Title:
航空機の燃料タンク
Document Type and Number:
Japanese Patent JP5101554
Kind Code:
B2
Abstract:
An aircraft fuel tank capable of suppressing electrostatic charging caused, for example, by flow electrification with the fuel. The aircraft fuel tank comprises an upper skin (5) and a lower skin (7) that exhibit conductivity and form a portion of a container for storing fuel, an internal structure (19) formed from a metal, and an inner surface layer (15) which has semiconductor properties or insulating properties and is formed in an integral manner on the inner surfaces of the upper skin (5) and the lower skin (7) in a location where the internal structure (19) contacts the upper skin (5) and the lower skin (7), and in the surrounding portion thereof, wherein the inner surface layer (15) is formed, at least in the surrounding portion, from a material having semiconductor properties.
More Like This:
| WO/2012/101439 | STRINGER, AIRCRAFT WING PANEL ASSEMBLY, AND METHOD OF FORMING THEREOF |
| JPH08151000 | INTEGRAL FUEL TANK |
| WO/2022/180355 | AIRCRAFT WING WITH FUEL TANK AND FUEL CELL |
Inventors:
Hiroaki Yamaguchi
Yuichiro Kano
Tohashi Hashigami
Kazuyuki Oguri
Koichi Nakamura
Yuichiro Kano
Tohashi Hashigami
Kazuyuki Oguri
Koichi Nakamura
Application Number:
JP2009083361A
Publication Date:
December 19, 2012
Filing Date:
March 30, 2009
Export Citation:
Assignee:
MITSUBISHI HEAVY INDUSTRIES,LTD.
Japan Aerospace Industry Association
Japan Aerospace Industry Association
International Classes:
B64C3/34; B64D37/02
Domestic Patent References:
| JP2008226296A |
Foreign References:
| US20080302545 | ||||
| US20080297967 | ||||
| US20080137259 | ||||
| DE3128581A |
Attorney, Agent or Firm:
Noriharu Fujita
Kunio Ueda
Kunio Ueda
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