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Influence of Different Steam Cooling Techniques for High Pressure Turbine Blades on the Performance of Gas Turbine

机译：不同蒸汽冷却技术对高压涡轮叶片对燃气轮机性能的影响

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1. The application of novel techniques for gas turbine inlet-cooling that improve both the power and efficiency of the modern commercial steam-air-cooled gas turbine combined cycle power plants in hot and humid climates [J] . Bassily A. M. Proceedings of the Institution of Mechanical Engineers . 2015,第A4期

机译：新技术在燃气轮机进气冷却中的应用，可在炎热和潮湿的气候下提高现代商业蒸汽-风冷燃气轮机联合循环发电厂的功率和效率
2. Influence of slashface leakage coupled with quasi-labyrinth seal technique on gas turbine endwall aerothermal performance and blade suction side surface phantom cooling [J] . Kaiyuan Zhang, Zhigang Li, Jun Li Proceedings of the Institution of Mechanical Engineers . 2021,第3期

机译：斜面泄漏与准迷宫密封技术对燃气涡轮机的燃气涡轮机的空泡性能和叶片吸入侧表面模光冷却的影响
3. Steam turbine injection generator performance estimation considering turbine blade cooling [J] . Nadir Mahmoud, Ghenaiet Adel Energy . 2017,第Auga1期

机译：考虑涡轮叶片冷却的汽轮机喷射发电机性能估算
4. Numerical Investigations on the Steam Cooling Performance of the First Two Middle Pressure Turbine Stages for Ultra-Supercritical Steam Turbines [C] . Wenhao HUO, Jun LI, Xin YAN, ASME turbo expo . 2012

机译：超超临界汽轮机前两个中压涡轮级蒸汽冷却性能的数值研究
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. The Influence of the Cooling Bores on Crystal Orientation and Lattice Parameter in Single-Crystalline Cored Turbine Blades [O] . Jacek Krawczyk, Włodzimierz Bogdanowicz, Jan Sieniawski 2021

机译：冷却孔对单晶芯片叶片晶体取向和晶格参数的影响
7. Discussion: “A Comparative Study of the Influence of Different Means of Cooling on the Performance of a Combined (Gas and Steam Turbine) Cycle” (Wu, Chuan shao, and Louis, J. F., 1984, ASME J. Eng. Gas Turbines Power, 106, pp. 750–755) [O] . I. G. Rice 1985

机译：讨论：“不同冷却手段对组合（气体和汽轮机）循环性能的影响的对比研究”（吴，川邵，Louis，JF，1984，Asme J. Eng。燃气轮机功率， 106，pp。750-755）
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.

Influence of Different Steam Cooling Techniques for High Pressure Turbine Blades on the Performance of Gas Turbine

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