A fuel tank in which it is possible to reduce working hours or cost in a manufacturing process and prevent an increase in weight in, a main wing, an aircraft fuselage, an aircraft, and a mobile body. The fuel tank is provided with a structural member using carbon fiber reinforced plastic in which a reinforcing material includes carbon fibers and a matrix includes plastic, wherein the matrix has electrical conductivity applied thereto. Furthermore, a cut surface of the structural member, which is formed by cutting the structural member, may be exposed to the inside in which fuel is accommodated, of a fuel tank.
Fuel tank, main wing, aircraft fuselage, aircraft, and mobile body
03.07.2018
Patent
Elektronische Ressource
Englisch
FUEL TANK, MAIN WING, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOBILE BODY
Europäisches Patentamt | 2023
|FUEL TANK, MAIN WING, AIRCRAFT FUSELAGE, AIRCRAFT AND MOVING BODY
Europäisches Patentamt | 2016
|FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY
Europäisches Patentamt | 2018
|FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY
Europäisches Patentamt | 2018
|Fuel tank, main wings, aircraft fuselage, aircraft, and moving body
Europäisches Patentamt | 2015
|