FUEL TANK FOR AIRCRAFT

摘要

Provided is a fuel tank for an aircraft, the fuel tank capable of suppressing electrostatic charge, for example, caused by flow electrification with fuel. Specifically, a fuel tank for an aircraft is provided with an upper outer plate (5) and a lower outer plate (7) which have electric conductivity and form part of a container for housing fuel, an inner structure (19) which is formed by metal, and an inner surface layer (15) which has a semiconductor property or an insulation property and is formed integrally on the inner surfaces of the upper outer plate (5) and the lower outer plate (7) in a location where the inner structure (19), and the upper outer plate (5) and the lower outer plate (7) are in contact with each other and in a surrounding portion thereof, wherein the inner surface layer (15) at least in the surrounding portion is formed by a material having the semiconductor property.