发明名称 STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
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 CA2885204(C) 申请公布日期 2017.02.28
申请号 CA20132885204 申请日期 2013.10.09
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 KAMIHARA, NOBUYUKI;ABE, TOSHIO;OKUDA, AKIHISA;IKADA, AKIRA;YAMASHITA, MASAYUKI;KISHIMOTO, KAZUAKI;KAMINO, YUICHIRO
分类号 C08J7/04;B64C3/34;B64D45/02 主分类号 C08J7/04
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