Effects of Near-Critical Condensation and Cavitation on the Performance of S-CO2 Compressor

被引:3
作者
Xie, Wenlin [1 ,2 ]
Tian, Yong [1 ,2 ]
Jiang, Peng [1 ]
Wang, Bo [1 ,2 ]
Xu, Xiang [1 ,2 ]
机构
[1] Chinese Acad Sci, Inst Engn Thermophys, Key Lab Adv Energy & Power, 11 Beisihuanxi Rd, Beijing 100190, Peoples R China
[2] Univ Chinese Acad Sci, 19 A Yuquan Rd, Beijing 100049, Peoples R China
基金
美国国家科学基金会;
关键词
S-CO2; centrifugal compressor; condensation; cavitation; CYCLE;
D O I
10.3390/en17040854
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
The supercritical carbon dioxide (S-CO2) Brayton cycle efficiency increases as the compressor inlet condition approaches the critical point. However, the thermodynamic properties of CO2 vary dramatically near the critical point, and phase change is most likely to happen. Both cavitation and condensation bring about significant adverse effects on the performance of compressors. In this paper, the quantitative effects of nonequilibrium condensation and cavitation on the performance of an S-CO2 centrifugal compressor with different inlet-relative entropy values are investigated. The properties of CO2 were provided by the real-gas property table, and the nonequilibrium phase-change model was adopted. The numerical simulation method with the nonequilibrium phase-change model was validated in the Lettieri nozzle and Sandia compressor. Furthermore, simulations were carried out in a two-stage centrifugal compressor under conditions of various inlet-relative entropy values. The type of nonequilibrium phase change can be distinguished by inlet-relative entropy. Cavitation makes the choke mass flow rate decrease due to the drop in the speed of sound. Condensation mainly occurs on the leading edge of the main blade at a large mass flow rate, but cavitation occurs on the splitter. The condensation is more evenly distributed on the main blade, but the cavitation is mainly centered on the leading edge.
引用
收藏
页数:18
相关论文
共 25 条
[1]  
Allison T.C., 2019, P ASME TURBO EXPO TU
[2]  
Anderson M.R., 2018, P 6 INT SUPERCRITICA
[3]  
[Anonymous], 2022, ANSYS Fluent Theory Guide
[4]   An Investigation of Real Gas Effects in Supercritical CO2 Centrifugal Compressors [J].
Baltadjiev, Nikola D. ;
Lettieri, Claudio ;
Spakovszky, Zoltan S. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2015, 137 (09)
[5]  
Brinckman KW, 2019, PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 9
[6]   Global parameter optimization and criterion formula of supercritical carbon dioxide Brayton cycle with recompression [J].
Cheng, Wen-Long ;
Huang, Wen-Xu ;
Nian, Yong-Le .
ENERGY CONVERSION AND MANAGEMENT, 2017, 150 :669-677
[7]   Preliminary experimental study of a supercritical CO2 power cycle test loop with a high-speed turbo-generator using R134a under similarity conditions [J].
Cho, Junhyun ;
Shin, Hyungki ;
Cho, Jongjae ;
Kang, Young-Seok ;
Ra, Ho-Sang ;
Roh, Chulwoo ;
Lee, Beomjoon ;
Lee, Gilbong ;
Kim, Byunghui ;
Baik, Young-Jin .
FRONTIERS IN ENERGY, 2017, 11 (04) :452-460
[8]  
Conboy T.M., 2011, Experimental Investigation of the S-CO>2 Condensing Cycle
[9]  
Dostal V., 2004, Ph.D. thesis
[10]  
Feher E. G., 1968, Energy Conversion, V8, P85, DOI 10.1016/0013-7480(68)90105-8