The GTE-65 gas turbine unit: Rig tests of the main components, possibilities of use and lines of further improvement

被引:0
|
作者
Lebedev A.S. [1 ]
Simin N.O. [1 ]
Petrenya Yu.K. [2 ]
Mikhailov V.E. [2 ]
机构
[1] Leningrad Metal Works (LMZ), OAO Silovye Mashiny, St. Petersburg 195009
[2] Central Boiler-Turbine Institute Research and Production Association (OAO NPO TsKTI), St. Petersburg 191167
关键词
Combustion Chamber; Rotor Blade; Guide Vane; CCPs; Model Compressor;
D O I
10.1134/S0040601508040095
中图分类号
学科分类号
摘要
This paper is a continuation of publication [1] on the project of a GTE-65 medium-capacity power-generating gas-turbine unit and describes rig tests of its components: the compressor, the turbine's cooled blades, and the combustion chamber. Alternative versions for possible use of the GTE-65 unit in the schemes of combined-cycle plants and its further improvement are described. © 2008 MAIK Nauka.
引用
收藏
页码:319 / 324
页数:5
相关论文
共 5 条
  • [1] The Project of a GTE-65 Power-Generating Gas-Turbine Unit
    A. S. Lebedev
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    [J]. Thermal Engineering, 2008, 55 (1) : 54 - 61
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    Central Boiler-Turbine Institute Research and Production Association , ul. Atamanskaya 3/6, St. Petersburg 191167, Russia
    不详
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    [J]. Thermal Engineering, 2008, 55 (1) : 50 - 53
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