| 摘要 |
FIELD: aviation. ^ SUBSTANCE: invention relates to aviation, namely to flight vehicles with cruising subsonic speeds. The proposed flight vehicle comprises fuselage with a flat lower surface representing a wing, flat parallel sides, wings with flaps, engines, two fins each arranged in the side plane, interconnected by tailplane. The fuselage features streamline shape in horizontal plane. The fuselage top represents a classical wing load-carrying part extending all along the vehicle length. The engines are mounted atop of the nose part and are distributed over the fuselage entire width. The walls extend above the parallel sides shaping the fuselage into a guide chute. ^ EFFECT: invention allows significantly increase many vehicle lifting efficiencies, its VTOL, increase control reliability. ^ 2 cl, 4 dwg |
