THE INTERACTION BETWEEN INLET GUIDE VANES AND THE IMPELLER RECIRCULATING FLOW IN A CENTRIFUGAL COMPRESSOR AND THE RESULTING IMPACT ON FLOW RANGE

被引:0
|
作者
Li, Xiangjun [1 ]
Spence, Stephen [2 ]
Wu, Yanhui [1 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, Xian, Shaanxi, Peoples R China
[2] Queens Univ Belfast, Belfast, Antrim, North Ireland
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper studies the interaction between the Inlet Guide Vane (IGV) and the typical recirculation flow that occurs close to surge in a turbocharger compressor to analyse its influence on compressor performance the potential to improve the surge margin. The CFD method was first validated by experimental data, then a series of simulations were conducted to study the lengths of various part-span IGVs and also the streamwise distance between the IGV and the impeller. The results showed that, when extensive recirculating flow was generated, the IGV no longer worked in a conventional way to guide the inflow in the tip region, but instead guided the recirculation flow ejected from the impeller inducer. A three-dimensional interaction occurred at the trailing edge of the IGV where the recirculation flow turned downwards along the span of the vane and caused blockage and swirling flow below the bottom of the part span IGV. All the cases with IGVs had a similar peak efficiency to the baseline compressor but produced different impacts on the mass flow rates at the near surge point and the choke point. The IGV with shortest length placed the three-dimensional recirculating flow at a higher span-wise position. The blockage and the pre-swirl were thereby generated closer to the shroud and produced a different flow field at the impeller inlet. Based on the numerical surge criteria, the shortest IGV was found to improve stability at the near surge point compared to the full-span IGV, with no reduction of the mass flow rate at the choke point to give 25% more flow range. The surge margin was mainly increased because of the improved pressure recovery in the diffuser due to the blockage being distributed in the higher-span region of the impeller inflow. The beneficial impact of the three-dimensional interaction on the flow range was found to be associated with the distance between the impeller and the IGV. Both the short and the full-span IGVs achieved less improvement of surge margin when the IGV was placed further upstream of the impeller, showing that the interaction between the reverse flow and the IGV was a beneficial flow feature for overall performance.
引用
下载
收藏
页数:16
相关论文
共 50 条
  • [41] Calculation of splitting vanes and inner flow analysis for centrifugal pump impeller
    Pan, Zhongyong
    Yuan, Shouqi
    Li, Hong
    Cao, Weidong
    Chinese Journal of Mechanical Engineering (English Edition), 2004, 17 (01): : 156 - 159
  • [42] DETERMINISTIC INTERACTION BETWEEN THE IMPELLER FLOW AND BOTH THE INLET AND OUTLET VOLUTE TONGUES FOR A DOUBLE SUCTION CENTRIFUGAL PUMP
    Fernandez Oro, Jesus Manuel
    Argueelles Diaz, Katia Maria
    Gonzalez, Jose
    Guerras Colon, Israel
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE, VOL 1, PTS A-C, 2009, : 357 - 369
  • [43] CALCULATION OF SPLITTING VANES AND INNER FLOW ANALYSIS FOR CENTRIFUGAL PUMP IMPELLER
    Pan ZhongyongYuan ShouqiLi HongCao WeidongResearch Center of Fluid MachineryEngineering and Technology
    Chinese Journal of Mechanical Engineering, 2004, (01) : 156 - 159
  • [44] Flow measurement and simulation of a radial inlet for centrifugal compressor
    Han, Fenghui
    Mao, Yijun
    Tan, Jiajian
    Zhao, Cun
    Zhang, Yiyun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2015, 229 (04) : 367 - 380
  • [45] Investigation and control of centrifugal compressor inlet flow field
    Zhang, Yang-Jun (yjzhang@tsinghua.edu.cn), 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
  • [46] CFD ANALYSIS OF INLET FLOW REGION IN A CENTRIFUGAL COMPRESSOR
    Sudheer, Meera
    Dhinne, Giridhar Kumar
    Hoch, Greg
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 9, 2024,
  • [47] A centrifugal compressor stage with wide flow range vaned diffusers and different inlet configurations
    Kim, Y
    Engeda, A
    Aungier, R
    Amineni, N
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2002, 216 (A4) : 307 - 320
  • [48] Effect of Inlet Guide Vanes on Flow Behavior and Performance of S-CO2 Centrifugal Compressors
    Pei, Jinze
    Wang, Shaocheng
    Zhao, Zhao
    Yu, Yongqiang
    Zhao, Yuanyang
    Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering, 2024, 44 (19): : 7717 - 7725
  • [49] Results of CFD Calculations Verification of High Pressure Centrifugal Compressor Stage with Inlet Guide Vanes
    Karabanova, V. V.
    Vanyashov, A. D.
    Yusha, V. L.
    OIL AND GAS ENGINEERING (OGE-2020), 2020, 2285
  • [50] A flow capacity function approach for centrifugal impeller inlet design
    Wan, Yu
    Guan, Jinping
    Wang, Qiwei
    Yang, Dong
    APPLIED ENERGY, 2024, 371