2
- 229940031769 diisobutyl adipate Drugs 0.000 description 2
- HBGGXOJOCNVPFY-UHFFFAOYSA-N diisononyl phthalate Chemical compound CC(C)CCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCC(C)C HBGGXOJOCNVPFY-UHFFFAOYSA-N 0.000 description 2
- PXJJSXABGXMUSU-UHFFFAOYSA-N disulfur dichloride Chemical compound ClSSCl PXJJSXABGXMUSU-UHFFFAOYSA-N 0.000 description 2
- QQVHEQUEHCEAKS-UHFFFAOYSA-N diundecyl benzene-1,2-dicarboxylate Chemical compound CCCCCCCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCCCCCC QQVHEQUEHCEAKS-UHFFFAOYSA-N 0.000 description 2
- 238000005227 gel permeation chromatography Methods 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- WNLRTRBMVRJNCN-UHFFFAOYSA-N hexanedioic acid Natural products OC(=O)CCCCC(O)=O WNLRTRBMVRJNCN-UHFFFAOYSA-N 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 2
- 239000001095 magnesium carbonate Substances 0.000 description 2
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910017604 nitric acid Inorganic materials 0.000 description 2
- 150000001451 organic peroxides Chemical class 0.000 description 2
- 150000003014 phosphoric acid esters Chemical class 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- KUAZQDVKQLNFPE-UHFFFAOYSA-N thiram Chemical compound CN(C)C(=S)SSC(=S)N(C)C KUAZQDVKQLNFPE-UHFFFAOYSA-N 0.000 description 2
- 229960002447 thiram Drugs 0.000 description 2
- BIKXLKXABVUSMH-UHFFFAOYSA-N trizinc;diborate Chemical compound [Zn+2].[Zn+2].[Zn+2].[O-]B([O-])[O-].[O-]B([O-])[O-] BIKXLKXABVUSMH-UHFFFAOYSA-N 0.000 description 2
- QEQBMZQFDDDTPN-UHFFFAOYSA-N (2-methylpropan-2-yl)oxy benzenecarboperoxoate Chemical compound CC(C)(C)OOOC(=O)C1=CC=CC=C1 QEQBMZQFDDDTPN-UHFFFAOYSA-N 0.000 description 1
- NALFRYPTRXKZPN-UHFFFAOYSA-N 1,1-bis(tert-butylperoxy)-3,3,5-trimethylcyclohexane Chemical compound CC1CC(C)(C)CC(OOC(C)(C)C)(OOC(C)(C)C)C1 NALFRYPTRXKZPN-UHFFFAOYSA-N 0.000 description 1
- HSLFISVKRDQEBY-UHFFFAOYSA-N 1,1-bis(tert-butylperoxy)cyclohexane Chemical compound CC(C)(C)OOC1(OOC(C)(C)C)CCCCC1 HSLFISVKRDQEBY-UHFFFAOYSA-N 0.000 description 1
- ZNCDSAZBKYUMAB-UHFFFAOYSA-N 1,1-bis(tert-butylperoxy)octane Chemical compound CCCCCCCC(OOC(C)(C)C)OOC(C)(C)C ZNCDSAZBKYUMAB-UHFFFAOYSA-N 0.000 description 1
- NYYLZXREFNYPKB-UHFFFAOYSA-N 1-[ethoxy(methyl)phosphoryl]oxyethane Chemical compound CCOP(C)(=O)OCC NYYLZXREFNYPKB-UHFFFAOYSA-N 0.000 description 1
- HQOVXPHOJANJBR-UHFFFAOYSA-N 2,2-bis(tert-butylperoxy)butane Chemical compound CC(C)(C)OOC(C)(CC)OOC(C)(C)C HQOVXPHOJANJBR-UHFFFAOYSA-N 0.000 description 1
- OHASXDUBONILDR-UHFFFAOYSA-N 2,3-dimethylbutylphosphonic acid Chemical compound CC(C)C(C)CP(O)(O)=O OHASXDUBONILDR-UHFFFAOYSA-N 0.000 description 1
- ODBCKCWTWALFKM-UHFFFAOYSA-N 2,5-bis(tert-butylperoxy)-2,5-dimethylhex-3-yne Chemical compound CC(C)(C)OOC(C)(C)C#CC(C)(C)OOC(C)(C)C ODBCKCWTWALFKM-UHFFFAOYSA-N 0.000 description 1
- DMWVYCCGCQPJEA-UHFFFAOYSA-N 2,5-bis(tert-butylperoxy)-2,5-dimethylhexane Chemical compound CC(C)(C)OOC(C)(C)CCC(C)(C)OOC(C)(C)C DMWVYCCGCQPJEA-UHFFFAOYSA-N 0.000 description 1
- WYGWHHGCAGTUCH-UHFFFAOYSA-N 2-[(2-cyano-4-methylpentan-2-yl)diazenyl]-2,4-dimethylpentanenitrile Chemical compound CC(C)CC(C)(C#N)N=NC(C)(C#N)CC(C)C WYGWHHGCAGTUCH-UHFFFAOYSA-N 0.000 description 1
- LIAWCKFOFPPVGF-UHFFFAOYSA-N 2-ethyladamantane Chemical compound C1C(C2)CC3CC1C(CC)C2C3 LIAWCKFOFPPVGF-UHFFFAOYSA-N 0.000 description 1
- 239000004808 2-ethylhexylester Substances 0.000 description 1
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- HLBZWYXLQJQBKU-UHFFFAOYSA-N 4-(morpholin-4-yldisulfanyl)morpholine Chemical compound C1COCCN1SSN1CCOCC1 HLBZWYXLQJQBKU-UHFFFAOYSA-N 0.000 description 1
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- AXKPBIUQVYVDHP-UHFFFAOYSA-N CCc1cccc(c1CC)P(O)=O Chemical compound CCc1cccc(c1CC)P(O)=O AXKPBIUQVYVDHP-UHFFFAOYSA-N 0.000 description 1
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- NEHDRDVHPTWWFG-UHFFFAOYSA-N Dioctyl hexanedioate Chemical compound CCCCCCCCOC(=O)CCCCC(=O)OCCCCCCCC NEHDRDVHPTWWFG-UHFFFAOYSA-N 0.000 description 1
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- QLZHNIAADXEJJP-UHFFFAOYSA-N Phenylphosphonic acid Chemical compound OP(O)(=O)C1=CC=CC=C1 QLZHNIAADXEJJP-UHFFFAOYSA-N 0.000 description 1
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- YSMRWXYRXBRSND-UHFFFAOYSA-N TOTP Chemical compound CC1=CC=CC=C1OP(=O)(OC=1C(=CC=CC=1)C)OC1=CC=CC=C1C YSMRWXYRXBRSND-UHFFFAOYSA-N 0.000 description 1
- KRADHMIOFJQKEZ-UHFFFAOYSA-N Tri-2-ethylhexyl trimellitate Chemical compound CCCCC(CC)COC(=O)C1=CC=C(C(=O)OCC(CC)CCCC)C(C(=O)OCC(CC)CCCC)=C1 KRADHMIOFJQKEZ-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
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- 125000001931 aliphatic group Chemical group 0.000 description 1
- 150000001339 alkali metal compounds Chemical class 0.000 description 1
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- 125000003545 alkoxy group Chemical group 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
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- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- OJMOMXZKOWKUTA-UHFFFAOYSA-N aluminum;borate Chemical compound [Al+3].[O-]B([O-])[O-] OJMOMXZKOWKUTA-UHFFFAOYSA-N 0.000 description 1
- VCNTUJWBXWAWEJ-UHFFFAOYSA-J aluminum;sodium;dicarbonate Chemical compound [Na+].[Al+3].[O-]C([O-])=O.[O-]C([O-])=O VCNTUJWBXWAWEJ-UHFFFAOYSA-J 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 230000003712 anti-aging effect Effects 0.000 description 1
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- 125000004104 aryloxy group Chemical group 0.000 description 1
- AYJRCSIUFZENHW-DEQYMQKBSA-L barium(2+);oxomethanediolate Chemical compound [Ba+2].[O-][14C]([O-])=O AYJRCSIUFZENHW-DEQYMQKBSA-L 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 239000000440 bentonite Substances 0.000 description 1
- 229910000278 bentonite Inorganic materials 0.000 description 1
- SVPXDRXYRYOSEX-UHFFFAOYSA-N bentoquatam Chemical compound O.O=[Si]=O.O=[Al]O[Al]=O SVPXDRXYRYOSEX-UHFFFAOYSA-N 0.000 description 1
- 235000019400 benzoyl peroxide Nutrition 0.000 description 1
- ZDWGXBPVPXVXMQ-UHFFFAOYSA-N bis(2-ethylhexyl) nonanedioate Chemical compound CCCCC(CC)COC(=O)CCCCCCCC(=O)OCC(CC)CCCC ZDWGXBPVPXVXMQ-UHFFFAOYSA-N 0.000 description 1
- BFPBWJGVRNQWEK-UHFFFAOYSA-N bis(4-methoxyphenyl)phosphinic acid Chemical compound C1=CC(OC)=CC=C1P(O)(=O)C1=CC=C(OC)C=C1 BFPBWJGVRNQWEK-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 239000011449 brick Substances 0.000 description 1
- 239000004566 building material Substances 0.000 description 1
- 229920005549 butyl rubber Polymers 0.000 description 1
