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叶尖间隙对离心叶轮偏置分流叶片工作机理的影响

陈杰 何敏祥 黄国平

陈杰, 何敏祥, 黄国平. 叶尖间隙对离心叶轮偏置分流叶片工作机理的影响[J]. 航空动力学报, 2016, 31(8): 1950-1956. doi: 10.13224/j.cnki.jasp.2016.08.021
引用本文: 陈杰, 何敏祥, 黄国平. 叶尖间隙对离心叶轮偏置分流叶片工作机理的影响[J]. 航空动力学报, 2016, 31(8): 1950-1956. doi: 10.13224/j.cnki.jasp.2016.08.021
CHEN Jie, HE Min-xiang, HUANG Guo-ping. Effect of tip clearance on the operating mechanism of offset splitter blades in a centrifugal compressor[J]. Journal of Aerospace Power, 2016, 31(8): 1950-1956. doi: 10.13224/j.cnki.jasp.2016.08.021
Citation: CHEN Jie, HE Min-xiang, HUANG Guo-ping. Effect of tip clearance on the operating mechanism of offset splitter blades in a centrifugal compressor[J]. Journal of Aerospace Power, 2016, 31(8): 1950-1956. doi: 10.13224/j.cnki.jasp.2016.08.021

叶尖间隙对离心叶轮偏置分流叶片工作机理的影响

doi: 10.13224/j.cnki.jasp.2016.08.021
基金项目: 

国家自然科学基金(51206078)

详细信息
    作者简介:

    陈杰(1980-),男,江苏姜堰人,讲师,博士,主要从事叶轮机械气体动力学研究.E-mail:chenj@nuaa.edu.cn

  • 中图分类号: V231.3;TH452

Effect of tip clearance on the operating mechanism of offset splitter blades in a centrifugal compressor

  • 摘要: 采用计算流体力学方法研究了不同叶尖间隙情况下偏置分流叶片提升离心叶轮性能的机理.叶尖间隙较小时,主叶片吸力面附近分离区导致主要损失,分流叶片偏向于主叶片吸力面利于削弱损失、提升叶轮性能;随着叶尖间隙的增加,泄漏流的影响增加以至损失集中于分流叶片和主叶片压力之间的通道,分流叶片宜向主叶片压力面偏置,以减少泄漏流在同一通道的聚集.叶尖间隙和分流叶片周向位置对间隙泄漏流、叶片吸力面分离形成的损失及相互关系有着耦合影响,分流叶片周向位置的改变可以调整通道的横向压力梯度、泄漏流掺混入主流的位置,改善分流叶片两侧通道的损失的分配,分流叶片最佳偏置方向随叶尖间隙的大小而发生改变.

     

