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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0383871 (1989-07-21) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 3 인용 특허 : 0 |
Gas turbine engine power plants of the ducted fan type. During reversed thrust operation of the power plant, air is induced into the bypass duct through two inlets in one type of power plant is concerned. One of these, a secondary inlet, is located between a stationary front section of the bypass du
A ducted fan type power plant which is capable of generating reverse thrust and comprises: a. a gas turbine engine; b. a fan driven by said engine; c. an elongated bypass duct which is open at its front and rear ends and surrounds said fan, said bypass duct having a fixed forward section and a rear
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