- UOKRBSXOBUKDGE-UHFFFAOYSA-N butylphosphonic acid Chemical compound CCCCP(O)(O)=O UOKRBSXOBUKDGE-UHFFFAOYSA-N 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- AXCZMVOFGPJBDE-UHFFFAOYSA-L calcium dihydroxide Chemical compound [OH-].[OH-].[Ca+2] AXCZMVOFGPJBDE-UHFFFAOYSA-L 0.000 description 1
- 239000000920 calcium hydroxide Substances 0.000 description 1
- 229910001861 calcium hydroxide Inorganic materials 0.000 description 1
- 239000000378 calcium silicate Substances 0.000 description 1
- 229910052918 calcium silicate Inorganic materials 0.000 description 1
- OYACROKNLOSFPA-UHFFFAOYSA-N calcium;dioxido(oxo)silane Chemical compound [Ca+2].[O-][Si]([O-])=O OYACROKNLOSFPA-UHFFFAOYSA-N 0.000 description 1
- DKVNPHBNOWQYFE-UHFFFAOYSA-N carbamodithioic acid Chemical compound NC(S)=S DKVNPHBNOWQYFE-UHFFFAOYSA-N 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 150000004649 carbonic acid derivatives Chemical class 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 239000002801 charged material Substances 0.000 description 1
- 229910052570 clay Inorganic materials 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 239000003484 crystal nucleating agent Substances 0.000 description 1
- 229910001647 dawsonite Inorganic materials 0.000 description 1
- GUJOJGAPFQRJSV-UHFFFAOYSA-N dialuminum;dioxosilane;oxygen(2-);hydrate Chemical compound O.[O-2].[O-2].[O-2].[Al+3].[Al+3].O=[Si]=O.O=[Si]=O.O=[Si]=O.O=[Si]=O GUJOJGAPFQRJSV-UHFFFAOYSA-N 0.000 description 1
- GDVKFRBCXAPAQJ-UHFFFAOYSA-A dialuminum;hexamagnesium;carbonate;hexadecahydroxide Chemical compound [OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[OH-].[Mg+2].[Mg+2].[Mg+2].[Mg+2].[Mg+2].[Mg+2].[Al+3].[Al+3].[O-]C([O-])=O GDVKFRBCXAPAQJ-UHFFFAOYSA-A 0.000 description 1
- HCQHIEGYGGJLJU-UHFFFAOYSA-N didecyl hexanedioate Chemical compound CCCCCCCCCCOC(=O)CCCCC(=O)OCCCCCCCCCC HCQHIEGYGGJLJU-UHFFFAOYSA-N 0.000 description 1
- KTLIMPGQZDZPSB-UHFFFAOYSA-N diethylphosphinic acid Chemical compound CCP(O)(=O)CC KTLIMPGQZDZPSB-UHFFFAOYSA-N 0.000 description 1
- VONWDASPFIQPDY-UHFFFAOYSA-N dimethyl methylphosphonate Chemical compound COP(C)(=O)OC VONWDASPFIQPDY-UHFFFAOYSA-N 0.000 description 1
- SWSQBOPZIKWTGO-UHFFFAOYSA-N dimethylaminoamidine Natural products CN(C)C(N)=N SWSQBOPZIKWTGO-UHFFFAOYSA-N 0.000 description 1
- GOJNABIZVJCYFL-UHFFFAOYSA-N dimethylphosphinic acid Chemical compound CP(C)(O)=O GOJNABIZVJCYFL-UHFFFAOYSA-N 0.000 description 1
- HAKMAMKAFTZXOZ-UHFFFAOYSA-N dioctoxyphosphorylbenzene Chemical compound CCCCCCCCOP(=O)(OCCCCCCCC)C1=CC=CC=C1 HAKMAMKAFTZXOZ-UHFFFAOYSA-N 0.000 description 1
- VJHINFRRDQUWOJ-UHFFFAOYSA-N dioctyl sebacate Chemical compound CCCCC(CC)COC(=O)CCCCCCCCC(=O)OCC(CC)CCCC VJHINFRRDQUWOJ-UHFFFAOYSA-N 0.000 description 1
- YTMRJBAHYSIRMZ-UHFFFAOYSA-N dioctylphosphinic acid Chemical compound CCCCCCCCP(O)(=O)CCCCCCCC YTMRJBAHYSIRMZ-UHFFFAOYSA-N 0.000 description 1
- 150000002013 dioxins Chemical class 0.000 description 1
- BEQVQKJCLJBTKZ-UHFFFAOYSA-N diphenylphosphinic acid Chemical compound C=1C=CC=CC=1P(=O)(O)C1=CC=CC=C1 BEQVQKJCLJBTKZ-UHFFFAOYSA-N 0.000 description 1
- NJLLQSBAHIKGKF-UHFFFAOYSA-N dipotassium dioxido(oxo)titanium Chemical compound [K+].[K+].[O-][Ti]([O-])=O NJLLQSBAHIKGKF-UHFFFAOYSA-N 0.000 description 1
- YXXXKCDYKKSZHL-UHFFFAOYSA-M dipotassium;dioxido(oxo)phosphanium Chemical compound [K+].[K+].[O-][P+]([O-])=O YXXXKCDYKKSZHL-UHFFFAOYSA-M 0.000 description 1
- 239000002270 dispersing agent Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000012990 dithiocarbamate Substances 0.000 description 1
- 239000000975 dye Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 229920005558 epichlorohydrin rubber Polymers 0.000 description 1
- NXHKQBCTZHECQF-UHFFFAOYSA-N ethyl(methyl)phosphinic acid Chemical compound CCP(C)(O)=O NXHKQBCTZHECQF-UHFFFAOYSA-N 0.000 description 1
- GATNOFPXSDHULC-UHFFFAOYSA-N ethylphosphonic acid Chemical compound CCP(O)(O)=O GATNOFPXSDHULC-UHFFFAOYSA-N 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 229920001973 fluoroelastomer Polymers 0.000 description 1
- 239000010881 fly ash Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 238000001879 gelation Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229920001519 homopolymer Polymers 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 229910001701 hydrotalcite Inorganic materials 0.000 description 1
- 229960001545 hydrotalcite Drugs 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- BDAGIHXWWSANSR-NJFSPNSNSA-N hydroxyformaldehyde Chemical compound O[14CH]=O BDAGIHXWWSANSR-NJFSPNSNSA-N 0.000 description 1
- 229920002681 hypalon Polymers 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000009830 intercalation Methods 0.000 description 1
- 230000002687 intercalation Effects 0.000 description 1
- 229920003049 isoprene rubber Polymers 0.000 description 1
- HFGPZNIAWCZYJU-UHFFFAOYSA-N lead zirconate titanate Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[Ti+4].[Zr+4].[Pb+2] HFGPZNIAWCZYJU-UHFFFAOYSA-N 0.000 description 1
- 229910052451 lead zirconate titanate Inorganic materials 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- VTHJTEIRLNZDEV-UHFFFAOYSA-L magnesium dihydroxide Chemical compound [OH-].[OH-].[Mg+2] VTHJTEIRLNZDEV-UHFFFAOYSA-L 0.000 description 1
- 239000000347 magnesium hydroxide Substances 0.000 description 1
- 229910001862 magnesium hydroxide Inorganic materials 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- 229910052943 magnesium sulfate Inorganic materials 0.000 description 1
- 235000019341 magnesium sulphate Nutrition 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 239000006247 magnetic powder Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- SZTJCIYEOQYVED-UHFFFAOYSA-N methyl(propyl)phosphinic acid Chemical compound CCCP(C)(O)=O SZTJCIYEOQYVED-UHFFFAOYSA-N 0.000 description 1
- YACKEPLHDIMKIO-UHFFFAOYSA-N methylphosphonic acid Chemical compound CP(O)(O)=O YACKEPLHDIMKIO-UHFFFAOYSA-N 0.000 description 1
- 239000010445 mica Substances 0.000 description 1
- 229910052618 mica group Inorganic materials 0.000 description 1
- 239000002480 mineral oil Substances 0.000 description 1
- 235000010446 mineral oil Nutrition 0.000 description 1
- 150000007522 mineralic acids Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 1
- 229910052901 montmorillonite Inorganic materials 0.000 description 1
- 229920003052 natural elastomer Polymers 0.000 description 1
- 229920001194 natural rubber Polymers 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- XNGIFLGASWRNHJ-UHFFFAOYSA-N o-dicarboxybenzene Natural products OC(=O)C1=CC=CC=C1C(O)=O XNGIFLGASWRNHJ-UHFFFAOYSA-N 0.000 description 1
- NJGCRMAPOWGWMW-UHFFFAOYSA-N octylphosphonic acid Chemical compound CCCCCCCCP(O)(O)=O NJGCRMAPOWGWMW-UHFFFAOYSA-N 0.000 description 1
