GYROPLANE Russian patent published in 2018 - IPC B64C27/22 B64C27/02 

FIELD: aviation.

SUBSTANCE: invention relates to the field of aviation, in particular to the combined aircraft designs. Gyroplane contains the frame mounted cockpit, chassis, the mast mounted main rotor, horizontal stabilizer, control fork, engine, rusher rotor. Gyroplane is additionally provided with at least one pair of auxiliary rotor engine-propeller combinations, made with the possibility of the main rotor preliminary unwinding performance and with the possibility of the air flow angle direction smooth change with the take-off rotation speed reaching and the thrust force change to the horizontal component. Pairs of auxiliary rotor engine-propeller combinations are installed on the gyroplane sides and are located around the main rotor rotation circumference. Additional auxiliary rotor engine-propeller combinations are made with the possibility of rotation on the remote beam at an angle of ±90 degrees.

EFFECT: enabling the possibility to perform the vertical hopping take-off without the rotor pitch changing mechanism, increase in the flight stability and dynamic characteristics.

4 cl, 2 dwg