  • [1] Krain H.Review of centrifugal compressor's application and development[J].Journal of Turbomachinery,2005,127(1):25-34.
    [2] 张金凤,袁野,叶丽婷,等.带分流叶片离心叶轮机械研究进展[J].流体机械,2011,39(11):38-44. ZHANG Jinfeng,YUAN Ye,YE Liting,et al.Research state of the centrifugal machineries with impeller adding splitter blades[J].Fluid Machinery,2011,39(11):38-44.(in Chinese)
    [3] 李学臣,席光.离心叶轮出口流动分离区影响因素的数值研究[J].西安交通大学学报,2013,47(9):16-22. LI Xuechen,XI Guang.Numerical research on influence factors of flow separation near centrifugal impeller outlet[J].Journal of Xi'an Jiaotong University,2013,47(9):16-22.(in Chinese)
    [4] Farge T Z,Johnson M W,Maksoud T M A.Tip leakage in a centrifugal impeller[J].Journal of Turbomachinery,1989,111(3):244-249.
    [5] 刘正先,陈丽英.半开式离心叶轮变工况间隙流动特征[J].工程热物理学报,2012,33(3):415-418. LIU Zhengxian,CHEN Liying.On nature of tip clearance flow in unshroud impeller of centrifugal compressor at different flow rate[J].Journal of Engineering Thermophysics,2012,33(3):415-418.(in Chinese)
    [6] 郭宫达,张扬军,郑新前,等.跨声速离心压气机叶尖区旋涡流动特征[J].清华大学学报,2008,48(11):1980-1984. GUO Gongda,ZHANG Yangjun,ZHENG Xinqian,et al.Vortex flows in the blade tip region of a transonic centrifugal compressor[J].Journal of Tsinghua University,2008,48(11):1980-1984.(in Chinese)
    [7] 彭森,杨策,马朝臣.离心压气机叶尖间隙泄漏流动数值研究[J].工程热物理学报,2005,26(6):935-937. PENG Sen,YANG Ce,MA Chaochen.Numerical simulation of centrifugal compressor with tip clearance[J].Journal of Engineering Thermophysics,2005,26(6):935-937.(in Chinese)
    [8] 戴韧,陈康民,王企鲲.离心压气机叶轮内部流动的数值研究:分流叶片的作用[J].工程热物理学报,2004,25(增刊):47-50. DAI Ren,CHEN Kangmin,WANG Qikun.Numerical study of flow inside centrifugal impeller:effect of splitter[J].Journal of Engineering Thermophysics,2004,25(Suppl.):47-50.(in Chinese)
    [9] Oana M,Kawamoto O,Ohtani H,et al.Approach to high performance transonic centrifugal compressor[R]AIAA-2002-3536,2002.
    [10] GUI Lichuan,GU Chuangang,CHANG Hongshou.Influences of splitter blades on the centrifugal fan performances[R].ASME Paper 89-GT-33,1989.
    [11] 朱士灿,陈正德.一种分流叶片偏置的径流式压气机的研制[J].内燃机学报,1986,4(1):40-55. ZHU Shican,CHEN Zhengde.The development of a radial flow compressor with offset splitter blades[J].Transactions of CSICE,1986,4(1):40-55.(in Chinese)
    [12] 谢蓉,海洋,王晓放.分流叶片周向位置设计及其对离心叶轮内部流动的影响[J].燃气轮机技术,2009,22(2):37-40. XIE Rong,HAI Yang,WANG Xiaofang.Design of the splitter blade circumferential position and its effect on the internal flow of centrifugal impeller[J].Gas Turbine Technology,2009,22(2):37-40.(in Chinese)
    [13] 刘瑞韬,徐忠.分流叶片位置对高转速离心压气机性能的影响[J].空气动力学报,2005,23(1):129-135. LIU Ruitao,XU Zhong.Effect of the splitter blade position on the characteristic of high-speed centrifugal compressor[J].Acta Aerodynamica Sinica,2005,23(1):129-135.(in Chinese)
    [14] 卜远远,楚武利.分流叶片周向位置对离心叶轮性能及内部流动的影响[J].流体机械,2011,39(9):16-20. BU Yuanyuan,CHU Wuli.Effect of the splitter blade position on the performance and the internal flow of centrifugal impeller[J].Fluid Machinery,2011,39(9):16-20.(in Chinese)
    [15] 刘飞,蔡兆麟.含分流叶片的离心压缩机级的数值分析[J].风机技术,2005(2):1-4. LIU Fei,CAI Zhaolin.Numerical analysis of centerifugal compressor stage with short blade[J].Compressor Blower & Fan Technology,2005(2):1-4.(in Chinese)
    [16] 陈杰,黄国平,梁德旺,等.叶片数对微型斜流叶轮性能的影响[J].航空动力学报,2008,23(9):1707-1712. CHEN Jie,HUANG Guoping,LIANG Dewang,et al.Effects of blade number on performance of transonic micro slope impeller[J].Journal of Aerospace Power,2008,23(9):1707-1712.(in Chinese)
    [17] 陈杰,钟榈,黄国平.微型离心叶轮流动损失分析与削弱[J].推进技术,2013,34(7):904-910. CHEN Jie,ZHONG Lü,HUANG Guoping.Analysis and reduction of the flow loss in a micro centrifugal impeller[J].Journal of Propulsion Technology,2013,34(7):904-910.(in Chinese)
    [18] Krain H.Investigation of the flow through a high pressure ratio centrifugal impeller[R].ASME Paper GT-30394,2002.
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出版历程
  • 收稿日期:  2014-12-02
  • 刊出日期:  2016-08-28

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