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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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