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跨声速风扇转子间隙流动结构分析

杨晰琼 刘波 曹志远 茅晓晨 夏树丹

杨晰琼, 刘波, 曹志远, 茅晓晨, 夏树丹. 跨声速风扇转子间隙流动结构分析[J]. 航空动力学报, 2016, 31(9): 2258-2267. doi: 10.13224/j.cnki.jasp.2016.09.027
引用本文: 杨晰琼, 刘波, 曹志远, 茅晓晨, 夏树丹. 跨声速风扇转子间隙流动结构分析[J]. 航空动力学报, 2016, 31(9): 2258-2267. doi: 10.13224/j.cnki.jasp.2016.09.027
YANG Xi-qiong, LIU Bo, CAO Zhi-yuan, MAO Xiao-chen, XIA Shu-dan. Analysis on tip flow structure in transonic fan rotor[J]. Journal of Aerospace Power, 2016, 31(9): 2258-2267. doi: 10.13224/j.cnki.jasp.2016.09.027
Citation: YANG Xi-qiong, LIU Bo, CAO Zhi-yuan, MAO Xiao-chen, XIA Shu-dan. Analysis on tip flow structure in transonic fan rotor[J]. Journal of Aerospace Power, 2016, 31(9): 2258-2267. doi: 10.13224/j.cnki.jasp.2016.09.027

跨声速风扇转子间隙流动结构分析

doi: 10.13224/j.cnki.jasp.2016.09.027
基金项目: 

国家自然科学基金(51236006);先进发动机协同创新中心资助

详细信息
    作者简介:

    杨晰琼(1990-),女,河南南阳人,硕士生,主要从事叶轮机械气动设计及试验研究.

  • 中图分类号: V231.3

Analysis on tip flow structure in transonic fan rotor

  • 摘要: 为探索跨声速转子间隙流动结构,归纳间隙泄漏涡(TLV)和激波相互作用机理,以跨声速转子为研究对象,数值模拟不同间隙下流动特性.此外,着重探究TLV与激波的相互作用,斜激波受到间隙泄漏流的干扰,被削弱打断向上游凹曲;建立三维模型,加深对跨声速叶尖区域流动的全面认识.研究表明:随间隙增大,相同流量下,效率越小,压比也越小;TLV强度更大,偏离吸力面程度增大,沿周向和展向影响范围都越大.压力差提供泄漏流迁移动力,间隙提供泄漏流形成通道.选取h/c=1.0%间隙,随着间隙高度的增大,泄漏流周向运动趋势更明显且二次泄漏现象更剧烈;沿泄漏流方向无量纲流向涡量有少量减少,无量纲螺旋度较高,集中涡特性明显.

     

  • [1] Camp 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):393-401.
    [2] Wheeler A P S,Korakianitis T,Banneheke S.Tip-leakage losses in subsonic and transonic blade rows[J].Journal of Turbomachinery,2013,135(1):751-759.
    [3] ZHANG Zhibo,YU Xianjun,LIU Baojie.Characteristics of the tip leakage vortex in a low-speed axial compressor with different rotor tip gaps[R].ASME Paper GT-2012-69148,2012.
    [4] DU Juan,LIN Feng,CHEN Jingyi,et al.Flow structures in the tip region for a transonic compressor rotor[J].Journal of Turbomachinery,2013,135(3):2561-2572.
    [5] Ahti J,Teemu T S,Aki G,et al.Experimental study of the effect of the tip clearance of the diffuser flow and stage performance of a centrifugal compressor[R].ASME Paper GT-2012-68445,2012.
    [6] ZHANG Desheng,SHI Weidong,WU Suqing.Numerical and experimental investigation of the tip leakage vortex trajectory in an axial flow pump[R].ASME Paper GT-2013-16058,2013.
    [7] WU Yanhui,CHU Wuli,LU Xingen,et al.Behavior of tip-leakage flow in an axial flow compressor rotor[R].ASME Paper GT2006-90399,2006.
    [8] Furukawa M,Saiki K,Nagayoshi K,et al.Effects of stream surface inclination on tip leakage flow fields in compressor rotor[J].Journal of Turbomachinery,1998,120(4):683-694.
    [9] Wheeler A P S,Atkins N R,He L.Turbine blade tip heat transfer in low speed and high speed flows[J].Journal of Tturbomachinery,2011,133(4):041025.1-041025.9.
    [10] 陈绍文,孙士珺,韩东,等.间隙大小对高负荷压气机叶栅流动特性的影响[J].工程热物理学报,2014,35(1):34-37. CHEN Shaowen,SUN Shijun,HAN Dong,et al.Experimental study of the effect of different gap height on the highly-loaded compressor cascade flow characteristics[J].Journal of Engineering Thermophysics,2014,35(1):34-37.(in Chinese)
    [11] 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,2010. DU Juan.Investigation on the unsteady mechanism of tip leakage flow in transonic compressor/fan rotors[D].Beijing:Chinese Academy of Sciences,2010.(in Chinese)
    [12] Hah C,Rabe D C,Wadia A R.Role of tip leakage vortices and passage shock in stall inception in a swept transonic compressor rotor[R].ASME Paper GT-2004-53867,2004.
    [13] ZHANG Qiang,HE Li.Over-tip choking and its implications on turbine blade tip aerodynamaic performance[J].Journal of Propulsion and Power,2012,27(5):1008-1014.
    [14] Hoffman W H,Ballman J.Some aspect s of tip vortex behavior in a transonic turbo compressor[R].ISABE Paper 2003-GT-1223,2003.
    [15] 张晨凯,胡骏,王志强,等.轴流压气机转子叶尖间隙流动结构的数值研究[J].航空学报,2014,35(5):1236-1245. ZHANG Chenkai,HU Jun,WANG Zhiqiang,et al.Numerical study on tip clearance flow structure of an axial flow compressor rotor[J].Acta Aeronautica et Astronautica Sinica,2014,35(5):1236-1245.(in Chinese)
    [16] 姜斌,王松涛,孙玺淼,等.跨音风扇顶部激波、泄漏流作用的数值研究[J].工程热物理学报,2008,28(10):1653-1656. JIANG Bin,WANG Songtao,SUN Ximiao,et al.Numerical simulation study on the effect of tip clearance on performance of a transonic axial fan[J].Journal of Engineering Thermophysics,2008,28(10):1653-1656.(in Chinese)
    [17] Messenger H E,Kennedy E E.Two-stage fan:I aerodynamic and mechanical design[R].NASA CR-120888,1972.
    [18] Kerrebrock J L,Epstein A H,Merchant A A,et al.Design and test of an aspirated counter-rotating fan[R].ASME Paper GT-2006-90582,2006.
    [19] Rugger R S,Benser W A.Performance of a highly loaded two-stage axial flow[R].NASA TMX-3076,1974.
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出版历程
  • 收稿日期:  2015-01-08
  • 刊出日期:  2016-09-28

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