JP5509756B2 - Carbon long fiber reinforced polyamide composite material - Google Patents
Carbon long fiber reinforced polyamide composite material Download PDFInfo
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- JP5509756B2 JP5509756B2 JP2009214339A JP2009214339A JP5509756B2 JP 5509756 B2 JP5509756 B2 JP 5509756B2 JP 2009214339 A JP2009214339 A JP 2009214339A JP 2009214339 A JP2009214339 A JP 2009214339A JP 5509756 B2 JP5509756 B2 JP 5509756B2
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- 239000002131 composite material Substances 0.000 title claims description 28
- 239000000835 fiber Substances 0.000 title claims description 27
- 239000004952 Polyamide Substances 0.000 title claims description 15
- 229920002647 polyamide Polymers 0.000 title claims description 15
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title claims description 12
- 229910052799 carbon Inorganic materials 0.000 title claims description 12
- -1 polymetaxylylene Polymers 0.000 claims description 31
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 28
- 239000004917 carbon fiber Substances 0.000 claims description 28
- GVNWZKBFMFUVNX-UHFFFAOYSA-N Adipamide Chemical compound NC(=O)CCCCC(N)=O GVNWZKBFMFUVNX-UHFFFAOYSA-N 0.000 claims description 26
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 24
- 239000003484 crystal nucleating agent Substances 0.000 claims description 18
- 238000002425 crystallisation Methods 0.000 claims description 18
- 230000008025 crystallization Effects 0.000 claims description 18
- 238000000465 moulding Methods 0.000 claims description 16
- 229920001577 copolymer Polymers 0.000 claims description 9
- 230000000737 periodic effect Effects 0.000 claims description 9
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- HQKMJHAJHXVSDF-UHFFFAOYSA-L magnesium stearate Chemical compound [Mg+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O HQKMJHAJHXVSDF-UHFFFAOYSA-L 0.000 claims description 6
- 239000004927 clay Substances 0.000 claims description 5
- 239000000454 talc Substances 0.000 claims description 5
- 229910052623 talc Inorganic materials 0.000 claims description 5
- 150000002894 organic compounds Chemical class 0.000 claims description 4
- FIASKJZPIYCESA-UHFFFAOYSA-L calcium;octacosanoate Chemical compound [Ca+2].CCCCCCCCCCCCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCCCCCCCCCCCC([O-])=O FIASKJZPIYCESA-UHFFFAOYSA-L 0.000 claims description 3
- 235000019359 magnesium stearate Nutrition 0.000 claims description 3
- CEGOLXSVJUTHNZ-UHFFFAOYSA-K aluminium tristearate Chemical compound [Al+3].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CEGOLXSVJUTHNZ-UHFFFAOYSA-K 0.000 claims description 2
- 229940063655 aluminum stearate Drugs 0.000 claims description 2
- 230000002787 reinforcement Effects 0.000 claims description 2
- XOOUIPVCVHRTMJ-UHFFFAOYSA-L zinc stearate Chemical compound [Zn+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O XOOUIPVCVHRTMJ-UHFFFAOYSA-L 0.000 claims description 2
- 239000000463 material Substances 0.000 description 15
- 238000000034 method Methods 0.000 description 14
- 229920006122 polyamide resin Polymers 0.000 description 12
- 229920005989 resin Polymers 0.000 description 10
- 239000011347 resin Substances 0.000 description 10
- 239000003795 chemical substances by application Substances 0.000 description 7
- 235000014113 dietary fatty acids Nutrition 0.000 description 7
- 239000000194 fatty acid Substances 0.000 description 7
- 229930195729 fatty acid Natural products 0.000 description 7
- POULHZVOKOAJMA-UHFFFAOYSA-N dodecanoic acid Chemical compound CCCCCCCCCCCC(O)=O POULHZVOKOAJMA-UHFFFAOYSA-N 0.000 description 6
- 150000004665 fatty acids Chemical class 0.000 description 6
- 229920006121 Polyxylylene adipamide Polymers 0.000 description 5
- 238000005470 impregnation Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 230000000704 physical effect Effects 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 238000010521 absorption reaction Methods 0.000 description 4
- 238000000748 compression moulding Methods 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 239000013078 crystal Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000011049 filling Methods 0.000 description 4
- 239000003365 glass fiber Substances 0.000 description 4
- 238000001746 injection moulding Methods 0.000 description 4
- UTOPWMOLSKOLTQ-UHFFFAOYSA-N octacosanoic acid Chemical compound CCCCCCCCCCCCCCCCCCCCCCCCCCCC(O)=O UTOPWMOLSKOLTQ-UHFFFAOYSA-N 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 150000003839 salts Chemical class 0.000 description 4
- 235000021355 Stearic acid Nutrition 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
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- 150000004985 diamines Chemical class 0.000 description 3
- 230000009477 glass transition Effects 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 3
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 3
- 239000012783 reinforcing fiber Substances 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 239000008117 stearic acid Substances 0.000 description 3
- 239000002344 surface layer Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- PBLZLIFKVPJDCO-UHFFFAOYSA-N 12-aminododecanoic acid Chemical compound NCCCCCCCCCCCC(O)=O PBLZLIFKVPJDCO-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 101000576320 Homo sapiens Max-binding protein MNT Proteins 0.000 description 2
- 239000005639 Lauric acid Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-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
- 150000001413 amino acids Chemical class 0.000 description 2
- 125000003118 aryl group Chemical group 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 239000000805 composite resin Substances 0.000 description 2
- 238000013329 compounding Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- JBKVHLHDHHXQEQ-UHFFFAOYSA-N epsilon-caprolactam Chemical compound O=C1CCCCCN1 JBKVHLHDHHXQEQ-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- NAQMVNRVTILPCV-UHFFFAOYSA-N hexane-1,6-diamine Chemical compound NCCCCCCN NAQMVNRVTILPCV-UHFFFAOYSA-N 0.000 description 2
- 229920000554 ionomer Polymers 0.000 description 2
- QQVIHTHCMHWDBS-UHFFFAOYSA-N isophthalic acid Chemical compound OC(=O)C1=CC=CC(C(O)=O)=C1 QQVIHTHCMHWDBS-UHFFFAOYSA-N 0.000 description 2
