Failure analysis and damage modeling of precipitate strengthened Cu-Ni-Si alloy under fatigue loading

被引:4
作者
Saadouki, Bouchra [1 ]
Sapanathan, Thaneshan [2 ,3 ]
Pelca, Philipe [4 ]
Elghorba, Mohamed [1 ]
Rachik, Mohamed [2 ]
机构
[1] ENSEM, LCCMMS, Casablanca, Morocco
[2] Univ Technol Compiegne, Sorbonne Univ, CNRS UMR 7337, Lab Roberval,Ctr Rech Royallieu, CS 60319, F-60203 Compiegne, France
[3] Catholic Univ Louvain, Inst Mech Mat & Civil Engn, B-1348 Louvain, Belgium
[4] Lebronzealloys Bornel, 11 Rue Menillet, F-60540 Bornel, France
来源
IGF WORKSHOP FRACTURE AND STRUCTURAL INTEGRITY | 2018年 / 9卷
关键词
Cu-Ni-Si alloy; fatigue; loading levels; cumulative damage; life fraction; MICROSTRUCTURE; BEHAVIOR;
D O I
10.1016/j.prostr.2018.06.029
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Failure analysis and damage evolution in precipitation hardened Cu-2.5Ni-0.6Si alloy are investigated in this study. Firstly, experimental fatigue tests were performed to determine the S-N curve of the material. Then, based on the results of fatigue tests, we have modeled the damage using four linear and cumulative models. The intersection of damage-reliability curves allowed to define three stages of damage during the life cycle for various loading levels. The life fraction Pp reveals the stage of slow crack propagation where a preventive action must be adopted to ensure the proper functioning of the structure. The life fraction Pc corresponds to the stage of sudden crack propagation when the damage becomes uncontrollable. (C) 2018 The Authors. Published by Elsevier B.V.
引用
收藏
页码:186 / 198
页数:13
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