Volume 29 Issue 10
Oct.  2014
Turn off MathJax
Article Contents
YAN Wei, HU Jun, YANG Fan, WANG Zhi-qiang, YIN Chao. Effect experiment of rotating distortion on the development of modal wave[J]. Journal of Aerospace Power, 2014, (10): 2443-2449. doi: 10.13224/j.cnki.jasp.2014.10.022
Citation: YAN Wei, HU Jun, YANG Fan, WANG Zhi-qiang, YIN Chao. Effect experiment of rotating distortion on the development of modal wave[J]. Journal of Aerospace Power, 2014, (10): 2443-2449. doi: 10.13224/j.cnki.jasp.2014.10.022

Effect experiment of rotating distortion on the development of modal wave

doi: 10.13224/j.cnki.jasp.2014.10.022
  • Received Date: 2013-06-15
  • Publish Date: 2014-10-28
  • In order to explorer the mechanism of the "dangerous frequency", a rotating distortion generator was designed to investigate the effects of rotating distortion on the stall inception of a two-stage low speed axial flow compressor. Experiment results show that the rotating distortion generator can output a rectangle-like total pressure distribution at different rotating speeds. The compressor exhibited significant loss in total-static pressure rise and stability margin arising from rotating distortion, especially when it rotated at a particular speed. Detailed measurements and analysis suggest that the modal wave appears firstly in the distorted area and is restrained when it spreads into un-distorted zone. When transmit frequency of modal wave is equal to the distortion rotating frequency, the modal wave needs least time to develop into rotating stall, the loss in stability margin is the maximum. The time-frequency analysis of the stall inception signal suggests that the "dangerous frequency" is equal to the transmit frequency of the modal wave.

     

  • loading
  • [1]
    Schäffler A,Miatt D C.Experimental evaluation of heavy fan-high-pressure compressor in a three-shaft engine:Part I experimental setup and result[J].Journal of Engineering for Gas Turbine and Power,1985,107(4):828-832.
    [2]
    Ludwig G R,Nenni J P,Arendt R H.Investigation of rotating stall in axial compressors and the development of a prototype stall control system[R].Air Force Aero Propulsion Laboratory,US-AFAPL-TR-73-45,1973.
    [3]
    Longly J P,Shin H W,Plumley R E,et al.Effects of rotating inlet distortion on multistage compressor stability[J].Journal of Turbomachinery,1996,118(2):181-188.
    [4]
    Peters T,Bürgener T,Fottner L.Effects of rotating inlet distortion on a 5-stage HP-compressor[R].ASME Paper 2001-GT-0300,2001.
    [5]
    Peters T,Fottner L.Effects of co-and counter-rotating inlet distortion on a 5-stage HP-compressor[R].ASME Paper GT-2002-30395,2002.
    [6]
    张环,胡骏,屠宝锋,等.旋转进气畸变对压气机气动稳定性即失速起始特性的影响[J].航空动力学报,2008,23(11):2095-2100. ZHANG Huan,HU Jun,TU Baofeng,et al.Effects of rotating inlet distortion on aerodynamic stability and stall inception of axial-flow compressor[J].Journal of Aerospace Power,2008,23(11):2095-2100.(in Chinese)
    [7]
    张环,胡骏,刘大响,等.旋转总压畸变对压气机稳定性影响的二维不可压缩模型[J].航空动力学报,2009,24(8):1773-1784. ZHANG Huan,HU Jun,LIU Daxiang,et al.Two-dimensional incompressible model of effects of rotating inlet distortion on flow instability in compression systems[J].Journal of Aerospace Power,2009,24(8):1773-1784.(in Chinese)
    [8]
    张环.旋转总压畸变对压气机稳定性影响的研究[D].南京:南京航空航天大学,2009. ZHANG Huan.An investigation of effects of rotating total pressure distortion on aerodynamic stability of compressors[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009.(in Chinese)
    [9]
    张靖煊.畸变条件下轴流压气机叶顶间隙流对流动失稳影响的非定常机制[D].北京:中国科学院,2007. ZHANG Jingxuan.The unsteady mechanism and the role of tip clearance flow in distortion induced instability in an axial compressor[D].Beijing:Chinese Academy of Sciences,2007.(in Chinese)
    [10]
    ZHANG Jingxuan,LIN Feng,CHEN Jingyi,et al.Effects of rotating inlet distortion on flow stability of an axial compressor[R].AIAA-2007-5062,2007.
    [11]
    屠宝锋,胡骏.旋转总压畸变对压气机稳定性影响的三维非定常模型[J].航空动力学报,2011,26(2):255-261. TU Baofeng,HU Jun.Three-dimensional unsteady model of effects of rotating inlet distortion on flow instability in compressor[J].Journal of Aerospace Power,2011,26(2):255-261.(in Chinese)
    [12]
    李传鹏,胡骏.旋转进气畸变对轴流压气机气动稳定性影响实验研究[J].航空动力学报,2004,19(4):433-437. LI Chuanpeng,HU Jun.Effects of rotating inlet distortion on a 5-stage HP-compressor[J].Journal of Aerospace Power,2004,19(4):433-437.(in Chinese)
    [13]
    Garnier V H,Epstein A H,Greitzer E M.Rotating waves as a stall inception indication in axial compressors[J].Journal of Turbomachinery,1991,113(2):290-302.
    [14]
    Day I J.Stall inception in axial flow compressors[J].Journal of Turbomachinery,1993,115(1):1-9.
    [15]
    Camps T R,Day I J.A study of spike and modal stall phenomena in a low-speed axial compressor[J].Journal of Turbomachinery,1998,120(3):116-125.
  • 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

    Article Metrics

    Article views (1491) PDF downloads(751) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return