3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes

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3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes

机译：高压涡轮机带有“经络收缩”和“经络”和悠闲扇形薄膜冷却孔的喷嘴叶片平台薄膜冷却效能研究

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As the result of ANSYS CFX calculation, a conclusion was drawn about the greater cooling effectiveness of vane platform with laidback fan-shaped perforation holes as compared with cooling effectiveness of vane platform with cylindrical holes.

机译：随着ANSYS CFX计算的结果，与曲线孔的冷却效能相比，朝向扇形穿孔孔的叶片平台的较大冷却效能绘制了结论。

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《Russian Aeronautics》 |2019年第3期|共8页
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正文语种 eng
中图分类航空;
关键词
vane platform; cooling effectiveness; nozzle set; high pressure turbine; gas turbine engine;

机译：叶片平台;冷却效果;喷嘴组;高压涡轮机;燃气轮机发动机;

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1. 3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes [J] . Russian Aeronautics . 2019,第3期

机译：高压涡轮机带有“经络收缩”和“经络”和悠闲扇形薄膜冷却孔的喷嘴叶片平台薄膜冷却效能研究
2. The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes [J] . Yu. G. Gorelov, K. V. Tyul’kov Russian Aeronautics . 2018,第1期

机译：涡轮喷嘴叶片薄膜冷却效能的3D计算研究，“经络收缩”和成型薄膜冷却孔
3. 3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling [J] . Yu. G. Gorelov, V. V. Anan’ev Russian Aeronautics . 2018,第3期

机译：高压涡轮叶片平台对流冷却和对流膜冷却的3D研究
4. SHAPE OPTIMIZATION OF A LAIDBACK FAN-SHAPED FILM-COOLING HOLE TO ENHANCE COOLING PERFORMANCE [C] . Ki-Don Lee, Kwang-Yong Kim ASME turbo expo . 2011

机译：倾斜式扇形薄膜冷却孔的形状优化，可提高冷却性能
5. A detailed study of fan-shaped film-cooling for a nozzle guide vane for an industrial gas turbine. [D] . Colban, William F., IV. 2005

机译：对用于工业燃气轮机的喷嘴导向叶片的扇形薄膜冷却的详细研究。
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

机译：燃气轮机叶片前缘旋流膜冷却的共轭传热研究
7. The Influence of Film-Cooling on the Aerodynamic Performance of a Turbine Nozzle Guide Vane [O] . C. Osnaghi, A. Perdichizzi, M. Savini, 1997

机译：薄膜冷却对涡轮喷嘴导向叶片空气动力学性能的影响

3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes

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