Title:
SLAT, WING OF AIRCRAFT, MOVING BLADE OF AIRCRAFT, AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2013/027388
Kind Code:
A1
Abstract:
The purpose of the present invention is to provide a moving blade such as a slat capable of maintaining and fulfilling a minimum necessary function even when suffering damage due to a collision with a bird or the like, and a wing using the same.
Both ends of one or more wire cables (15) are fastened to a pair of rib members (10A, 10B) provided in the short side direction of a slat (3). The wire cable (15) is disposed through through-holes (13) formed in respective rib members (10) located between the rib members (10A, 10B).
This wire cable (15) prevents the slat (3) from getting separated into pieces between the rib members (10A, 10B) even if a bird or the like collides with the slat (3) during the flight of an aircraft and not only the outer skin (4) of the slat (3) but also the rib members (10) suffer damage such as deformation.
Inventors:
TANAKA HIDEAKI (JP)
Application Number:
PCT/JP2012/005228
Publication Date:
February 28, 2013
Filing Date:
August 21, 2012
Export Citation:
Assignee:
MITSUBISHI AIRCRAFT CORP (JP)
TANAKA HIDEAKI (JP)
TANAKA HIDEAKI (JP)
International Classes:
B64C9/24
Foreign References:
| GB525400A | 1940-08-28 | |||
| JP2009006987A | 2009-01-15 |
Other References:
MAIKURU C-Y NIU: "Airframe Structural Design Kokuki Kozo Sekkei - Kitai Sekkei no Tameno Jitsuyosho", YUGEN KAISHA NAGOYA KOKU GIJUTSU, 21 February 2000 (2000-02-21), pages 343 - 344
Attorney, Agent or Firm:
OBA, Mitsuru et al. (JP)
Mitsuru Oba (JP)
Mitsuru Oba (JP)
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Claims: