다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.NTIS 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.DataON 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.Edison 바로가기
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.Kafe 바로가기
|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/232 ; 239/26525|
|발명자 / 주소|
|인용정보||피인용 횟수 : 10 인용 특허 : 4|
A vectored thrust compressor for use in remote controlled aircraft comprising a housing having a forwardly facing air intake is disclosed. Two pair of vectorable thrust nozzles connect to the housing and project from opposite sides of the housing. A first pair is disposed at the forward end of the housing and a second pair is located at the aft end. Each thrust nozzle is adjustable such that the thrust nozzles are rotatable simultaneously by remote control. A first ducted-fan is located in the forward end of the housing and is connected to a drive shaft....
A vectored thrust compressor, comprising: (a) a first ducted-fan; (b) a first pair of adjustable directional thrust nozzles arranged opposingly behind said first ducted-fan; (c) means for diverting a portion of an air flow through said first pair of thrust nozzles; (d) a second ducted-fan; (e) a second pair of adjustable directional thrust nozzles arranged opposingly behind said second ducted-fan; (f) means for simultaneously rotating said thrust nozzles by remote control; and (g) a drive shaft connected to said first and second ducted-fans.