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自适应流通处理机匣喷气位置对压气机性能的影响

张皓光 吴俊 王云鹏 楚武利 吴艳辉

张皓光, 吴俊, 王云鹏, 楚武利, 吴艳辉. 自适应流通处理机匣喷气位置对压气机性能的影响[J]. 航空动力学报, 2016, 31(5): 1149-1158. doi: 10.13224/j.cnki.jasp.2016.05.017
引用本文: 张皓光, 吴俊, 王云鹏, 楚武利, 吴艳辉. 自适应流通处理机匣喷气位置对压气机性能的影响[J]. 航空动力学报, 2016, 31(5): 1149-1158. doi: 10.13224/j.cnki.jasp.2016.05.017
ZHANG Hao-guang, WU Jun, WANG Yun-peng, CHU Wu-li, WU Yan-hui. Influence of the injecting position of self recirculation casing treatment on compressor performance[J]. Journal of Aerospace Power, 2016, 31(5): 1149-1158. doi: 10.13224/j.cnki.jasp.2016.05.017
Citation: ZHANG Hao-guang, WU Jun, WANG Yun-peng, CHU Wu-li, WU Yan-hui. Influence of the injecting position of self recirculation casing treatment on compressor performance[J]. Journal of Aerospace Power, 2016, 31(5): 1149-1158. doi: 10.13224/j.cnki.jasp.2016.05.017

自适应流通处理机匣喷气位置对压气机性能的影响

doi: 10.13224/j.cnki.jasp.2016.05.017
基金项目: 

航空科学基金(2014ZB53014)

国家自然科学基金(51006084)

中央高校基本科研业务费专项资金(3102014JCY01004)

国家自然科学基金重点项目(51236006)

详细信息
    作者简介:

    张皓光(1981-),男,广西宾阳人,副教授,博士,研究领域为叶轮机械气动热力学.

  • 中图分类号: V231.3

Influence of the injecting position of self recirculation casing treatment on compressor performance

  • 摘要: 采用数值模拟方法研究了跨声风扇转子Rotor 67的失速机理和3个喷气位置的自适应流通处理机匣对转子性能的影响.结果表明:叶顶间隙泄漏涡中低速团是诱发失稳的主要原因;3个喷气位置的处理机匣均增大了压气机的稳定工作范围,喷气位置居中和后移的处理机匣综合稳定裕度改进量分别为13.43%,9.47%,均大于前移的2.72%;喷气位置居中和后移有利于抑制间隙泄漏流的发展,减小低能流体泄漏范围;相比前移和居中,后移不能激励压力面前缘处的低速团和抑制低能流体从叶顶前部泄漏.

     

  • [1] Yamada K,Funazaki K,Furukawa M,et al.The behavior of tip clearance flow at near-stall condition in a transonic axial compressor rotor[R].ASME Paper GT2007-27725,2007.
    [2] Muller M W,Biela C,Schiffer H P,et al.Interaction of rotor and casing treatment flow in an axial single-stage transonic compressor with circumferential grooves[R].ASME Paper GT2008-50135,2008.
    [3] Müller M W,Biela C,Schiffer H P,et al.Effect of circumferential on the aerodynamic performance of an axial single-stage transonic compressor[R].ASME Paper GT2007-27365,2007.
    [4] LU Xingen,CHU Wuli,ZHU Junqiang.Mechanism of the interaction between casing treatment and tip leakage flow in a subsonic axial compressor[R].ASME Paper GT2006-90077,2006.
    [5] 李相君,楚武利,张皓光.高负荷跨声速轴流压气机周向浅槽处理机匣扩稳机理[J].推进技术,2013,34(5):629-637. LI Xiangjun,CHU Wuli,ZHANG Haoguang.Stabilizing mechanism of shallow circumferential grooves on a high loaded transonic axial-flow compressor[J].Journal of Propulsion Technology,2013,34(5):629-637.(in Chinese)
    [6] 张皓光,楚武利,吴艳辉,等.轴向倾斜缝机匣处理影响压气机性能的机理[J].推进技术,2010,31(5):555-561. ZHANG Haoguang,CHU Wuli,WU Yanhui,el al.Investigation of the flow mechanism of affecting compressor performance with axial skewed slots casing treatment[J].Journal of Propulsion Technology,2010,31(5):555-561.(in Chinese)
    [7] 张皓光,楚武利,吴艳辉.缝式处理机匣轴向位置对压气机特性影响的机理[J].航空动力学报,2011,26(1):92-98. ZHANG Haoguang,CHU Wuli,WU Yanhui.Mechanism of influences of axial positions of axial skewed slot on a compressor performance[J].Journal of Aerospace Power,2011,26(1):92-98.(in Chinese)
    [8] Hathaway M D.Self-recirculating casing treatment concept for enhanced compressor performance[R].ASME Paper GT2002-30368,2002.
    [9] Yang H,Nuernberger D,Nicke E,et al.Numerical investigation of casing treatment mechanisms with a conservative mixed-cell approach[R].ASME Paper GT2003-38483,2003.
    [10] Strazisar A J,Bright M M.Compressor stall control through endwall recirculation[R].ASME Paper GT2004-54295,2004.
    [11] Weichert S,Day I,Freeman C,et al.Self-regulating casing treatment for axial compressor stability enhancement[R].ASME Paper GT2011-46024,2011.
    [12] 张皓光,楚武利,吴艳辉,等.压气机端壁自适应流通延迟失速的数值分析[J].推进技术,2009,30(2):202-208. ZHANG Haoguang,CHU Wuli,WU Yanhui,et al.Numerical investigation of the flow mechanisms of compressor stall delay through end wall self recirculation[J].Journal of Propulsion Technology,2009,30(2):202-208.(in Chinese)
    [13] 张皓光,楚武利,吴艳辉,等.自适应流通机匣处理改善压气机性能的机理[J].推进技术,2010,31(3):301-308. ZHANG Haoguang,CHU Wuli,WU Yanhui,et al.Flow mechanisms of improving compressor performance through self recirculation casing treatment[J].Journal of Propulsion Technology,2010,31(3):301-308.(in Chinese)
    [14] 张皓光,吴俊,楚武利,等.带自适用流通处理机匣的轴流压气机全通道数值研究[J].推进技术,2013,34(7):918-924. ZHANG Haoguang,WU Jun,CHU Wuli,et al.Full-annulus numerical investigation of axial flow compressor with self recirculation casing treatment[J].Journal of Propulsion Technology,2013,34(7):918-924.(in Chinese)
    [15] Strazisar A J,Wood J R,Hathaway M D,et al.Laser anemometer measurements in a transonic axial flow fan rotor[R].NASA TP-2879,1989.
    [16] 杜娟.跨音压气机/风扇转子叶顶泄漏流动的非定常机制研究[D].北京:中国科学院工程热物理研究所,2010. DU Juan.Investigation on the unsteady mechanism of tip leakage flow in transonic compressor/fan rotors[D].Beijing:Institute of Engineering Thermophysics,Chinese Academy of Sciences,2010.(in Chinese)
    [17] 童秉纲.非定常流与涡运动[M].北京:国防工业出版社,1993:350-351.
    [18] Wilke I,Kau H P.A numerical investigation of the influence of casing treatments on the tip leakage flow in a HPC front stage[R].ASME Paper GT2002-30642,2002.
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出版历程
  • 收稿日期:  2014-08-29
  • 刊出日期:  2016-05-28

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