Effects of Variable Diffuser Vanes on Performance of a Centrifugal Compressor with Pressure Ratio of 8.0

被引:36
|
作者
Ebrahimi, Mohsen [1 ]
Huang, Qiangqiang [1 ]
He, Xiao [1 ]
Zheng, Xinqian [1 ]
机构
[1] Tsinghua Univ, Turbomachinery Lab, State Key Lab Automot Safety & Energy, Beijing 100084, Peoples R China
来源
ENERGIES | 2017年 / 10卷 / 05期
基金
中国国家自然科学基金;
关键词
centrifugal compressor; gas turbine; turbocharger; variable geometry; diffuser; high pressure ratio; diffuser impeller interaction; incidence angle; matching; IMPELLER;
D O I
10.3390/en10050682
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
In numerous applications, centrifugal compressors are required to provide a high pressure ratio with good efficiency while also working in a wide operating range. This is a challenge because as pressure ratio increases, efficiency and operating range inevitably decline. This paper studies the effects of a variable geometry diffuser on the performance and operating range of a centrifugal compressor with high pressure ratios of up to 8.0. The numerical method employed three-dimensional Reynolds-averaged Navier-Stokes simulations. An analysis of the matching of the vaned diffuser with the impeller for different working conditions and diffuser vane angles is presented. The results show that improved matching of the adjusted diffuser increased efficiency by 4.5%. The range extension mechanism of the variable diffuser is explained, and it is shown that adjusting the vane angle by +6 degrees to 6 degrees extended the operating range of the compressor by up to 30.0% for pressure ratios between 5.0 and 6.0. The interaction between diffuser and impeller was examined, and the independent characteristic of the impeller is illustrated. The connection between the incidence angle at the leading edge of the impeller and flow separation near the tip of the impeller is discussed.
引用
收藏
页数:15
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