METHOD OF CIRCULATING AIR IN TURBINE COMPRESSOR, COMPRESSOR EXPLOITING THIS METHOD, COMPRESSOR STAGE OF AFORESAID DESIGN AND AIRCRAFT ENGINE INCORPORATING SAID COMPRESSOR Russian patent published in 2009 - IPC F04D27/02 F04D29/32 F04D29/38 

Abstract RU 2370674 C2

FIELD: engines.

SUBSTANCE: compressor comprises several stage, fixed and rotary wheels. To eliminate parasitic air flows inside the compressor, it incorporates outer and inner casings to form gas-air duct made up of outer and inner ducts. Proposed method comprises sucking in air in inner duct and directing it onto fixed wheel fixed vane. It comprises also bleeding air from aforesaid fixed vane and directing it outside the compressor.

EFFECT: higher compression ratio.

47 cl, 9 dwg

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RU 2 370 674 C2

Authors

Lardell'E Alen

Dates

2009-10-20Published

2005-09-29Filed