发明名称 CARBON FIBER REINFORCED RESIN COMPOSITE MATERIAL AND PREPREG
摘要 <p>PURPOSE:To obtain a carbon fiber-reinforced resin composite material which is excellent in impact resistance characteristic by reinforcing the composite material with carbon fiber wherein specific gravity is a specific value or lower, tensil elastic modulus is a specific value or higher, tensil strength is a specific value or higher, and peel strength at end of plate is a specific value or higher. CONSTITUTION:For carbon fiber composing carbon fiber reinforced resin composite material or prepreg, specific gravity is 1.75 or lower, tensile elastic modulus and tensile strength which are measured by a strand tensile test are respectively 29tf/mm<2> or higher and 500kgf/mm<2>, and peel strength at end of plate measured by a composite test is 22kgf/mm<2> or higher. For carbon fiber of which specific gravity is larger than 1.75, neight reducing effect is small. Further for carbon fiber wherein tensile elastic modulus is under 29tf/mm<2>, and tensile strength is under 500kg/mm<2>, impact resistance is low, and besides thick composite material is necessarily produced in order to develop a specific characteristic. Then, merits by the weight-reduction are decreased. Further, when peel strength at end of plate is under 22kgf/mm<2>, the maximum load is decreased because of ply separation at impact.</p>
申请公布号 JPH07214551(A) 申请公布日期 1995.08.15
申请号 JP19940008388 申请日期 1994.01.28
申请人 TORAY IND INC 发明人 MATSUHISA YOJI;KOBAYASHI MASANOBU;SHIMIZU KAZUHARU
分类号 A63B53/10;B29B11/16;B29B15/08;B29K105/08;B29L31/52;C08J5/24;(IPC1-7):B29B11/16 主分类号 A63B53/10
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