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Effect of Aging on Fatigue-Crack Growth Behavior of a High-Temperature Titanium Alloy

机译:老化对高温钛合金疲劳裂纹生长行为的影响

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The effects of aging on the fatigue-crack growth (FCG) behavior of a newly developed high-temperature titanium alloy (Ti-6Al-4.8Sn-2Zr-lMo-0.4Si-lNd) with bimodal and lamellar microstructures were investigated at room temperature. The results indicate that aging had a more pronounced effect on the lamellar than on the bimodal microstructure. The effect is weakened with prolonged aging time especially for lamellar microstructure. TEM and SEM studies of microstructures and fracture surfaces were performed to gain insight into the deformation characteristics and crack propagation mechanisms of these microstructures. The differences in FCG behavior in different aging conditions were interpreted in terms of the effect of aging time on the microstructure, the crack path tortuosity and crack closure. The dependence of FCG behavior on aging condition can be attributed to the precipitation of the α_2 phase based on Ti_3Al from the two microstructures, and the silicide was found to play a limited role in the present investigation.
机译:新开发的高温钛合金(Ti系6AL-4.8Sn-2ZR-LMO-0.4Si-LND)双峰和层状的微结构的对疲劳裂纹扩展老化的影响(FCG)行为在室温下进行了研究。结果表明,衰老对层状比在双峰组织一个更明显的效果。效果减弱随老化时间的延长尤其是对于层状微观结构。进行微结构和断裂表面的TEM和SEM研究深入了解的变形特性和这些微结构的裂纹扩展的机制。在不同老化条件在FCG行为的差异在对微结构,裂纹路径曲折度和裂纹闭合陈化时间的效果的观点进行了解释。的FCG行为对老化状态的依赖可以归因于基于Ti_3Al从两个微观结构的α_2相的析出,与硅化物被发现在本次调查中发挥的作用有限。

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