王晓放

个人信息Personal Information

教授

博士生导师

硕士生导师

任职 : 现任中国工程热物理学会流体机械专委员会委员、中国航空学会学轻型燃气轮机分会委员、教育部重型燃气轮机教学资源库专家委员会委员、辽宁省能动类专业教指委副主任、大连市核事故应急指挥部专家组成员等职。

性别:女

毕业院校:大连理工大学

学位:硕士

所在单位:能源与动力学院

电子邮箱:dlwxf@dlut.edu.cn

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Effects of Difference Leading Edge Shapes on Numerical Simulation of Centrifugal Compressor

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论文类型:会议论文

发表时间:2011-12-01

收录刊物:EI、CPCI-S、Scopus

卷号:455-456

页面范围:351-355

关键字:Centrifugal compressor; impeller; Leading edge; stree; numerical simulation; Von Mises

摘要:In order to research the effects of leading edge shapes on the strength of centrifugal compressor compeller, the shrouded impellers of a large centrifugal compressor were introduced for finite element analysis. In the present study, the geometric models of 3 shrouded impellers were established in Solidworks 2007, and then numerical simulations were carried out using ANSYS. Through visualization of the computational result of the impellers with a square leading edge, a semi-circular leading edge and a elliptical leading edge, it was clarified by comparison that different leading edge shapes had significant influences on the compressor strength. According to the charts of the Von Mises stress versus leading edge shapes, it was indicated that approximately a 27% drop and a 32% drop in maximum Von Mises stress value occurred in the shrouded impellers of a semi-circular leading edge and a elliptical leading edge compared to a square leading edge respectively. That is, the semi-circular leading edge or elliptical leading edge employed in a centrifugal compressor would dramatically improve structural strength. This paper aims to provide the reference significance the structural optimization and reliability improvement of a large flow centrifugal compressor.