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Microstructure effects on fatigue crack growth in additively manufactured Ti-6A1-4V

机译:显微结构对疲劳裂纹增长的疲劳裂纹增长造成的Ti-6a1-4V

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In this work we investigate the relationship between the different microstructural features in additively-manufactured (AM) Direct Metal Laser Deposited Ti-6A1-4V alloys and the observed fatigue and fracture behaviors, using high resolution Digital Image Correlation experiments and microstructural imaging. Fatigue cracks in the AM specimens were observed to periodically propagate parallel to the α' laths and deflect at prior β grain boundaries. Corresponding plastic strain distributions show needle-like regions of high strain that correlated to the a' laths, suggesting significant influence of the microstructure on the plastic zone. In many cases, the fatigue cracks also propagated towards voids from unsintered powder or gas entrapment in the vicinity. In several experiments, premature failure of the AM specimens occurred under monotonic fracture or cyclic fatigue loading, which we attribute to the presence of void clusters located near the crack-tip. These fatigue and fracture characteristics were similar for AM specimens of different build-orientations.
机译:在这项工作中,我们研究了使用高分辨率数字图像相关实验和微观结构成像的加工制造(AM)直接金属激光沉积的Ti-6a1-4V合金和观察到的疲劳和断裂行为之间的不同微观结构特征与观察到的疲劳和断裂行为之间的关系。观察到AM标本中的疲劳裂缝,以定期平行于α'板条并在先前的β晶界偏转。相应的塑料应变分布显示与'车床相关的高菌株的针状区域,这表明微观结构对塑料区的显着影响。在许多情况下,疲劳裂缝也朝向来自附近的未烧结粉末或气体滞留的空隙繁殖。在几个实验中,在单调骨折或循环疲劳负载下发生AM标本的过早失效,我们将位于裂缝尖端附近的空隙簇存在。这些疲劳和骨折特性对于不同构建方向的AM标本类似。

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