发明名称 構造体用構造材、燃料タンク、主翼及び航空機
摘要 The purpose of the present invention is to provide: a structural material for structures which is capable of attaining reductions in working time and cost in production steps and of preventing an increase in weight; a fuel tank; a main wing; and an aircraft. A rib (11) as the structural material for structures is characterized by comprising a carbon-fiber-reinforced plastic wherein the reinforcement comprises carbon fibers and the matrix comprises a plastic, and the surface of the carbon-fiber-reinforced plastic was coated with a low-viscosity surface-protective material (18) having conductivity imparted thereto.
申请公布号 JP5852255(B2) 申请公布日期 2016.02.03
申请号 JP20140540861 申请日期 2013.10.09
申请人 三菱重工業株式会社 发明人 神原 信幸;阿部 俊夫;奥田 晃久;井加田 朗;山下 政之;岸本 和昭;神納 祐一郎
分类号 C08J7/04;B32B5/00;B64C1/00;B64C3/34;B64D45/02 主分类号 C08J7/04
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