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叶身融合技术在涡轮中的应用

田勇 季路成 邵卫卫 肖云汉

田勇, 季路成, 邵卫卫, 肖云汉. 叶身融合技术在涡轮中的应用[J]. 航空动力学报, 2015, 30(12): 2949-2959. doi: 10.13224/j.cnki.jasp.2015.12.019
引用本文: 田勇, 季路成, 邵卫卫, 肖云汉. 叶身融合技术在涡轮中的应用[J]. 航空动力学报, 2015, 30(12): 2949-2959. doi: 10.13224/j.cnki.jasp.2015.12.019
TIAN Yong, JI Lu-cheng, SHAO Wei-wei, XIAO Yun-han. Application of blended blade/endwall in turbines[J]. Journal of Aerospace Power, 2015, 30(12): 2949-2959. doi: 10.13224/j.cnki.jasp.2015.12.019
Citation: TIAN Yong, JI Lu-cheng, SHAO Wei-wei, XIAO Yun-han. Application of blended blade/endwall in turbines[J]. Journal of Aerospace Power, 2015, 30(12): 2949-2959. doi: 10.13224/j.cnki.jasp.2015.12.019

叶身融合技术在涡轮中的应用

doi: 10.13224/j.cnki.jasp.2015.12.019
基金项目: 

国家自然科学基金(51176012,51376023)

详细信息
    作者简介:

    田勇(1985-),男,湖北崇阳人,博士生,研究方向为叶轮机气动热力学.

    通讯作者:

    季路成(1970-),男,山东蓬莱人,教授,博士,研究方向为航空发动机能源动力、叶轮机气动热力学和计算流体力学.E-mail:jilc@bit.edu.cn

  • 中图分类号: V231.3

Application of blended blade/endwall in turbines

  • 摘要: 将叶身融合技术进一步应用于涡轮,探索其技术应用效果.为此,以TTM-stage为原型,施加7种不同的叶身融合模型,并采用数值模拟方法进行了对比研究.结果表明:前缘融合面可削弱马蹄涡;侧融合面可削弱角区分离;对静叶实施融合使动叶进口总温附面层厚度降低,在通道涡作用下高总温流体被部分推离,明显降低了轮毂壁温.

     

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出版历程
  • 收稿日期:  2014-05-07
  • 刊出日期:  2015-12-28

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