- 150000003951 lactams Chemical class 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- BDJRBEYXGGNYIS-UHFFFAOYSA-N nonanedioic acid Chemical compound OC(=O)CCCCCCCC(O)=O BDJRBEYXGGNYIS-UHFFFAOYSA-N 0.000 description 2
- KIDHWZJUCRJVML-UHFFFAOYSA-N putrescine Chemical compound NCCCCN KIDHWZJUCRJVML-UHFFFAOYSA-N 0.000 description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- CXMXRPHRNRROMY-UHFFFAOYSA-N sebacic acid Chemical compound OC(=O)CCCCCCCCC(O)=O CXMXRPHRNRROMY-UHFFFAOYSA-N 0.000 description 2
- 238000004513 sizing Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- GEYOCULIXLDCMW-UHFFFAOYSA-N 1,2-phenylenediamine Chemical compound NC1=CC=CC=C1N GEYOCULIXLDCMW-UHFFFAOYSA-N 0.000 description 1
- GUOSQNAUYHMCRU-UHFFFAOYSA-N 11-Aminoundecanoic acid Chemical compound NCCCCCCCCCCC(O)=O GUOSQNAUYHMCRU-UHFFFAOYSA-N 0.000 description 1
- 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 1
- VOZKAJLKRJDJLL-UHFFFAOYSA-N 2,4-diaminotoluene Chemical compound CC1=CC=C(N)C=C1N VOZKAJLKRJDJLL-UHFFFAOYSA-N 0.000 description 1
- SMZOUWXMTYCWNB-UHFFFAOYSA-N 2-(2-methoxy-5-methylphenyl)ethanamine Chemical compound COC1=CC=C(C)C=C1CCN SMZOUWXMTYCWNB-UHFFFAOYSA-N 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N 2-Propenoic acid Natural products OC(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- JZUHIOJYCPIVLQ-UHFFFAOYSA-N 2-methylpentane-1,5-diamine Chemical compound NCC(C)CCCN JZUHIOJYCPIVLQ-UHFFFAOYSA-N 0.000 description 1
- UFMBOFGKHIXOTA-UHFFFAOYSA-N 2-methylterephthalic acid Chemical compound CC1=CC(C(O)=O)=CC=C1C(O)=O UFMBOFGKHIXOTA-UHFFFAOYSA-N 0.000 description 1
- SLXKOJJOQWFEFD-UHFFFAOYSA-N 6-aminohexanoic acid Chemical compound NCCCCCC(O)=O SLXKOJJOQWFEFD-UHFFFAOYSA-N 0.000 description 1
- 239000005995 Aluminium silicate Substances 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229920003043 Cellulose fiber Polymers 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- 229920006060 Grivory® Polymers 0.000 description 1
- JHWNWJKBPDFINM-UHFFFAOYSA-N Laurolactam Chemical compound O=C1CCCCCCCCCCCN1 JHWNWJKBPDFINM-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- OFOBLEOULBTSOW-UHFFFAOYSA-N Malonic acid Chemical compound OC(=O)CC(O)=O OFOBLEOULBTSOW-UHFFFAOYSA-N 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-N Methacrylic acid Chemical compound CC(=C)C(O)=O CERQOIWHTDAKMF-UHFFFAOYSA-N 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 229910004298 SiO 2 Inorganic materials 0.000 description 1
- ISKQADXMHQSTHK-UHFFFAOYSA-N [4-(aminomethyl)phenyl]methanamine Chemical compound NCC1=CC=C(CN)C=C1 ISKQADXMHQSTHK-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 235000012211 aluminium silicate Nutrition 0.000 description 1
- 229960002684 aminocaproic acid Drugs 0.000 description 1
- QCTBMLYLENLHLA-UHFFFAOYSA-N aminomethylbenzoic acid Chemical compound NCC1=CC=C(C(O)=O)C=C1 QCTBMLYLENLHLA-UHFFFAOYSA-N 0.000 description 1
- 229960003375 aminomethylbenzoic acid Drugs 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- CJZGTCYPCWQAJB-UHFFFAOYSA-L calcium stearate Chemical compound [Ca+2].CCCCCCCCCCCCCCCCCC([O-])=O.CCCCCCCCCCCCCCCCCC([O-])=O CJZGTCYPCWQAJB-UHFFFAOYSA-L 0.000 description 1
- 239000008116 calcium stearate Substances 0.000 description 1
- 235000013539 calcium stearate Nutrition 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000007334 copolymerization reaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- AAOVKJBEBIDNHE-UHFFFAOYSA-N diazepam Chemical compound N=1CC(=O)N(C)C2=CC=C(Cl)C=C2C=1C1=CC=CC=C1 AAOVKJBEBIDNHE-UHFFFAOYSA-N 0.000 description 1
- 150000001990 dicarboxylic acid derivatives Chemical class 0.000 description 1
- 238000002845 discoloration Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- QFTYSVGGYOXFRQ-UHFFFAOYSA-N dodecane-1,12-diamine Chemical compound NCCCCCCCCCCCCN QFTYSVGGYOXFRQ-UHFFFAOYSA-N 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000407 epitaxy Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000003063 flame retardant Substances 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000012778 molding material Substances 0.000 description 1
- KYTZHLUVELPASH-UHFFFAOYSA-N naphthalene-1,2-dicarboxylic acid Chemical compound C1=CC=CC2=C(C(O)=O)C(C(=O)O)=CC=C21 KYTZHLUVELPASH-UHFFFAOYSA-N 0.000 description 1
- 229910017604 nitric acid Inorganic materials 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- SXJVFQLYZSNZBT-UHFFFAOYSA-N nonane-1,9-diamine Chemical compound NCCCCCCCCCN SXJVFQLYZSNZBT-UHFFFAOYSA-N 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 125000005702 oxyalkylene group Chemical group 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 238000013001 point bending Methods 0.000 description 1
- 229920002239 polyacrylonitrile Polymers 0.000 description 1
- 229920006123 polyhexamethylene isophthalamide Polymers 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000011342 resin composition Substances 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- RPACBEVZENYWOL-XFULWGLBSA-M sodium;(2r)-2-[6-(4-chlorophenoxy)hexyl]oxirane-2-carboxylate Chemical compound [Na+].C=1C=C(Cl)C=CC=1OCCCCCC[C@]1(C(=O)[O-])CO1 RPACBEVZENYWOL-XFULWGLBSA-M 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
- 238000004781 supercooling Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- KLNPWTHGTVSSEU-UHFFFAOYSA-N undecane-1,11-diamine Chemical compound NCCCCCCCCCCCN KLNPWTHGTVSSEU-UHFFFAOYSA-N 0.000 description 1
- 229940072690 valium Drugs 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
- 238000009279 wet oxidation reaction Methods 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Landscapes
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Description
本発明は、炭素長繊維とポリアミド樹脂からなる複合材料に関する。詳しくは、炭素長繊維とポリメタキシリレンアジパミドからなる複合材料に関する。更に詳しくは、スタンピング成形における成形品表面の結晶性と生産性が著しく改善された高耐熱性で比強度の高い構造材用複合材料に関する。 The present invention relates to a composite material composed of long carbon fibers and a polyamide resin. Specifically, the present invention relates to a composite material composed of carbon long fibers and polymetaxylylene adipamide. More specifically, the present invention relates to a composite material for a structural material having high heat resistance and high specific strength, in which the crystallinity and productivity of the surface of a molded product in stamping molding are remarkably improved.
