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Multi-component and multi-objective coupling optimization of turbocharger centrifugal compressor
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Rui Wang1, Zhengxian Liu1, Xiaojian Li1, Ye Liu2
Transactions of CSICE | 2025, 43(2) : 173 - 182
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收藏切换
Transactions of CSICE | 2025, 43(2): 173-182
Multi-component and multi-objective coupling optimization of turbocharger centrifugal compressor
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Rui Wang1, Zhengxian Liu1, Xiaojian Li1, Ye Liu2
Affiliations
  • 1.School of Mechanical Engineering,Tianjin University,Tianjin 300350,China
  • 2.China North Engine Research Institute,Tianjin 300400,China
Published: 2025-03-25 doi: 10.16236/j.cnki.nrjxb.202502021
Outline
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Casing treatment improves the flow stability of turbocharger centrifugal compressors,but often leads to additional aerodynamic losses. Based on the optimal Latin hypercube sampling,radial basis function(RBF) neural network and gradient mutation hybrid optimization algorithm,a coupling optimization of the impeller and the casing treatment for a turbocharger centrifugal compressor was implemented by taking the efficiencies of the large-flow-rate condition,the design condition and the near-stall condition as the optimization objectives. Results show that the efficiencies of the large-flow-rate condition,the design condition and the near-stall condition are increased by 3.90%,3.02% and 1.10%,and the pressure ratios are improved by 9.28%,6.38% and 4.49%,respectively. The choke flow rate is increased by 1.13%,and the stable operating range is expanded by 0.83%. Compared with the solid casing compressor,the efficiencies of the design condition and the large-flow-rate condition are improved by 1.70% and 0.68%,respectively. The coupling optimization realizes the improvements of aerodynamic performances of the compressor in all operating conditions,and solves the problem of the traditional optimization that the aerodynamic performances of the design condition or the large-flow-rate condition decrease after introducing the casing treatment. By combining the global sensitivity analysis of the design space and the comparative analyses of the flow fields before and after optimization,the mechanisms of stability and efficiency improvements of the centrifugal compressor are obtained.

centrifugal compressor  /  casing treatment  /  coupling optimization  /  sensitivity analysis  /  mechanisms of stability and efficiency improvements
王睿, 刘正先, 李孝检, 刘烨. 增压器离心压气机多部件多目标耦合优化. 内燃机学报, 2025 , 43 (2) : 173 -182 . DOI: 10.16236/j.cnki.nrjxb.202502021
Rui Wang, Zhengxian Liu, Xiaojian Li, Ye Liu. Multi-component and multi-objective coupling optimization of turbocharger centrifugal compressor[J]. Transactions of CSICE, 2025 , 43 (2) : 173 -182 . DOI: 10.16236/j.cnki.nrjxb.202502021
Year 2025 volume 43 Issue 2
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3
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Article Info
doi: 10.16236/j.cnki.nrjxb.202502021
  • Receive Date:2024-03-15
  • Online Date:2026-11-06
  • Published:2025-03-25
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  • Received:2024-03-15
  • Revised:2024-07-02
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    1.School of Mechanical Engineering,Tianjin University,Tianjin 300350,China
    2.China North Engine Research Institute,Tianjin 300400,China
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表12种不同金属材料的力学参数
科
Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)
属
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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