Reduction of Disk Friction Loss by Applying a Fin to the Back of a Centrifugal Impeller

Satoshi Maeda, Takeshi Sano, Kazuyoshi Miyagawa, Kento Sakai
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Abstract

It is well known that the ratio of disk friction loss of low specific speed pumps is large. When the specific speed is 100min-1, m3/min, m or less, the disk friction loss increases remarkably. In this study, focusing on the clearance flow from the diffuser outlet to the impeller outlet (This is called the outward flow) behind the centrifugal pump, a fin was installed on outer diameter side of the rotating wall on the back side of a centrifugal pump as a countermeasure, and the influence of changes in velocity distribution near the wall on disk friction loss was investigated by torque measurements, velocity measurement, and CFD analysis. As a result, it was clarified that disk friction loss is decreasing by installing the fin in both torque measurements and CFD results, because the clearance flow is separated by fin and circumferential velocity is increased in the wake region of the fin in both measurements and CFD. In addition, it was clarified that disk friction coefficient (normalized torque) can be expressed as a function of the inlet swirl ratio and Reynolds number. Also, prediction equation is derived for each shape (with and without fin). According to the equation, it was found that disk friction loss reduction effect by installing a fin becomes larger when Reynolds number and the inlet swirl ratio are small.
通过在离心叶轮背面安装鳍片减少盘摩擦损失
众所周知,低比转速泵的盘摩擦损失比很大。当比转速为 100min-1、m3/min、m 或更低时,盘摩擦损失显著增加。本研究针对离心泵后部从扩散器出口到叶轮出口的间隙流(称为外向流),在离心泵后部旋转壁外径侧安装了一个翅片作为对策,并通过扭矩测量、速度测量和 CFD 分析研究了壁附近速度分布的变化对盘摩擦损失的影响。结果表明,在扭矩测量和 CFD 结果中,安装鳍片后,盘摩擦损失均有所减少,这是因为在测量和 CFD 结果中,间隙流被鳍片隔开,鳍片尾流区的圆周速度增加。此外,还明确了盘摩擦系数(归一化扭矩)可表示为入口漩涡比和雷诺数的函数。此外,还推导出了每种形状(带翅片和不带翅片)的预测方程。根据该方程,可以发现当雷诺数和进气漩涡比很小时,安装翅片对减少盘摩擦损失的作用会更大。
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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