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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0834877 (1997-04-10) |
우선권정보 | FR-0005137 (1996-04-24) |
발명자 / 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 | 피인용 횟수 : 2 인용 특허 : 3 |
A bypass engine including a fan which has its blades disposed in both the imary gas flow path and the secondary gas flow path of the engine is provided with an annular intermediate gas flow path in the space between the primary and secondary flow paths, and gas take-off means is connected to a compr
[ We claim:] [1.] A bypass engine comprising a primary gas flow path and a secondary gas flow path, a fan having blades disposed both in said primary gas flow path and in said secondary gas flow path, said fan also having first and second annular platforms partly bounding said primary and secondary
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