- QRMPKOFEUHIBNM-UHFFFAOYSA-N p-dimethylcyclohexane Natural products CC1CCC(C)CC1 QRMPKOFEUHIBNM-UHFFFAOYSA-N 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- MLCHBQKMVKNBOV-UHFFFAOYSA-N phenylphosphinic acid Chemical compound OP(=O)C1=CC=CC=C1 MLCHBQKMVKNBOV-UHFFFAOYSA-N 0.000 description 1
- ZOGYOOUMDVKYLM-UHFFFAOYSA-N phosphane phosphorous acid Chemical class P.OP(O)O ZOGYOOUMDVKYLM-UHFFFAOYSA-N 0.000 description 1
- 150000003021 phthalic acid derivatives Chemical class 0.000 description 1
- JQCXWCOOWVGKMT-UHFFFAOYSA-N phthalic acid diheptyl ester Natural products CCCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCC JQCXWCOOWVGKMT-UHFFFAOYSA-N 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 229920002589 poly(vinylethylene) polymer Polymers 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 229920006350 polyacrylonitrile resin Polymers 0.000 description 1
- 229920005668 polycarbonate resin Polymers 0.000 description 1
- 239000004431 polycarbonate resin Substances 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920013716 polyethylene resin Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920005672 polyolefin resin Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 229920001021 polysulfide Polymers 0.000 description 1
- 239000005077 polysulfide Substances 0.000 description 1
- 150000008117 polysulfides Polymers 0.000 description 1
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 1
- 239000004810 polytetrafluoroethylene Substances 0.000 description 1
- 239000004800 polyvinyl chloride Substances 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 239000010734 process oil Substances 0.000 description 1
- NSETWVJZUWGCKE-UHFFFAOYSA-N propylphosphonic acid Chemical compound CCCP(O)(O)=O NSETWVJZUWGCKE-UHFFFAOYSA-N 0.000 description 1
- 229920005604 random copolymer Polymers 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000012744 reinforcing agent Substances 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
- QYHFIVBSNOWOCQ-UHFFFAOYSA-N selenic acid Chemical compound O[Se](O)(=O)=O QYHFIVBSNOWOCQ-UHFFFAOYSA-N 0.000 description 1
- 229910052624 sepiolite Inorganic materials 0.000 description 1
- 235000019355 sepiolite Nutrition 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 229920002379 silicone rubber Polymers 0.000 description 1
- 239000004945 silicone rubber Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000010802 sludge Substances 0.000 description 1
- 239000001488 sodium phosphate Substances 0.000 description 1
- 229910000162 sodium phosphate Inorganic materials 0.000 description 1
- 229910000018 strontium carbonate Inorganic materials 0.000 description 1
- QAZLUNIWYYOJPC-UHFFFAOYSA-M sulfenamide Chemical compound [Cl-].COC1=C(C)C=[N+]2C3=NC4=CC=C(OC)C=C4N3SCC2=C1C QAZLUNIWYYOJPC-UHFFFAOYSA-M 0.000 description 1
- FWMUJAIKEJWSSY-UHFFFAOYSA-N sulfur dichloride Chemical compound ClSCl FWMUJAIKEJWSSY-UHFFFAOYSA-N 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N sulfuric acid Substances OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- 239000012756 surface treatment agent Substances 0.000 description 1
- 239000004094 surface-active agent Substances 0.000 description 1
- 230000008961 swelling Effects 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- ISIJQEHRDSCQIU-UHFFFAOYSA-N tert-butyl 2,7-diazaspiro[4.5]decane-7-carboxylate Chemical compound C1N(C(=O)OC(C)(C)C)CCCC11CNCC1 ISIJQEHRDSCQIU-UHFFFAOYSA-N 0.000 description 1
- DLSMLZRPNPCXGY-UHFFFAOYSA-N tert-butylperoxy 2-ethylhexyl carbonate Chemical compound CCCCC(CC)COC(=O)OOOC(C)(C)C DLSMLZRPNPCXGY-UHFFFAOYSA-N 0.000 description 1
- OGDSVONAYZTTDA-UHFFFAOYSA-N tert-butylphosphonic acid Chemical compound CC(C)(C)P(O)(O)=O OGDSVONAYZTTDA-UHFFFAOYSA-N 0.000 description 1
- 229920002803 thermoplastic polyurethane Polymers 0.000 description 1
- 150000003557 thiazoles Chemical class 0.000 description 1
- VMFOHNMEJNFJAE-UHFFFAOYSA-N trimagnesium;diphosphite Chemical compound [Mg+2].[Mg+2].[Mg+2].[O-]P([O-])[O-].[O-]P([O-])[O-] VMFOHNMEJNFJAE-UHFFFAOYSA-N 0.000 description 1
- 125000005591 trimellitate group Chemical group 0.000 description 1
- JNXDCMUUZNIWPQ-UHFFFAOYSA-N trioctyl benzene-1,2,4-tricarboxylate Chemical compound CCCCCCCCOC(=O)C1=CC=C(C(=O)OCCCCCCCC)C(C(=O)OCCCCCCCC)=C1 JNXDCMUUZNIWPQ-UHFFFAOYSA-N 0.000 description 1
- KOWVWXQNQNCRRS-UHFFFAOYSA-N tris(2,4-dimethylphenyl) phosphate Chemical compound CC1=CC(C)=CC=C1OP(=O)(OC=1C(=CC(C)=CC=1)C)OC1=CC=C(C)C=C1C KOWVWXQNQNCRRS-UHFFFAOYSA-N 0.000 description 1
- FJFYFBRNDHRTHL-UHFFFAOYSA-N tris(8-methylnonyl) benzene-1,2,4-tricarboxylate Chemical compound CC(C)CCCCCCCOC(=O)C1=CC=C(C(=O)OCCCCCCCC(C)C)C(C(=O)OCCCCCCCC(C)C)=C1 FJFYFBRNDHRTHL-UHFFFAOYSA-N 0.000 description 1
- SMYKBXMWXCZOLU-UHFFFAOYSA-N tris-decyl benzene-1,2,4-tricarboxylate Chemical compound CCCCCCCCCCOC(=O)C1=CC=C(C(=O)OCCCCCCCCCC)C(C(=O)OCCCCCCCCCC)=C1 SMYKBXMWXCZOLU-UHFFFAOYSA-N 0.000 description 1
- RYFMWSXOAZQYPI-UHFFFAOYSA-K trisodium phosphate Chemical compound [Na+].[Na+].[Na+].[O-]P([O-])([O-])=O RYFMWSXOAZQYPI-UHFFFAOYSA-K 0.000 description 1
- NCPXQVVMIXIKTN-UHFFFAOYSA-N trisodium;phosphite Chemical compound [Na+].[Na+].[Na+].[O-]P([O-])[O-] NCPXQVVMIXIKTN-UHFFFAOYSA-N 0.000 description 1
- 239000004636 vulcanized rubber Substances 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011667 zinc carbonate Substances 0.000 description 1
- 235000004416 zinc carbonate Nutrition 0.000 description 1
- 229910000010 zinc carbonate Inorganic materials 0.000 description 1
- PGNWIWKMXVDXHP-UHFFFAOYSA-L zinc;1,3-benzothiazole-2-thiolate Chemical compound [Zn+2].C1=CC=C2SC([S-])=NC2=C1.C1=CC=C2SC([S-])=NC2=C1 PGNWIWKMXVDXHP-UHFFFAOYSA-L 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C2/00—Fire prevention or containment
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K3/00—Use of inorganic substances as compounding ingredients
- C08K3/02—Elements
- C08K3/04—Carbon
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L101/00—Compositions of unspecified macromolecular compounds
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L21/00—Compositions of unspecified rubbers
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09K—MATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
- C09K21/00—Fireproofing materials
- C09K21/02—Inorganic materials
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B5/00—Doors, windows, or like closures for special purposes; Border constructions therefor
- E06B5/10—Doors, windows, or like closures for special purposes; Border constructions therefor for protection against air-raid or other war-like action; for other protective purposes
- E06B5/16—Fireproof doors or similar closures; Adaptations of fixed constructions therefor
Definitions
- the present invention relates to a thermally expandable refractory material containing thermally expandable graphite.
