FIELD: aviation.
SUBSTANCE: invention relates to the structure of vertical takeoff and landing aircraft (VTOL). VTOL comprises a fuselage, and a high-wing. Between the left and right wing panels, the gas distribution chamber is placed. Over the chamber, bypass turbojet engines are installed, with exhaust channels at outlet. Inside channels, valves are installed, allowing to redirect the gas mixture flow from the engine or to create a marching VTOL thrust, or for injection into the distribution chamber. On the upper wings surface, slotted nozzles are made, to which the gas-air mixture is supplied for working motors. At the rear wing edge, a flap is installed that has the ability to rise and fall. Under the flap, blinds are installed, which, when the flap is lowered into a horizontal position, while in the raised position, the flap is upright. Shutters being upright are able to deviate within a few degrees. From the gas-distributing chamber, the gas air mixture through a channel is also fed to the longitudinal stability wheel.
EFFECT: improved handling and maneuverability in the takeoff and landing modes, aerodynamic qualities in the horizontal flight mode.
3 cl, 7 dwg
