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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0475198 (1983-03-14) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 9 인용 특허 : 1 |
Canards are pivotally mounted on the fuselage of a variable sweep wing jet aircraft and project laterally with respect to the fuselage forwardly of the wings. The canards are positioned and configured to produce pitch control moments about the center of gravity. Thrust-vectoring devices extend from
An aircraft having a fuselage with a nose, jet engine means and wings mounted on and projecting from said fuselage for supplying lift to said aircraft, said wings being pivotally mounted on said fuselage for swinging movement between a forwardly disposed position, wherein the included angle between
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