従来、電線被覆法を応用したガラス長繊維強化ポリアミド樹脂複合材料は知られていた(例えば、非特許文献1参照)。しかし、かかる従来技術は、ガラス繊維とポリアミド樹脂のコンパウンド材料を射出成形により成形品を得ていた。コンパウンド工程や射出成形工程でガラス繊維の折損が著しく、ガラス繊維の強度や弾性率への補強効果が低下し、構造材としての実用性能には不満足であった。 Conventionally, a long glass fiber reinforced polyamide resin composite material using an electric wire coating method has been known (see, for example, Non-Patent Document 1). However, according to such conventional technology, a molded product is obtained by injection molding a compound material of glass fiber and polyamide resin. In the compounding process and injection molding process, breakage of the glass fiber was remarkable, the reinforcing effect on the strength and elastic modulus of the glass fiber was lowered, and the practical performance as a structural material was unsatisfactory.
高強度・高剛性成形品を得るために、炭素繊維とポリアミド樹脂の複合材料も研究開発された。しかし、射出成形や押出成形工程で炭素繊維が折損し、その効果は要求に大幅に未達であった。また、強化繊維の折損を避けるために、成形時のせん断変形の小さい圧縮成形についても検討された。しかし、強化繊維が長くなると繊維のからみ合いが起こり、流動性が著しく低下して、大型成形品や細いリブやボス構造を有する成形品は、欠肉が起こり良好な成形品が得られなかった。
繊維の絡み合いが起こらないように、繊維のロービングを単繊維状に開繊した後、ポリアミド樹脂を含浸して、強化繊維とポリアミド樹脂からなる一軸のテープ状プリプレグを予備成形した後、加熱圧縮成形する方法も開示された(例えば、非特許文献2参照)。しかし、一般のポリアミド樹脂の場合、絶乾状態では、高い剛性や強度が得られるが、空気中の水分を吸湿しやすく、多湿状態では、剛性や強度が著しく低下して、目的とする構造材の要求には未達であった。
In order to obtain high-strength and high-rigidity molded products, composite materials of carbon fiber and polyamide resin have also been researched and developed. However, the carbon fiber was broken in the injection molding and extrusion molding processes, and the effect was not fully met. In order to avoid breakage of the reinforcing fiber, compression molding with small shear deformation at the time of molding was also examined. However, when the reinforcing fiber becomes longer, the fibers are entangled and the fluidity is remarkably lowered, and a large molded product or a molded product having a thin rib or boss structure is thinned and a good molded product cannot be obtained. .
To prevent fiber entanglement, fiber roving is opened into a single fiber, then impregnated with polyamide resin, pre-molded with a uniaxial tape-shaped prepreg composed of reinforcing fibers and polyamide resin, and then heat compression molded The method of doing is also disclosed (for example, refer nonpatent literature 2). However, in the case of a general polyamide resin, high rigidity and strength can be obtained in the absolutely dry state, but it easily absorbs moisture in the air. The request was not met.
ポリアミド樹脂としては、吸湿率の低い、芳香族環を有するポリアミド樹脂の複合材料も、特許文献1や特許文献2に開示されている。しかし、芳香族環を有するポリアミド樹脂を成形した場合、分子が剛直なために、急冷された成形品の表層は、殆ど結晶化しえず、本来の耐熱性や剛性を有する成形品が得られなかった。また、成形品の表層の結晶化は、金型温度を高い温度にすれば、可能であることが示されたが、固化が遅く、また高温における剛性は低く、成形品を金型から取り出すときに変形し、脱型が困難で工業生産出来なかった。
また更に機械特性・導電性・成形性のよい炭素繊維強化樹脂についても特許文献3に開示されている。しかし、オキシアルキレン基を有するジアミンとジカルボン酸の塩とアミノ酸、ラクタムおよび/またはジアミンとジカルボン酸塩を含む共重合体を炭素繊維に付着させることにより一般的な熱可塑性樹脂複合材との界面状態を改善した物性改良であり、結晶化速度が遅く成形生産性の低いことが重要な問題であるポリメタキシリレンアジパミドを母相とした炭素繊維強化材の成形性改善や結晶化促進による耐熱性改善には、無効であった。
As the polyamide resin, a composite material of a polyamide resin having an aromatic ring with a low moisture absorption rate is also disclosed in Patent Document 1 and Patent Document 2. However, when a polyamide resin having an aromatic ring is molded, since the molecule is rigid, the surface layer of the rapidly cooled molded product can hardly be crystallized, and a molded product having original heat resistance and rigidity cannot be obtained. It was. In addition, it was shown that crystallization of the surface layer of the molded product is possible if the mold temperature is raised, but the solidification is slow and the rigidity at high temperature is low, and when the molded product is removed from the mold. It was difficult to remove the mold and industrial production was impossible.
Further, Patent Document 3 discloses a carbon fiber reinforced resin having good mechanical properties, conductivity, and moldability. However, interfacial state with general thermoplastic resin composites by attaching oxyalkylene group-containing diamine and dicarboxylic acid salt and copolymer containing amino acid, lactam and / or diamine and dicarboxylate to carbon fiber. Improved physical properties, low crystallization speed and low molding productivity is an important issue. Improvement of moldability of carbon fiber reinforced materials using polymetaxylylene adipamide as a matrix and heat resistance by promoting crystallization It was ineffective in improving sex.
平衡吸湿下でも高い剛性を有し、表層結晶化が可能であり生産性の高い、耐熱変形性を有する構造材用ポリアミド複合材料について、市場の高い開発要求があった。
本発明は、かかる従来技術の課題を背景になされたものである。すなわち、本発明の目的は、使用環境下の温度や湿度における強度や剛性が飛躍的に優れた比強度の高く構造材用複合材組成物を提供することにある。
There has been a high market development demand for polyamide composite materials for structural materials that have high rigidity even under equilibrium moisture absorption, can be crystallized on the surface, and have high productivity and heat distortion resistance.
The present invention has been made against the background of such prior art problems. That is, an object of the present invention is to provide a composite material composition for a structural material having a high specific strength that is remarkably excellent in strength and rigidity at temperature and humidity under the use environment.
本発明者らは鋭意検討した結果、以下に示す手段により、上記課題を解決できることを見出し、本発明に到達した。
すなわち、本発明は、以下の構成からなる。
重量平均繊維長30mm以上の炭素長繊維(A)100質量部に対して、ポリメタキシリレンアジパミドおよび/または70モル%以上のポリメタキシリレンアジパミドからなる共重合ポリアミド(B)30〜250質量部、タルク、クレイ、周期表第1a属金属含有の有機化合物から選ばれた一種以上の結晶核剤(C)0.01〜10質量部を含有することを特徴とする炭素長繊維強化ポリアミド複合材料である。
また溶融状態からの結晶化温度が180〜240℃であることを好ましい態様とする請求項1の炭素長繊維強化ポリアミド複合材料である。また(D)成分として、周期表第2a属、周期表第3属、周期表第4属から選ばれた1種以上の金属の高級脂肪酸塩(D)0.01〜5質量部を含有することを好ましい態様とする請求項1の炭素長繊維強化ポリアミド複合材料である。さらに、表面温度が160〜280℃の金型により成形するスタンピング成形用であることを好ましい態様とする請求項1、請求項2、請求項3の炭素長繊維強化ポリアミドである。
As a result of intensive studies, the present inventors have found that the above problems can be solved by the following means, and have reached the present invention.
