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1. (WO2010113793) FUEL TANK FOR AIRCRAFT

Pub. No.:    WO/2010/113793    International Application No.:    PCT/JP2010/055361
Publication Date: Fri Oct 08 01:59:59 CEST 2010 International Filing Date: Sat Mar 27 00:59:59 CET 2010
IPC: B64C 3/34
B64D 37/02
Applicants: MITSUBISHI HEAVY INDUSTRIES, LTD.
三菱重工業株式会社
THE SOCIETY OF JAPANESE AEROSPACE COMPANIES
社団法人日本航空宇宙工業会
YAMAGUCHI, Hiroaki
山口 弘晃
KAMINO, Yuichiro
神納 祐一郎
HASHIGAMI, Tooru
橋上 徹
OGURI, Kazuyuki
小栗 和幸
NAKAMURA, Koichi
中村 康一
Inventors: YAMAGUCHI, Hiroaki
山口 弘晃
KAMINO, Yuichiro
神納 祐一郎
HASHIGAMI, Tooru
橋上 徹
OGURI, Kazuyuki
小栗 和幸
NAKAMURA, Koichi
中村 康一
Title: FUEL TANK FOR AIRCRAFT
Abstract:
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.