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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0212924 (1998-12-16) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 7 인용 특허 : 14 |
A short take-off and vertical landing ("STOVL") aircraft has a conventional gas turbine engine that is selectively mechanically connected to a vertically-oriented lift fan by a drive shaft when the aircraft operates in a vertical flight mode. An engine control provides for rapid response attitude co
[ Having thus described the invention, what is claimed is:] [1.]1. A control system for a gas turbine engine disposed on an aircraft, the aircraft also having a lift fan, the engine being coupled to the lift fan during operation of the aircraft in a vertical mode of flight, the engine having a compr
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