Airflow Bypass in Centrifugal Compressor and Operational Stability
- 作者: Lazarev E.A.1, Mashkov O.G.2, Martynov A.A.2, Pomaz A.N.2
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隶属关系:
- South Ural State University
- AO SKB Turbina
- 期: 卷 38, 编号 11 (2018)
- 页面: 840-843
- 栏目: Article
- URL: https://journals.rcsi.science/1068-798X/article/view/227557
- DOI: https://doi.org/10.3103/S1068798X18110072
- ID: 227557
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详细
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.
作者简介
E. Lazarev
South Ural State University
编辑信件的主要联系方式.
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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