发明名称 VERTICAL TAKE-OFF AND LANDING AIRCRAFT
摘要 FIELD: transport.SUBSTANCE: invention relates to rotorcraft, namely, to VTOL aircraft. VTOL aircraft consists of wings actuator, cabin, engines and fan. Wings drive consists of four frames composed by guides of the wing pipe bearings, angle pieces and strips. Wings can generate air flow. Wings and pulleys are secured to toothed belts. Pulleys and levers for control over wing angle of attack are fitted on two shafts. Guide bearings allow levers welded to the left and right frames to run therein. There are two driven sprockets and guard sheet. Angle of attack of the wings does not vary at flight at straight section atop and at bottom. Wings can vary said angle of attack at flight in semicircle.EFFECT: efficient vertical takeoff and landing, higher efficiency of power plant.4 cl, 12 dwg
申请公布号 RU2521862(C1) 申请公布日期 2014.07.10
申请号 RU20120152131 申请日期 2012.12.04
申请人 SHARYPOV VALERIJ NIKOLAEVICH 发明人 SHARYPOV VALERIJ NIKOLAEVICH;SHARYPOV JURIJ VALER'EVICH
分类号 B64C29/00 主分类号 B64C29/00
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