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Variable specific thrust turbofan engine

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F02K-003/02
출원번호 US-0982167 (1992-11-24)
발명자 / 주소
  • Giffin
  • III Rollin G. (Cincinnati OH)
출원인 / 주소
  • General Electric Company (Cincinnati OH 02)
인용정보 피인용 횟수 : 76  인용 특허 : 0

초록

An aircraft turbofan engine and method of operation effect variable specific thrust. The engine includes a fan disposed in a fan casing and a booster compressor disposed in a first flow splitter and powered by a core engine. A second flow splitter is disposed inside the fan casing and defines fan ou

대표청구항

A turbofan gas turbine engine comprising: a fan disposed in a fan casing defining an annular fan duct for receiving fan air compressed by said fan; a booster compressor disposed in an annular first flow splitter and in serial flow communication with said fan; a second compressor disposed in an inner

이 특허를 인용한 특허 (76)

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