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Flow calculation method of supercritical carbon dioxide centrifugal compressor based on streamline curvature method
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Yi RONG1, Kailong LIAO2, Enhui SUN2, Lizhi WANG1
Thermal Power Generation | 2024, 53(2) : 124 - 132
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Thermal Power Generation | 2024, 53(2): 124-132
Thermal energy science research
Flow calculation method of supercritical carbon dioxide centrifugal compressor based on streamline curvature method
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Yi RONG1, Kailong LIAO2, Enhui SUN2, Lizhi WANG1
Affiliations
  • 1.Yangzhou Collaborative Innovation Research Institute of Shenyang Aircraft Design and Research Institute Co., Ltd., Yangzhou 225111, China
  • 2.Beijing Key Laboratory of Multiphase Flow and Heat Transfer for Low Grade Energy Utilization (North China Electric Power University), Beijing 102206, China
Published: 2024-02-25 doi: 10.19666/j.rlfd.202307140
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The real gas characteristics of supercritical carbon dioxide (S-CO2) make it difficult to obtain stable convergence results in three-dimensional numerical simulation of S-CO2 centrifugal compressor, and the time cost of numerical calculation further increases the difficulty of compressor design optimization. To establish a flow calculation method suitable for S-CO2 centrifugal compressor, three-dimensional numerical simulation is carried out on the compressor to obtain the flow field information and corresponding loss distribution. Then, the one-dimensional loss model is superimposed in the conventional flow line curvature method, and the CO2 compression factor is calculated in segments along the flow line, thus to reflect the real gas compression process. Comparison between the calculation results and the three-dimensional numerical simulation results shows that, the distribution of meridian relative velocity field and enthalpy obtained by streamline curvature method are consistent with the computational Fluid dynamics (CFD) results. The temperature and pressure data at the blade outlet are close to the CFD results, with errors of 0.23% and 1.08%, respectively, and a difference of 1.5% in total static isentropic efficiency. The results indicate that the performance parameters of S-CO2 centrifugal compressor impeller can be obtained quickly and accurately by using streamline curvature method.

centrifugal compressor  /  streamline curvature method  /  loss model  /  performance prediction
Yi RONG, Kailong LIAO, Enhui SUN, Lizhi WANG. Flow calculation method of supercritical carbon dioxide centrifugal compressor based on streamline curvature method[J]. Thermal Power Generation, 2024 , 53 (2) : 124 -132 . DOI: 10.19666/j.rlfd.202307140
  • National Natural Science Foundation of China(52206010)
Year 2024 volume 53 Issue 2
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Article Info
doi: 10.19666/j.rlfd.202307140
  • Receive Date:2023-07-25
  • Online Date:2025-12-31
  • Published:2024-02-25
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  • Received:2023-07-25
Funding
National Natural Science Foundation of China(52206010)
Affiliations
    1.Yangzhou Collaborative Innovation Research Institute of Shenyang Aircraft Design and Research Institute Co., Ltd., Yangzhou 225111, China
    2.Beijing Key Laboratory of Multiphase Flow and Heat Transfer for Low Grade Energy Utilization (North China Electric Power University), Beijing 102206, China
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https://castjournals.cast.org.cn/joweb/rlfd/EN/10.19666/j.rlfd.202307140
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
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Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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