Airflow Bypass in Centrifugal Compressor and Operational Stability


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Abstract

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.

About the authors

E. A. Lazarev

South Ural State University

Author for correspondence.
Email: lea2@mail.ru
Russian Federation, Chelyabinsk

O. G. Mashkov

AO SKB Turbina

Email: lea2@mail.ru
Russian Federation, Chelyabinsk

A. A. Martynov

AO SKB Turbina

Email: lea2@mail.ru
Russian Federation, Chelyabinsk

A. N. Pomaz

AO SKB Turbina

Email: lea2@mail.ru
Russian Federation, Chelyabinsk

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