Volume 35 Issue 11
Nov.  2020
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2020  >  35(11): 2378-2384
HE Xiang, MA Hongwei, YIN Yueqian. Experiment of rotor-stator interaction behaviors in ,a small multi-stage axial compressor[J]. Journal of Aerospace Power, 2020, 35(11): 2378-2384. doi: 10.13224/j.cnki.jasp.2020.11.015
Citation: HE Xiang, MA Hongwei, YIN Yueqian. Experiment of rotor-stator interaction behaviors in ,a small multi-stage axial compressor[J]. Journal of Aerospace Power, 2020, 35(11): 2378-2384. doi: 10.13224/j.cnki.jasp.2020.11.015
shu

Experiment of rotor-stator interaction behaviors in ,a small multi-stage axial compressor

doi: 10.13224/j.cnki.jasp.2020.11.015
  • 1.

    Hunan Key Laboratory of Turbomachinery on Small and Medium Aero-Engine,Hunan Aviation Powerplant Research Institute,Aero Engine Corporation of China,Zhuzhou Hunan 412002,China

  • 2.

    National Key Laboratory of Science and Technology on Aero-Engine,Aero-thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China

  • Received Date: 2020-04-13
  • Publish Date: 2020-11-28
    Abstract
  • The dynamic pressure signals were measured and analyzed by the Kulite transducers and the fast response pressure probes to investigate the rotor-stator interaction phenomenon in small multistage axial compressor. Results indicated that, at higher rotor speed, the 1st rotor tip flow-field agreed well with the typical supersonic-cascade flow features, and only the flow-field at the 1st rotor trailing-edge was disturbed by the rotor-stator interactions. However, at lower rotor speed, the rotor-stator interaction obviously increased in intensity and appeared at the 1st rotor leading-edge with the compressor throttling. Modal analysis was carried out for these frequency components of rotor-stator interactions, and then the propagation speed and modal number were obtained finally.

     

