离心涡轮通风机设计程序的开发与应用研究

Kim Jang Kweon, Seok-Hyung Oh
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引用次数: 1

摘要

本文介绍了离心涡轮通风机的设计方法及设计程序的开发过程。通过实验性能数据验证了设计方案的适用性。在这里,我们提出了新的速度系数,并考虑了各种损失,如叶轮进口损失、叶片通道流动损失、机匣压力损失、再循环损失功率和圆盘摩擦损失功率。特别是根据实验结果,重新确定了叶轮的进出口宽度。因此,无论叶轮类型如何,该风机设计程序都显示出良好的性能结果,有望成为一个非常有用的设计工具。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Study on the Development and Application of a Design Program for Centrifugal Turbo Fan
: This paper introduces the design method of the centrifugal turbo fan and the process of developing the design program of it. The developed design program confirmed the applicability by experimental performance data. Here, we proposed new velocity coefficients and considered various losses such as impeller inlet loss, vane passage flow loss, casing pressure loss, recirculation loss power, and disk friction loss power. Especially, the inlet and outlet widths of the impeller were newly determined by reflecting the experimental results. As a result, this fan design program shows a good performance result regardless of the types of impeller and is expected to be a very useful design tool.
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