AIRCRAFT ENGINE MULTI-STAGE AXIAL-FLOW COMPRESSOR Russian patent published in 2001 - IPC

Abstract RU 2165547 C2

FIELD: aircraft industry. SUBSTANCE: proposed multi-stage axial-flow compressor of aircraft engine has two or more stages mounted in tandem. Compressor has also device made to provide possibility of disconnection of one or more last stages. EFFECT: improved control of compressor. 5 dwg

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RU 2 165 547 C2

Authors

Belous Vladimir Iosifovich

Dates

2001-04-20—Published

1998-10-08—Filed