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个人信息Personal Information
教授
博士生导师
硕士生导师
任职 : 现任中国工程热物理学会流体机械专委员会委员、中国航空学会学轻型燃气轮机分会委员、教育部重型燃气轮机教学资源库专家委员会委员、辽宁省能动类专业教指委副主任、大连市核事故应急指挥部专家组成员等职。
性别:女
毕业院校:大连理工大学
学位:硕士
所在单位:能源与动力学院
电子邮箱:dlwxf@dlut.edu.cn
Investigation on One-Dimensional Loss Models for Predicting Performance of Multistage Centrifugal Compressors in Supercritical CO(2)Brayton Cycle
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论文类型:期刊论文
发表时间:2021-03-05
发表刊物:JOURNAL OF THERMAL SCIENCE
卷号:30
期号:1
页面范围:133-148
ISSN号:1003-2169
关键字:supercritical carbon dioxide Brayton cycle; centrifugal compressor; one-dimensional performance analysis; loss model; three-dimensional CFD simulation
摘要:The main compressor in a supercritical carbon dioxide (SCO2) Brayton cycle works near the critical point where the physical properties of CO(2)are far away from the ideal gas. To investigate the effectiveness of the conventional one-dimensional (1D) loss models for predicting the performance of compressors working in such nontraditional conditions, detailed comparisons of 1D predicted performance, experimental data and threedimensional CFD results are made. A 1D analysis method with enthalpy and total pressure based loss system is developed for multistage SCO(2)centrifugal compressors, and it is firstly validated against the experimental results of a single stage SCO(2)centrifugal compressor from the Sandia National Laboratory. A good agreement of pressure ratios with experiments can be achieved by the 1D method. But the efficiency deviations reveal the potential deficiencies of the parasitic loss models. On the basis of the validation, a two-stage SCO(2)centrifugal compressor is employed to do the evaluation. Three-dimensional CFD simulations are performed. Detailed comparisons are made between the CFD and the 1D results at different stations located in the compressor. The features of the deviations are analyzed in detail, as well as the reasons that might cause these deviations.