STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
- New search for: KAMIHARA NOBUYUKI
- New search for: ABE TOSHIO
- New search for: OKUDA AKIHISA
- New search for: IKADA AKIRA
- New search for: YAMASHITA MASAYUKI
- New search for: KISHIMOTO KAZUAKI
- New search for: KAMINO YUICHIRO
- New search for: KAMIHARA NOBUYUKI
- New search for: ABE TOSHIO
- New search for: OKUDA AKIHISA
- New search for: IKADA AKIRA
- New search for: YAMASHITA MASAYUKI
- New search for: KISHIMOTO KAZUAKI
- New search for: KAMINO YUICHIRO
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.
Document information
STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
2015-10-01
Patent
Electronic Resource
English
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