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Effect of groove structures on the performance of liquid‑sealing impeller of liquid oxygen turbopump
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Lei ZHONG1, Kaifu XU2, Kai WANG1, Le XIANG2, Denghao WU3, Xiaohui WANG4
Fluid Machinery | 2025, 53(7) : 69 - 78
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Fluid Machinery | 2025, 53(7): 69-78
Effect of groove structures on the performance of liquid‑sealing impeller of liquid oxygen turbopump
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Lei ZHONG1, Kaifu XU2, Kai WANG1, Le XIANG2, Denghao WU3, Xiaohui WANG4
Affiliations
  • 1Research Center of Fluid Machinery Engineering and Technology,Jiangsu University,Zhenjiang 212013,China
  • 2Xi'an Aerospace Propulsion Institute,Xi'an 710199,China
  • 3College of Metrology Measurement and Instrument,China Jiliang University,Hangzhou 310018,China
  • 4School of Energy and Power Engineering,Lanzhou University of Technology,Lanzhou 730050,China
Published: 2025-07-30 doi: 10.3969/j.issn.1005-0329.2025.07.010
Outline
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In order to enhance the gas‑liquid interface stability and cryogenic cavitation characteristics of the liquid‑sealing impeller,the effects of different groove structures on the sealing performance and cryogenic cavitation characteristics of the first‑stage liquid‑sealing impeller of the liquid oxygen turbopump were numerically analyzed.The results show that the sealing performance of the liquid‑sealing impeller is jointly influenced by the groove/blade structure,fluid flow guidance design(radial/backward‑leaning/backward‑bending),and configuration(blade‑type/flow passage‑type).Radial blade structure demonstrates outstanding advantages in achieving low leakage and lower temperature rise,making them the preferred choice for most operating conditions.Compared to the radial flow channel structure,the radial blade structure reduces leakage by 96.3%,shaft power increases by 14.8%,and sealing power ratio reduces by 2%.Backward‑leaning/ backward‑bending structure significantly enhance gas‑liquid interface stability by optimizing flow guidance,serving as the primary option for prioritizing stability.A backflow vortex is formed in the outer clearance of the groove on the outer diameter side of backward‑leaning/ backward‑bending structure,which increases the shaft power by about 14.8% and 25.0% respectively compared to the radial flow channel structure.Flow channel structure(especially backward‑leaning) can be considered as alternative solutions under high‑speed conditions.The research results can provide a reference for the design of liquid‑sealing impeller of liquid oxygen turbopump.

liquid‑sealing impeller  /  liquid oxygen turbopump  /  groove structure  /  sealing performance  /  cryogenic cavitation characteristics
钟磊, 许开富, 王凯, 项乐, 吴登昊, 王晓晖. 槽型结构对液氧涡轮泵液封轮性能的影响. 流体机械, 2025 , 53 (7) : 69 -78 . DOI: 10.3969/j.issn.1005-0329.2025.07.010
Lei ZHONG, Kaifu XU, Kai WANG, Le XIANG, Denghao WU, Xiaohui WANG. Effect of groove structures on the performance of liquid‑sealing impeller of liquid oxygen turbopump[J]. Fluid Machinery, 2025 , 53 (7) : 69 -78 . DOI: 10.3969/j.issn.1005-0329.2025.07.010
Year 2025 volume 53 Issue 7
52
14
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Article Info
doi: 10.3969/j.issn.1005-0329.2025.07.010
  • Receive Date:2024-10-14
  • Online Date:2026-10-20
  • Published:2025-07-30
Article Data
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History
  • Received:2024-10-14
  • Revised:2025-05-11
Affiliations
    1Research Center of Fluid Machinery Engineering and Technology,Jiangsu University,Zhenjiang 212013,China
    2Xi'an Aerospace Propulsion Institute,Xi'an 710199,China
    3College of Metrology Measurement and Instrument,China Jiliang University,Hangzhou 310018,China
    4School of Energy and Power Engineering,Lanzhou University of Technology,Lanzhou 730050,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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