That is, this invention consists of the following structures.
Copolymer polyamide (B) 30 to 30 consisting of polymetaxylylene adipamide and / or 70 mol% or more polymetaxylylene adipamide with respect to 100 parts by mass of carbon long fiber (A) having a weight average fiber length of 30 mm or more. Carbon long fiber reinforcement characterized by containing 0.01-10 mass parts of 1 or more types of crystal nucleating agent (C) chosen from the organic compound containing 250 mass parts, talc, clay, and 1a group metal containing periodic table metal It is a polyamide composite material.
Moreover, it is a carbon long fiber reinforced polyamide composite material of Claim 1 which makes it a preferable aspect that the crystallization temperature from a molten state is 180-240 degreeC. The component (D) contains 0.01 to 5 parts by mass of a higher fatty acid salt (D) of one or more metals selected from Group 2a, Periodic Table 3 and Periodic Table 4 of the Periodic Table. The carbon long fiber reinforced polyamide composite material according to claim 1, which is a preferred embodiment. Furthermore, the carbon long fiber reinforced polyamide according to claim 1, 2 or 3, wherein the polyamide is preferably used for stamping molding with a mold having a surface temperature of 160 to 280 ° C.
本発明により、強度や弾性率が飛躍的に高く、構造材の要求を満たす複合材料を工業的に提供することができる。本発明により得られた複合材組成物を成形して得られる成形品は、自動車のフレーム部品や機械器具の構造部材やスポーツ器具などに使用される。本発明により、高い強度や弾性率が得られる複合材組成物が提供される理由は、未だ明確でないが、ポリメタキシリレンアジパミドの炭素繊維表面への濡れ性がよく接着強度が高いことと、ポリメタキシリレンアジパミドの結晶性を飛躍的に高め、結晶化による収縮により、ポリメタキシリレンアジパミドが炭素繊維を強く抱きこむことが出来たことと、低吸水率性により、母相を形成するポリメタキシリレンアジパミドが平衡状態においても高い剛性と強度が維持されるため、母相の物性向上と炭素繊維界面の物性向上の相乗効果と考えられる。 According to the present invention, it is possible to industrially provide a composite material that has remarkably high strength and elastic modulus and satisfies the requirements of a structural material. A molded product obtained by molding the composite composition obtained according to the present invention is used for a frame part of an automobile, a structural member of a mechanical instrument, a sports instrument, and the like. The reason why the present invention provides a composite composition capable of obtaining high strength and elastic modulus is not yet clear, but the wettability of polymetaxylylene adipamide to the carbon fiber surface is good and the adhesive strength is high. , The crystallinity of polymetaxylylene adipamide has been dramatically improved, and due to the shrinkage caused by crystallization, the polymetaxylylene adipamide was able to strongly hold the carbon fiber and the low water absorption rate Since the polymetaxylylene adipamide that forms bismuth maintains high rigidity and strength even in an equilibrium state, it is considered to be a synergistic effect of improving the physical properties of the matrix and the physical properties of the carbon fiber interface.
以下、本発明を詳述する。
本発明には、重量平均繊維長が30mm以上、好ましくは33mm以上、更に好ましくは100mm以上の炭素長繊維や連続繊維が使用される。重量平均繊維長が30mm未満では、構造材としての強度が未達となり、好ましくない。機械物性上は連続繊維が好ましいが、成形時の金型内における流動性が必要なことからプリプレグとしてより短く切断されたものが使用される。炭素繊維としては、製造法に特に制限されないが、ポリアクリロニトル繊維やセルロース繊維などの繊維を空気中で200〜300℃にて処理した後、不活性ガス中で1000〜3000℃以上で焼成され炭化製造された引っ張り強度20t/cm2以上、引っ張り弾性率200GPa以上の炭素繊維が好ましい。本発明に使用される単繊維径は、特に制限されないが、複合化の製造ライン工程から3〜25μmが好ましく、特に4〜15μm好ましい。3μm未満では、含浸や脱泡が難しく、25μmを超えると、比表面積が小さくなり、複合化の効果が小さくなり好ましくない。本発明に使用される炭素繊維は、空気や硝酸による湿式酸化、乾式酸化、ヒートクリーニング、ウイスカライジングなどによる接着性改良のための処理されたものが好ましい。また本発明の複合材料製造に使用される炭素繊維は、作業工程の取り扱い性から、100℃以下で軟化する集束剤により集束されていることが好ましい。集束フィラメント数には特に制限ないが、1000〜30000フィラメント、好ましくは、3000〜25000フィラメントが好ましい。本発明に使用される炭素繊維の集束剤は特に限定されないが、炭素繊維と母相のメタキシリレンアヂパミドに高い接着力を有するウレタン系やエポキシ系集束剤が好ましい。
The present invention is described in detail below.
In the present invention, carbon long fibers or continuous fibers having a weight average fiber length of 30 mm or more, preferably 33 mm or more, more preferably 100 mm or more are used. If the weight average fiber length is less than 30 mm, the strength as a structural material is not achieved, which is not preferable. In view of mechanical properties, continuous fibers are preferable, but since fluidity in the mold at the time of molding is required, a prepreg that is cut shorter is used. Although it does not restrict | limit especially in a manufacturing method as carbon fiber, After processing fibers, such as a polyacrylonitrile fiber and a cellulose fiber, in air at 200-300 degreeC, it is baked at 1000-3000 degreeC or more in inert gas. Carbon fibers produced by carbonization and having a tensile strength of 20 t / cm 2 or more and a tensile modulus of 200 GPa or more are preferred. Although the diameter of the single fiber used in the present invention is not particularly limited, it is preferably 3 to 25 μm, particularly preferably 4 to 15 μm, from the production line process of the composite. If it is less than 3 μm, impregnation and defoaming are difficult, and if it exceeds 25 μm, the specific surface area becomes small and the effect of compositing becomes unfavorable. The carbon fiber used in the present invention is preferably treated for improving adhesion by wet oxidation with air or nitric acid, dry oxidation, heat cleaning, whiskerizing, or the like. Moreover, it is preferable that the carbon fiber used for composite material manufacture of this invention is bundled by the bundling agent which softens at 100 degrees C or less from the handleability of a work process. Although there is no restriction | limiting in particular in the number of focusing filaments, 1000-30000 filaments, Preferably 3000-25000 filaments are preferable. The carbon fiber sizing agent used in the present invention is not particularly limited, but a urethane-based or epoxy-based sizing agent having high adhesion to the carbon fiber and the parent phase metaxylylene adipamide is preferable.
