Investigation of the Cooled Stator Blade of the First Stage of the GTN-25 Gas Turbine.

被引：0
|
作者：
Zolotogorov, M.S.
Korenevevskii, L.G.
Nosovitskii, L.Sh.
Temirov, A.M.
机构：
来源：
Energomashinostroenie | 1982年 / 12期
关键词：
NATURAL GAS PIPELINES - Compressor Stations;
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学科分类号：
摘要：
An increase in the initial gas temperature to 900 degree C before the turbine of the GTN-25 gas pumping unit has necessitated the cooling of the stator blades of the high-pressure turbine. The hollow blade air cooling system is described. Tests at gas temperatures of 800-1050 degree C and cooling air temperatures of 120 to 410 degree C were carried out and results are presented. It is shown that even at 1000 degree C gas temperatures the cooled blade temperatures do not exceed 870 degree C, which is acceptable with corrosion-resistant coatings.
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页码：15 / 19
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