Airflow Bypass in Centrifugal Compressor and Operational Stability
- Authors: Lazarev E.A.1, Mashkov O.G.2, Martynov A.A.2, Pomaz A.N.2
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Affiliations:
- South Ural State University
- AO SKB Turbina
- Issue: Vol 38, No 11 (2018)
- Pages: 840-843
- Section: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/227557
- DOI: https://doi.org/10.3103/S1068798X18110072
- ID: 227557
Cite item
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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