Volume 23 Issue 8
Aug.  2008
Turn off MathJax
Article Contents
TONG Qi-bao, WANG Suo-fang. Numerical simulation of a steam-cooled vane[J]. Journal of Aerospace Power, 2008, 23(8): 1364-1369.
Citation: TONG Qi-bao, WANG Suo-fang. Numerical simulation of a steam-cooled vane[J]. Journal of Aerospace Power, 2008, 23(8): 1364-1369.

Numerical simulation of a steam-cooled vane

  • Received Date: 2007-07-18
  • Rev Recd Date: 2007-12-17
  • Publish Date: 2008-08-28
  • The steam cooling method was applied in this paper to study the design and characteristics of cooling structure for a vane of gas turbine.The unstructured meshes and realizable k turbulence model were used to study the flow behaviors both inside and outside the grid-ribbed rectangular channel with 15°,30° and 45° rib-roughened wall through 3-Dcoupled numerical simulation.Coupling heat exchange was achieved by heat transfer and solid conduction on the coupled-side of fluid and solid.The cooling medium was steam which had greater Cp and lower viscidity than air.Results show that the flow of the passage is very complex.Heat transfer is enhanced because of the ribs.Ribbed wall has better heat transfer effect than the no rib wall and the cooling effect is obvious.Cooling effect is better by using the steam than by using the air.The numerical result shows the temperature on pressure surface is lower than suction surface.

     

  • loading
  • [1]
    Facchini B,Ferrara G,Innocenti L.Blade cooling improvement for heavy duty gas turbine:the air coolant temperature reduction and the introduction of steam and mixed steam/air cooling[J].Int,J,Therm.Sci.,2000,39:74-84.
    [2]
    Kruger U,Kusterer K,Lang G.Analysis of the influence of cooling steam conditions on the cooling efficiency of a steam-cooled vane using the conjugate calculation technique[R].ASME Turbo Expo 2001-GT-0166.
    [3]
    胡宗军,吴铭岚.采用蒸汽冷却的各种燃气轮机循环性能分析[J].上海交通大学学报,1999,33(3):335-338.HU Zongjun,WU Minglan.Performance analysis of various gas turbine cycles using steam cooling[J].Journal of Shanghai Jiao Tong University,1999,33(3):335-338.(in Chinese)
    [4]
    李海滨,冯国泰,王松涛,等.涡轮三维叶栅的气热耦合数值模拟[J].工程热物理学报,2003,24(5):770-772.LI Haibin,FENG Guotai,WANG Songtao,et al.Numerical simulation method of aerodynamigs-themodynamics coupling in 3-D turbine cascade[J].Journal of Engineering Thermophysics,2003,24(5):770-772.(in Chinese)
    [5]
    张勃,吉洪湖,张靖周,等.网格式肋化通道换热与总压损失特性研究[J].航空动力学报,2004,19(2):201-205.ZHANG Bo,Jl Honghu,ZHANG Jingzhou,et al.Experimental study of heat transfer and total pressure drop of a grid-ribbed rectangular channel[J].Journal of Aerospace Power,2004,19(2):201-205.(in Chinese)
    [6]
    董威,黄维娜.某型发动机涡轮冷却叶片的流动换热耦合计算研究[J].燃气涡轮实验与研究,2006,19(2):14-17.DONG Wei,HUANG Weina.Coupled computation study of the cooling turbine blade[J].Gas Turbine Experiment and Research,2006,19(2):14-17.(in Chinese)
    [7]
    董瑜,郑洪涛,杨凡.蒸汽冷却叶片耦合传热的数值模拟[R].南京:中国航空学会第六届动力年会,2006,CSAA 06-P-116.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1532) PDF downloads(442) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return