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动静干涉对涡轮转子叶片气膜冷却的影响

李虹杨 郑赟

李虹杨, 郑赟. 动静干涉对涡轮转子叶片气膜冷却的影响[J]. 北京航空航天大学学报, 2016, 42(1): 139-146. doi: 10.13700/j.bh.1001-5965.2015.0054
引用本文: 李虹杨, 郑赟. 动静干涉对涡轮转子叶片气膜冷却的影响[J]. 北京航空航天大学学报, 2016, 42(1): 139-146. doi: 10.13700/j.bh.1001-5965.2015.0054
LI Hongyang, ZHENG Yun. Effect of rotor-stator interaction on film-cooling of turbine blade[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 139-146. doi: 10.13700/j.bh.1001-5965.2015.0054(in Chinese)
Citation: LI Hongyang, ZHENG Yun. Effect of rotor-stator interaction on film-cooling of turbine blade[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1): 139-146. doi: 10.13700/j.bh.1001-5965.2015.0054(in Chinese)

动静干涉对涡轮转子叶片气膜冷却的影响

doi: 10.13700/j.bh.1001-5965.2015.0054
详细信息
    作者简介:

    李虹杨男,博士研究生。主要研究方向:流、热耦合数值模拟,转捩预测及仿真。E-mail:buaalihy@hotmail.edu.cn;郑赟男,博士,讲师。主要研究方向:计算流体力学,叶轮机流、热、固耦合仿真,航空发动机叶片振动数值仿真。Tel.:010-82338753E-mail:zheng_yun@buaa.edu.cn

    通讯作者:

    郑赟,Tel.:010-82338753E-mail:zheng_yun@buaa.edu.cn

  • 中图分类号: V211.6

Effect of rotor-stator interaction on film-cooling of turbine blade

  • 摘要: 为研究动静干涉对涡轮转子叶片气膜冷却效果的影响,选取AGTB涡轮叶栅作为研究对象,匹配前排导叶并对整级叶栅进行非定常数值模拟。对不同时刻流场截面的流动情况以及叶片表面温度随时间的演化规律进行了详细的分析,此外,总结了尾迹和势干涉对下游叶片气膜冷却的影响。主要结论如下:导叶强烈的势干涉作用在幅值为12°的范围内改变下游叶片的入射角,对冷却射流有非常大的影响;尾迹和势干涉作用诱导冷却射流的"上扬"现象,并使其冷气流量增加20%以上,有利于提高瞬时的冷却效果;势干涉对前缘冷却射流的作用时间约为1/2个静子周期,尾迹的作用时间约为1/6个静子周期,前者作用时间长,且效果更强。受到输运效果的影响,整个叶片冷却效果的变化与气膜孔射流状态的变化不是同步的,滞后时间可达1/3个静子周期甚至更长。

     

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出版历程
  • 收稿日期:  2015-01-26
  • 网络出版日期:  2016-01-20

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