FIELD: engine building.
SUBSTANCE: invention relates to structures of power reactive plants, which operate as LPFD or PVSTDD, create changing directions of front gas thrusts and provide work onboard electromagnetic generators of electric currents, and also, as a liquid-propellant engine, create rear gas drafts. Universal jet turbine engine comprises a housing, a combustion chamber, rotary dampers, a gas rudder, as well as a turbine transverse-wings wheel, which provides operation of onboard electromagnetic generator. Combustion chamber is equipped with fuel and fuel-oxidizing nozzles, ignition plug, which enable operation of the device in air and in vacuum media.
EFFECT: invention makes it possible to create rear gas thrust and to generate torque by changing direction of front gas draft, and also reduces wear of semi-shafts and side wall of direct-flow combustion chamber.
1 cl, 2 dwg
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