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The Advanced Cooling Technology for the 1500 °C Class Gas Turbines: The Steam Cooled Vanes and the Air Cooled Blades

机译：1500°C汽轮机的先进冷却技术：蒸汽冷却叶片和空气冷却刀片

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H. Nomoto; A. Koga; S. Ito; Y. Fukuyama; F. Otomo; S. Shibuya; M. Sato; Y. Kobayashi; H. Matsuzaki;
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1. Blade cooling improvement for heavy duty gas turbine: the air coolant temperature reduction and the introduction of steam and mixed steam/air cooling [J] . Bruno Facchini, Giovanni Ferrara, Luca Innocenti International Journal of Thermal Sciences . 2000,第1期

机译：重型燃气轮机叶片冷却的改进：降低空气冷却剂的温度以及引入蒸汽和蒸汽/空气混合冷却
2. MHI sees a future for both steam and all-air cooling: Recently launched gas turbine concepts from MHI include the J-series, a further evolution of its well established steam cooled technology and the M501GAC return to all-air cooling [J] . James Varley Modern Power Systems: Communicating Power Technology Worldwide . 2009,第7期

机译：三菱重工看到蒸汽和全空气冷却的未来：三菱重工最近推出的燃气轮机概念包括J系列，其完善的蒸汽冷却技术的进一步发展以及M501GAC重返全空气冷却
3. Cooling performance analysis of steam cooled gas turbine nozzle guide vane [J] . Wei Wang, Jianmin Gao, Xiaojun Shi, International Journal of Heat and Mass Transfer . 2013,第jula期

机译：汽冷燃气轮机喷嘴导叶的冷却性能分析
4. ADVANCED GAS TURBINE AND HIGH PERFORMANCE GAS-STEAM COMBINED CYCLE PLANT WITH BLADE COOLING AIR CONTROLLING [C] . Tadashi Tsuji ASME(American Society of Mechanical Engineers) Turbo Expo vol.4; 20060506-11; Barcelona(ES) . 2006

机译：先进的燃气轮机和高性能燃气-蒸汽联合循环叶片冷却风系统
5. Comparison of the cooling effectiveness of superheated steam and hot air in internal turbine blade cooling. [D] . Pudupatty, Ramakrishnan Thiruvengadam. 1998

机译：涡轮内部叶片冷却中过热蒸汽和热空气的冷却效果比较。
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. Advanced Gas Turbine and High Performance Gas-Steam Combined Cycle Plant with Blade Cooling Air Controlling. [O] . Tadashi TSUJI, Toshimi TAKAGI, Shinichi KINOSHITA 2002

机译：先进的燃气轮机和高性能气体蒸汽联合循环厂，具有叶片冷却空气控制。
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.

The Advanced Cooling Technology for the 1500 °C Class Gas Turbines: The Steam Cooled Vanes and the Air Cooled Blades

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