FIELD: transport.
SUBSTANCE: invention relates to VTOL aircraft. The airborne vehicle contains frame of axially symmetric shape, fuel tank, instrument compartment, gas-turbine engine including compressor, combustion chamber, turbine, adjustable guide vein including nozzle blades installed with possibility to be rotated, and jet nozzle. Gas-turbine engine is installed along vertical axis of frame. Combustion chamber is made multisectional with fuel systems including fuel governors for each section. Each nozzle blade is equipped with drive. Number of nozzle blades is equal to number of combustion chamber sections. Nozzle blades are fitted between sections of combustion chamber. Compressor is made centrifugal with axial inlet and axial outlet. Fuel tank is installed inside the gas-turbine engine. Emergency landing engine is installed inside the jet nozzle.
EFFECT: higher maneuverability of airborne vehicle.
5 cl, 4 dwg
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