COOLED TURBINE BLADES IN THE GTE-65 GAS TURBINE POWER UNIT

V. V. Rtishchev; V. V. Krivonosova; Yu. M. Sundukov; V. E. Mikhailov; M. S. Zolotogorov

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COOLED TURBINE BLADES IN THE GTE-65 GAS TURBINE POWER UNIT

机译：GTE-65燃气轮机动力装置中的冷却涡轮叶片

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摘要

Experience with the development, study, and manufacturing of cooled blades for the GTE-65 high temperature gas turbine is described.

机译：描述了开发，研究和制造用于GTE-65高温燃气轮机的冷却叶片的经验。

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来源
《Power technology and engineering》 |2009年第6期|P.376-381|共6页
作者
V. V. Rtishchev; V. V. Krivonosova; Yu. M. Sundukov; V. E. Mikhailov; M. S. Zolotogorov;
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作者单位

'Lcningradskii metallicheskii zavod' (Leningrad Metals Plant), Branch of JSC 'Silovye mashiny,' St. Petersburg, Russia;

rn'Lcningradskii metallicheskii zavod' (Leningrad Metals Plant), Branch of JSC 'Silovye mashiny,' St. Petersburg, Russia;

rn'Lcningradskii metallicheskii zavod' (Leningrad Metals Plant), Branch of JSC 'Silovye mashiny,' St. Petersburg, Russia;

rnJSC 'NPO TsKTI,' St. Petersburg, Russia;

rnJSC 'NPO TsKTI,' St. Petersburg, Russia;

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原文格式 PDF
正文语种 eng
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关键词
gas turbine unit; high temperature gas turbine; turbine blades; thermal-hydraulic testing;

机译：燃气轮机高温燃气轮机涡轮叶片;热工液压测试;

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专利

1. The Cooled Blade Assembly for the First Three Stages of the High-Temperature Turbine of a GTE-65 Medium-Capacity Gas-Turbine Power-Generating Unit [J] . A. S. Lebedev, Yu. M. Sundukov, V. V. Krivonosova Thermal engineering . 2007,第10期

机译：GTE-65中型燃气轮发电机组高温涡轮前三级冷却叶片组件
2. Experimental-Calculation Investigations of the Cooled Blades of the GTE-65 Gas-Turbine Unit [J] . L. A. Khomenok, M. S. Zolotogorov, A. G. Nikolaev, Thermal engineering . 2008,第1期

机译：GTE-65燃气轮机冷却叶片的实验计算研究
3. 90-MW SINGLE-SHAFT POWER GENERATING STEAM-GAS UNIT BASED ON THE GTE-65 GAS TURBINE AND K-30-60 STEAM TURBINE [J] . A. S. Lebedev, O. V. Antonyuk, V. A. Martyanov, Hydrotechnical Construction . 2011,第5期

机译：基于GTE-65燃气轮机和K-30-60汽轮机的90兆瓦单轴发电燃气装置
4. EXPLORING THE IMPACT OF ELEVATED TURBINE BLADE COOLING EFFECTIVENESS AND TURBINE MATERIAL TEMPERATURES ON GAS TURBINE ENGINE PERFORMANCE AND COST [C] . Aaron R. Byerley, August J. Rolling ASME turbo expo: turbine technical conference and exposition . 2015

机译：探讨涡轮叶片冷却效率和涡轮材料温度对燃气轮机性能和成本的影响
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: “Effect of New Blade Cooling System With Minimized Gas Temperature Dilution on Gas Turbine Performance” (Kawaike, K., Kobayashi, N., and Ikeguchi, T., 1984, ASME J. Eng. Gas Turbines Power, 106, pp. 756–764) [O] . I. G. Rice 1985

机译：讨论：“新叶片冷却系统对燃气轮机性能最小化气体温度稀释的影响”（Kawaike，K.，Kobayashi，N.和Ikeguchi，T.，1984，Asme J. Eng。燃气轮机电源，106，PP 。756-764）
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.

COOLED TURBINE BLADES IN THE GTE-65 GAS TURBINE POWER UNIT

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