CONVERTIBLE AIRCRAFT Russian patent published in 2017 - IPC B64C27/22 B64C27/30 B64C37/00 

FIELD: aviation.

SUBSTANCE: convertible aircraft contains fuselage, front and rear fenders, power units containing engines and propellers, chassis, pylons, made rotatable. Two lifting power units are located on pylons with two degrees of freedom in the angles of pitch and yaw along the sides of the fuselage with a possibility to fixing the position and retraction into the fuselage niches with horizontal flight forward or backward. The propulsion system is located on the pylon with two degrees of freedom in the angles of pitch and yaw with a possibility to fix the position in the fuselage tail.

EFFECT: increased reliability, safety, increased flight range.

5 cl, 3 dwg