发明名称 METHOD OF ROTORCRAFT HORIZONTAL FLIGHT
摘要 FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to rotorcraft. Proposed method consists in that on changing the rotorcraft to horizontal plane by two coaxial rotors, their blades are equipped with compressor air-jet engines and fuel combustion chamber intake valve control system to open the valves only at advancing blades and only at the path of blades at azimuth varying from 45 to 135 degrees.EFFECT: efficient operation on horizontal flight.1 dwg
申请公布号 RU2494925(C1) 申请公布日期 2013.10.10
申请号 RU20120115932 申请日期 2012.04.20
申请人 BOJARER MIKHAIL ZELIKOVICH 发明人 BOJARER MIKHAIL ZELIKOVICH
分类号 B64C27/18 主分类号 B64C27/18
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