GAS TURBINE ENGINE COMPRESSOR Russian patent published in 2011 - IPC F04D29/60 

Abstract RU 2430276 C1

FIELD: engines and pumps.

SUBSTANCE: proposed compressor comprises stator 1 with bosses 2 with bores to receive journals 4 of vane box vanes 14. The are arranged in said bores of bosses 2 by means of housings of 3 of journals 4 either fixed or turning relative to axis of bosses 2 by means of moving elements to allow dismantling without disassembly of compressor stator 1.

EFFECT: increased reparability.

5 dwg

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RU 2 430 276 C1

Authors

Krjuchkov Jurij Aleksandrovich

Dates

2011-09-27Published

2010-04-21Filed