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Patent Searching and Data


Title:
FUEL TANK, MAIN WINGS, AIRCRAFT FUSELAGE, AIRCRAFT, AND MOVING BODY
Document Type and Number:
WIPO Patent Application WO/2014/156274
Kind Code:
A1
Abstract:
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 quality management to be reduced, and weight increases to be prevented. The fuel tank is provided with a reinforcing material containing carbon fibers, and a structural member that uses a carbon fiber reinforced plastic (CFRP) (15) having a matrix containing plastic. The structural member is molded with conductive sheets (17) laminated between prepregs of the CFRP (15), and a fastening hole (22) through which a bolt is fastened is formed.

Inventors:
KAMIHARA NOBUYUKI (JP)
KISHIMOTO KAZUAKI (JP)
ABE TOSHIO (JP)
KAMINO YUICHIRO (JP)
Application Number:
PCT/JP2014/051831
Publication Date:
October 02, 2014
Filing Date:
January 28, 2014
Export Citation:
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Assignee:
MITSUBISHI HEAVY IND LTD (JP)
International Classes:
B64C3/34; B32B5/00; B32B7/08; B60K15/03; B64D45/02; H01M8/00; H01M8/04
Domestic Patent References:
WO2011050040A12011-04-28
Foreign References:
US6327132B12001-12-04
JP2010132286A2010-06-17
US4755904A1988-07-05
US20110255205A12011-10-20
JP2007521995A2007-08-09
JP2010235133A2010-10-21
JP2007301838A2007-11-22
JP2010280904A2010-12-16
JP2011168792A2011-09-01
Other References:
See also references of EP 2979977A4
Attorney, Agent or Firm:
FUJITA, Takaharu et al. (JP)
Takaharu Fujita (JP)
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