发明名称 INTERMEDIATE FOR COMPOSITE MATERIAL
摘要 PURPOSE:An intermediate for composite materials, excellent in mechanical properties such as rigidity and suitable for use in aircraft, prepared by impregnating a reinforcement with a resin composition comprising a specified additive for epoxy resins, an epoxy resin and a curing agent. CONSTITUTION:An additive for epoxy resins of formula III (wherein R1, R2, R3 and R4 are each H, a 1-17C aliphatic group, alicyclic group, aromatic group, heterocyclic group, or the like, and X is oxygen, sulfur, or the like) is prepared by reacting a compound of formula I (e.g., N-methylformamide) with a compound of formula II (e.g., propylene oxide). This additive is mixed with an epoxy resin, a curing agent (e.g., m-phenylenediamine) and, optionally, a cure accelerator (e.g., 2-methylimidazole). A reinforcement (e.g., glass fiber or carbon fiber) is impregnated with the obtained resin composition to form the purpose intermediate for composite materials.
申请公布号 JPS60231735(A) 申请公布日期 1985.11.18
申请号 JP19840065605 申请日期 1984.04.02
申请人 MITSUBISHI RAYON KK 发明人 TADA TAKASHI;AGATA AKIRA;II YASUAKI
分类号 C08J5/24 主分类号 C08J5/24
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