TURBOJET ENGINE Russian patent published in 1997 - IPC

Abstract RU 2088781 C1

FIELD: aeronautical engineering. SUBSTANCE: turbojet engine includes combustion chamber arranged in gas duct and nozzle and gas turbine with rotor and blades arranged in diffuser. Engine is also provided with cylindrical rods secured on turbine rotor before combustion chamber located in confuser of gas duct. Number of cylindrical rods is equal to number of blades of last stage of compressor and their diameter is equal to maximum thickness of blade. EFFECT: enhanced reliability. 3 cl, 3 dwg

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RU 2 088 781 C1

Authors

Chudikov N.N.

Dates

1997-08-27—Published

1991-12-05—Filed