- fireproof materials are used for building materials such as fittings, columns, and wall materials for fire prevention.
- a thermally expandable refractory material or the like in which thermally expandable graphite is blended with a resin in addition to a flame retardant, an inorganic filler, or the like is used (see, for example, Patent Document 1).
- Such a thermally expandable refractory material expands when heated, and the combustion residue forms a refractory and heat insulating layer, thereby exhibiting refractory and heat insulating performance.
- the thermally expandable refractory material containing thermally expandable graphite is provided, for example, in the gap between fittings such as doors and windows provided in openings of buildings and frames such as door frames and window frames surrounding these.
- the sheet expands in the thickness direction to block the gap between the fitting and the frame material, thereby preventing the spread of the fire.
- thermally expandable refractory material containing thermally expandable graphite in the case of a refractory material that cannot expand sufficiently when heated at a slow heating rate, the surface of the door or window that is not in contact with the flame (non-heated surface) ), it was found that the refractory material strength on the non-heated surface was brittle and sufficient refractoriness was not exhibited.
- SUMMARY OF THE INVENTION Accordingly, it is an object of the present invention to provide a thermally expansible fire-resistant material that can expand sufficiently even when the temperature is raised at a slow heating rate and that has excellent fire resistance.
- thermally expandable refractory material containing at least one matrix component selected from resins and rubber components and thermally expandable graphite contains a specific It has been found that the above problem can be solved by setting the ratio (II/I) between the expansion ratio (expansion ratio I) and the expansion ratio (expansion ratio II) within a predetermined range.
- the gist of the present invention is as follows [1] to [10].
- the thermally expandable refractory material according to any one of [1] to [4], wherein the content of the thermally expandable graphite is 20 to 500 parts by mass with respect to 100 parts by mass of the matrix component.
- the matrix component is at least one selected from the group consisting of ethylene-vinyl acetate copolymer, polyvinyl acetate resin, styrene-butadiene rubber, acrylonitrile-butadiene rubber, urethane elastomer, chloroprene rubber, and EPDM.
- the thermally expandable fireproof material according to any one of [1] to [5].
- the thermally expandable refractory material according to any one of [1] to [6], wherein the rubber component is acrylonitrile-butadiene rubber having a nitrile content of 10 to 35% by mass.
- the thermally expandable fireproof material according to any one of [1] to [7], wherein the rubber component is an acrylo-nitrile-butadiene rubber having a Mooney viscosity of 30 to 80 at 100°C.
- the resin is at least one selected from the group consisting of an ethylene-vinyl acetate copolymer containing a high Vac component having a vinyl acetate content of 20% by mass or more, and a polyvinyl acetate resin. ] to [8].
- the thermally expandable refractory material of the present invention is a thermally expandable refractory material containing a matrix component and thermally expandable graphite, and comprises an expansion ratio (expansion ratio I) when the refractory material is expanded at 300° C.,
- the ratio (II/I) of the expansion ratio (expansion ratio II) when the refractory material is expanded by increasing the temperature from 20° C. to 300° C. at a heating rate of 5° C./min is 0.5 to 1.0.
- the thermally expandable fireproof material of the present invention may be simply referred to as fireproof material.
- the refractory material of the present invention has an expansion ratio (expansion ratio I) when the refractory material is expanded at 300 ° C., and the refractory material is heated from 20 ° C. to 300 ° C. at a heating rate of 5 ° C./min.
- the ratio (II/I) of the expansion ratio (expansion ratio II) when the material is expanded (hereinafter referred to as “ratio (II/I)”) is 0.5 to 1.0. If the ratio (II/I) is less than the above lower limit, the refractory material will not expand sufficiently when the temperature of the refractory material is gradually increased, and the fire resistance will be impaired. From this point of view, the ratio (II/I) is preferably 0.6 or more, more preferably 0.7 or more. The ratio (II/I) can be adjusted by appropriately selecting matrix components.
- the expansion ratio II in the refractory material of the present invention is 7 from the viewpoint that the refractory material expands sufficiently even when the temperature of the refractory material is gradually increased, and the ratio (II/I) can be easily adjusted to the desired range. It is preferably at least 15 times, more preferably at least 30 times, even more preferably at least 30 times. On the other hand, although the upper limit of the expansion ratio II is not particularly limited, it is preferably 55 times or less, more preferably 50 times or less, and still more preferably from the viewpoint of maintaining a certain level or more of the residue residual rate and residue hardness. 45 times or less.
- the expansion ratio I in the refractory material of the present invention is not particularly limited as long as the ratio (II/I) satisfies the above range. From the viewpoint of security, it is preferably 8 times or more, more preferably 17 times or more, still more preferably 33 times or more, and preferably 70 times or less, more preferably 60 times or less, further preferably 50 times or less.
- the refractory material of the present invention contains at least one matrix component selected from rubber components and resins.
- the matrix component is preferably a rubber component.
- Rubber components include natural rubber, isoprene rubber, butyl rubber, butadiene rubber (BR), 1,2-polybutadiene rubber, styrene-butadiene rubber (SBR), chloroprene rubber, acrylonitrile rubber-butadiene rubber (NBR), ethylene- Propylene rubber, ethylene-propylene-diene rubber (EPDM), chlorosulfonated polyethylene, acrylic rubber, epichlorohydrin rubber, polyvulcanized rubber, non-vulcanized rubber, silicone rubber, fluororubber, urethane elastomer and the like.
- natural rubber isoprene rubber, butyl rubber, butadiene rubber (BR), 1,2-polybutadiene rubber, styrene-butadiene rubber (SBR), chloroprene rubber, acrylonitrile rubber-butadiene rubber (NBR), ethylene- Propylene rubber, ethylene-propylene-diene rubber (EPDM), chlorosulfon
- At least one selected from the group consisting of acrylonitrile-butadiene rubber, chloroprene rubber, and styrene-butadiene rubber is more preferable from the viewpoint of easily adjusting the ratio (II/I) to a desired range, acrylonitrile-butadiene rubber, At least one selected from the group consisting of chloroprene rubber is more preferred, and acrylonitrile-butadiene rubber is particularly preferred.
- Acrylonitrile-butadiene rubber has a stable structure even when the temperature of the refractory material is gradually raised, so it can maintain an appropriate viscosity when a fire occurs, and the ratio (II/I) can be adjusted to the desired range. It is easy to improve fire resistance.
- the nitrile content of the acrylonitrile-butadiene rubber is preferably 8 to 40% by mass, more preferably 10 to 35% by mass, even more preferably 15 to 25% by mass.
- An acrylonitrile-butadiene rubber having a nitrile content within the above range can easily increase the expansion pressure of the refractory material, and can easily adjust the ratio (II/I) within the desired range.
- Mooney viscosity ML(1+4) at 100° C. of acrylonitrile-butadiene rubber is preferably 20-90, more preferably 30-80, and even more preferably 40-70.
- An acrylonitrile-butadiene rubber having a Mooney viscosity ML(1+4) at 100° C. within the above range can easily increase the expansion pressure of the refractory material and easily adjust the ratio (II/I) within the desired range.
