FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY

摘要

The purpose of the present invention is to provide a fuel tank, main wings, an aircraft fuselage, an aircraft, and a moving body, which enable working hours and costs involved in a manufacturing process to be reduced, and weight increases to be prevented. The fuel tank comprises a structural member in which carbon fiber reinforced plastic (CFRP) (15) is used, the carbon fiber reinforced plastic (CFRP) (15) comprising a reinforcing material that includes carbon fibers and a matrix that includes plastic. The structural member is formed by laminating a conductive sheet (17) between prepregs of the carbon fiber reinforced plastic (CFRP) (15). In this case, a cut surface (11a) of the structural member formed by cutting the structural member may be exposed on the inside in which fuel is stored.