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The Analysis of Flow Separation Loss of Impeller in Centrifugal Compressor under Variable Conditions

机译:可变条件下离心压缩机叶轮流动分离损耗分析

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In order to study the change condition of the influence on the centrifugal compressor blade field, we change the size of the centrifugal compressor inlet flow and the centrifugal compressor impeller rotational speed, using the realizable κ - ε ii equation model to do the steady numerical simulation for the full port of centrifugal compressor. Through calculation, we get different inlet flow and rotate speed of centrifugal compressor internal flow field distribution of relative velocity, at the same time using the concept of Degree of Separation Loss to analyze the separation loss within impeller passage. The results show that under the condition of variable working condition, the change of Angle of attack is the primary factor for the the impeller separation, and when the Angle of attack of the same time, the smaller the relative velocity, the greater the separation loss. Therefore in the process of actual production, in order to reduce the loss of separation, we should reduce the size of Angle of attack, appropriatly increase import flow or impeller rotational speed.
机译:为了研究在离心压缩机叶片场影响的改变条件,我们改变离心式压缩机的尺寸入口流动和离心式压缩机叶轮的旋转速度,使用可实现的κ - εII方程模型做稳定数值模拟用于离心式压缩机的全部端口。通过计算,我们使用分离损失的程度的概念来分析叶轮通道内的分离损失得到不同的入口流量和相对速度的离心式压缩机内部流场分布的转速,在同一时间。该结果表明,变工况的条件下,攻角的变化是主要的因素为叶轮分离,并且当同时迎角,该相对速度越小,更大的分离损失。因此,在实际生产过程中,为了减少分离的损失,我们应该减少攻角的大小,appropriatly增加进口流量或叶轮转速。

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