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Gas turbine performance enhancement via utilizing different integrated turbine inlet cooling techniques

机译：利用不同的集成式涡轮进口冷却技术提高燃气轮机性能

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El-Shazly Alaa A.; Elhelw Mohamed; Sorour Medhat M.; El-Maghlany Wael M.;
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1. Performance improvement of gas turbine power plants by utilizing turbine inlet air-cooling (TIAC) technologies in Riyadh, Saudi Arabia [J] . Baakeem Saleh S., Orfi Jamel, Al-Ansary Hany Applied thermal engineering: Design, processes, equipment, economics . 2018,第期

机译：利用沙特阿拉伯利雅得汽轮机入口空气冷却（TIAC）技术通过汽轮机发电厂的性能改进
2. 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
3. Enhancing micro gas turbine performance in hot climates through inlet air cooling vapour compression technique [J] . Comodi G., Renzi M., Caresana F., Applied Energy . 2015,第juna1期

机译：通过进气冷却蒸汽压缩技术提高炎热气候下的微型燃气轮机性能
4. GAS TURBINE PERFORMANCE ENHANCEMENT BY INLET AIR COOLING AND COOLANT PRE-COOLING USING AN ABSORPTION CHILLER [C] . Hyun Min Kwon, Jeong Ho Kim, Tong Seop Kim ASME turbo expo: turbine technical conference and exposition . 2016

机译：使用吸收式冷却器通过进气冷却和冷却剂预冷却来提高燃气轮机性能
5. An investigation of river kinetic turbines: Performance enhancements, turbine modelling techniques, and an assessment of turbulence models. [D] . Gaden, David L. F. 2007

机译：对河流动力涡轮机的研究：性能增强，涡轮机建模技术以及湍流模型评估。
6. Comparative Evaluation of Integrated Waste Heat Utilization Systems for Coal-Fired Power Plants Based on In-Depth Boiler-Turbine Integration and Organic Rankine Cycle [O] . Shengwei Huang, Chengzhou Li, Tianyu Tan, 2018

机译：基于深入锅炉 - 汽轮机集成和有机朗肯循环的燃煤发电厂综合废热利用系统对比较评价
7. Gas turbine performance enhancement via utilizing different integrated turbine inlet cooling techniques [O] . Alaa A. El-Shazly, Mohamed Elhelw, Medhat M. Sorour, 2016

机译：通过利用不同的集成涡轮机入口冷却技术提高燃气轮机性能
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.

Gas turbine performance enhancement via utilizing different integrated turbine inlet cooling techniques

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