FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. Airplane with short or vertical takeoff and landing includes integral streamline fuselage, wings with mechanization elements, power plant of air-jet engines, control cabin, integral control system. There are two bearing wings of wings on both sides of fuselage consisting of front section, angular section, longitudinal side section and tail section. Front section has a streamlined shape, which is articulated with fuselage surface. Angular section is made either of rectilinear contour at an angle to fuselage longitudinal axis, or in form of annular sector with angle of annular sector from 50 to 90°, or in the form of a sector of an annular polygon described or inscribed into an annular sector with angle of 50 to 90°. Longitudinal side section is made rectilinear, which coincides with fuselage longitudinal axis. Tail section is made in the form of straight or sweep side support cantilever, which is articulated with fuselage body. Angular and lateral sections or only lateral section are used in takeoff, hovering and landing mode to create lifting reactive moments relative to center of gravity of aircraft.
EFFECT: invention is aimed at optimizing the shape of the wings.
1 cl, 22 dwg
