A study on impeller-diffuser interaction - Part II: Detailed flow analysis

被引:103
|
作者
Ziegler, KU [1 ]
Gallus, HE [1 ]
Niehuis, R [1 ]
机构
[1] Rhein Westfal TH Aachen, Inst Jet Prop & Turbomachinery, D-52062 Aachen, Germany
来源
关键词
Diffusers;
D O I
10.1115/1.1516815
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The interaction between impeller and diffuser is considered to have strong influence on the flow in centrifugal compressors. However, the knowledge about this influence is still. not satisfying. This two-part paper presents an experimental investigation of the effect of impeller-diffuser interaction on the unsteady and the time-averaged flow field in impeller and diffuser and the performance of these components. The flat wedge vaned diffuser of the investigated compressor allows an independent adjustment of diffuser vane angle and radial gap between impeller exit and diffuser vane inlet. Attention is mainly directed to the radial gap, as it determines the intensity of the impeller-diffuser interaction. In Part I it was shown that smaller radial gaps improve diffuser pressure recovery, whereas impeller efficiency is hardly affected. Part II focuses on the reasons for these effects. Measurements with a laser-2-focus velocimeter in the highly unsteady flow field between the impeller exit region and diffuser throat were performed at three different diffuser geometries allowing a detailed flow analysis. Especially the unsteady results show that for a smaller radial gap more impeller wake fluid is conveyed towards the highly loaded diffuser vane pressure side reducing its loading and leading to a better diffusion in the diffuser channel. Concerning the impeller flow, it was found that a smaller radial gap is leading to a noticeable reduction of the wake region at impeller exit. The experimental results are intended to be published as an open CFD test case under the name "Radiver."
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页码:183 / 192
页数:10
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