FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to combined helicopter designs. Aircraft made in form of combined helicopter has fuselage (1) of aircraft, located on fuselage (1) of aircraft rotor (2) and cyclone pulling screws (3, 3’) located on side of fuselage (1) of aircraft with outer end surface. Cycloidal pulling screws (3, 3’) are connected to fuselage (1) of aircraft by means of suspension device (4, 4’), which holds cycloid pulling screws (3, 3’) beyond their outer end. Each cycloid pulling screw (3, 3’) is made with possibility of separate control and independent from other.
EFFECT: by means of cycloid pulling screws (3, 3’) providing torque compensation of rotor (2) and reduction of its dimensions.
13 cl, 8 dwg
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