AIRCRAFT WITH REDUCED LOAD ON THE TAIL FUSELAGE AND HORIZONTAL TAIL Russian patent published in 2023 - IPC B64C9/12 B64C21/00 

FIELD: aviation technology.

SUBSTANCE: invention concerns aircraft with reduced load on the horizontal tail and tail section of the fuselage, operated at supersonic flight speeds. The aircraft includes a fuselage, a wing with control surfaces, including left and right flaperons, all-moving horizontal tail. At the same time, the flaperons are configured with the possibility of in-phase deviation in supersonic flight modes depending on the Mach number and the angle of deviation of the horizontal tail.

EFFECT: reduction of aerodynamic loads on the horizontal tail and on the tail section of the fuselage, improvement of the performance characteristics of the aircraft.

1 cl, 4 dwg