A Numerical Study of Volute Design in Centrifugal Compressor

Weilin Yang, P. Grant, J. Hitt
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Abstract

Our principle goal of this study is to develop a CFD based analysis procedure that could be used to analyze the geometric tradeoffs in scroll geometry when space is limited. In the study, a full centrifugal compressor stage at four different operating points from near surge to near choke is analyzed using Computational Fluid Dynamics (CFD) and laboratory measurement. The study concentrates on scroll performance and its interaction with a vaneless diffuser and impeller. The numerical results show good agreement with test data in scroll circumferential pressure distribution at different ΛAR, total pressure loss coefficient, and pressure distortion at the tongue. The CFD analysis also predicts a reasonable choke point of the stage. The numerical results provide overall flow field in the scroll and diffuser at different operating points. From examining the flow fields, one can have a much better understanding of rather complicated flow behavior such as jet-wake mixing, and choke. One can examine total pressure loss in detail to provide crucial direction for scroll design improvement in areas such as volute tongue, volute cross-section geometry and exit conical diffuser.
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离心压缩机蜗壳设计的数值研究
本研究的主要目标是开发一种基于CFD的分析程序,用于在空间有限的情况下分析涡旋几何的几何权衡。在研究中,利用计算流体动力学(CFD)和实验室测量分析了从近喘振到近节流四个不同工作点的全离心式压缩机级。研究的重点是涡旋性能及其与无叶扩压器和叶轮的相互作用。数值计算结果与试验数据吻合较好,包括不同ΛAR工况下涡旋周向压力分布、总压损失系数和舌部压力畸变。CFD分析还预测了一个合理的节流点。数值结果给出了涡旋和扩压器在不同工况下的整体流场。通过研究流场,人们可以更好地理解相当复杂的流动行为,如射流尾流混合和节流。可以详细检查总压力损失,为涡旋设计改进提供关键方向,如蜗壳舌、蜗壳横截面几何形状和出口锥形扩散器。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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