Material testing for fatigue design of heavy-duty gas turbine blading with film cooling

被引：0

作者：

Pan, Y ^{[1
]}

Bischoff-Beiermann, B ^{[1
]}

Schulenberg, T ^{[1
]}

机构：

[1] Siemens AG, Power Generat Grp, KWU, Mulheim, Germany

来源：

FATIGUE DESIGN 1998, VOL II | 1998年 / 182卷

关键词：

heavy-duty gas turbine; film cooling hole; low cycle fatigue; fatigue life; FE-calculation;

D O I：

暂无

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Heavy-duty gas turbine blades, which contain film cooling holes, are subjected to a complicated dynamic mechanical loading. Special material tests have been developed to ensure the long-term operational reliability of the blading. This paper presents results of the testing and appropriate finite element (FE-) calculations, showing that a reliable fatigue life assessment can be achieved with the local approach concept.

引用

页码：433 / 440

页数：8

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