首页>
外国专利>
SUPERSONIC AIRPLANE WITH VERTICAL TAKE-OFF AND LANDING
SUPERSONIC AIRPLANE WITH VERTICAL TAKE-OFF AND LANDING
展开▼
机译:垂直起降的超音速飞机
展开▼
页面导航
摘要
著录项
相似文献
摘要
The invention relates to a supersonic airplane, with vertical take-off and landing, used for transportation or military missions. According to the invention, the supersonic airplane is propelled by two orientable turbo-jet engines (2), laterally situated, on some wings (3 and 4) which, during the vertical take-off or landing, may rotate 90 around a transverse axle (6), fastened on the fuselage (1), situated in the airplane centroid area, together with the wings (3 and 4) which flank each turbo-jet engine (2).
展开▼