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Experimental study on the impact of intake methods on the performance and flow field of centrifugal compressors
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Zongwu HU1, 2, Ning HUANG1, Yang ZHAO3, Jie ZHANG1, Guanyan CHEN1
Fluid Machinery | 2025, 53(7) : 22 - 29
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Fluid Machinery | 2025, 53(7): 22-29
Experimental study on the impact of intake methods on the performance and flow field of centrifugal compressors
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Zongwu HU1, 2, Ning HUANG1, Yang ZHAO3, Jie ZHANG1, Guanyan CHEN1
Affiliations
  • 1School of Civil Engineering and Mechanics,Lanzhou University,Lanzhou 730000,China
  • 2School of Petrochemical Engineering,Lanzhou University of Technology,Lanzhou 730050,China
  • 3China North Engine Research Institute,Tianjin 300400,China
Published: 2025-07-30 doi: 10.3969/j.issn.1005-0329.2025.07.004
Outline
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To investigate the impact of intake configuration on the performance and flow field of a centrifugal compressor,characteristic tests were conducted to measure performance,while PDA and PIV techniques were employed to characterize the inlet‑duct flow.The effects of curved‑duct intake on the compressor′s pressure ratio,efficiency and inlet uniformity were analyzed.The results reveal how a 90° elbow affects both performance and flow behavior.Compared with a straight inlet,the elbow reduces the pressure ratio(-0.8 % to -2.7 %) and efficiency(-1.4% to -9.8%) at the maximum efficiency point across the tested speed range(60 000~100 000 r/min),and the deterioration grows as rotational speed increases.Especially under high‑flow conditons,the decline in pressure ratio and efficiency is more pronounced.When the speed exceeds 70 000 r/min,the circumferential static‑pressure non‑uniformity at the compressor inlet becomes pronounced;The maximum static‑pressure ratio at the 120° location rises from 1.002 8 to 1.011 5.With a straight inlet,the flow at the maximum efficiency point is nearly uniform,whereas the bent inlet generates severe inlet distortion:two counter‑rotating vortex cores appear on the radial section.The research results provide a theoretical basis for optimizing the inlet conditions of centrifugal compressors and improving their actual operating efficiency and stability in the future.

centrifugal compressor  /  intake method  /  rotational speeds  /  performance  /  flow field
胡宗武, 黄宁, 赵洋, 张洁, 陈冠言. 进气方式对离心压气机性能及流场影响的试验研究. 流体机械, 2025 , 53 (7) : 22 -29 . DOI: 10.3969/j.issn.1005-0329.2025.07.004
Zongwu HU, Ning HUANG, Yang ZHAO, Jie ZHANG, Guanyan CHEN. Experimental study on the impact of intake methods on the performance and flow field of centrifugal compressors[J]. Fluid Machinery, 2025 , 53 (7) : 22 -29 . DOI: 10.3969/j.issn.1005-0329.2025.07.004
Year 2025 volume 53 Issue 7
83
33
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Article Info
doi: 10.3969/j.issn.1005-0329.2025.07.004
  • Receive Date:2024-11-25
  • Online Date:2026-10-20
  • Published:2025-07-30
Article Data
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History
  • Received:2024-11-25
  • Revised:2025-03-27
Affiliations
    1School of Civil Engineering and Mechanics,Lanzhou University,Lanzhou 730000,China
    2School of Petrochemical Engineering,Lanzhou University of Technology,Lanzhou 730050,China
    3China 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
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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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