Title:
STRUCTURAL MATERIAL FOR STRUCTURE, FUEL TANK, MAIN WING, AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2014/057960
Kind Code:
A1
Abstract:
The purpose of the present invention is to provide: a structural material for structures which is capable of attaining reductions in working time and cost in production steps and of preventing an increase in weight; a fuel tank; a main wing; and an aircraft. A rib (11) as the structural material for structures is characterized by comprising a carbon-fiber-reinforced plastic wherein the reinforcement comprises carbon fibers and the matrix comprises a plastic, and the surface of the carbon-fiber-reinforced plastic was coated with a low-viscosity surface-protective material (18) having conductivity imparted thereto.
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Inventors:
KAMIHARA NOBUYUKI (JP)
ABE TOSHIO (JP)
OKUDA AKIHISA (JP)
IKADA AKIRA (JP)
YAMASHITA MASAYUKI (JP)
KISHIMOTO KAZUAKI (JP)
KAMINO YUICHIRO (JP)
ABE TOSHIO (JP)
OKUDA AKIHISA (JP)
IKADA AKIRA (JP)
YAMASHITA MASAYUKI (JP)
KISHIMOTO KAZUAKI (JP)
KAMINO YUICHIRO (JP)
Application Number:
PCT/JP2013/077434
Publication Date:
April 17, 2014
Filing Date:
October 09, 2013
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
International Classes:
B64C3/34; B64D45/02; C08J7/044
Domestic Patent References:
| WO2012111704A1 | 2012-08-23 |
Foreign References:
| JPH0263725A | 1990-03-05 | |||
| JP2011168792A | 2011-09-01 | |||
| JPH11138669A | 1999-05-25 | |||
| JP2003154591A | 2003-05-27 | |||
| JPH0796579A | 1995-04-11 | |||
| JPH0616846A | 1994-01-25 | |||
| JP2010194749A | 2010-09-09 |
Attorney, Agent or Firm:
FUJITA, Takaharu et al. (JP)
Takaharu Fujita (JP)
Takaharu Fujita (JP)
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