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
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