The Design and Performance Analysis of a 15 g/mol Helium-Xenon Mixture Centrifugal Compressor

被引:0
作者
Zheng, Jinchao [1 ]
Tian, Zhitao [1 ]
Malik, Adil [2 ]
Xin, Jianchi [1 ]
Lu, Huawei [1 ]
机构
[1] Dalian Maritime Univ, Naval Architecture & Ocean Engn Coll, Dalian 116026, Peoples R China
[2] Natl Univ Sci & Technol, Pakistan Navy Engn Coll Karachi, Islamabad 44000, Pakistan
基金
中国国家自然科学基金;
关键词
closed Brayton cycle; centrifugal compressor; helium-xenon compressor; CYCLE GAS-TURBINE; BRAYTON CYCLE; BINARY-MIXTURES; POWER; REACTOR; UNIT;
D O I
10.3390/aerospace11110869
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
One of the primary parts of a closed Brayton cycle that uses a helium-xenon mixture as the working medium is a centrifugal compressor. Nowadays, there has been minimal research on the theoretical underpinnings and design procedures of a helium-xenon mixture centrifugal compressors, and the internal flow mechanisms remain poorly understood. In this study, we present a redesign of the 15 g/mol helium-xenon centrifugal compressor originally developed by Bruno M, utilizing a helium-xenon mixture as the working fluid to enhance compressor performance and facilitate an in-depth analysis of the internal flow dynamics. The findings indicate a significant expansion of the stable operating range of the redesigned compressor under identical outlet conditions, with a 33.27% increase in flow margin and substantial improvements in the pressure ratio. Furthermore, under consistent inlet conditions, at an operational flow rate of 0.8657 kg/s, the redesigned compressor exhibits a pressure ratio that is 2.11% greater than that of the original design, along with a variable efficiency increase of 1.1%.
引用
收藏
页数:20
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