期刊文献+

1.5级透平动叶端壁泄漏流换热与冷却研究 被引量:1

Prediction of Heat Transfer and Film Cooling on Blade Platform With Stator-Rotor Purge Flow in a 1-1/2 Turbine Stage
原文传递
导出
摘要 本文数值研究了一级半透平中动静间隙泄漏流对动叶端壁表面换热与冷却的影响,分析了冷气质量流量比、密度比和动叶转速等三个重要因素对动叶端壁表面换热与冷却的作用规律。结果显示,质量流量比和密度比增加会强化端壁上游区域和主通道涡分离线下游区域的换热,但在冷却方面仅在端壁上游区域进一步产生过冷现象而对端壁通道下游的冷却几乎没有任何影响;转速的上升则会削弱端壁换热,并且会抑制通道涡,但对冷气的覆盖面积没有明显的提升作用。 Heat transfer and film cooling on a platform from stator-rotor platform purge flow were numerically investigated in a 1-1/2 turbine stage. The effects of coolant mass flow ratio, coolant-to-mainstream density ratio and rotating speed were examined in detail. The results show that higher mass flow- rates and density ratios could enhance heat transfer level in tile upstream region and the downstream area of the passage vortex lift-off line on the platform, but slightly affected film cooling distributions, particularly in the downstream area. In addition, increasing rotating speed reduced heat transfer over the platform surface. Higher rotating speeds could suppress the passage vortex, but had little effect on film coolant coverage.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2018年第1期62-67,共6页 Journal of Engineering Thermophysics
基金 国家自然科学基金重点项目资助(No.51336007)
关键词 燃气透平端壁 泄漏流 旋转 换热冷却 数值模拟 gas turbine endwall purge flow rotating heat transfer and film cooling numericalsimulation
  • 相关文献

同被引文献6

引证文献1

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部