DOUBLE-ROW GAS TURBINE ENGINE Russian patent published in 2018 - IPC F02C5/02 F02C5/12 

Abstract RU 2673838 C2

FIELD: motors and pumps.

SUBSTANCE: gas turbine engine with the pulsating operation of the combustion chambers contains pairs of combustion chambers, a shaft, a turbine rotor and a compressor, a cooling system, a combustion chamber disk. Disc of the combustion chambers is made with a pair of inlet and outlet windows and is adjacent to the turbine rotor. Rotor of the turbine has blades alternating with blind projections, as well as a scouring window. On the opposite side of the disk to the rotor there are exhaust pipes.

EFFECT: invention is aimed at creating a powerful and reliable engine with low weight and dimensions.

1 cl, 1 dwg

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RU 2 673 838 C2

Authors

Bakhirev Viktor Serafimovich

Dates

2018-11-30Published

2017-03-28Filed