Fatigue crack growth behavior of beta-annealed Ti–6Al–2Sn–4Zr–xMo (x=2, 4 and 6) alloys: Influence of microstructure and stress ratio

•Attempt to experimentally separate the effects of microstructure and stress ratio on the FCG behavior in three beta-annealed Ti alloys.•Identified the most important microstructural parameter as the alpha/beta colony size which in turn depends strongly on the Mo-content.•An increased stress ratio w...

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Bibliographic Details
Published in:International journal of fatigue 2016-02, Vol.83 (Part 2), p.150-160
Main Authors: Qiu, Jianke, Feng, Xin, Ma, Yingjie, Lei, Jiafeng, Liu, Yuyin, Huang, Aijun, Rugg, David, Yang, Rui
Format: Article
Language:English
Subjects:
Alloys
Colonies
Crack closure
Crack propagation
Fatigue crack growth
Fatigue cracks
Fatigue failure
Fracture mechanics
Microstructure
Stress ratio
Ti624x
Titanium base alloys
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Summary:•Attempt to experimentally separate the effects of microstructure and stress ratio on the FCG behavior in three beta-annealed Ti alloys.•Identified the most important microstructural parameter as the alpha/beta colony size which in turn depends strongly on the Mo-content.•An increased stress ratio was found to reduce the roughness induced crack closure both through larger crack opening levels and through reduced crack deflection.•A prominent transition on the da/dN vs. ΔK plots was observed in the extra-coarse microstructure tested under R=0.1. The influence of microstructures (β grain size, α/β colony size and width of α lath) and stress ratios (R=0.1, 0.7) on fatigue crack growth (FCG) behavior of beta-annealed Ti624x (x=2, 4 and 6) alloys was investigated. The FCG rate curves, crack paths, and the plastic zone ahead of the crack tip were compared. The reducing FCG resistance from Ti6242 to Ti6246 was found to stem from decreasing α/β colony size. Increasing stress ratio also reduced crack deflection and crack closure, and thus decreased the FCG resistance. The relevant mechanisms were discussed in terms of Kmax and crack closure effect.
ISSN:0142-1123
1879-3452
DOI:10.1016/j.ijfatigue.2015.10.009