Airflow Bypass in Centrifugal Compressor and Operational Stability
- Авторлар: Lazarev E.A.1, Mashkov O.G.2, Martynov A.A.2, Pomaz A.N.2
-
Мекемелер:
- South Ural State University
- AO SKB Turbina
- Шығарылым: Том 38, № 11 (2018)
- Беттер: 840-843
- Бөлім: Article
- URL: https://journals.rcsi.science/1068-798X/article/view/227557
- DOI: https://doi.org/10.3103/S1068798X18110072
- ID: 227557
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
E. Lazarev
South Ural State University
Хат алмасуға жауапты Автор.
Email: lea2@mail.ru
Ресей, Chelyabinsk
O. Mashkov
AO SKB Turbina
Email: lea2@mail.ru
Ресей, Chelyabinsk
A. Martynov
AO SKB Turbina
Email: lea2@mail.ru
Ресей, Chelyabinsk
A. Pomaz
AO SKB Turbina
Email: lea2@mail.ru
Ресей, Chelyabinsk
Қосымша файлдар