本発明には、炭素繊維(A)100質量部当り、ポリメタキシリレンアジパミドおよび/または70モル%以上のポリメタキシリレンアジパミドからなる共重合ポリアミド(B)30〜250質量部、好ましくは35〜200質量部、さらに好ましくは40〜150質量部複合される。30質量部未満では、炭素繊維へのポリアミド樹脂の含浸が困難であり、また250質量部を超えると、炭素繊維補強の効果が不十分となり、本発明の目的である構造部材としての要求を満たせず好ましくない。 In the present invention, 30 to 250 parts by mass of a copolyamide (B) composed of polymetaxylylene adipamide and / or 70 mol% or more of polymetaxylylene adipamide per 100 parts by mass of the carbon fiber (A), preferably Is 35 to 200 parts by mass, more preferably 40 to 150 parts by mass. If the amount is less than 30 parts by mass, it is difficult to impregnate the carbon fiber with the polyamide resin. If the amount exceeds 250 parts by mass, the effect of reinforcing the carbon fiber becomes insufficient, and the requirements as a structural member that is the object of the present invention can be satisfied. Not preferable.
本発明には、70モル%以上、好ましくは80モル%以上のポリメタキシリレンアジパミドからなるポリアミド共重合体が用いられる。70モル%未満のポリアミド共重合体は、結晶化速度が遅いことや、融点が低く耐熱性が低いことや剛性が低いことや吸水率が高いことから好ましくない。本発明に使用される共重合成分は特に限定されない。共重合されるジアミン成分としては、パラキシリレンジアミン、フェニレンジアミン、トルエンジアミン、テトラメチレンジアミン、ヘキサメチレンジアミン、ノナメチレンジアミン、2−メチルペンタメチレンジアミン、ウンデカメチレンジアミン、ドデカメチレンジアミンなどが例示される。また、共重合されるジカルボン酸成分としては、スペリン酸、アゼライン酸、セバシン酸、ドデカン酸、テレフタル酸、イソフタル酸、ナフタレンジカルボン酸、2−メチルテレフタル酸等が挙げられる。また6−アミノカプロン酸、11−アミノウンデカン酸、12−アミノドデカン酸、p−アミノメチル安息香酸などのアミノ酸や、ε―カプロラクタム、ω―ラウロラクタムなどのラクタムなどが挙げられる。
ポリメタキシリレンアジパミドおよび/またはポリメタキシリレンアジパミド共重合体の分子量は特に限定されないが、25℃において測定した98質量%硫酸の0.05g/l濃度における相対粘度が1.8〜2.8の範囲にあるやや低分子量のものが、炭素繊維への含浸性から好ましい。
In the present invention, a polyamide copolymer comprising 70% by mole or more, preferably 80% by mole or more of polymetaxylylene adipamide is used. Polyamide copolymers of less than 70 mol% are not preferred because of their slow crystallization rate, low melting point, low heat resistance, low rigidity, and high water absorption. The copolymerization component used in the present invention is not particularly limited. Examples of the diamine component to be copolymerized include paraxylylenediamine, phenylenediamine, toluenediamine, tetramethylenediamine, hexamethylenediamine, nonamethylenediamine, 2-methylpentamethylenediamine, undecamethylenediamine, and dodecamethylenediamine. Is done. Examples of the dicarboxylic acid component to be copolymerized include speric acid, azelaic acid, sebacic acid, dodecanoic acid, terephthalic acid, isophthalic acid, naphthalenedicarboxylic acid, and 2-methylterephthalic acid. Further, amino acids such as 6-aminocaproic acid, 11-aminoundecanoic acid, 12-aminododecanoic acid and p-aminomethylbenzoic acid, and lactams such as ε-caprolactam and ω-laurolactam can be mentioned.
The molecular weight of polymetaxylylene adipamide and / or polymetaxylylene adipamide copolymer is not particularly limited, but the relative viscosity at a concentration of 0.05 g / l of 98% by mass sulfuric acid measured at 25 ° C. is 1.8 to A slightly lower molecular weight in the range of 2.8 is preferable from the viewpoint of impregnation with carbon fibers.
また、本発明には、ポリメタキシリレンアジパミドやポリメタキシリレンアジパミド共重合体は、低温結晶化しにくく、成形材料として使用する場合、結晶核剤が必須である。結晶核剤が配合されていないと、溶融状態から固化される成形過程で結晶化せずに非晶状超えた温度では分子のフローがおこるから、荷重たわみ温度が低く、耐熱性が低く、本来の耐熱性を有せず高温下において使用できない。また、成形品がガラス転移温度以下にならないと脱型が難しいことから、生産性が極度に低くなる。本発明において使用される結晶核剤としては、タルク、クレイ、周期表第1a属金属の有機化合物から選ばれた1種以上の組み合わせを用いる。これらの結晶核剤は、ポリメタキシリレンアジパミドやポリメタキシリレンアジパミド共重合体の溶融状態から冷却固化するときに、結晶核剤として作用し、過冷却度が小さい状態から結晶の成長を促進し、球晶状結晶の数を増加して、そのサイズを微細化する。結晶核剤が配合されていないと、固化の過程で成形品コア部が徐冷される以外結晶化せず、結晶が光の波長サイズに到達せずに殆ど透明な成形品となる。タルクやクレイのような珪酸塩が結晶核剤として有効である。これらは、天然石を微細化したものや合成された珪酸塩でもよい。結晶核剤としては、これらの表面の結晶からエピタキシー状に成長することや表面と樹脂界面の自由エネルギーの低下の効果と推察される。表面積が大きい微細なほど好ましい。平均粒径としては、0.1〜20μmが好ましい。また、周期表1a属の有機化合物も有効な結晶核剤として作用する。特に、高級脂肪酸のNa塩、高級脂肪酸のK塩、高級脂肪酸のLi塩が有効である。高級脂肪酸としては、ステアリン酸、モンタン酸、ラウリル酸などが例示される。またアクリル酸やメタクリル酸とポリオレフィンの共重合体をケン化してえられるアイオノマー共重合体が例示される。 In the present invention, polymetaxylylene adipamide and polymetaxylylene adipamide copolymer are difficult to crystallize at low temperature, and a crystal nucleating agent is essential when used as a molding material. If the crystal nucleating agent is not blended, the flow of molecules occurs at a temperature exceeding the amorphous state without crystallizing in the molding process that is solidified from the molten state, so the deflection temperature under load is low, the heat resistance is low, It does not have the heat resistance of and cannot be used at high temperatures. Moreover, since it is difficult to demold unless the molded product is below the glass transition temperature, the productivity is extremely low. As the crystal nucleating agent used in the present invention, one or more combinations selected from organic compounds of talc, clay and Group 1a metal of the periodic table are used. These crystal nucleating agents act as crystal nucleating agents when cooled and solidified from the molten state of polymetaxylylene adipamide or polymetaxylylene adipamide copolymer, and crystal growth from a state of low supercooling degree And increase the number of spherulites to refine their size. If the crystal nucleating agent is not blended, the molded product core is not crystallized except for the slow cooling during the solidification process, and the crystal does not reach the wavelength of light and becomes an almost transparent molded product. Silicates such as talc and clay are effective as crystal nucleating agents. These may be a refined natural stone or a synthesized silicate. As the crystal nucleating agent, it is presumed that the crystal grows in an epitaxy form from these surface crystals and the effect of lowering the free energy between the surface and the resin interface. The finer the surface area, the better. As an average particle diameter, 0.1-20 micrometers is preferable. In addition, organic compounds belonging to Group 1a of the periodic table also act as effective crystal nucleating agents. In particular, Na salts of higher fatty acids, K salts of higher fatty acids, and Li salts of higher fatty acids are effective. Examples of higher fatty acids include stearic acid, montanic acid, lauric acid and the like. Moreover, the ionomer copolymer obtained by saponifying the copolymer of acrylic acid, methacrylic acid, and polyolefin is illustrated.
