INTERMITTENT-CYCLE GAS TURBINE ENGINE (IGTE) Russian patent published in 2013 - IPC F02C5/12 

FIELD: engines and pumps.

SUBSTANCE: gas turbine engine with intermittent operation of combustion chambers includes a housing, combustion chambers, a rotor, a turbine with blades, a centrifugal compressor, and power supply and ignition systems. Combustion chambers are uniformly located in the engine housing in circumferential direction so that they can be divided by five, with inlet and outlet openings above them, which are adjacent to the end face of the rotor disc. Alternating projections and cavities, in which the turbine blades are fixed, are symmetrically made on the rotor disc, at least on one fourth of the circle. Opposite inlet openings of combustion chambers, the rotor disc has two diametrically located blowdown openings interconnected with a centrifugal compressor adjacent on the opposite side of the rotor disc. Outlet branch pipes are uniformly adjacent on the opposite side of the rotor disc, opposite outlet openings of combustion chambers. The ignition plug is installed in one of the combustion chambers, which is interconnected by means of a channel with the combustion chamber that is adjacent in the rotation direction.

EFFECT: improving the power of the engine and simplifying its design.

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