Airflow Bypass in Centrifugal Compressor and Operational Stability


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The influence of the airflow bypass at the impeller input on the operational stability of a compressor is considered. The bypass structure is discussed, and a new chamber design is proposed for a compressor with diffuser blades. Numerical analysis of the flow structure is conducted. The compressor’s margin of operational stability is assessed experimentally for bypass chambers of different geometry.

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E. Lazarev

South Ural State University

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Email: lea2@mail.ru
俄罗斯联邦, Chelyabinsk

O. Mashkov

AO SKB Turbina

Email: lea2@mail.ru
俄罗斯联邦, Chelyabinsk

A. Martynov

AO SKB Turbina

Email: lea2@mail.ru
俄罗斯联邦, Chelyabinsk

A. Pomaz

AO SKB Turbina

Email: lea2@mail.ru
俄罗斯联邦, Chelyabinsk

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