結晶核剤の配合量は特に限定されないが、ポリメタキシリレンアジパミドやポリメタキシリレンアジパミド共重合体100質量部に対して、0.05〜20質量部、好ましくは0.01〜10質量部、さらに好ましくは0.06〜7質量部配合される。
結晶核剤の有効性は、示差走査熱量計(DSC)を使用して、ISO11357−3に準じて、溶融は、溶融状態である270℃から20℃/分で冷却した場合、結晶化発熱のピーク温度は180〜240℃が好ましい態様であり、210〜235℃にあることが更に好ましい態様である。このピーク温度は、結晶核剤の種類、分散状態による表面積、配合量に制御される。結晶化温度が高いと、溶融状態からの冷却過程における結晶化が速く進行し、早期に結晶化することにより、180℃以下好ましくは150℃以下まで冷却されれば脱型が可能であり、短時間で固化するので成形時間を短縮することが出来る。ポリメタキシリレンアジパミドのガラス転移点の80℃以下の金型温度を使用した場合、分子の凍結固化は速く進行するがこの場合結晶化の程度は極めて低く、結晶化度が不十分のため使用時変形が起こりやすく本来の耐熱性を有しないので好ましくない。このように、本来の高い耐熱性を有する成形品が、高い生産性で成形できることが本発明の特徴である。
Although the compounding quantity of a crystal nucleating agent is not specifically limited, 0.05-20 mass parts with respect to 100 mass parts of polymetaxylylene adipamide and a polymetaxylylene adipamide copolymer, Preferably it is 0.01-10. Part by mass, more preferably 0.06 to 7 parts by mass is blended.
The effectiveness of the crystal nucleating agent is determined according to ISO11357-3 using a differential scanning calorimeter (DSC). When the melting is cooled from 270 ° C. in a molten state at 20 ° C./min, the crystallization exotherm The peak temperature is preferably 180 to 240 ° C, and more preferably 210 to 235 ° C. This peak temperature is controlled by the type of crystal nucleating agent, the surface area depending on the dispersion state, and the amount of the compound. When the crystallization temperature is high, crystallization in the cooling process from the molten state proceeds rapidly, and by early crystallization, demolding is possible if it is cooled to 180 ° C. or less, preferably 150 ° C. or less. Since it solidifies with time, the molding time can be shortened. When a mold temperature of 80 ° C. or lower of the glass transition point of polymetaxylylene adipamide is used, freezing and solidification of the molecule proceeds rapidly, but in this case, the degree of crystallization is extremely low and the crystallinity is insufficient. Deformation is likely to occur during use, and it is not preferable because it does not have the inherent heat resistance. As described above, it is a feature of the present invention that an original molded product having high heat resistance can be molded with high productivity.
本発明においては、さらに高級脂肪酸の周期表第IIa属の金属塩が、炭素繊維100質量部に対して、0.05〜5質量部、特に0.1〜2質量部含有することが好ましい態様である。0.05質量部未満では、スタンピング成形後の離型性が低く深絞り成形品では離型時に変形することや取り出し可能までの冷却時間が長く好ましくない。また、5質量部を超えると成形品表面の外観を損なうことがあり、好ましくない。高級脂肪酸としては、ステアリン酸、ラウリル酸、モンタン酸などが例示される。周期表第IIa属としては、マグネシュウム、カルシュウム、バリュウムが挙げられる。具体的な化合物としては、ステアリン酸マグネシュウム、ステアリン酸カルシュウム、モンタン酸カルシュウムが挙げられる。 In the present invention, the metal salt of Group IIa of the periodic table of higher fatty acids is preferably contained in an amount of 0.05 to 5 parts by mass, particularly 0.1 to 2 parts by mass with respect to 100 parts by mass of the carbon fiber. It is. If it is less than 0.05 parts by mass, the releasability after stamping molding is low, and a deep-drawn molded product is not preferable because it is deformed at the time of mold release and the cooling time until it can be taken out is long. Moreover, when it exceeds 5 mass parts, the external appearance of the molded article surface may be impaired, and it is not preferable. Examples of higher fatty acids include stearic acid, lauric acid, and montanic acid. Examples of periodic table group IIa include magnesium, calcium, and valium. Specific examples of the compound include magnesium stearate, calcium stearate, and calcium montanate.
また、本発明の複合材料の成形法は、スタンピング成形が適当な成形法である。従って、金型温度(金型表面温度)が150℃以下、好ましくは100℃以下の通常の射出成形法とは全く異なり、驚いたことに金型温度160〜280℃、好ましくは、180〜260℃の金型にて成形することが好ましい態様である。金型表面温度が160℃未満では、流動性が低く、流動末端やリブ部の充填不足になることがあり好ましくない。また、280℃を超えると、樹脂表面が酸化し、変色や劣化が起こり好ましくない。充填初期に160〜280℃という高温の金型を使用することにより、本発明の特徴を発揮することができる。より高温の金型において充填することで、充填時の材料温度か充填後の材料温度が、材料の結晶化温度より高くなり。成形品取り出しまでの冷却過程で、母相のポリメタキシリレンアジパミドが降温過程での最も結晶化速度が速くなる結晶化ピーク温度を経過することにより、ポリメタキシリレンアジパミド成形品表面の結晶化が十分進行するため、耐熱変形性の高い成形品が得られるためと考察される。もし、ポリメタキシリレンアジパミドが非晶状態や結晶化度が低い成形品は、樹脂のガラス転移点である75℃を超えると変形や流動するので使用できない。 The molding method of the composite material of the present invention is a molding method suitable for stamping molding. Therefore, the mold temperature (mold surface temperature) is completely different from the usual injection molding method of 150 ° C. or less, preferably 100 ° C. or less, and surprisingly the mold temperature is 160 to 280 ° C., preferably 180 to 260. It is a preferred embodiment to mold with a metal mold at ° C. If the mold surface temperature is less than 160 ° C., the fluidity is low, and the flow ends and the ribs may be insufficiently filled. Moreover, when it exceeds 280 degreeC, the resin surface will oxidize and discoloration and deterioration will occur and it is not preferable. By using a high-temperature mold of 160 to 280 ° C. in the initial stage of filling, the characteristics of the present invention can be exhibited. By filling in a higher temperature mold, the material temperature at the time of filling or the material temperature after filling becomes higher than the crystallization temperature of the material. In the cooling process until removal of the molded product, the polymetaxylylene adipamide of the parent phase passes through the crystallization peak temperature at which the crystallization speed becomes the highest in the temperature lowering process. It is considered that a molded article with high heat distortion resistance is obtained because crystallization proceeds sufficiently. If the polymetaxylylene adipamide is in an amorphous state or has a low degree of crystallinity, it cannot be used because it deforms or flows when it exceeds 75 ° C., which is the glass transition point of the resin.
