FIELD: mechanical engineering. SUBSTANCE: jet engine nozzles are positioned on arms of a rotor mounted in a casing and connected to feed branch pipes by inner channels made in the rotor, the branch pipes are connected to a working medium source through a distributing device. A reduction gear is connected to the output rotor shaft on one side and to the screw of a helical gear - on the other side. The gear nut is mounted for translational movement and is kinematically connected to a controllable object by a motion converter. The converter is made in the form of a rack gear positioned symmetrically relative to the longitudinal plane of symmetry of the helical gear. All nozzles of the engine point in one direction. All feed branch pipes are made on the side of the casing opposite to the reduction gear and are parted by an annular slot. An annular channel isolator made on the rotor coaxially to the output shaft is positioned in the slot. EFFECT: improved structure. 6 cl, 7 dwg
