|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/226.1; 060/266; 060/785|
|우선권정보||FR-06 00473 (2006-01-19)|
|§371/§102 date||20080707 (20080707)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 9 인용 특허 : 6|
A pre-cooler having an annular cross-sectional shape about the axis of a pod and arranged inside the rear part of an inner shroud in external contact with a cold flow exiting a fan duct channel and in close contact with a cooling air stream drawn from the cold flow.
1. A bypass turbine engine for an aircraft, comprising: a hollow nacelle of longitudinal axis provided, at the front, with an air inlet and, at the rear, with an air outlet;a central hot-stream generator, positioned axially in said nacelle;a fan positioned axially in said nacelle forward of said central generator and able to generate a cold stream for said turbine engine;an outer fairing borne internally by said nacelle and an inner fairing surrounding said central generator, said outer and inner fairings between them delimiting a fan duct of annular cro...