发明名称 VERTICAL TAKE-OFF AND LANDING FLIGHT VEHICLE
摘要 A vertical take-off and landing flight vehicle comprises a bent wing along the contour, inside which a fuselage is installed with a clearance, and a power plant. For effective use the wing has a profile of aircraft wing. Power plant is installed in such a way that it forces the air flow mainly into the wing plane in the direction from the center of fuselage to the wing.
申请公布号 UA28455(U) 申请公布日期 2007.12.10
申请号 UA20070008756U 申请日期 2007.07.30
申请人 发明人
分类号 B64C29/00;B64C39/00 主分类号 B64C29/00
代理机构 代理人
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