Detailed Thermometry of Flow Paths of Cooled Gas Turbines as a Way to Increase Their Technical and Economical Efficiency

I. L. Osipov

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Detailed Thermometry of Flow Paths of Cooled Gas Turbines as a Way to Increase Their Technical and Economical Efficiency

机译：冷却燃气轮机流路的详细测温，以提高其技术和经济效率

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摘要

It is shown what technical and economical gain can be obtained by reducing the cooling-air flowrate in modern high-temperature gas turbines. The conclusion is drawn that such a reduction in the coolant flowrate can be accomplished after thorough thermometrie analysis of the turbine flow path.

机译：它显示了通过降低现代高温燃气轮机中的冷却空气流量可以获得什么技术和经济收益。得出的结论是，在对涡轮机流动路径进行全面的热计量分析之后，可以实现冷却剂流量的这种降低。

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《Thermal engineering》 |2008年第6期|p.469-472|共4页
作者
I. L. Osipov;
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作者单位

Federal State Unitary Enterprise Salut Moscow Machine Building Works (FGUP MMPP Salut), pr. Budyonnogo 16, Moscow, 105118 Russia;

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正文语种 eng
中图分类发电、发电厂;
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1. Coordinated optimization of the parameters of the cooled gas-turbine flow path and the parameters of gas-turbine cycles and combined-cycle power plants [J] . A.M. Kler, Yu.B. Zakharov, Yu.M. Potanina Thermophysics and Aeromechanics . 2014,第3期

机译：冷却后的燃气轮机流路参数与燃气轮机循环及联合循环电厂参数的协调优化
2. An Investigation of Turbine Wheelspace Cooling Flow Interactions With a Transonic Hot Gas Path-Part II: CFD Simulations [J] . G. M. Laskowski, R. S. Bunker, J. C. Bailey, Journal of turbomachinery . 2011,第4期

机译：跨音速热气路径对涡轮机叶轮空间冷却流相互作用的研究-第二部分：CFD模拟
3. An Investigation of Turbine Wheelspace Cooling Flow Interactions With a Transonic Hot Gas Path-Part 1: Experimental Measurements [J] . R. S. Bunker, G. M. Laskowski, J. C. Bailey, Journal of turbomachinery . 2011,第2期

机译：跨音速热气路径对涡轮机叶轮空间冷却流相互作用的研究-第1部分：实验测量
4. TECHNICAL AND ECONOMICAL FEASIBILITY OF GAS TURBINE INLET COOLING USING EVAPORATIVE FOGGING SYSTEM IN TWO DIFFERENT LOCATIONS IN OMAN [C] . Yousef H. Zurigat, Belal Dawoud, Jamal N. Al-Bortmany, American Society of Mechanical Engineers(ASME) Turbo Expo vol.4; 20040614-17; Vienna(AT) . 2004

机译：在阿曼的两个不同地点使用蒸发雾化系统进行燃气轮机进气冷却的技术和经济可行性
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

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7. Study and Comparison of Inlet Air Cooling Technique of Gas Turbines and Their Effects on Increase of the Efficiency and Outlet Power [O] . Seyed Ali Sakhaei, Mahbod Safari 2014

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Detailed Thermometry of Flow Paths of Cooled Gas Turbines as a Way to Increase Their Technical and Economical Efficiency

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