Insights into thermomechanical fatigue behavior of nitrogen alloyed 316LN stainless steel under various temperature cycling ranges

被引:3
作者
Zheng, Yiming [1 ]
Li, Bingbing [1 ]
Yang, Jingyu [1 ]
Zhang, Zhe [1 ]
Chen, Xu [1 ,2 ,3 ,4 ]
机构
[1] Tianjin Univ, Sch Chem Engn & Technol, Tianjin 300072, Peoples R China
[2] Tianjin Key Lab Chem Proc Safety & Equipment Techn, Tianjin 300072, Peoples R China
[3] State Key Lab Chem Engn, Tianjin 300072, Peoples R China
[4] Zhejiang Inst Tianjin Univ, Zhejiang Inst, Ningbo 315201, Zhejiang, Peoples R China
来源
JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T | 2024年 / 29卷
关键词
316LN stainless steel; Thermomechanical fatigue; Dynamic strain aging; Damage mechanism; Fatigue life; DEFORMATION; PREDICTION; MECHANISM; EVOLUTION; DAMAGE; PHASE;
D O I
10.1016/j.jmrt.2024.02.112
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Thermomechanical fatigue (TMF) failure has become one of the most important life-limiting factors of components exposure to the high temperature in the fourth-generation sodium-cooled fast reactor (SFR) nuclear power plant. Therefore, TMF tests at different temperature cycling ranges are performed to study the cyclic deformation behavior and damage mechanism of a nitrogen alloyed 316LN stainless steel. Moreover, the isothermal fatigue (IF) tests at the maximum temperature of TMF cycling are conducted for comparison. The cyclic hardening and softening response are analyzed, taking into account the phenomenon of dynamic strain aging which occurs at the temperature range of 350 degrees C-650 degrees C. Furthermore, the critical strain corresponding to the occurrence of serrated stress flow in engineering stress-strain curves keeps decreasing from 28.94% at 350 degrees C to 0.09% at 650 degrees C. The distribution of plastic deformation and the degree of strain localization are evaluated by the characterization results of kernel average misorientation map, high/low angle grain boundary map and dislocation configuration. The dominant damage mechanism and its corresponding cracking behavior in both IF and TMF tests are analyzed based on the observation of fracture surface morphology. In addition, the sequence order of fatigue life is determined as IF < IP-TMF < OP-TMF. Moreover, the maximum difference of fatigue life between IF test and TMF test occurs at the temperature range of 400 degrees C-600 degrees C, in which the IP and OP life is about 2.91 and 3.65 times larger than the IF life. The results in this work provide reliable data support and theoretical guidance for the fatigue design of high-temperature components in SFR.
引用
收藏
页码:3990 / 4003
页数:14
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