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Numerical Simulation on the Influence of Inlet Flow Characteristics on the Performance of a Centrifugal Compressor

Author

Listed:
  • Xing Li

    (Key Laboratory of Mechanics on Disaster and Environment in Western China, Lanzhou University, Lanzhou 730000, China
    College of Civil Engineering and Mechanics, Lanzhou University, Lanzhou 730000, China)

  • Ning Huang

    (Key Laboratory of Mechanics on Disaster and Environment in Western China, Lanzhou University, Lanzhou 730000, China
    College of Civil Engineering and Mechanics, Lanzhou University, Lanzhou 730000, China)

  • Guanyan Chen

    (Key Laboratory of Mechanics on Disaster and Environment in Western China, Lanzhou University, Lanzhou 730000, China
    College of Civil Engineering and Mechanics, Lanzhou University, Lanzhou 730000, China)

  • Yanli Zhang

    (China North Engine Research Institute, Tianjin 300400, China)

  • Yang Zhao

    (China North Engine Research Institute, Tianjin 300400, China)

  • Jie Zhang

    (Key Laboratory of Mechanics on Disaster and Environment in Western China, Lanzhou University, Lanzhou 730000, China
    College of Civil Engineering and Mechanics, Lanzhou University, Lanzhou 730000, China)

  • Ding Tong

    (China North Engine Research Institute, Tianjin 300400, China)

Abstract

Although inlet bent pipes are usually adopted due to limited installation space, the influences of different bend pipes on the inlet flow characteristics and performance of centrifugal compressors are still unclear. The numerical simulation of a centrifugal compressor is established and validated by experimental results with the case of a straight inlet pipe. Then, the internal flow characteristics of the centrifugal compressor with a 90-degree bent pipe (p 90 ) and Z-shaped bent pipe (p z ) are simulated and discussed. The results show that the adoption of two inlet bent pipes reduces the performance of the centrifugal compressor to a certain extent, which reduces more greatly with p z , with a maximum reduction of 6.82% in pressure ratio and 14.83% in efficiency, respectively. The pressure ratio and efficiency reduction of the centrifugal compressor both increase with the increment of distortion degree, which maintains the increasing trend as the flow rate increases, and the maximum distortion degree of p 90 and p z reaches 0.0351 and 0.0479, respectively. The reduction degree of the pressure ratio shows a power–law relationship with the distortion degree, while the reduction degree of efficiency shows an exponential relationship with it. The flow characteristics at the outlet section of the inlet pipe affect the flow field distribution at the inlet of the impeller, and the distortion area ranges of the total pressure and axial velocity at the inlet of the impeller are near 72°–144° in the circumferential direction for p 90 , while those of p z are close to 108°–180° and 288°–360°. When the flow with a high distortion degree enters the impeller, a large area with high turbulent kinetic energy is formed in the downstream flow channel, resulting in an increase in the flow loss.

Suggested Citation

  • Xing Li & Ning Huang & Guanyan Chen & Yanli Zhang & Yang Zhao & Jie Zhang & Ding Tong, 2023. "Numerical Simulation on the Influence of Inlet Flow Characteristics on the Performance of a Centrifugal Compressor," Energies, MDPI, vol. 16(9), pages 1-24, May.
    • Handle: RePEc:gam:jeners:v:16:y:2023:i:9:p:3869-:d:1138333
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    References listed on IDEAS

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    1. Carlo Cravero & Philippe Joe Leutcha & Davide Marsano, 2022. "Simulation and Modeling of Ported Shroud Effects on Radial Compressor Stage Stability Limits," Energies, MDPI, vol. 15(7), pages 1-20, April.
    2. Guangfeng An & Zhu Fan & Ying Qiu & Ruoyu Wang & Xianjun Yu & Baojie Liu, 2022. "Numerical Investigation of the Effect of Hub Gaps on the 3D Flows Inside the Stator of a Highly Loaded Axial Compressor Stage," Energies, MDPI, vol. 15(19), pages 1-20, September.
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    Cited by:

    1. Hongyan Tian & Kang Hou & Ding Tong & Sen Lin & Chicheng Ma, 2023. "Effect of Leading/Trailing Edge Swept Impeller on Flow Characteristics of Low Specific Speed Centrifugal Compressor," Energies, MDPI, vol. 16(11), pages 1-18, May.

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