航空学报 > 2007, Vol. 28 Issue (3): 540-544

旋转状态下曲率对气膜冷却影响的分析

杨晓军,陶智,丁水汀,徐国强,罗翔   

  1. 北京航空航天大学 能源与动力工程学院 航空发动机气动热力重点实验室
  • 收稿日期:2006-04-27 修回日期:2007-04-09 出版日期:2007-05-10 发布日期:2007-05-10
  • 通讯作者: 杨晓军

Analysis of Curvature Effects on the Film Cooling Under the Rotation Frame

YANG Xiao-jun,TAO Zhi,DING Shui-ting,XU Guo-qiang,LUO Xiang   

  1. National Key Laboratory on Aeroengines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
  • Received:2006-04-27 Revised:2007-04-09 Online:2007-05-10 Published:2007-05-10
  • Contact: YANG Xiaojun

摘要:

作为广泛应用于航空发动机涡轮叶片上的气膜冷却技术,其效果会受到叶片表面曲率、旋转、密度比等因素的影响。在通过理论分析着重研究了旋转状态下曲面上的气膜出流后,给出了评价曲面气膜出流受旋转速度影响的无量纲量局部旋转数。并且对各种影响因素进行了分析。在凸表面上,小局部旋转数会导致气膜趋于脱离壁面;大局部旋转数会使气膜趋于吸附壁面;对于凹表面,局部旋转数的影响正好相反。当局部旋转数很小时,动量流量比成为影响气膜出流脱离壁面与否的重要因素。文中并且给出了数值验证。

关键词: 旋转, 曲率, 气膜冷却, 旋转数, 动量流量比,

Abstract:

A theoretical analysis was carried out to comprehend the mechanism of the rotation and curvature effects on the film cooling which is important in understanding the mixing process between the film coolant and the hot stream air over the high pressure turbine blade. Under the rotation frame, the effects of curvature on film cooling effectiveness can be explained by determining whether the injected fluid moves closer or further from the wall surface.

Key words: rotation,  , curvature,  , film , cooling,  , rotational , number,  , momentum , flux , ratio

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