Numerical Investigation of the Impact of Intake Pipelines on the Performance and Flow Characteristics of a Centrifugal Compressor

被引:0
|
作者
Li, X. [1 ,2 ]
Huang, N. [1 ,2 ]
Han, W. [3 ,4 ]
Tong, D. [5 ]
Zhang, Y. [5 ]
Zhang, J. [1 ,2 ]
机构
[1] Lanzhou Univ, Coll Civil Engn & Mech, Lanzhou 730000, Peoples R China
[2] Key Lab Mech Disaster & Environm Western China, Lanzhou 730000, Gansu, Peoples R China
[3] Lanzhou Univ Technol, Dept Energy & Power Engn, Lanzhou 730050, Peoples R China
[4] Key Lab Fluid Machinery & Syst, Lanzhou 730050, Gansu, Peoples R China
[5] China North Engine Res Inst, Tianjin 300400, Peoples R China
关键词
Centrifugal compressor; Flow characteristics; Plane superimposed distortion intensity; Performance reduction degree; Exponential correlation; DISTORTION; RATIO;
D O I
10.47176/jafm.18.6.3150
中图分类号
O414.1 [热力学];
学科分类号
摘要
Due to the installation space constraints in practical applications, centrifugal compressors often utilize bent intake pipes. Quantifying the correlation between the centrifugal compressor's operating performance and the flow dynamics within curved inlet tubes is essential. In this research, the accuracy of the numerical methodology was validated using the experimental outcomes. Subsequently, the centrifugal compressor's performance was simulated for two intake curved ducts, i.e., Pc with a coplanar central axis and Pnc with a non- coplanar central axis, followed by the analysis of the flow characteristics for each intake configuration. The results indicated that Pc produced a symmetrical swirling flow field at the outlet, which was characterized by a lower plane superimposed distortion intensity (PSDI), while Pnc generated an asymmetrical offset swirling flow field with a higher PSDI. The PSDI increased with the flow rate, reaching maximum values of 0.137 for Pc and 0.386 for Pnc. Compared to the inlet straight tube, the performances of the centrifugal compressor connected to Pc and Pnc both decreased, while Pnc exhibited a more significant performance deterioration degree. Under high-speed conditions, the maximum degradation degrees of pressure ratio for Pc and Pnc reached approximately 5.7% and 9.8%, respectively, while the efficiency reduction degree reached approximately 5.3% and 8.7%, respectively. The performance reduction degree for both bent pipes increased with the rising PSDI, exhibiting an exponential correlation. The flow characteristics of the intake pipelines affected the flow behavior within the impeller, with the flow field variation locations closely resembling the distorted regions of the bent pipes.
引用
收藏
页码:1483 / 1501
页数:19
相关论文
共 50 条
  • [21] Numerical investigation of flow mechanisms of tandem impeller inside a centrifugal compressor
    Li, Ziliang
    Lu, Xin'gen
    Zhao, Shengfeng
    Han, Ge
    Yang, Chengwu
    Zhang, Yanfeng
    CHINESE JOURNAL OF AERONAUTICS, 2019, 32 (12) : 2627 - 2640
  • [22] EXPERIMENTAL AND NUMERICAL INVESTIGATION OF THE FLOW FIELD IN THE RADIAL INLET OF A CENTRIFUGAL COMPRESSOR
    Han, Fenghui
    Qi, Datong
    Tan, Jiajian
    Wang, Li
    Mao, Yijun
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 8, PTS A-C, 2012, : 831 - +
  • [23] Numerical investigation of aerodynamic load on the impellers of centrifugal compressor with leakage flow
    Xin J.
    Wang X.
    Liu H.
    Wei W.
    Zhou L.
    International Journal of Fluid Machinery and Systems, 2020, 13 (02): : 409 - 424
  • [24] INVESTIGATION ON THE IMPACT OF CIRCUMFERENTIAL GROOVES ON AERODYNAMIC CENTRIFUGAL COMPRESSOR PERFORMANCE
    Bareiss, Simon
    Vogt, Damian M.
    Chebli, Elias
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 2C, 2015,
  • [25] Numerical study on the flow characteristics of centrifugal compressor impeller with crack damage
    Liang, Zhaoyu
    Xiang, Longhao
    Wei, Xuesong
    Chen, Songying
    Liu, Jingting
    Hao, Zongrui
    ADVANCES IN MECHANICAL ENGINEERING, 2021, 13 (07)
  • [26] A NUMERICAL INVESTIGATION OF THE DESIGN POINT PERFORMANCE FOR A CENTRIFUGAL COMPRESSOR WITH A PARAMETERIZED VOLUTE
    McLaughlin, Laura
    Stuart, Charles
    Spence, Stephen
    Rusch, Daniel
    Geron, Marco
    So, Kwok Kai
    Kreiselmaier, Erich
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 13D, 2023,
  • [27] INVESTIGATION OF THE FLOW IN CENTRIFUGAL COMPRESSOR VOLUTE
    Xu, C.
    Amano, R. S.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 1, 2008, : 751 - 765
  • [28] Numerical investigation of the effect of tip clearance to the performance of a small centrifugal compressor
    Tang, Jin
    Turunen-Saaresti, Teemu
    Reunanen, Arttu
    Honkatukia, Juha
    Larjola, Jaakko
    Proceedings of the ASME Turbo Expo 2006, Vol 5, Pts A and B, 2006, : 411 - 418
  • [29] Numerical Investigation on Labyrinth Seal Leakage Flow and Its Effects on Aerodynamic Performance for a Multistage Centrifugal Compressor
    Qiao, Bing
    Ju, Yaping
    Zhang, Chuhua
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2019, 141 (07):
  • [30] Numerical analysis of centrifugal compressor performance and flow at low Reynolds number
    Huo, L., 1600, Beijing University of Aeronautics and Astronautics (BUAA) (28):