期刊
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES
卷 29, 期 1, 页码 11-22出版社
WILEY-BLACKWELL
DOI: 10.1111/j.1460-2695.2006.00950.x
关键词
crack growth; directionally solidified; fatigue; gas turbine; nickel-base superalloy
GTD-111 is a General Electric proprietary nickel-base superalloy widely employed in a growing fleet of industrial gas turbines. However, much of the published research to date has focused on creep damage and coating durability, with no available data on fatigue crack growth rate (FCGR). Accordingly, FCGR has been measured at several load ratios and an elevated temperature, 760 degrees C (1400 degrees F) corresponding to typical turbine bucket conditions. In order to account for load ratio effect, several different methods for determining Walker model parameters are discussed in terms of methodological consistency and accuracy.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据