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Microstructure stability and damage mechanisms in an α/β Ti-6Al-4V-0.55Fe alloy during low cycle dwell-fatigue at room temperature
International Journal of Fatigue ( IF 5.7 ) Pub Date : 2021-10-07 , DOI: 10.1016/j.ijfatigue.2021.106585
Shan Shi 1 , Qinghua Deng 1 , Hang Zhang 1 , Liang Feng 1 , Xiangjun Xu 2 , Jie Ding 1 , Hui Chang 1 , Lian Zhou 1
Affiliation  

The cyclic behavior and microstructure evolution of Ti-6Al-4V-0.55Fe alloy were investigated with three different total strain amplitudes. A slight softening was occurred with Δεt/2 = 1.20%, and the alloy mainly suffered α recrystallization. Besides, a gentle softening can be observed with Δεt/2 = 1.60%, which led to more substructure deformation. Furthermore, a sudden drop of the stress amplitude was occurred with Δεt/2 = 4.00% which resulted in more plastic deformation. The phase transformation and α recrystallization were observed. Cracks were propagated along the α grain boundaries and the α/β lamellar interfaces due to the concentrated dislocations at the α/β lamellar interfaces.



中文翻译:

α/β Ti-6Al-4V-0.55Fe 合金在室温下低周停留疲劳期间的显微组织稳定性和损伤机制

用三种不同的总应变幅值研究了 Ti-6Al-4V-0.55Fe 合金的循环行为和显微组织演变。Δ ε t /2 = 1.20%,合金发生轻微软化,主要发生α再结晶。此外,在 Δ ε t /2 = 1.60% 时可以观察到温和的软化,这导致更多的子结构变形。此外,当 Δ ε t /2 = 4.00% 时,应力幅值突然下降,导致更多的塑性变形。观察到相变和α重结晶。由于 α/β 层状界面处的集中位错,裂纹沿 α 晶界和 α/β 层状界面传播 

更新日期:2021-10-13
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