Investigation of self-recirculating casing treatment with preswirl blowing for centrifugal compressor
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Investigation of self-recirculating casing treatment with preswirl blowing for centrifugal compressor
Vol. 27, Issue 6, (2012)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 中国科学院 工程热物理研究所 轻型动力重点实验室,北京,100190
3. 中国航空工业集团公司 中国航空动力机械研究所,湖南,株洲,412002
作者简介:
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Published:2012
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KANG Jian-xiong, DU Qiang, HUANG Guo-ping, et al. Investigation of self-recirculating casing treatment with preswirl blowing for centrifugal compressor[J]. 2012, 27(6).
DOI:
KANG Jian-xiong, DU Qiang, HUANG Guo-ping, et al. Investigation of self-recirculating casing treatment with preswirl blowing for centrifugal compressor[J]. 2012, 27(6).DOI:
Investigation of self-recirculating casing treatment with preswirl blowing for centrifugal compressor
Numerical and experimental investigations have been conducted on a self-recirculating casing treatment for a centrifugal compressor.Stall margin improved due to redirecting the low-momentum fluid to increase the mass flow in the impeller passage and decreasing the positive attack angle in the tip region with preswirl blowing.Based on the working mechanism
parametric studies were conducted to design the casing treatment geometry.It was found that the angle of the grooves
the position and the length of overlap were three key parameters for the “best casing configuration” in terms of larger stall margin improvement and smaller lowering of efficiency according to the given range of rotating speeds.The effectiveness of this casing treatment was verified by the single stage centrifugal compressor experiments
and it was observed that the stall margin and efficiency can be improved simultaneously at lower rotating speed.