蠕动
燃气轮机
涡轮叶片
本构方程
压力(语言学)
材料科学
机械
阶段(地层学)
结构工程
涡轮机
机械工程
工程类
复合材料
地质学
物理
有限元法
哲学
古生物学
语言学
作者
Zhu Jiang-jiang,Zichun Yang
标识
DOI:10.1109/appeec.2010.5448719
摘要
A creep life model of the blade has been studied out of consideration for scientific management of gas turbine. The paper has studied creep constitutive equation alternatively for each creep stage based on the classical creep curve. It has been find that there is no the second stage of creep when material under the condition of higher stress. Then judgment criterion has been proposed to deal with that phenomenon. Different creep constitutive equations of coupled damage have been derived for different stress level .Finally, comparison of experimental results with creep model has been made to validate it.
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