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.
Structural material for structure, fuel tank, main wing, and aircraft
20.05.2015
Patent
Elektronische Ressource
Englisch
Structural material for structure, fuel tank, main wing, and aircraft
Europäisches Patentamt | 2017
|STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
Europäisches Patentamt | 2017
|STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
Europäisches Patentamt | 2015
|STRUCTURAL MATERIAL FOR MAKING STRUCTURAL ELEMENTS, FUEL TANK, MAIN WING AND AIRCRAFT
Europäisches Patentamt | 2016
|Fuel tank, main wing, aircraft fuselage, aircraft, and mobile body
Europäisches Patentamt | 2018
|