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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Gas turbine engine assembly and method of assembling same

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 060/226.1; 060/792
출원번호 UP-0461019 (2006-07-31)
등록번호 US-7694505 (2010-05-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Andes, Esq., William Scott
인용정보 피인용 횟수 : 119  인용 특허 : 7
초록

A method of assembling a gas turbine assembly includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine, coupling a low-pressure turbine axially aft from the core gas turbine engine, coupling a fan assembly axially forward from the core gas turbine engine, and coupling a booster compressor to the low-pressure turbine such that the booster compressor and the low-pressure turbine rotate at a first rotational speed.

대표
청구항
▼

What is claimed is: 1. A method of assembling a gas turbine engine assembly, said method comprising: providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine; coupling a low-pressure turbine axially aft of the core gas turbine engine; coupling a fan assembly axially forward of the core gas turbine engine; and coupling a booster compressor to the low-pressure turbine; and coupling the fan assembly to the booster compressor via a gearbox and a drive shaft such that, upon rotation of the drive shaft in a first ro...

이 특허에 인용된 특허 (7)

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  4. Orlando,Robert Joseph; Venkataramani,Kattalaicheri Srinivasan; Lee,Ching Pang; Moniz,Thomas Ory; Murrow,Kurt David. High thrust gas turbine engine with improved core system. USP2006087096674.
  5. Boeck, Alexander. Method and apparatus for the cooling of jet-engine turbine casings. USP2003096625989.
  6. Parnes Marvin J. (Norwalk CT) Vogel Herman (Newtown CT). Oil cooler for fan jet engines. USP1990044914904.
  7. Adamson Arthur P. (Cincinnati OH) Wall Robert A. (Wyoming OH). Turbofan engine having a counterrotating partially geared fan drive turbine. USP1990114969325.

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