The objective of the present invention is to provide: a fuel tank that can prevent an increase in weight and can have reduced cost and working time during a production process, a main wing; an aircraft fuselage; an aircraft, and a mobile body. The fuel tank is provided with a structural member that uses a carbon-fiber-reinforced plastic of which the reinforcing material (15) contains carbon fibers and the matrix (17) contains plastic. The matrix (17) is imparted electrical conductivity. Also, a cut surface (11a) That is of the structural member and that is formed by the strcutural member being cut may be exposed within the fuel tank where a fuel is housed.
FUEL TANK, MAIN WING, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOBILE BODY
KRAFTSTOFFTANK, HAUPTFLÜGEL, FLUGZEUGRUMPF, FLUGZEUG UND MOBILER KÖRPER
RÉSERVOIR DE CARBURANT, AILE PRINCIPALE, FUSELAGE D'AÉRONEF, AÉRONEF ET CORPS MOBILE
2023-03-08
Patent
Elektronische Ressource
Englisch
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