    • FullText(HTML)
  • loading
    • References(21)
  • [1]
    PFEIL H,HERBST R,SCHRDER T.Investigation of the laminar-turbulent transition of boundary layers disturbed by wakes［J］.Journal of Engineering for Power,1983,105(1):130-137.
    [2]
    HODSON H P.Boundary layer and loss measurements on the rotor on an axial flow turbine［R］.ASME Paper 83-GT-4,1983.
    [3]
    POENSGEN C,GALLUS H E.Three-dimensional wake decay inside of a compressor cascade and its influence on the downstream unsteady flow field［R］.ASME Paper 90-GT-21,1990.
    [4]
    GORELL S E,COPENHAVER W W,CHRISS R M.Effects of upstream wakes on the performance of a transonic compressor stage［R］.International Society of Air Breathing Engines,ISABE 97-7070,1997.
    [5]
    GORELL S E,OKIISHI T H,COPENHAVER W W.Stator-rotor interactions in a transonic compressor:Part 1 effect of blade row spacing on performance［R］.ASME Paper 2002-GT-30494,2002.
    [6]
    GORELL S E,CAR D,PUTERBAUGH S L.An investigation of wake-shock interactions in a transonic compressor with DPIV and time-accurate CFD［R］.ASME Paper 2005-GT-69107,2005.
    [7]
    ISABELLE T,CHRISTOPHE V.Experimental analysis of the rotor stator interaction within a high pressure centrifugal compressor［J］.Journal of Thermal Science,2002,11(1):1-9.
    [8]
    XAVIER O,ISABELLE T.Laser measurements in high speed compressors for rotor-stator interaction analysis［J］.Journal of Thermal Science,2003,12(4):310-317.
    [9]
    MERSINLIGIL M,BROUCKAERT J F,COURTIADE N,et al.A high temperature high bandwidth fast response total pressure probe for measurements in a multistage axial compressor［R］.ASME Paper GT2011-45558,2011.
    [10]
    COURTIADE N,XAVIER O,GOURDAIN N.Modal decomposition for the analysis of the rotor-stator interactions in multistage compressors［J］.Journal of Thermal Science,2012,21(3):276-285.
    [11]
    ARNAUD D,XAVIER O,VOUILLARMET A.Experimental investigation of the rotor-stator interactions,within a high speed,multi-stage,axial compressor,part1-experimental facilities and results［R］.ASME Paper GT2004-53764,2004.
    [12]
    ARNAUD D,XAVIER O,VOUILLARMET A.Experimental investigation of the rotor-stator interactions,within a high speed,multi-stage,axial compressor:Part 2 modal analysis of the interactions［R］.ASME Paper GT2004-53778,2004.
    [13]
    ERNST M,MICHEL A,JESCHKE P.Analysis of rotor-stator-interaction and blade-to-blade measurements in a two stage axial flow compressor［J］.Journal of Turbomachinery,2011,133(1):0110271-01102712.
    [14]
    MAILACH R,LEHMANN I,VOGELER K.Periodical unsteady flow within a rotor blade row of an axial compressor:Part Ⅱ wake-tip clearance vortex interaction［J］.Journal of Turbomachinery,2008,130(4):0410051-04100510.
    [15]
    吴先鸿,陈矛章.非定常动静叶干涉作用的二维数值模拟［J］.航空动力学报,1998,13(2):128-132,216. WU Xianhong,CHEN Maozhang.Two-dimensional numerical simulation of unsteady-rotor/stator interaction［J］.Journal of Aerospace Power,1998,13(2):128-132,216.(in Chinese)
    [16]
    侯安平,周盛.轴流式叶轮机时序效应的机理探讨［J］.航空动力学报,2003,18(1):70-75. HOU Anping,ZHOU Sheng.Probe into the mechanism of clocking effect in turbomachinery［J］.Journal of Aerospace Power,2003,18(1):70-75.(in Chinese)
    [17]
    毛明明,宋彦萍,王仲奇.跨声压气机动静干涉效应的数值模拟研究［J］.航空动力学报,2007,22(9):1468-1474. MAO Mingming,SONG Yanping,WANG Zhongqi.Numerical research on influence of rotor-stator interactions in transonic compressor［J］.Journal of Aerospace Power,2007,22(9):1468-1474.(in Chinese)
    [18]
    王英锋,胡骏,罗标能,等.上游叶片尾迹对转子叶片非定常表面压力频谱特性影响的研究［J］.航空动力学报,2006,21(4):693-699. WANG Yingfeng,HU Jun,LUO Biaoneng,et al.Effects of the upstream blade wakes on the spectrum of rotor blade unsteady surface pressure［J］.Journal of Aerospace Power,2006,21(4):693-699.(in Chinese)
    [19]
    党政,席光,王尚锦.轴向间隙对动/静相干叶排内部非定常特性的影响［J］.工程热物理学报,2000,21(5):584-586. DANG Zheng,XI Guang,WANG Shangjin.Axial spaceing effects on unsteady rotor/stator interaction flow［J］.Journal of Engineering Thermophysics,2000,21(5):584-586.(in Chinese)
    [20]
    蒋康涛,徐纲,张宏武,等.单级跨声压气机整圈三维动静叶干涉的数值模拟［J］.航空动力学报,2002,17(5):549-555. JIANG Kangtao,XU Gang,ZHANG Hongwu,et al.Three-dimensional numerical simulation of whole-ring rotor/stator interaction in a single-stage compressor［J］.Journal of Aerospace Power,2002,17(5):549-555.(in Chinese)
    [21]
    柳阳威,刘宝杰.离心叶轮和扩压器相互作用［J］.航空动力学报,2009,24(12):2695-2702. LIU Yangwei,LIU Baojie.Numerical investigation of impeller-diffuser interaction in a centrifugal compressor［J］.Journal of Aerospace Power,2009,24(12):2695-2702.(in Chinese)
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(3601.0KB)
    XML

    Article Metrics

    Article views (356) PDF downloads(210) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return