|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-015/12 B64C-029/04 B64D-027/00|
|미국특허분류(USC)||244/52 ; 244/123 ; 244/125 ; 244/56|
|발명자 / 주소|
|인용정보||피인용 횟수 : 11 인용 특허 : 0|
An unmanned aerial vehicle incorporates a single engine with bifurcated exhausts which are coupled to side mounted rotating nozzles through a swivel joint. Jet deflection means are mounted to the end of the rotating nozzles to achieve additional degrees of freedom for the aircraft.
In an aircraft, an improved thrust system comprising: a single engine located forwardly of the aircraft\s center of gravity, at a forwardly, upwardly acute angle to a longitudinal axis of the aircraft, and enclosed within a fuselage and having bifurcated exhausts; first conduit means for directing respective exhaust flows in a first direction transverse of the engine, the flows equaling an entire exhaust output of the engine; first and second nozzles rotatably mounted to ends of corresponding first conduit means for movement in mutually parallel planes s...