流体机械Issue(10)：52-56,51,6.DOI:10.3969/j.issn.1005-0329.2015.10.011
离心压缩机径向吸气室性能改进的数值研究
Numerical Research on the Performance Improvement of Radial Inlet for a Centrifugal Compressor
张义 1韩凤翚 1赵忖 1谭佳健2
作者信息
- 1. 西安交通大学，陕西西安 710049
- 2. 沈阳鼓风机集团股份有限公司，辽宁沈阳 110142
- 折叠
摘要
Abstract
Radial inlet as an important stationary component of centrifugal compressor gets more attention from the industry re-searchers.In this paper,numerical study has been carried out for a radial inlet of centrifugal compressor to improve its geometry and structure.The results show that,under the design condition,the structure modification improved the flow condition inside the radial inlet,significantly decreased the total pressure loss coefficient,and made the polytropic efficiency of the radial inlet increase by 5%.In addition,the uniformity of flow parameters at the outlet of the radial inlet has also been improved to some extent.关键词
离心压缩机/径向吸气室/性能改进/数值研究Key words
centrifugal compressor/radial inlet/performance improvement/numerical research分类
机械制造引用本文复制引用
张义,韩凤翚,赵忖,谭佳健..离心压缩机径向吸气室性能改进的数值研究[J].流体机械,2015,(10):52-56,51,6.
