|국가/구분||United States(US) Patent 등록|
|우선권정보||FR-08 06381 (2008-11-14)|
|§371/§102 date||20110509 (20110509)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 7|
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.
1. An air inlet of an aeroengine including unducted pusher propellers, the engine being for connection via a pylon to a fuselage of an airplane, wherein a local length of the air inlet, measured parallel to an axis of the engine between a point of a leading edge of the air inlet and a transverse plane situated level with an upstream rotor of the compressor of the engine is longer in a zone of the air inlet that is connected to the pylon, and shorter in a zone of the air inlet opposite from the pylon. 2. An air inlet according to claim 1, wherein the rati...