Title:
ダクトなしのプロペラを備えた航空機エンジンの空気取入口
Document Type and Number:
Japanese Patent JP5416786
Kind Code:
B2
Abstract:
An air intake for an aeroplane engine of type with unducted propellers, which intake can be connected by a pylon to a fuselage of an aeroplane, a local length of the air intake, measured parallel to the axis of the engine between a point on a leading edge of the air intake and a transverse plane situated at an inlet impeller of the engine compressor, is longer in a region of the air intake connected to the pylon and shorter in a region of the air intake opposite the pylon.
Inventors:
Basilan, Stephane Emanuel Daniel
Application Number:
JP2011543789A
Publication Date:
February 12, 2014
Filing Date:
November 09, 2009
Export Citation:
Assignee:
SNECMA
International Classes:
B64D33/02; B64D27/14
Domestic Patent References:
| JP2164695A | ||||
| JP1101296A | ||||
| JP2009530173A | ||||
| JP7179199A | ||||
| JP5153111A |
Attorney, Agent or Firm:
Kawaguchi International Patent Office