- chloroprene rubber can reduce the content of carbon in the refractory material, it is also preferable to use chloroprene rubber as the rubber contained in the refractory material from the viewpoint of enhancing fire resistance.
- chloroprene rubber a sulfur-modified type (G type), a non-sulfur-modified type (W type), and the like can also be used.
- the Mooney viscosity ML(1+4) at 100° C. of the chloroprene rubber is preferably 60-120, more preferably 70-90.
- a chloroprene rubber having a Mooney viscosity ML(1+4) at 100° C. within the above range can easily increase the expansion pressure of the refractory material, and can easily adjust the ratio (II/I) within the desired range.
- Mooney viscosity is measured based on JISK6300 in this specification.
- the refractory material preferably contains a plasticizer, which will be described later.
- a plasticizer which will be described later.
- aliphatic ester plasticizers are preferred, among them, aliphatic ester plasticizers having ether bonds are more preferred, and dibutoxyethoxyethyl adipate is even more preferred.
- Commercial products of dibutoxyethoxyethyl adipate include, for example, Adekasizer RS-107 manufactured by ADEKA Co., Ltd., which is called an adipic acid ether ester. The amount of the plasticizer to be used for the resin will be described later.
- Styrene-butadiene rubber includes random copolymers of styrene and butadiene.
- the styrene content of the styrene-butadiene rubber is preferably 20 to 60% by mass, more preferably 25 to 50% by mass, even more preferably 30 to 45% by mass.
- a styrene-butadiene rubber having a styrene content within the above range can easily increase the expansion pressure of the refractory material, and can easily adjust the ratio (II/I) within the desired range.
- styrene-butadiene rubber is preferably 20-60, more preferably 30-55, even more preferably 40-50.
- a styrene-butadiene rubber having a Mooney viscosity ML(1+4) at 100° C. within the above range can easily increase the expansion pressure of the refractory material and can easily adjust the ratio (II/I) within the desired range.
- the resin may be a thermosetting resin or a thermoplastic resin, preferably a thermoplastic resin.
- the thermoplastic resin is not particularly limited, but examples include polypropylene resin, polyethylene resin, polyolefin resin such as ethylene-vinyl acetate copolymer, polyvinyl acetate resin, polyvinyl chloride resin, fluororesin such as polytetrafluoroethylene, Urethane resins such as phenol resins, polycarbonate resins, polyacrylonitrile resins, and urethane elastomers can be used.
- thermoplastic resins ethylene-vinyl acetate copolymers and polyvinyl acetate resins are preferable from the viewpoint of increasing the ratio (II/I) to improve fire resistance.
- a thermoplastic resin having a high vinyl acetate content is preferred.
- the thermoplastic resin is at least one selected from an ethylene-vinyl acetate copolymer containing a high Vac component having a vinyl acetate content of 20% by mass or more, and a polyvinyl acetate resin.
- Polyvinyl acetate resin is preferred, and polyvinyl acetate resin is more preferred.
- the high Vac component having a vinyl acetate content of 20% by mass or more means an ethylene-vinyl acetate copolymer component having a vinyl acetate content of 20% by mass or more.
- Ethylene-vinyl acetate copolymers and polyvinyl acetate resins are non-chlorinated resins, so dioxins are less likely to occur, and they are kneaded with thermally expandable graphite at relatively low temperatures without containing plasticizers. It is preferable to use it as a resin contained in the refractory material because it can be used and the moldability of the refractory material is improved.
- the vinyl acetate content of the high-Vac component is preferably 25% by mass or more, more preferably 30% by mass or more, and still more preferably from the viewpoint of easily adjusting the ratio (II/I) to a desired range. is 50% by mass or more, more preferably 70% by mass or more.
- the ethylene-vinyl acetate copolymer may contain an ethylene-vinyl acetate copolymer component (low Vac component) with a vinyl acetate content of less than 20% by mass to the extent that the effects of the present invention are not impaired.
- the content of the high Vac component is preferably 50% by mass or more based on the total amount of the ethylene-vinyl acetate copolymer, and more It is preferably 70% by mass or more, more preferably 100% by mass.
- the ethylene-vinyl acetate copolymer is an ethylene-vinyl acetate copolymer having a melt flow rate (MFR) at 190°C of 8.0 g/10 min or less from the viewpoint of increasing the expansion pressure of the refractory material and improving the moldability. It preferably contains a polymer component (hereinafter also referred to as a low MFR component).
- the melt flow rate (MFR) of the low MFR component at 190° C. is more preferably 6.0 g/10 min or less, still more preferably 1.0 g/10 min or less.
- the melt flow rate of the ethylene-vinyl acetate copolymer at 190°C is a value measured under a load of 2.16 kg, and is measured according to JIS K7210:1999.
- the content of the low-MFR component is preferably 70% by mass or more, more preferably 90% by mass or more, based on the total amount of the ethylene-vinyl acetate copolymer.
- MFR and vinyl acetate content are separate parameters representing the structure of the ethylene-vinyl acetate copolymer, there are also components that correspond to low MFR components and high Vac components.
- the high Vac component when using a high Vac component having a vinyl acetate content of 20% by mass or more and less than 50% by mass, the high Vac component is used from the viewpoint of increasing the expansion pressure and improving fire resistance.
- the MFR (190° C.) of the high-Vac component is preferably 8.0 g/10 min or less, more preferably 6.0 g/10 min or less, even more preferably 1.0 g/10 min or less, and preferably 0 05 g/10 min or more, more preferably 0.1 g/10 min or more, and still more preferably 0.3 g/10 min or more.
- the Mooney viscosity ML(1+4) at 100° C. of the high-Vac component is preferably 10-50, more preferably 20-40.
- Polyvinyl acetate resin is a homopolymer of vinyl acetate, and by using this as a resin contained in a fireproof material, the ratio (II/I) can be easily adjusted to the desired range, and fire resistance can be effectively improved. do.
- the weight average molecular weight of the polyvinyl acetate resin is preferably 100,000 to 1,000,000, more preferably 200,000 to 600,000, and still more preferably from the viewpoint of increasing the expansion pressure while improving the moldability of the refractory material. is 300,000 to 500,000.
- the weight average molecular weight is a standard polystyrene conversion value obtained by measuring by gel permeation chromatography (GPC).
- the refractory material of the present invention has a viscosity A of the matrix component at 250 ° C. when heated at a temperature increase rate of 40 ° C./min at 100 ° C. to 300 ° C. at 5 ° C./min at 100 ° C. to 300 ° C.
- the ratio (B/A) of the viscosity B of the matrix component at 250° C. when the temperature is raised (hereinafter referred to as “ratio (B/A)”) is preferably 2.0 or less. When the ratio (B/A) is 2.0 or less, it is possible to prevent the viscosity of the matrix component from excessively increasing even when the temperature of the refractory material is gradually increased.
- the refractory material expands easily, the ratio of the expansion ratio can also satisfy a predetermined range, and the fire resistance is improved. Moreover, in the process of manufacturing the refractory material, the fluidity of the resin composition can be ensured to some extent, and excellent moldability can be obtained, making it possible to provide a high-quality refractory material. Based on these points of view, 1.8 or less is more preferable, and 1.6 or less is even more preferable.
- the lower limit of the ratio (B/A) is not particularly limited. From the viewpoint of obtaining moldability, it is preferably 0.7 or more, more preferably 0.8 or more, and still more preferably 1.0 or more.
- the ratio (B/A) can be appropriately adjusted depending on the type, viscosity, molecular weight, etc. of the matrix component.
- the viscosity B of the matrix component in the present invention is preferably 7500 Pa s or less from the viewpoint of making the refractory material sufficiently expand easily and obtaining excellent moldability even when the temperature of the refractory material is gradually increased. , 5000 Pa ⁇ s or less, and more preferably 3000 Pa ⁇ s or less.
- the lower limit of the viscosity B of the matrix component is not particularly limited, but from the viewpoint of improving moldability, it is preferably 1000 Pa ⁇ s or more, more preferably 1200 Pa ⁇ s or more, and still more preferably 1300 Pa ⁇ s. s or more.
- the viscosity A of the matrix component in the present invention is not particularly limited as long as the ratio (B/A) satisfies the above range. From the viewpoints of sufficient expansion and excellent moldability, the viscosity is preferably 6000 Pa ⁇ s or less, more preferably 4500 Pa ⁇ s or less, and even more preferably 2500 Pa ⁇ s or less.
