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

摘要

The purpose of the present invention is to provide a fuel tank, mainwings, an aircraft fuselage, an aircraft, and a moving body, which enableworking hours and costs involved in quality management to be reduced, andweight increases to be prevented. The fuel tank comprises a structural memberthat uses a carbon fiber reinforced plastic (CFRP) (15) including areinforcingmaterial containing carbon fiber and a matrix containing plastic. Thestructuralmember is formed by laminating conductive sheets (17) between prepregs ofthe carbon fiber reinforced plastic (CFRP) (15), and being formed with afastening hole (22) in which a bolt is fastened.