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특허 상세정보

Gas turbine aircraft engine with power variability

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 060/226.1; 060/268; 060/802; 060/039.162
출원번호 US-0114962 (2008-05-05)
등록번호 US-8181442 (2012-05-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Norton Rose Canada LLP
인용정보 피인용 횟수 : 5  인용 특허 : 49
초록

A gas turbine aircraft engine with power variability is provided. The gas turbine aircraft engine comprises a compressor and a turbine mounted on a common shaft, and, a continuously variable transmission coupled to the shaft for transmitting power to a propulsion load.

대표
청구항

1. A gas turbine aircraft engine with power variability comprising: an engine case;a single spool comprising a compressor and a turbine mounted on a common shaft inside the engine case;a propulsion load selected from a group comprising of: a fan and a propeller; anda continuously variable transmission provided between the single spool and the propulsion load, the continuously variable transmission being coupled to the shaft within the engine case for transmitting power to the propulsion load, the continuously variable transmission being operable to vary ...

이 특허에 인용된 특허 (49)

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