- the lower limit of the viscosity B of the matrix component is not particularly limited, but from the viewpoint of obtaining the minimum moldability, it is preferably 800 Pa ⁇ s or more, more preferably 900 Pa ⁇ s or more, and still more preferably 1100 Pa. - s or more.
- Thermally expandable graphite is a conventionally known substance that expands when heated, and is produced by acid-treating a raw material powder such as natural flake graphite, pyrolytic graphite, or Kish graphite with a strong oxidizing agent to form a graphite intercalation compound.
- strong oxidizing agents include inorganic acids such as concentrated sulfuric acid, nitric acid and selenic acid, concentrated nitric acid, perchloric acid, perchlorates, permanganates, bichromates, and hydrogen peroxide.
- Thermally expandable graphite is a crystalline compound that maintains the layered structure of carbon.
- Thermally expandable graphite may be neutralized. That is, the thermally expandable graphite obtained by treatment with a strong oxidizing agent or the like as described above may be further neutralized with ammonia, an aliphatic lower amine, an alkali metal compound, an alkaline earth metal compound, or the like.
- the content of thermally expandable graphite in the refractory material of the present invention is preferably 20 to 500 parts by mass, more preferably 30 to 250 parts by mass, and still more preferably 70 parts by mass with respect to 100 parts by mass of the matrix component. ⁇ 150 parts by mass.
- the content of thermally expandable graphite is at least these lower limits, it becomes easier to increase the expansion pressure of the thermally expandable refractory material, and it becomes easier to adjust the expansion ratio ratio (II/I) within a desired range.
- the content of the thermally expandable graphite is not more than these upper limits, the shape retainability, workability, etc. are improved.
- the thermally expandable graphite in the present invention preferably has an average aspect ratio of 15 or more, more preferably 20 or more, and usually 1000 or less.
- the aspect ratio of thermally expandable graphite is obtained by measuring the maximum dimension (major axis) and the minimum dimension (minor axis) of 10 or more (for example, 50) thermally expandable graphite, and calculating the ratio (maximum dimension / minimum dimension).
- the average particle size of the thermally expandable graphite is preferably 50 to 500 ⁇ m, more preferably 100 to 400 ⁇ m, from the viewpoint of achieving a desired expansion pressure.
- the average particle size of the thermally expandable graphite is determined as the average value of the maximum dimensions of 10 or more (for example, 50) thermally expandable graphites.
- the minimum and maximum dimensions of the thermally expandable graphite described above can be measured using, for example, a field emission scanning electron microscope (FE-SEM).
- the refractory material of the present invention preferably contains a flame retardant. Fire resistance improves by containing a flame retardant.
- flame retardants include various phosphoric acid esters such as triphenyl phosphate (triphenyl phosphate), tricresyl phosphate, trixylenyl phosphate, cresyl diphenyl phosphate, and xylenyl diphenyl phosphate, sodium phosphate, phosphorus phosphites such as sodium phosphite, potassium phosphite, magnesium phosphite, aluminum phosphite and the like, ammonium polyphosphate, red phosphorus, and the like. be done.
- flame retardants include compounds represented by the following general formula (1).
- R 1 and R 3 are the same or different and represent hydrogen, a linear or branched alkyl group having 1 to 16 carbon atoms, or an aryl group having 6 to 16 carbon atoms.
- R 2 is a hydroxyl group, a linear or branched alkyl group having 1 to 16 carbon atoms, a linear or branched alkoxyl group having 1 to 16 carbon atoms, an aryl group having 6 to 16 carbon atoms, or a carbon number Represents 6-16 aryloxy groups.
- Specific examples of the compound represented by the general formula (1) include methylphosphonic acid, dimethyl methylphosphonate, diethyl methylphosphonate, ethylphosphonic acid, n-propylphosphonic acid, n-butylphosphonic acid and 2-methylpropylphosphonic acid.
- t-butylphosphonic acid 2,3-dimethyl-butylphosphonic acid, octylphosphonic acid, phenylphosphonic acid, dioctylphenylphosphonate, dimethylphosphinic acid, methylethylphosphinic acid, methylpropylphosphinic acid, diethylphosphinic acid, dioctylphosphinic acid , phenylphosphinic acid, diethylphenylphosphinic acid, diphenylphosphinic acid, bis(4-methoxyphenyl)phosphinic acid and the like.
- the flame retardants may be used alone or in combination of two or more.
- Zinc borate etc. are mentioned as a boron-type compound.
- metal hydroxides include aluminum hydroxide, magnesium hydroxide, calcium hydroxide, hydrotalcite, and the like. When a metal hydroxide is used, water is produced by heat generated by ignition, and the fire can be quickly extinguished.
- red phosphorus, phosphoric acid esters such as triphenyl phosphate (triphenyl phosphate), aluminum phosphite, ammonium polyphosphate, and zinc borate are preferable from the viewpoint of safety and cost.
- aluminum phosphite and ammonium polyphosphate are more preferable.
- the flame retardants listed above may be used alone or in combination of two or more, but it is preferable to use one alone, and phosphorous acid More preferably, aluminum is used. Since aluminum phosphite has expansive properties, the expansion pressure of the refractory material containing the aluminum phosphite tends to increase, and the fire resistance tends to be improved more effectively.
- the average particle size of the flame retardant is preferably 1-200 ⁇ m, more preferably 1-60 ⁇ m, still more preferably 3-40 ⁇ m, and even more preferably 5-20 ⁇ m.
- the average particle size of the flame retardant is within the above range, the dispersibility of the flame retardant in the refractory material is improved, the flame retardant is uniformly dispersed in the resin, and the amount of the flame retardant compounded in the resin is increased. be able to.
- the average particle size is outside the above range, the flame retardant will be difficult to disperse in the resin, making it difficult to uniformly disperse the flame retardant in the resin or to mix a large amount of the flame retardant.
- the average particle size of the flame retardant is the value of the median size (D50) measured with a laser diffraction/scattering particle size distribution analyzer.
- the content of the flame retardant in the refractory material of the present invention is preferably 15 to 1000 parts by mass, more preferably 20 to 300 parts by mass, and even more preferably 30 to 100 parts by mass with respect to 100 parts by mass of the matrix component. .
- the content of the flame retardant is at least these lower limit values, the fire resistance of the fire resistant material is improved.
- the content of the flame retardant is not more than these upper limits, it becomes easier to uniformly disperse in the resin, and moldability and the like are excellent.
- the refractory material of the present invention may contain a cross-linking agent. Especially when acrylonitrile-butadiene rubber is used as the rubber component, the combined use of the cross-linking agent can increase the expansion pressure and improve the fire resistance. When the refractory material contains a cross-linking agent, it is believed that the heat generated during a fire promotes the cross-linking of the matrix component such as the rubber component, increasing the viscosity and increasing the expansion pressure.
- any known cross-linking agent can be used without limitation, and examples thereof include sulfur-based cross-linking agents, organic peroxides, and azo compounds.
- the sulfur-based cross-linking agent may be an inorganic cross-linking agent such as sulfur, insoluble sulfur, precipitated sulfur, sulfur chloride, sulfur monochloride, sulfur dichloride, or a sulfur-containing organic cross-linking agent.
- sulfur-containing organic cross-linking agents examples include morpholine disulfide, alkylphenol disulfide, N,N'-dithio-bis(hexahydro-2H-azepinone-2), thiuram polysulfide, 2-(4'-morpholino-dithio)benzothiazole and the like. be done.
- organic peroxides examples include 2,5-dimethylhexane, 2,5-dihydroperoxide, 2,5-dimethyl-2,5-di(t-butylperoxy)hexane, 3-di-t -butyl peroxide, t-dicumyl peroxide, 2,5-dimethyl-2,5-di(t-butylperoxy)hexyne, dicumyl peroxide, ⁇ , ⁇ '-bis(t-butylperoxyisopropyl ) benzene, n-butyl-4,4-bis(t-butylperoxy)butane, 2,2-bis(t-butylperoxy)butane, 1,1-bis(t-butylperoxy)cyclohexane, 1 ,1-bis(t-butylperoxy)3,3,5-trimethylcyclohexane, t-butylperoxybenzoate: benzoyl peroxide: t-but
- cross-linking agents when producing a refractory material, a cross-linking reaction is unlikely to occur at the temperature (for example, 70 ° C. to 150 ° C.) at which each component is kneaded, and acrylonitrile-butadiene rubber etc. It is preferable that the cross-linking reaction of the rubber component easily occurs.
