Volume 27 Issue 7
Jul.  2012
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KUANG Kai-xin, WANG Suo-fang. Effect of splitter on performance of inlet particle separator[J]. Journal of Aerospace Power, 2012, 27(7): 1542-1548.
Citation: KUANG Kai-xin, WANG Suo-fang. Effect of splitter on performance of inlet particle separator[J]. Journal of Aerospace Power, 2012, 27(7): 1542-1548.

Effect of splitter on performance of inlet particle separator

  • Received Date: 2011-09-04
  • Publish Date: 2012-07-28
  • In order to investigate how the position and the size of splitter affect the performance of integral particle separator (IPS),a numerical simulation was conducted by using the Realizable k-ε turbulence model.The simulation came out with the effects of splitter movements in axial direction and radial direction on flowfield,separation efficiency and total pressure loss in IPS.On this basis,the ratio of axial distance to radial distance at splitter lip,the highest point of inner wall surface,and the shape of the splitter's effect on IPS were studied.The results show that:When the ratio is large,with the increase of the axial distance,total pressure loss declines with a large gradient descent.When the ratio is small,total pressure loss tends to decrease at first and then increase;after the shape of the splitter changes,the total pressure loss becomes much lower while the separation efficiency getting much higher,and the highest Mach number at the splitter lip also decreases.

     

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  • [1]
    Hamed A.Particle dynamic of inlet flow fields with swirling vanes[J].Journal of Aircraft,1982,19(9):707-712.
    [2]
    Hamed A.An investigation in the variance in particle surface interactions and their effects in gas turbines[J].Journal of Engineering for Gas Turbines and Power,1992,114(2):235-241.
    [3]
    Hamed A,Jun Y D,Yeuan J J.Particle dynamic simulations in inlet separator with an experimentally based bounce model[J].Journal of Propulsion and Power,1995,11(2):230-235.
    [4]
    Vittal B V R,Tipto D L,Bennett W A.Development of an advanced vane less inlet particle separator for helicopter engines .AIAA Paper 85-1277,1985.
    [5]
    Al-Faris E F,Saeed F.Design and optimization method for inertial particle separator (IPS) systems .AIAA Paper 2008-6066,2008.
    [6]
    侯凌云,严传俊.二维粒子分离器的流场及分离效率的数值模拟[J].航空动力学报,1997,12(4):374-376. HOU Lingyun,YAN Chuanjun.Numerical simulation of two-dimensional flow field in particle separator[J].Journal of Aerospace Power,1997,12(4):374-376.(in Chinese)
    [7]
    侯凌云,严传俊.直升机粒子分离器三维两相流场的数值模拟[J].航空动力学报,2000,15(2):215-217. HOU Lingyun,YAN Chuanjun.Numerical simulation of 3-d two-phase flow field in inlet particle separator for helicopter[J].Journal of Aerospace Power,2000,15(2):215-217.(in Chinese)
    [8]
    吴恒刚,王锁芳.整体式粒子分离器数值模拟[J].航空学报,2007,28(5):1073-1079. WU Henggang,WANG Suofang.Numerical simulation of inertial particle separators[J].Acta Aeronautica et Astronautica Sinica,2007,28(5):1073-1079.(in Chinese)
    [9]
    吴恒刚.无叶片整体式粒子分离器性能研究 .南京:南京航空航天大学,2007. WU Henggang.Characteristic study on vaneless integral particle separator .Nanjing:Nanjing University of Aeronautics and Astronautics,2007.(in Chinese)
    [10]
    董晓婷,王锁芳.有叶片整体式粒子分离器三维两相流数值模拟[J].机床与液压,2008,36(10):136-139. DONG Xiaoting,WANG Suofang.Numerical simulation of three-dimensions two-phase flow in inlet particle separator with vanes[J].Machine Tool & Hydraulics,2008,36(10):136-139.(in Chinese)
    [11]
    叶静,胡柏安,熊焰.涡轴发动机无叶片粒子分离器流道设计[J].现代机械,2007(2):39-42. YE Jing,HU Boan,XIONG Yan.Flow path design of vanless particle separator for turbo shaft engine[J].Modern Machinery,2007(2):39-42.(in Chinese)
    [12]
    Duffy R J,Shttuck B F.Integral engine inlet particle separator Volume Ⅱ:design guide .AD Paper A015 064,1975.
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