发明名称 VERTICAL TAKE-OFF AND LANDING AIRCRAFT
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to VTOL aircraft. aircraft comprises round or oval fuselage with convex top surface and flat bottom surface with central part extending downward whereat cabin with control system and power plant are arranged. Fuselage has four through annular openings to accommodate four airscrews to be turned from horizontal plane into vertical plane. Two vertical airscrews are arranged at fuselage front and rear to turn from vertical plane into horizontal plane. All airscrews feature pitch varying both jointly and separately and are driven by two engines via transmission. Aircraft is equipped with hydraulic system, robot pilot, rescue parachute, observation system, and emergent solid engines. ^ EFFECT: higher maneuverability and safety. ^ 3 dwg
申请公布号 RU2458822(C1) 申请公布日期 2012.08.20
申请号 RU20110119769 申请日期 2011.05.18
申请人 DUROV PETR IVANOVICH 发明人 DUROV PETR IVANOVICH
分类号 B64C29/00 主分类号 B64C29/00
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