本発明の樹脂組成物には、上記の必須成分の他に物性改良・成形性改良、耐久性改良を目的として、滑剤、酸化防止剤、難燃剤、耐光剤、耐候剤などが配合できる。
本発明の複合材料の製造法は特に限定されない。例えば、ポリメタキシリレンアジパミドの融点以上に温度調節されたスクリュータイプ押出機のホッパーにポリメタキシリレンアジパミドおよび/またはポリメタキシリレンアジパミド共重合体と結晶核剤などを所定割合に予備混合して供給する。溶融樹脂をギアポンプの回転数にて計量して、樹脂の融点以上に温度調節された含浸用押出機の上流に供給する。一方、ロービング状の炭素繊維を拡張開繊し、含浸用押出機の下流に供給する。下流先端に開口部を絞ったスリットダイを備えた含浸用押出機中で樹脂圧により、炭素繊維ロービングに樹脂を含浸・脱泡する。下流開口部から吐出されたテープ状の炭素繊維とポリメタキシリレンアジパミドからなる複合材料を冷却してかせに巻き取る。さらに、このテープ状複合材料を30mm以上にカットすることや、テープ状複合材料をカットせずに織物状に織って成形用に提供される。また、樹脂の融点以上に温度調節されたスクリュータイプ押出機の上流ホッパーにポリメタキシリレンアジパミドと結晶核剤などを所定割合に予備混合して供給する。下流の出口ダイにロービング状炭素繊維を供給して、繊維の送り速度と樹脂の吐出量を調節して、所定の繊維含有率からなるストランド状の炭素繊維の樹脂被覆材を得る。このストランドを冷却してかせに巻き取る。このストランドを30mm以上にカットするか、織物状に織って成形用に提供される方法などが上げられる。
本発明の複合材は、赤外線加熱や高周波加熱して、樹脂を加熱溶融して、圧縮成形機の好ましくは、ポリメタクリルアジパミドの結晶化温度より高い160〜280℃金型に供給して、賦形冷却後脱型して構造材の部品が成形される。
In addition to the above essential components, the resin composition of the present invention may contain a lubricant, an antioxidant, a flame retardant, a light resistance agent, a weather resistance agent, and the like for the purpose of improving physical properties, moldability, and durability.
The method for producing the composite material of the present invention is not particularly limited. For example, polymetaxylylene adipamide and / or polymetaxylylene adipamide copolymer and crystal nucleating agent, etc. at a predetermined ratio in a hopper of a screw type extruder whose temperature is controlled to be higher than the melting point of polymetaxylylene adipamide. Premixed and supplied. The molten resin is measured at the number of revolutions of the gear pump and supplied upstream of the impregnation extruder whose temperature is adjusted to be equal to or higher than the melting point of the resin. On the other hand, roving-like carbon fibers are expanded and supplied downstream of the impregnation extruder. Carbon fiber roving is impregnated and defoamed with resin pressure in an extruder for impregnation equipped with a slit die having a narrowed opening at the downstream end. A composite material composed of tape-like carbon fiber and polymetaxylylene adipamide discharged from the downstream opening is cooled and wound up skein. Furthermore, the tape-shaped composite material is cut into 30 mm or more, or the tape-shaped composite material is woven into a woven shape without being cut and provided for molding. In addition, polymetaxylylene adipamide and a crystal nucleating agent are premixed at a predetermined ratio and supplied to an upstream hopper of a screw type extruder whose temperature is controlled to be equal to or higher than the melting point of the resin. A roving-like carbon fiber is supplied to the downstream exit die, and a fiber-coating speed and a resin discharge amount are adjusted to obtain a strand-like carbon fiber resin coating material having a predetermined fiber content. The strand is cooled and wound into skeins. A method of cutting the strands into 30 mm or more, or weaving them into a woven shape and providing them for molding can be raised.
The composite material of the present invention is heated and melted by infrared heating or high-frequency heating, and is preferably supplied to a mold at 160 to 280 ° C. higher than the crystallization temperature of polymethacryladipamide in a compression molding machine. Then, after forming and cooling, the mold is removed to form a structural material part.
本発明の複合材から得られた成形部品は、自動車のフレーム、バンパーフェースバーサポート材、シャシーシェル、座席フレーム、サスペンジョン支持部、サンルーフフレーム、バンパービーム、2輪車のフレーム、農機具のフレーム、OA機器のフレーム、機械部品など高い強度と剛性の必要な部品に利用される。 Molded parts obtained from the composite material of the present invention include automobile frames, bumper face bar support materials, chassis shells, seat frames, suspension support parts, sunroof frames, bumper beams, two-wheeled vehicle frames, farm equipment frames, OA. Used for parts that require high strength and rigidity, such as equipment frames and machine parts.
以下に実施例を示して本発明を具体的に説明するが、本発明は実施例に限定されるものではない。
実施例 1〜19
ポリメタキシリレンアジパミド、結晶核剤〔(C)成分〕、離型剤〔(D)成分〕を表1に示した質量部に配合して、265℃に温度調節されたスクリュー式押し出し機のホッパーに投入した。また表1にし示した炭素繊維のロービングを100質量部になる速度で拡張開繊して押出機のダイヘッドに供給した。幅10mm・高さ0.2mmのダイから含浸被覆されたテープ状プリプレグを水槽に浸漬して固化した後、枷に巻き取った。
成形性や物性評価は次のように行った。
(1)離型性
テープ状プリプレグを100mmにカットして15枚重ねて、IRヒータにより、240℃に予熱した後、温度120〜260℃のある温度に温度調節された12X150X3mmの金型にセットして、5分間30MPa圧縮保持した。金型を圧縮成形機から取り出した。1〜30分のある時間放冷後、金型を開き、成形品の離型性を評価した。判断基準は、次のようにした。○:成形品が変形することなく取り出せる。△:成形品がやや変形するが取り出せる。×:成形品に突き出しピンが刺さり離型できない。
(2)荷重たわみ温度
上述の成形品を、デシケータ中で23℃にて48時間保管後、ISO75−2に準じて、フラットワイズにて、1.82MPa荷重下の荷重たわみ温度を測定した。
(3)結晶化温度
上述の試験の表層から試料10mgをDSC用サンプル容器に採取し、ISO11357−3に準拠し、窒素40ml/min流動下で270℃から10℃/minで降温し、発熱がピークを示す温度を測定した。
(3)曲げ特性
また、得られた成形品を、デシケータ中で23℃にて48時間保管後、ISO178に準拠した3点曲げ試験機を使用して、スパン長120mm、クロスヘッド速度1mm/minによる曲げ強度、及び15×20×3mmの試験片を使用してISO14130に準じて、スパン長10mm・クロスヘッド速度1mm/minとして層間せん断強度を測定した。
本発明の目的のひとつである軽量性は、圧縮成形して得られた成形品をアルキメデスの原理により比重を測定し、曲げ強度の比強度により評価した。
EXAMPLES The present invention will be specifically described below with reference to examples, but the present invention is not limited to the examples.
