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특허 상세정보

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Geared turbofan gas turbine engine architecture

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/36    F02K-003/06    F02C-003/04    F02K-001/78    F01D-009/02    F02C-003/107    F04D-029/32    F02C-009/18    F04D-027/00    F01D-005/06   
출원번호 US-0420155 (2017-01-31)
등록번호 US-9828944 (2017-11-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds, PC
인용정보 피인용 횟수 : 0  인용 특허 : 81
초록

A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5.

대표
청구항
▼

1. A gas turbine engine comprising: a fan section including less than 18 fan blades, the low fan pressure ratio measured across the fan blades alone;a gear train;a compressor section;a combustor in fluid communication with the compressor section;a turbine section in fluid communication with the combustor and including a fan drive turbine and a second turbine, the fan drive turbine driving a fan rotor through the gear train wherein: a power density greater than 4.0 and less than 5.5 lbf/in3 wherein power density is defined as Sea Level Takeoff Thrust in l...

이 특허에 인용된 특허 (81)

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