MULTIPASS GAS-TURBINE JET ENGINE Russian patent published in 1997 - IPC

Abstract RU 2079688 C1

FIELD: aero-engine manufacture. SUBSTANCE: fan air duct of engine is provided with additional compressor connected with shaft of fan by means of hydraulically controlled clutch. Gas turbine is connected with shaft of fan by means of overrunning clutch. EFFECT: enhanced efficiency. 5 dwg

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RU 2 079 688 C1

Authors

Platonov Nikolaj Vasil'Evich

Dates

1997-05-20Published

1994-04-25Filed