Title:
FLAP AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2016/189793
Kind Code:
A1
Abstract:
An aircraft flap 3 is equipped with: a flap body 8 which is provided so as to be deployable with respect to a main wing 2; and inclined portions 5 which are provided so as to protrude on the upper surface 301 of at least the end 40 on the outboard OTB side in the span direction D2 of the flap body 8, and are inclined to the aircraft axial direction D1; and a protruding portion 7 which protrudes smoothly from the lower surface 302 of at least the end 40 on the outboard side. The rear end 52 of each of the inclined portions 5 is located closer to the side end edge 301A of the end 40 in the span direction D2 of the flap body 8 than the virtual line VL that passes through the front end 51 of the inclined portion 5 and is parallel to the aircraft axis direction.
Inventors:
HAYASHI KENSUKE (JP)
MURAYAMA MITSUHIRO (JP)
YAMAMOTO KAZUOMI (JP)
MURAYAMA MITSUHIRO (JP)
YAMAMOTO KAZUOMI (JP)
Application Number:
PCT/JP2016/002012
Publication Date:
December 01, 2016
Filing Date:
April 14, 2016
Export Citation:
Assignee:
MITSUBISHI AIRCRAFT CORP (JP)
JAPAN AEROSPACE EXPLORATION (JP)
JAPAN AEROSPACE EXPLORATION (JP)
International Classes:
B64C3/50; B64C9/18; B64C23/06
Domestic Patent References:
| WO2011007759A1 | 2011-01-20 |
Foreign References:
| US6105904A | 2000-08-22 | |||
| US5253828A | 1993-10-19 | |||
| US20040129838A1 | 2004-07-08 | |||
| US20110008174A1 | 2011-01-13 | |||
| US20080265102A1 | 2008-10-30 |
Other References:
See also references of EP 3305654A4
Attorney, Agent or Firm:
OBA, Mitsuru et al. (JP)
Mitsuru Oba (JP)
Mitsuru Oba (JP)
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