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

气膜孔附近粒子沉积特性的数值研究

周君辉 张靖周

周君辉, 张靖周. 气膜孔附近粒子沉积特性的数值研究[J]. 航空动力学报, 2014, 29(9): 2166-2173. doi: 10.13224/j.cnki.jasp.2014.09.021
引用本文: 周君辉, 张靖周. 气膜孔附近粒子沉积特性的数值研究[J]. 航空动力学报, 2014, 29(9): 2166-2173. doi: 10.13224/j.cnki.jasp.2014.09.021
ZHOU Jun-hui, ZHANG Jing-zhou. Numerical investigation on particle deposition characteristics in vicinity of film cooling holes[J]. Journal of Aerospace Power, 2014, 29(9): 2166-2173. doi: 10.13224/j.cnki.jasp.2014.09.021
Citation: ZHOU Jun-hui, ZHANG Jing-zhou. Numerical investigation on particle deposition characteristics in vicinity of film cooling holes[J]. Journal of Aerospace Power, 2014, 29(9): 2166-2173. doi: 10.13224/j.cnki.jasp.2014.09.021

气膜孔附近粒子沉积特性的数值研究

doi: 10.13224/j.cnki.jasp.2014.09.021
基金项目: 

国家自然科学基金(51276090);江苏省普通高校研究生科研创新计划(CXLX13_166);中央高校基本科研业务费专项资金

详细信息
    作者简介:

    周君辉(1984-),男,河南鹤壁人,博士生,主要从事叶轮机械气动热力学研究.

  • 中图分类号: V231.1

Numerical investigation on particle deposition characteristics in vicinity of film cooling holes

  • 摘要: 研究了气膜孔附近的粒子运动与沉积特性,重点研究了粒子直径和气膜出流吹风比对粒子运动与沉积特性的影响. 基于EI-Batsh粒子沉积模型,考虑了粒子的黏附/反弹和离去机制,编制了相应的粒子沉积计算模块集成在Fluent软件中,并利用相关实验数据对该计算方法进行了验证.结果表明:1,2μm直径粒子沉积率随吹风比增大而增大;3,4μm直径粒子沉积率则随吹风比增大而减小.1μm直径粒子易受气膜出流卵形涡对的卷吸作用而沉积于相邻气膜孔之间区域,当吹风比为2时粒子沉积率比吹风比为0时高约5倍;5μm直径粒子运动轨迹受气膜出流影响较小.总体沉积率随吹风比升高而不断降低,吹风比为2时总体沉积率比吹风比为0时减小1.7%.

     

  • [1] Brun K,Nored M,Kurz R.Particle transport analysis of sand ingestion in gas turbine engines[J].Journal of Engineering for Gas Turbines and Power,2012,134(1):012402.1-012402.8.
    [2] Dunn M G,Padova C,Moller J C,et al.Performance deterioration of a turbofan and a turbojet engine upon exposure to a dust environment[J].Journal of Engineering for Gas Turbines and Power,1987,109(3):336-343.
    [3] Kim J,Dunn M G,Baran A J,et al.Deposition of volcanic materials in the hot sections of two gas turbine engines[J].Journal of Engineering for Gas Turbines and Power,1993,115(3):641-651.
    [4] Sundaram N,Thole K A.Effects of surface deposition,hole blockage,and thermal barrier coating spallation on vane endwall film cooling[J].Journal of Turbomachinery,2007,129(3):599-607.
    [5] Hamed A,Tabakoff W,Wenglarz R.Erosion and deposition in turbomachinery[J].Journal of Propulsion and Power,2006,22(2):350-360.
    [6] Hamed A A,Tabakoff W,Rivir R B,et al.Turbine blade surface deterioration by erosion[J].Journal of Turbomachinery,2005,127(3):445-452.
    [7] Zhang Y L,McLaury B S,Shirazi S A.Improvements of particle near-wall velocity and erosion predictions using a commercial CFD code[J].Journal of Fluids Engineering,2009,131(3):031303.1-031303.9.
    [8] 伊景海,史峰,徐忠.平面叶栅内固体粒子运动特性的研究[J].航空动力学报,1995,10(3):277-279,313. YI Jinghai,SHI Feng,XU Zhong.A study on motion behaviours of particles through turbine cascade[J]. Journal of Aerospace Power,1995,10(3):277-279,313.(in Chinese)
    [9] 饶江,葛满初,徐建中,等.固体颗粒与通道壁面相互作用的实验研究[J].工程热物理学报,2003,24(1):134-136. RAO Jiang,GE Manchu,XU Jiangzhong,et al.Experimental investigation on interaction between solid particle and wall surface[J].Journal of Engineering Thermophysics,2003,24(1):134-136.(in Chinese)
    [10] 席光,贾会霞,王晓锋,等.轴流压缩机叶栅内固体微粒沉积的数值研究[J].工程热物理学报,2003,24(1):55-58. XI Guang,JIA Huixia,WANG Xiaofeng,et al.Numerical study of the deposition of solid particles in the blade cascade of axial compressors[J].Journal of Engineering Thermophysics,2003,24(1):55-58.(in Chinese)
    [11] Brach R M,Dunn P F.A mathematical model of the impact and adhesion of microspheres[J].Aerosol Science and Technology,1992,16(1):51-64.
    [12] El-Batsh H,Haselbacher H.Numerical investigation of the effect of ash particle deposition on the flow field through turbine cascades[R].ASME Paper GT-2002-30600,2002.
    [13] Wammack J E,Crosby J,Fletcher D,et al.Evolution of surface deposits on a high pressure turbine blade:Part Ⅰ physical characteristics[J].Journal of Turbomachinery,2008,130(2):021020.1-021020.8.
    [14] Guha A.Transport and deposition of particles in turbulent and laminar flow[J].Annual Review Fluid Mechanics,2008,40:311-341.
    [15] Crosby J M,Ai W G,Lewis S,et al.Effects of particle size,gas temperature,and metal temperature on high pressure turbine deposition in land based gas turbines from various synfuels[J].Journal of Engineering for Gas Turbines and Power,2008,130(5):051503.1-051503.9.
    [16] Cardwell N D,Thole K A,Burd S W.Investigation of sand blocking within impingement and film-cooling holes[J]. Journal of Turbomachinary,2010,132(2):021020.1-021020.10.
    [17] Ai W G,Fletcher T H.Computational analysis of conjugate heat transfer and particulate deposition on a high pressure turbine vane[J].Journal of Turbomachery,2012,134(4):041020.1-041020.12.
    [18] Ai W G,Murray N,Fletcher T H,et al.Effect of hole spacing on deposition of fine coal flyash near film cooling holes[J].Journal of Turbomachinery,2012,134(4):041021.1-041021.9.
    [19] YAO Yu,ZHANG Jingzhou.Investigation on film cooling characteristics from a row of converging slot-holes on flat plate[J].Science China:Technological Sciences,2011,54(7):1793-1800.
    [20] YANG Chengfeng,ZHANG Jingzhou.Experimental investigation on film cooling characteristics from a row of holes with ridge-shaped tabs[J].Experimental Thermal and Fluid Science,2012,37:113-120.
  • 加载中
计量
  • 文章访问数:  2586
  • HTML浏览量:  1
  • PDF量:  868
  • 被引次数: 0
出版历程
  • 收稿日期:  2013-06-13
  • 刊出日期:  2014-09-28

目录

    /

    返回文章
    返回