航空学报 > 2009, Vol. 30 Issue (5): 825-831

大子午扩张涡轮的分离控制

唐洪飞,颜培刚,黄洪雁,韩万金   

  1. 哈尔滨工业大学 能源科学与工程学院
  • 收稿日期:2008-03-05 修回日期:2008-07-02 出版日期:2009-05-25 发布日期:2009-05-25
  • 通讯作者: 唐洪飞

Flow Separation and Control in Large Meridional Expansion Turbine

Tang Hongfei, Yan Peigang, Huang Hongyan, Han Wanjin   

  1. School of Energy Science and Engineering, Harbin Institute of Technology
  • Received:2008-03-05 Revised:2008-07-02 Online:2009-05-25 Published:2009-05-25
  • Contact: Tang Hongfei

摘要: 大子午扩张涡轮易发生外端壁流动分离,并产生较强顶部二次流。采用对叶型型线外壁和内壁侧逐次前掠宽弦的方法对顶部分离进行控制,并对多个前掠宽弦方案进行全三维数值模拟、流场拓扑分析和流动对比,研究了前掠宽弦叶型在此类涡轮中的应用。结果表明:合理的前掠宽弦叶型能够有效地减弱甚至消除外端壁流动分离,改善顶部压力流向分布;同时也能很好地控制顶部二次流的发展,提高大子午扩张涡轮的气动性能。

关键词: 子午扩张, 低压涡轮, 数值模拟, 前掠宽弦叶型

Abstract: As two common flow characteristics, the upper endwall separation and strong upper endwall secondary flow have great impact on the aerodynamic performance of large meridional expansion turbines. In the present study, forward-swept and wide-chord blade profiles were used to control the upper endwall separation. In blade profiles with different forward-swept and wide-chord schemes, three-dimentional numerical simulation, analysis of flow field topology, as well as comparison of various flow situations were conducted. What’s more, the application potentiality of forward-swept and wide-chord blade profile in the abovementioned turbine was investigated. The results show that with a properlydesigned forward-swept and wide-chord blade profile, the upper endwall separation can be effectively reduced or even eliminated, and then the streamwise pressure distribution at the upper wall can be improved. Meanwhile, the secondary flow at the upper endwall can also be well controlled, and thus the aerodynamic performance of the turbine is optimized.

Key words: meridional expansion, low-pressure turbine, numerical simulation, forward-swept and wide-chord blade profile

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