- a sulfur-based cross-linking agent is preferred, and among these, an inorganic cross-linking agent is preferred from the viewpoint of cross-linkability, and sulfur is more preferred.
- the content of the cross-linking agent is preferably 0.1 to 10 parts by mass, more preferably 0.2 to 5 parts by mass, with respect to 100 parts by mass of the matrix component. Yes, more preferably 0.5 to 3 parts by mass.
- the refractory material of the present invention preferably contains a cross-linking accelerator in addition to the cross-linking agent.
- cross-linking accelerators include metal oxides.
- metal oxides include zinc oxide and magnesium oxide. When using metal oxides in the present invention, it is preferred to use zinc oxide.
- These metal oxides are more preferably used in combination with a long-chain aliphatic carboxylic acid having 12 to 24 carbon atoms, preferably 16 to 20 carbon atoms, such as stearic acid.
- the long-chain aliphatic carboxylic acid used in combination with the metal oxide is also referred to as a cross-linking accelerator.
- cross-linking accelerators examples include, in addition to those described above, thiazole-based compounds, sulfenamide-based compounds, thiuram-based compounds, dithiocarbamate-based compounds, and guanidine-based compounds.
- Thiazole compounds include bis(benzothiazol-2-ylthio)zinc.
- a crosslinking accelerator may be used individually by 1 type, and may use 2 or more types together.
- the cross-linking accelerator at least one selected from metal oxides and thiazole-based compounds is preferable, and a mode in which these are used in combination is also preferable. At this time, the metal oxide may be used in combination with a long-chain aliphatic carboxylic acid having 16 to 20 carbon atoms such as stearic acid.
- the amount of the cross-linking accelerator when it is used in the refractory material of the present invention is not particularly limited, but is preferably 0.1 to 15 parts by mass, more preferably 100 parts by mass of the matrix component. is 0.5 to 10 parts by mass, more preferably 1 to 8 parts by mass.
- the refractory material of the present invention may contain a plasticizer.
- a plasticizer By using a plasticizer, moldability tends to be improved.
- the content of the plasticizer is not particularly limited, but is preferably 10 to 200 parts by mass, more preferably 20 to 60 parts by mass, based on 100 parts by mass of the matrix component. If the content of the plasticizer is at least these lower limits, the moldability of the refractory material will be improved. When the content of the plasticizer is below these upper limits, it becomes easier to adjust the ratio (II/I) within the desired range, and the expansion pressure also increases, making it easier to improve the fire resistance.
- plasticizers include di-2-ethylhexyl phthalate (DOP), di-n-octyl phthalate, diisononyl phthalate (DINP), diisodecyl phthalate (DIDP), diundecyl phthalate (DUP), or those having 10 to 10 carbon atoms.
- Phthalic acid ester plasticizers such as phthalic acid esters of higher alcohols or mixed alcohols of about 13, di-2-ethylhexyl adipate (DOA), diisobutyl adipate (DIBA), dibutyl adipate (DBA), di-n-octyl adipate, Aliphatic ester plasticizers such as di-n-decyl adipate, diisodecyl adipate, di-2-ethylhexyl azelate, dibutyl sebacate, di-2-ethylhexyl sebacate, dibutoxyethoxyethyl adipate, tri-2-ethylhexyl Trimellitate ester plasticizers such as trimellitate (TOTM), tri-n-octyl trimellitate, tridecyl trimellitate, triisodecyl trimellitate, and di-n-octyl-n-decy
- the refractory material of the present invention may further contain an inorganic filler other than the flame retardant and thermally expandable graphite.
- Inorganic fillers other than flame retardants and thermally expandable graphite are not particularly limited, and examples include metal carbonates such as alumina, basic magnesium carbonate, calcium carbonate, magnesium carbonate, zinc carbonate, strontium carbonate, and barium carbonate, and silica.
- diatomaceous earth dawsonite, barium sulfate, talc, clay, mica, montmorillonite, bentonite, activated clay, sepiolite, imogolite, sericite, glass fiber, glass beads, silica-based balloons, aluminum nitride, boron nitride, silicon nitride, carbon black, Graphite, carbon fiber, carbon balloon, charcoal powder, various metal powders, potassium titanate, magnesium sulfate, lead zirconate titanate, aluminum borate, molybdenum sulfide, silicon carbide, stainless steel fiber, various magnetic powders, slag fiber, fly ash, and dehydrated sludge.
- These inorganic fillers may be used alone or in combination of two or more.
- the average particle size of the inorganic filler is preferably 0.5-100 ⁇ m, more preferably 1-50 ⁇ m.
- the particle size of the inorganic filler is small from the viewpoint of improving dispersibility. Therefore, those having a large particle size are preferable.
- the refractory material of the present invention contains an inorganic filler other than a flame retardant and thermally expandable graphite
- the content thereof is preferably 10 to 300 parts by mass, more preferably 10 to 200 parts by mass, based on 100 parts by mass of the resin. part by mass.
- the content of the inorganic filler is within the above range, the mechanical properties of the refractory material can be improved.
- the refractory material of the present invention can contain various additive components as necessary within a range that does not impair the object of the present invention.
- the type of additive component is not particularly limited, and various additives can be used.
- Such additives include, for example, lubricants, anti-shrinking agents, crystal nucleating agents, coloring agents (pigments, dyes, etc.), ultraviolet absorbers, antioxidants, anti-aging agents, dispersants, gelation accelerators, fillers, , reinforcing agents, flame retardant aids, antistatic agents, surfactants, vulcanizing agents, and surface treatment agents.
- the amount of the additive to be added can be appropriately selected within a range that does not impair the moldability and the like. Additives may be used alone or in combination of two or more.
- the refractory material of the present invention preferably has a residual hardness of 0.10 kgf/cm 2 or more, more preferably 0.13 kgf/cm 2 or more, and still more preferably 0.13 kgf/cm 2 or more after thermal expansion. It is 17 kgf/cm 2 or more, more preferably 0.22 kgf/cm 2 or more.
- the residual hardness is preferably 1.00 kgf/cm 2 or less, more preferably 0.95 kgf/cm 2 or less, and even more preferably, from the viewpoint of ensuring fire resistance by making the refractory material expand easily. is 0.85 kgf/cm 2 or less.
- the refractory material of the present invention preferably exhibits residual hardness within the above range even after being immersed in water at 60° C. for one week. If the swelling residue is within the above range after being immersed in water for a long period of time, the water resistance is also good.
- the hardness of the residue can be obtained by measuring the hardness of the expanded residue after heating and expanding the refractory material.
- the refractory material of the present invention is preferably in the form of a sheet, and its thickness is not particularly limited. preferable.
- the refractory material of the present invention can be produced, for example, as follows. First, a predetermined amount of thermally expandable graphite, a resin, a plasticizer, a flame retardant, a cross-linking agent, an inorganic filler, and other components blended as necessary are kneaded with a kneader such as a kneading roll to obtain a refractory product. to obtain a flexible resin composition. Next, the resulting refractory resin composition can be formed into a sheet by a known molding method such as press molding, calendar molding, extrusion molding, etc., to obtain a refractory material.
- a kneader such as a kneading roll
- the temperature during kneading and the temperature for forming into a sheet are preferably lower than the expansion initiation temperature of the thermally expandable graphite. Therefore, the kneading temperature is preferably 70 to 150°C, more preferably 90 to 140°C.
- the temperature for forming into a sheet is preferably 80 to 130°C, more preferably 90 to 120°C.
- the refractory material of the present invention may be laminated with another sheet member or adhesive layer to form a laminated sheet.
- a laminated sheet includes, for example, a base material and a fireproof material laminated on one side or both sides of the base material. Substrates are typically woven or non-woven. Fibers used for woven fabrics or non-woven fabrics are not particularly limited, but nonflammable or quasi-flammable materials are preferred, such as glass fibers, ceramic fibers, cellulose fibers, polyester fibers, carbon fibers, graphite fibers, thermosetting A flexible resin fiber or the like is preferable.
- the laminated sheet can be obtained, for example, by molding the fire-resistant resin composition into a sheet on a base material.
