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水平喷流对叶顶气膜冷却效率影响的数值研究

姜伟 谢诞梅

姜伟, 谢诞梅. 水平喷流对叶顶气膜冷却效率影响的数值研究[J]. 航空动力学报, 2016, 31(4): 807-815. doi: 10.13224/j.cnki.jasp.2016.04.006
引用本文: 姜伟, 谢诞梅. 水平喷流对叶顶气膜冷却效率影响的数值研究[J]. 航空动力学报, 2016, 31(4): 807-815. doi: 10.13224/j.cnki.jasp.2016.04.006
JIANG Wei, XIE Dan-mei. Numerical study on the effect of parallel injection on film-cooling effectiveness at turbine blade tip[J]. Journal of Aerospace Power, 2016, 31(4): 807-815. doi: 10.13224/j.cnki.jasp.2016.04.006
Citation: JIANG Wei, XIE Dan-mei. Numerical study on the effect of parallel injection on film-cooling effectiveness at turbine blade tip[J]. Journal of Aerospace Power, 2016, 31(4): 807-815. doi: 10.13224/j.cnki.jasp.2016.04.006

水平喷流对叶顶气膜冷却效率影响的数值研究

doi: 10.13224/j.cnki.jasp.2016.04.006
详细信息
    作者简介:

    姜伟(1991-),男,湖北鄂州人,硕士生,主要从事燃气轮机叶片冷却设计方面的研究.

    通讯作者:

    谢诞梅(1963-),女,湖北武汉人,教授、博士生导师,博士,主要从事转子动力学方面的研究.E-mail:dmxie@whu.edu.cn

  • 中图分类号: V231.1

Numerical study on the effect of parallel injection on film-cooling effectiveness at turbine blade tip

  • 摘要: 为进一步提高燃气轮机叶顶区域的气膜冷却效率,在叶顶模型结构上对4种叶顶冷却结构的流动和传热进行了数值模拟,结果显示带有盖板的水平喷流结构能够有效地提高叶顶区域的气膜冷却效率,对于圆孔,可以将气膜冷却效率提高至原来的2倍以上.通过流场的分析发现:水平喷流结构可以调整冷却工质的流动,使得冷却工质的贴壁性更好、分布更加均匀,进而提高气膜冷却效率.此外还研究了间隙宽度、盖板尾缘厚度、盖度和整流栅对水平喷流结构气膜冷却效率的影响.结果表明:增加盖度和减小间隙宽度可以提高气膜冷却效率,但是盖度和间隙宽度的选取受到了强度、工艺和冷却工质入口压力等因素的限制.水平盖板结构的冷却效果比倾斜盖板结构的好.整流栅足够长时可以调整流动、提高气膜冷却效率.

     

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出版历程
  • 收稿日期:  2014-07-29
  • 刊出日期:  2016-04-28

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