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특허 상세정보

Actuation mechanism for a convertible gas turbine propulsion system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00    B64D-035/02    B64C-027/22    B64D-033/04    F02C-003/10    F02C-006/08    F02C-006/20    F02C-007/36    F02K-003/02   
출원번호 US-0271196 (2011-10-11)
등록번호 US-9580183 (2017-02-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Carlson, Gaskey & Olds, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 30
초록

A method of powering a rotary-wing aircraft includes selectively coupling and uncoupling a first power turbine to change a power distribution between the rotor system and the secondary propulsion system.

대표
청구항

1. A method of powering a rotary-wing aircraft, comprising: selectively coupling and uncoupling a first power turbine which drives a rotor system and a second power turbine which drives a secondary propulsion system to change a power distribution between the rotor system and the secondary propulsion system, wherein exhaust gas from the first power turbine is free to move to the second power turbine when the first and second power turbines are both coupled and uncoupled, wherein work is extracted from the second power turbine to drive the secondary propul...

이 특허에 인용된 특허 (30)

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