FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to hybrid aircraft design. Aircraft (1) comprises fuselage (2), engine (10), rotary bearing surface (15) equipped with at least one rotor (16), wing (20) including two half-wings (21, 22) extending from one side of fuselage (2) to opposite side, two propellers (30) each fitted on said half-wing (21, 22). Aircraft (1) includes tail propeller (35) for compensation for jet moment and yaw control. Transmission system (40) couples engine (10) with every rotor (16), tail screw (35) and every propeller (30) via differential mechanism (50). The latter is controlled so that every aircrew (30) runs in cruising flight and cannot be driven by engine (10) on ground and at hovering.
EFFECT: better controllability at hovering, higher safety of personnel and passengers.
6 cl, 1 dwg
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