SUPERSONIC AIRCRAFT WITH VARIABLE DURING THE FLIGHT WING CURVATURE Russian patent published in 2017 - IPC B64C30/00 B64C3/50 

FIELD: aviation.

SUBSTANCE: supersonic aircraft with variable during the flight curvature of the wing includes a fuselage, a wing with variable curvature, formed as a rigidly attached to the fuselage of the central section box and longitudinal section boxes rotatable about it, connected to the central section box along the upper surface by means of the sliding connection, and along the lower surface by means of the hinged connection and provided with locks of the extreme positions. Sliding connection of the longitudinal sections boxes with the central section box along the upper surface is made as a comb.

EFFECT: reduction of the weight.

18 dwg