发明名称 VERTICAL TAKE-OFF AND LANDING AIRCRAFT
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to aircraft, namely, to VTOL aircraft. Proposed aircraft comprises streamlined fuselage, ring-shaped wing arranged inside and/or outside of said fuselage. Fuselage houses fly wheel made up of hollow disk equipped with remote control valves, power plant consisting of signal blower or turbofan engine, and ejector device. Besides, aircraft comprises control system consisting of vertical rudders, thrust vector, bank and pitch control rudders made up of shaped rings arranged in symmetry relative to each other and to fuselage axis. ^ EFFECT: increased lift, reduced fuel consumption and better maneuverability. ^ 13 cl, 5 dwg
申请公布号 RU2435707(C2) 申请公布日期 2011.12.10
申请号 RU20090134950 申请日期 2008.10.31
申请人 PAVLIKOV VJACHESLAV ANATOL'EVICH;POLIN ALEKSANDR NIKOLAEVICH 发明人 PAVLIKOV VJACHESLAV ANATOL'EVICH;POLIN ALEKSANDR NIKOLAEVICH
分类号 B64C29/00 主分类号 B64C29/00
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