- the laminated sheet may include a refractory material and an adhesive layer.
- the adhesive layer may be laminated on one side or both sides of the refractory material, for example.
- the laminated sheet may comprise a refractory material, a substrate, and an adhesive layer.
- Such a laminated sheet may have a refractory material on one side of the substrate and an adhesive layer on the other side, or a refractory material and an adhesive layer on one side of the substrate. They may be provided in order.
- the pressure-sensitive adhesive layer can be formed, for example, by transferring the pressure-sensitive adhesive applied to the release paper to the laminated sheet.
- the refractory material of the present invention, and the laminated sheet using the same are specifically used for various fittings such as detached houses, collective housing, high-rise housing, high-rise buildings, commercial facilities, public facilities, automobiles, trains, etc. It can be used for various vehicles, ships, aircraft, etc. Among these, it is preferably used for fittings.
- fixtures concretely, it can be used for walls, beams, pillars, floors, bricks, roofs, board materials, windows, shoji screens, doors, doors, doors, fusuma, transoms, wiring, piping, and the like.
- refractory material of the present invention and the laminated sheet using the same are particularly applied to the gaps of fittings such as windows, doors, and doors to prevent flames from penetrating through the gaps in the event of a fire or the like. can be prevented.
- expansion ratio I The refractory materials of each example and comparative example were made to have a predetermined size (thickness 1.8 mm, width 25 mm, length 25 mm). A refractory material of a predetermined size is placed on the bottom surface of a stainless steel plate (98 mm square, thickness 0.3 mm), and the refractory material is placed in an electric furnace that has been set to 300 ° C in advance. heated for a minute. The expansion ratio I was obtained by dividing the thickness of the refractory material after heating by the thickness of the refractory material before heating.
- Viscosity A of matrix component Among the formulations shown in Table 1, the matrix component was hot-pressed at 100° C. to prepare a circular test piece with a thickness of 1 mm and a diameter of 2 cm. After that, using "MCR 302" (manufactured by Anton Paar), the viscosity was evaluated while heating from 100 ° C. to 300 ° C. at a temperature increase rate of 40 ° C./min at an angular frequency of 63 rad / s. Viscosity was measured.
- Viscosity B of matrix component The viscosity of the matrix component at 250° C. was measured when the temperature was gradually raised in the same manner as in the measurement of (3) except that the temperature was raised at a rate of 5° C./min.
- Residual hardness Put the refractory material in an electric furnace preliminarily heated to 600 ° C. and heat the test piece for 30 minutes. It was compressed with an indenter of 0.25 cm 2 at a rate of 0.1 cm/sec, and the stress at break was measured.
- a door member for fire-resistant time evaluation was prepared, which consisted of a door made of a calcium silicate plate (manufactured by Nippon Insulation Co., Ltd.) and a door frame. A gap of 1 cm was provided between the side surface of the door member for fire resistance time evaluation and the door frame. A refractory material (thickness: 1.8 mm, width: 25 mm, length: 1000 mm) of each example and comparative example having a predetermined size was attached to the side of the door. Then, in a refractory furnace, it was heated according to the standard heating curve of ISO834, and the time until the refractory material peeled off was measured.
- the evaluation criteria of the fire resistance time are as follows. A: Time until peeling off 90 minutes or more B: Time until peeling off 75 minutes or more and less than 90 minutes C: Time until peeling off 60 minutes or more and less than 75 minutes D: Time until peeling off less than 60 minutes
- Formability When kneading with rolls, if the material is too hard to flow, or too soft to flow easily and the shape cannot be maintained, the yield will deteriorate.
- the formability was determined by the yield of the material that was taken out in the form of a sheet after kneading, out of the charged materials, as follows. A: 90% or more B: 70% or more and less than 90% C: 50% or more and less than 70% D: less than 50%
- (matrix component) Rubber component/NBR (1) “Nipol DN401L” manufactured by Nippon Zeon Co., Ltd. Mooney viscosity ML (1+4): 70, nitrile content 18% by mass ⁇ NBR (2) “Nipol 1052J” manufactured by Nippon Zeon Co., Ltd. Mooney viscosity ML (1+4): 46, nitrile content 33.5% by mass ⁇ NBR (3) “Nipol DN101L” manufactured by Nippon Zeon Co., Ltd.
- Mooney viscosity ML (1+4) 60, nitrile content 42.5% by mass ⁇ NBR (4) “Nipol DN401” manufactured by Nippon Zeon Co., Ltd. Mooney viscosity ML (1+4): 77.5, nitrile content 18% by mass ⁇ NBR (5) “Nipol DN101LL” manufactured by Nippon Zeon Co., Ltd. Mooney viscosity ML (1+4): 32, nitrile content 18% by mass ⁇ SBR (1) “Nipol 1502” manufactured by Nippon Zeon Co., Ltd.
- Mooney viscosity ML (1+4) 52, styrene content 23.5% by mass ⁇ SBR (2) “Nipol 1739” manufactured by Nippon Zeon Co., Ltd. Mooney viscosity ML (1+4): 49, styrene content 40% by mass ⁇ Chloroprene rubber (1) “Skyprene TSR-56” manufactured by Tosoh Corporation Mooney viscosity ML(1+4) at 100°C: 70 ⁇ Chloroprene rubber (2) “Skyprene 640” manufactured by Tosoh Corporation Mooney viscosity ML(1+4) at 100°C: 85
- Polyvinyl acetate resin/Polyvinyl acetate (1) “VINNAPAS 4FS” manufactured by Tomoe Chemical Industry Co., Ltd. Weight average molecular weight: 300,000 g/mol ⁇ Polyvinyl acetate (2) “VINNAPAS 25FS” manufactured by Tomoe Chemical Industry Co., Ltd. Weight average molecular weight: 500,000 g/mol
- EVM Ethylene-Vinyl Acetate Copolymer
- EVM Ethylene-Vinyl Acetate Copolymer
- Thermal expandable graphite (Thermal expandable graphite) ⁇ Thermal expandable graphite “ADT351” manufactured by ADT Average aspect ratio: 21.3
- Examples 1 to 17, Comparative Examples 1 to 3 A matrix component, thermally expandable graphite, a flame retardant, a cross-linking agent, and a plasticizer were put into a roll and kneaded at 120° C. for 5 minutes to obtain a fire-resistant resin composition.
- the resulting refractory resin composition was press-molded at 100° C. for 3 minutes to obtain a sheet-like refractory material with a thickness of 1.8 mm.
- the evaluation results are shown in Table 1.
- the refractory material of the present invention containing a matrix component and thermally expandable graphite and having an expansion ratio within a predetermined range was found to have a long fire resistance time and excellent fire resistance. rice field.
- the refractory materials of each comparative example having expansion ratios outside the predetermined range had a short fire resistance time and poor fire resistance.
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Abstract
La présente invention concerne un matériau résistant au feu thermo-expansible contenant du graphite thermo-expansible et au moins un type de composant de matrice choisi dans le groupe constitué d'un composant de caoutchouc et d'une résine, et ayant un rapport (II /I) de 0,5 à 1,0 d'un facteur d'expansion (facteur d'expansion II) lorsque le matériau résistant au feu se dilate tout en étant chauffé de 20 °C à 300 °C à une vitesse de 5 °C/min à un facteur d'expansion (facteur d'expansion I) lorsque le matériau résistant au feu se dilate à 300° C.
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JP2019116606A (ja) * | 2017-12-26 | 2019-07-18 | 清典 藏田 | 熱膨張性耐火断熱塗料およびこれを用いたケーブル用耐火断熱シート |
JP2020128089A (ja) * | 2018-02-20 | 2020-08-27 | 積水化学工業株式会社 | 耐火積層体及びバッテリー |
JP2020139058A (ja) * | 2019-02-28 | 2020-09-03 | 積水化学工業株式会社 | 耐火材 |
JP2021187974A (ja) * | 2020-06-01 | 2021-12-13 | 積水化学工業株式会社 | 耐火性樹脂組成物、耐火シート及び建具 |
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JP2019116606A (ja) * | 2017-12-26 | 2019-07-18 | 清典 藏田 | 熱膨張性耐火断熱塗料およびこれを用いたケーブル用耐火断熱シート |
JP2020128089A (ja) * | 2018-02-20 | 2020-08-27 | 積水化学工業株式会社 | 耐火積層体及びバッテリー |
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