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Volume 40 Issue 6
Jun.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(6): 797-802.
Zhou Yuhui, Kang Rui, Su Li, et al. Life prediction of thrust bearings based on accelerated wear test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(8): 1016-1020. (in Chinese)
Citation: Wang Zhuoqi, Lu Lipeng, Yuan Wei, et al. Experimental investigation on critical stall stage of counter-rotating fan at different speed ratio[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 797-802. doi: 10.13700/j.bh.1001-5965.2013.0425(in Chinese)
shu

Experimental investigation on critical stall stage of counter-rotating fan at different speed ratio

doi: 10.13700/j.bh.1001-5965.2013.0425

  • 1. Research Institute of Unmanned Aerial Vehicle, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;

  • 2. National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 06 Nov 2013
  • Publish Date: 20 Jun 2014
    Abstract
  • Theoretical analysis on a low-speed counter-rotating fan shows that the critical stall stage is determined by two parameters, one is the critical stall mass flow coefficient of each rotor, the other is the real mass flow coefficient of the two rotors at stall point. An experiment was taken to confirm this supposition. The experiment was carried out on investigating the stall characteristic of a counter-rotating fan at different speed ratio. 36 cases was taken at 100%, 90%, 80%,70%,60%, 50% speed of each rotor. The result shows that the second rotor is the critical stall stage at design speed, and the critical stall stage could be changed by adjusting the speed ratio of the two rotors. It is also observed that the hysteresis stall loop appears when the first rotor is the critical stall stage, while it doesn't appears when the second rotor is the critical stall stage.

     

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    • References(20)
  • [1]
    Lynam F C, Hawes S P.Contra rotating axial flow fans[C]//The Engineers,1946
    [2]
    Ozgur C. Rotating guide apparatus for axial pumps and turbines[C]//Water Power,1961
    [3]
    Minato R, Ota T,Fukutomi K,et al.Development of counter rotating axial fan turbojet engine for supersonic unmanned plane[C]//Joint Propulsion Conference.Reston,VA:AIAA,2007:191-196
    [4]
    Sharma P B, Pundhir D S,Chaudhry K K.A study of aeroacoustic performance of a contra-rotating axial flow compressor stage[J].Defence Science Journal,2013,41(2):165-180
    [5]
    Pundhir D S, Sharma P B,Chaudhary K K.Effect of casing treatment on aerodynamic performance of a contrarotating axial compressor stage[J].Journal of Power and Energy,1990,204(1):47-55
    [6]
    Kerrebrock J L, Adamczyk J J,Shabbir A,et al.Design and test of an aspirated counter-rotating fan[J].Journal of Turbomachinery,2008,130(2):021004-1-8
    [7]
    Nagano S, Takata H,Macmida Y.Dynamic performance of stalled blade flow[J].Bulletin of JSME,1971(11):1-12
    [8]
    Sharma P B. Development of a contra-rotating axial flow compressor[R].IITD/ME-86001,1986
    [9]
    Sharma P B. Development and testing of contra-rotating axial flow fan[R].IITD/ME-86001,1994
    [10]
    Rao P S. Development and testing of contra-rotating axial flow fan[C]//M Tech Dissertation.Bombay:IIT,1988
    [11]
    Celestina M L, Adamczyk J J,Mulac R A.A numerical simulation of the inviscid flow through a counterrotating propeller[J].Journal of Turbomachinery,1986,108(2):187-193
    [12]
    Adekoya. Analytical study of performance of a contra-rotating axial flow compressor[D].Delhi,India:Delhi College of Engineering,1995
    [13]
    李秋实,陆亚钧. 对旋轴流压缩系统的增压扩稳途径实验分析[J].北京航空航天大学学报,2000,26(6):669-672 Li Qiushi,Lu Yajun.Exploring the means of raising pressure and stable range contra-rotating axial compressor system[J].Journal of Beijing University of Aeronautics and Astronautics,2000,26(6):669-672(in Chinese)
    [14]
    李志平,李秋实, 陆亚钧.从非定常效应看对旋风扇/压气机的工程实现[J].工程热物理学报,2002,23(2):183-186 Li Zhiping,Li Qiushi,Lu Yajun.The unsteady effect of counter-rotating fan/compressor and its application[J].Journal of Engineering Thermophysics,2002,23(2):183-186(in Chinese)
    [15]
    季路成. 对转叶轮机技术挑战分析[J].推进技术,2007, 28(1): 40-44 Ji Lucheng.Analysis for technique challenges on counter-rotating turbomachinery[J].Journal of Propulsion Technology,2007,28(1):40-44(in Chinese)
    [16]
    刘波,杨艳,王掩刚, 等.设计压比和转速变化对对转压气机性能的影响研究[J].西北工业大学学报,2007,25(4): 576-580 Liu Bo,Yang Yan,Wang Yangang,et al,Investigation of influence of rotational speed and pressure ratio on performance of two-stage counter-rotating compressor[J].Journal of Northwestern Polytechnical University,2007,25(4):576-580(in Chinese)
    [17]
    刘波,侯为民, 陈云永,等.对转压气机转差特性试验与数值模拟[J].航空动力学报,2009,24(2):403-408 Liu Bo,Hou Weimin,Chen Yunyong,et al.Experiment and numerical simulation of rotating-speed difference effects on a dual-stage counter-rotating compressor flow field and performance[J].Journal of Aerospace Power,2009,24(2):403-408(in Chinese)
    [18]
    侯为民,刘波, 赵旭民,等.对转压气机转子间不同转差下非定常流动的PIV测量[J].航空工程进展,2011,2(2): 220-225 Hou Weimin,Liu Bo,Zhao Xumin,et al.PIV investigation of the internal flow between two rotors in a dual-stage counter-rotating compressor under rotating-speed differences[J].Advances in Aeronautical Science and Engineering, 2011,2(2):220-225(in Chinese)
    [19]
    Wang Z Q, Yuan W,Li Q S,et al.An unsteady numerical investigation on the hysteresis stall loop of a counter-rotating compressor[C]//ASME IMECE2011.New York:American Society of Mechanical Engineers,2011:801-806
    [20]
    Wang Z Q, Yuan W,Li Q S,et al.Experimental investigation on the stall inception of a counter-rotating compressor[C]//ASME-GT2012.New York:American Society of Mechanical Engineers,2012:2405-2415
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