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CONJUGATE HEAT TRANSFER INVESTIGATION ON COOLING PERFORMANCE OF AIR-COOLED TURBINE STATOR BLADE

机译：空冷汽轮机定子叶片冷却性能的共轭传热研究

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《Jilin Institute of Chemical Technology;International Conference on New Materials and Intelligent Manufacturing;International Engineering and Technology Institute》||31-35|共5页
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作者
Su Li-chao; Shi Jing-cheng; Zhang Jing-yu; Huang Yong-hui;
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中图分类工程材料学;
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机译：用共轭传热技术研究热障涂层非膜冷式涡轮叶片的冷却性能
3. Prediction of Film Cooling and Heat Transfer on a Rotating Blade Platform With Stator-Rotor Purge and Discrete Film-Hole Flows in a 1-1/2 Turbine Stage [J] . H. Yang, Z. Gao, H. C. Chen, Journal of turbomachinery . 2009,第4期

机译：在1-1 / 2涡轮级中利用定子-转子吹扫和离散的膜孔流量在旋转叶片平台上预测膜的冷却和传热
4. CONJUGATE HEAT TRANSFER INVESTIGATION ON COOLING PERFORMANCE OF AIR-COOLED TURBINE STATOR BLADE [C] . Su Li-chao, Shi Jing-cheng, Zhang Jing-yu, International Conference on New Materials and Intelligent Manufacturing . 2018

机译：缀合热传递调查空气冷却汽轮机定子叶片的冷却性能
5. An experimental investigation of turbine blade heat transfer and turbine blade trailing edge cooling. [D] . Choi, Jungho. 2004

机译：涡轮叶片传热和涡轮叶片后缘冷却的实验研究。
6. Conjugate Heat Transfer Investigation on Swirl-Film Cooling at the Leading Edge of a Gas Turbine Vane [O] . Haifen Du, Ziyue Mei, Jiayao Zou, 2019

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7. An experimental investigation of turbine blade heat transfer and turbine blade trailing edge cooling [O] . Choi Jungho 2005

机译：涡轮叶片传热和叶片后缘冷却的实验研究
8. Investigations on an Experimental Air-Cooled Turbine Part Ⅲ.—the Effects of Cooling on the Overall Turbine Aerodynamic Performance and Initial Operation at an Inlet Gas Temperature of 140° deg K PartⅣ.—Examination of Sintered Vitallium Air-Cooled Turbine Blades Following 100 Hours' Operation at a Turbine Inlet Mean Gas Temperature of 1400 deg K [R] . N. E. WALDREN, C. J. HART, D. E. FRAY 1960

机译：实验风冷涡轮机的研究Ⅲ。冷却对整体涡轮气动性能和入口气体温度140°K时的初始运行的影响第四部分 - 100小时后烧结的Vitallium空冷涡轮叶片的检查'在涡轮机入口处的操作平均气体温度为1400度K.

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