|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-015/12 B64C-029/00 B64C-015/14 B64C-003/38|
|미국특허분류(USC)||244/124 ; 244/23B ; 244/46 ; 244/48|
|§371/§102 date||19820929 (19820929)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 10 인용 특허 : 2|
A short takeoff and landing aircraft (10) and vertical/short takeoff and landing aircraft (10), having upper surface blowing engines (12, 14) on gull-shaped wings (24, 26) which may be tilted and translated by a variable incidence translation device (52). The translation means (80, 62, 64) is adapted to provide center of gravity travel trim and critical engine out moment trim. Thrust vectoring of the upper surface blowing engines is accomplished by a combination of the upper surface blowing and wing tilt, and vectoring of lower lift/boost engines (124, 1...
A short takeoff and short landing aircraft or vertical/short takeoff and vertical short landing aircraft, comprising: variable incidence wings, one on each side of the aircraft; at least one primary jet engine on each wing, each engine being positioned for upper surface blowing of the jet exhaust over the top of the wing; each engine having a nacelle fixed in a respective wing adapted to be tilted with the wing when its incidence is varied; incidence varying means in the aircraft adjacent each wing for respectively tilting each wing and its engine for ta...