|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/125 ; 244/23D ; 244/55 ; 244/45R|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 15 인용 특허 : 0|
A vertical lift and short takeoff airplane achieving a powered lift which is generated by deflecting downward on the order of nearly 90°the slipstream from the driven propellors by means of the wing flap system of the airplane.
A deflected propellor slipstream vertical lift airplane structure, comprising a fuselage, wing means in connection with said fuselage, said wing means being secured to the fuselage having a section thereof extending outwardly of each side of the fuselage, three or more engines spanning said wing means, inboard of said engines being adjacent said fuselage and outboard of said engines being outwardly of said fuselage, a first means to independently adjust the power of each of said engines, propellors being respectively carried by said engines and extending...