AIRCRAFT CONFIGURATION HAVING SPIN RESISTANCE Russian patent published in 2018 - IPC B64C3/10 B64C23/06 B64C35/00 

FIELD: aviation.

SUBSTANCE: aircraft comprising of a fuselage, configuration with a T-tail assembly and a high wing, having a leading edge connected to the upper part of the fuselage, where the high wing comprises of the first region adjacent to the fuselage and the second region adjacent to the wing tip, with the first region being adjacent to the second region, and where, at large angles of attack, the stall element and a separate air flow, associated with it, are isolated by discontinuity at the leading edge of the wing within the first region and the air flow below the T-tail assembly in such a way as to stay away from the flight controls located within the second region and controls relating to the T-tail assembly. The wing of the aircraft contains the first region near the root of the wing and the second region near the wing tip. The first region and the second region adjoin each other along a continuous boundary. Discontinuity of the leading edge is done to form at high angles of attack aerodynamic partitions along the continuous boundary, isolating the stall element and separate air flow, associated with it, within the first region and air flow below T-tail assembly. The aircraft is characterized by the use of a wing.

EFFECT: increase of spin resistance by isolating the stall element.

22 cl, 6 dwg