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Environment effect on internal fatigue crack propagation studied with in-situ X-ray microtomography
被引:7
|作者:
Hebrard, Louis
[1
]
Buffiere, Jean-Yves
[1
]
Palin-Luc, Thierry
[2
,3
]
Ranc, Nicolas
[4
]
Majkut, Marta
[1
,5
]
King, Andrew
[6
]
Weck, Arnaud
[7
,8
,9
]
机构:
[1] Univ Lyon, INSA Lyon, MATEIS, CNRS,UMR 5510, F-69621 Villeurbanne, France
[2] Univ Bordeaux, CNRS, Bordeaux INP, I2M,UMR 5295, F-33400 Talence, France
[3] Hesam Univ, Arts & Metiers Inst Technol, CNRS, Bordeaux INP,I2M,UMR 5295, F-33400 Talence, France
[4] HESAM Univ, Arts & Metiers Inst Technol, PIMM Lab, CNRS,Cnam, 151 Blvd lHop, F-75013 Paris, France
[5] ESRF European Synchrotron, 71 Ave Martyrs,BP 220, F-38043 Grenoble 9, France
[6] LOrme Merisiers St Aubin, Synchrotron SOLEIL, F-91192 Gif Sur Yvette, France
[7] Univ Ottawa, Dept Mech Engn, 161 Louis Pasteur, Ottawa, ON K1N 6N5, Canada
[8] Univ Ottawa, Ctr Res Photon, 25 Templeton, Ottawa, ON K1N 6N5, Canada
[9] Univ Ottawa, Dept Phys, 150 Louis Pasteur, Ottawa, ON K1N 6N5, Canada
来源:
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING
|
2023年
/
882卷
关键词:
Fatigue;
Internal crack;
Environment;
Synchrotron;
Ultrasonic;
Short crack;
HIGH-CYCLE FATIGUE;
TITANIUM-ALLOY;
STRESS RATIO;
TI-6AL-4V;
INITIATION;
BEHAVIOR;
GROWTH;
MECHANISM;
FAILURE;
THERMOGRAPHY;
D O I:
10.1016/j.msea.2023.145462
中图分类号:
TB3 [工程材料学];
学科分类号:
0805 ;
080502 ;
摘要:
In the present study, physically short fatigue cracks initiated from an artificial internal notch under vacuum conditions are observed in smooth specimens made of titanium alloy. The crack initiated from such a notch is not in contact with the surface during the majority of its propagation. Another batch of artificially notched specimens in the same alloy having their internal notch linked with the surface to bring air to the initiated short crack were tested too. All the specimens were ultrasonically cycled with synchrotron micro-computed tomography acquisitions which were regularly acquired from crack initiation detection to final failure without demounting the specimen. The number of cycles to failure, the internal crack growth rate and the crack growth mechanisms of internal cracks are compared for propagation under either air conditions or in the core of the alloy (i.e. under vacuum environment). It is shown that the environment plays a key role in the explanation of the very low crack growth rate of internal short crack loaded at very low stress amplitude leading to the gigacycle regime.
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页数:13
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