High temperature effects on fatigue performance and crack initiation mechanisms of 316LN stainless steel for nuclear power pipelines

被引:0
|
作者
Zheng, Jianneng [1 ]
Hu, Junchao [2 ,4 ]
Jiang, Yuehui [3 ]
Wang, Qingyuan [2 ,3 ,4 ]
Yang, Kun [2 ,3 ,4 ]
机构
[1] Erzhong Deyang Heavy Equipment Co Ltd, Natl Engn Res Ctr Adv Mfg Technol & Equipment Heav, Deyang 618000, Peoples R China
[2] Sichuan Univ, Failure Mech & Engn Disaster Prevent Key Lab Sichu, Chengdu 610065, Peoples R China
[3] Chengdu Univ, Inst Adv Study, Sch Mech Engn, Chengdu 610106, Peoples R China
[4] Sichuan Univ, Key Lab Deep Earth Sci & Engn, Minist Educ, Chengdu 610065, Peoples R China
来源
JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T | 2025年 / 35卷
基金
中国国家自然科学基金;
关键词
316LN austenitic stainless steel; High temperature; Tensile behavior; High cycle fatigue (HCF) property; Fatigue crack initiation mechanism; LOW-CYCLE FATIGUE; BEHAVIOR; DISLOCATIONS; DEFORMATION; ALLOY; LIFE;
D O I
10.1016/j.jmrt.2025.02.041
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study performed high-cycle fatigue tests on 316LN stainless steel (SS) for nuclear power application to evaluate its fatigue behavior at both room temperature (RT) and 350 degrees C. Moreover, its microstructural features and fatigue crack nucleation mechanisms were further studied. It was found that fatigue crack initiation predominantly occurs at the SS specimen surface. At RT, microcrack initiation modes include both transgranular and intragranular mechanisms, with the {100} slip plane contributing to crack initiation alongside the preferential {111} slip plane. At 350 degrees C, the crack initiation mode shifts primarily to intragranular mechanisms, with active slip planes identified as {111} and {110}.
引用
收藏
页码:3281 / 3292
页数:12
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