|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/226.1; 060/226.3; 060/229; 239/265.17|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 10 인용 특허 : 6|
The present invention relates to a variable cycle boost propulsor system for use on an aircraft. The variable cycle boost propulsor system includes an engine, a turbine, a fan connected to the turbine, and a valve system for delivering the fluid output from the engine to the turbine for driving the turbine and the fan and thereby generating additional thrust for the aircraft. The engine is also used to provide power to one or more systems onboard the aircraft.
1. A variable boost cycle propulsor system for a vehicle comprising:an engine; a turbine mounted within a casing; a bypass passageway formed between an inner surface of a fuselage of said vehicle and an outer surface of said casing; a fan driven by said turbine, said fan being positioned within said bypass passageway; and means for selectively delivering a fluid output from said engine to said turbine for selectively creating thrust. 2. The variable boost cycle propulsor system according to claim 1, further comprising said engine being embedded within sa...