Examples 1-19
A screw type extruder in which polymetaxylylene adipamide, a crystal nucleating agent [component (C)] and a release agent [component (D)] are blended in parts by mass shown in Table 1 and the temperature is adjusted to 265 ° C. Was put into the hopper. Further, the carbon fiber roving shown in Table 1 was expanded and opened at a speed of 100 parts by mass and supplied to the die head of the extruder. A tape-shaped prepreg impregnated and coated from a die having a width of 10 mm and a height of 0.2 mm was immersed in a water bath and solidified, and then wound on a basket.
The moldability and physical properties were evaluated as follows.
(1) Releasable tape-like prepreg is cut into 100 mm, stacked 15 sheets, preheated to 240 ° C. with an IR heater, and then set in a 12 × 150 × 3 mm mold whose temperature is adjusted to a temperature of 120 to 260 ° C. And kept at 30 MPa compression for 5 minutes. The mold was removed from the compression molding machine. After allowing to cool for a period of 1 to 30 minutes, the mold was opened, and the releasability of the molded product was evaluated. Judgment criteria were as follows. ○: The molded product can be taken out without deformation. Δ: The molded product is slightly deformed but can be taken out. X: The protruding pin sticks into the molded product and cannot be released.
(2) Deflection temperature under load After the molded product was stored at 23 ° C. for 48 hours in a desiccator, the deflection temperature under a load of 1.82 MPa was measured flatwise in accordance with ISO75-2.
(3) Crystallization temperature 10 mg of sample from the surface layer of the above test was collected in a DSC sample container, and the temperature was decreased from 270 ° C. to 10 ° C./min under a flow of nitrogen of 40 ml / min according to ISO 11357-3. The temperature showing the peak was measured.
(3) Bending characteristics The obtained molded product was stored in a desiccator at 23 ° C. for 48 hours, and then a span length of 120 mm and a crosshead speed of 1 mm / min using a three-point bending tester compliant with ISO178. In accordance with ISO14130, the interlaminar shear strength was measured at a span length of 10 mm and a crosshead speed of 1 mm / min using a test piece of 15 × 20 × 3 mm.
Lightness, which is one of the objects of the present invention, was evaluated by measuring the specific gravity of a molded product obtained by compression molding according to Archimedes' principle and the specific strength of bending strength.
比較例1〜9
ポリアミド樹脂、結晶核剤、離型剤の種類や配合比を表2に示したように変更した以外は、実施例と全く同様にプリプレグを作製した後、テストピースを成形した。得られた試験片について,実施例と全く同様に曲げ強度と層間せん断強度を測定した。得られた試験データを表2に合わせて示した。
Comparative Examples 1-9
A prepreg was prepared in the same manner as in Example except that the types and blending ratios of polyamide resin, crystal nucleating agent, and release agent were changed as shown in Table 2, and then a test piece was molded. About the obtained test piece, the bending strength and the interlaminar shear strength were measured in exactly the same manner as in the example. The obtained test data is shown in Table 2 together.
実験に使用した原料と記号
MXD6−1:PA MXD6(東洋紡績製、T600、MFR50g/10min)
MXD6−2:PA MXD6/6(東洋紡績製試作品、 MXD6/6=80/20(モル比)、MFR72g/10min)
MXD6−3:PA MXD6/6(東洋紡績製試作品、MXD6/6=60/40(モル比、MFR 68g/10min)
T842:PA6 (東洋紡績製、 T842,MFR42g/10min)
炭素繊維:帝人社製東邦テナックス IMS40(単繊維径6.4μm、6000フィラメント)
G21:PA6I/X(エムスケミー製、グリボリーG21)
MW5000:タルク (林化成製、ミクロンホワイト)平均粒径 4μm
ASP200:クレイ(林化成製、カオリンASP200)平均粒径 0.5μm
1707:Na塩アイオノマー(三井化学製、ハイミラン)
SiO2:シリカ(林化成製、ハイシレックス)平均粒径15μm)
St−Mg:ステアリン酸マグネシュウム(淡南化学製)
CAV102:モンタン酸カルシュウム塩(クラリアント製)
St−Al:ステアリン酸アルミニュウム(ナカライテスク製)
St−Zn:ステアリン酸亜鉛(ナカライテスク製)
St−A:ステアリン酸(ナカライテスク製)
Raw materials and symbols used in the experiment MXD6-1: PA MXD6 (Toyobo, T600, MFR 50 g / 10 min)
MXD6-2: PA MXD6 / 6 (Toyobo Prototype, MXD6 / 6 = 80/20 (molar ratio), MFR 72g / 10min)
MXD6-3: PA MXD6 / 6 (Toyobo Prototype, MXD6 / 6 = 60/40 (molar ratio, MFR 68g / 10min)
T842: PA6 (Toyobo, T842, MFR42g / 10min)
Carbon fiber: Toho Tenax IMS40 manufactured by Teijin Ltd. (single fiber diameter 6.4 μm, 6000 filaments)
G21: PA6I / X (Ms Chemie, Grivory G21)
MW5000: Talc (manufactured by Hayashi Kasei Co., Ltd., micron white) average particle size 4 μm
ASP200: Clay (manufactured by Hayashi Kasei, Kaolin ASP200) average particle size 0.5 μm
1707: Na salt ionomer (Mitsui Chemicals, High Milan)
SiO 2 : Silica (manufactured by Hayashi Kasei, Hi-Silex) average particle size 15 μm)
St-Mg: Magnesium stearate (manufactured by Tamnan Chemical)
CAV102: Montanic acid calcium salt (manufactured by Clariant)
St-Al: Aluminum stearate (manufactured by Nacalai Tesque)
St-Zn: Zinc stearate (manufactured by Nacalai Tesque)
St-A: Stearic acid (manufactured by Nacalai Tesque)
本発明により、生産性に優れ、強度や剛性や耐熱変形性に優れたスタンピング成形品を得ることが可能となり、プリプレグ製造法や成形法も非常に容易であることからも、構造部材やハウジングの樹脂化が可能となり、軽量化や省エネルギーの面から産業界に大きく寄与することが期待される。 According to the present invention, it becomes possible to obtain a stamped molded product having excellent productivity, excellent strength, rigidity and heat distortion resistance, and the prepreg manufacturing method and molding method are very easy. Resinization is possible, and it is expected to make a significant contribution to the industry in terms of weight reduction and energy saving.
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