涡轮冲击冷却 turbine impingement cooling
Impingement cooling and film cooling could protect blade effectively. Serpentine passage with turbulent ribs enhanced the rotor cooling effect.
冲击冷却和气膜冷却等措施能够有效保证叶片正常工作,蛇形通道加扰流肋片能够提高叶片的冷却效果。
参考来源 - 燃气涡轮复杂结构冷却叶片数值研究·2,447,543篇论文数据，部分数据来源于NoteExpress
对浸没冷却和射流冲击冷却的基本传热特征进行了研究。
The fundamental characteristics of immersion cooling and jet impingement cooling were investigated.
热图像真实地反映出每一股射流的冲击冷却局部换热特征。
The thermal images show truly the features of local heat transfer for each jet impingement cooling.
同时也获得了多股射流冲击冷却的对流换热系数等值线谱图。
The isograms of heat transfer coefficients of impingement cooling are also obtained.
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