留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

叶尖泄漏流/尾迹掺混对串列转子非设计点性能影响

钱煜平 李秋实 陆亚钧

钱煜平, 李秋实, 陆亚钧. 叶尖泄漏流/尾迹掺混对串列转子非设计点性能影响[J]. 航空动力学报, 2013, 28(6): 1350-1356.
引用本文: 钱煜平, 李秋实, 陆亚钧. 叶尖泄漏流/尾迹掺混对串列转子非设计点性能影响[J]. 航空动力学报, 2013, 28(6): 1350-1356.
QIAN Yu-ping, LI Qiu-shi, LU Ya-jun. Effect of tip leakage flow and wake interactions on off-design point performance of tandem rotors[J]. Journal of Aerospace Power, 2013, 28(6): 1350-1356.
Citation: QIAN Yu-ping, LI Qiu-shi, LU Ya-jun. Effect of tip leakage flow and wake interactions on off-design point performance of tandem rotors[J]. Journal of Aerospace Power, 2013, 28(6): 1350-1356.

叶尖泄漏流/尾迹掺混对串列转子非设计点性能影响

基金项目: 国家自然科学基金(10902008,51176005)

Effect of tip leakage flow and wake interactions on off-design point performance of tandem rotors

  • 摘要: 在串列转子设计中,为研究前后排叶片周向位置的变化所引起的泄漏流/尾迹之间掺混的变化对串列转子近失速点性能的影响,首先建立了泄漏流/尾迹掺混分析模型.模型分析结果指出流动掺混可以有效减小通道下游堵塞.在模型分析的基础上,进一步在高负荷串列转子中进行了不同周向位置的对比研究,对模型进行了验证;研究发现在近失速工况,对比无掺混情况,后排叶尖泄漏流/前排尾迹掺混使叶尖堵塞减少了近20%,从而使得高负荷串列转子的失速裕度相对提高了11.7%.

     

  • [1] Bammert K,Staude R.Optimization for rotor blades of tandem design for axial flow compressors[R].ASME Paper 79-GT-125,1979.
    [2] Ihlenfeld H.Stromungsvorgange an stark verzogernden spaltflugelgittern[J].Maschinenbautechnik,1965,14(7/8):361-365.
    [3] Linnemann H.Untersuchungen eines einstufigen axialgeblases mit tandemgittern[J].Konstruktion,1964(4):128-135.
    [4] QIAN Yuping,LI Zhiping,LU Yajun,et al.Flow mechanics in tandem rotors[R].ASME Paper GT2012-69665, 2012.
    [5] Khalid S A.The effects of tip clearence on axial compressor pressure rise[D].Boston,US:Massachusetts Insitute of Technology,1995.
    [6] Hah C,Bergner J,Schiffer H P.Short length-scale rotating stall inception in a transonic axial compressor:criteria and mechanism[R].ASME Paper GT2006-90045,2006.
    [7] Vo H D,Tan C S,Greitzer E M.Criteria for spike initiated rotating stall[J].Journal of Turbomachinery,2008,130(1):011023.1-011023.9.
    [8] Yamada K,Furukawa M,Nakano T.Unsteady three-dimensional flow phenomena due to breakdown of tip leakage vortex in a transonic axial compressor rotor[R].ASME Paper GT2004-53745,2004.
    [9] Adamczyk J J,Celestina M L,Greitzer E M.The role of tip clearance in high-speed fan stall[J].Journal of Turbomachinery,1993,115(1):28-38.
    [10] Hah C,Rabe D C.Role of tip clearance flows on flow instability in axial flow compressors[R].ISABE Paper 2001-1223,2001.
    [11] Schlechtriem S,Loetzerich M.Breakdown of tip leakage vortices in compressors at flow conditions close to stall[R].ASME Paper 97-GT-41,1997.
    [12] Yamada K,Funazaki K,Furukawa M.The behavior of tip clearance flow at near-stall condition in a transonic axial compressor rotor[R].ASME Paper GT2007-27725,2007.
    [13] Yamada K,Furukawa M,Inoue M,et al.Numerical analysis of tip leakage flow field in a transonic axial compressor rotor[R].IGTC Paper 2003-095,2003.
    [14] Hoffman W H,Ballman J.Some aspects of tip vortex behavior in a transonic turbocompressor[R].ISABE Paper 2003-1223,2003.
    [15] Chima R V.Calculation of tip clearance effects in a transonic compressor rotor[J].Journal of Turbomachinery,1998,20(1):131-139.
  • 加载中
计量
  • 文章访问数:  1604
  • HTML浏览量:  124
  • PDF量:  907
  • 被引次数: 0
出版历程
  • 收稿日期:  2012-10-17
  • 刊出日期:  2013-06-28

目录

    /

    返回文章
    返回