Fatigue crack tip strain evolution and crack growth prediction under single overload in laser melting deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si titanium alloy

被引:20
作者
Wu, Yanzeng [1 ]
Bao, Rui [1 ]
机构
[1] Beihang Univ, Inst Solid Mech, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Crack tip strain field; Overload; Fatigue crack growth; Laser melting deposition; Digital image correlation; DIGITAL IMAGE CORRELATION; MECHANICAL-PROPERTIES; DISPLACEMENT-FIELDS; STRESS; RETARDATION; TI-6AL-4V; PROPAGATION; CLOSURE; MICROSTRUCTURE; DEFORMATION;
D O I
10.1016/j.ijfatigue.2018.07.011
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper focuses on the fatigue crack tip strain evolution in laser melting deposited Ti-6.5Al-3.5Mo-1.5Zr-0.3Si titanium alloy under constant amplitude loading plus single overload (OL). The digital image correlation (DIC) technique was used to capture and evaluate the crack tip strain fields and crack closure variation; the results showed that the strains near the crack tip become larger and the crack opening load increases after the application of the OL. The size of the retardation distance is consistent with the analysis results of the crack tip strain fields. The crack closure model based on the DIC analysis results can provide good predictions of the crack growth life for both the low and high overload ratios.
引用
收藏
页码:462 / 472
页数:11
相关论文
共 45 条
[1]  
[Anonymous], 2013, ASTM13
[2]   Effect of crack closure on non-linear crack tip parameters [J].
Antunes, F. V. ;
Sousa, T. ;
Branco, R. ;
Correia, L. .
INTERNATIONAL JOURNAL OF FATIGUE, 2015, 71 :53-63
[3]   Perspectives on Titanium Science and Technology [J].
Banerjee, Dipankar ;
Williams, J. C. .
ACTA MATERIALIA, 2013, 61 (03) :844-879
[4]  
Bathias C., 2010, FATIGUE MAT STRUCTUR
[5]   Low- and high-cycle fatigue resistance of Ti-6Al-4V ELI additively manufactured via selective laser melting: Mean stress and defect sensitivity [J].
Benedetti, M. ;
Fontanari, V. ;
Bandini, M. ;
Zanini, F. ;
Carmignato, S. .
INTERNATIONAL JOURNAL OF FATIGUE, 2018, 107 :96-109
[6]   Crack propagation and fracture toughness of Ti6A14V alloy produced by selective laser melting [J].
Cain, V ;
Thijs, L. ;
Van Humbeeck, J. ;
Van Hooreweder, B. ;
Knutsen, R. .
ADDITIVE MANUFACTURING, 2015, 5 :68-76
[7]  
Elber W., 1970, Engineering Fracture Mechanics, V2, P37, DOI 10.1016/0013-7944(70)90028-7
[8]   Fatigue performance of additive manufactured TiAl6V4 using electron and laser beam melting [J].
Greitemeier, Daniel ;
Palm, Frank ;
Syassen, Freerk ;
Melz, Tobias .
INTERNATIONAL JOURNAL OF FATIGUE, 2017, 94 :211-217
[9]  
Irwin GR., 2021, J APPL MECH, V24, P361, DOI [DOI 10.1115/1.4011547, 10.1115/1.4011547]
[10]   Crack tip deformation fields and fatigue crack growth rates in Ti-6Al-4V [J].
Korsunsky, Alexander M. ;
Song, Xu ;
Belnoue, Jonathan ;
Jun, Terry ;
Hofmann, Felix ;
De Matos, Paulo F. P. ;
Nowell, David ;
Dini, Daniele ;
Aparicio-Blanco, Olivier ;
Walsh, Michael J. .
INTERNATIONAL JOURNAL OF FATIGUE, 2009, 31 (11-12) :1771-1779