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Distribution of internal crack initiation sites in high-cycle fatigue for titanium alloys

机译:钛合金高周疲劳中内部裂纹萌生部位的分布

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摘要

In order to clarify how the internal crack initiation site distributes according to microstructure in high-cycle fatigue, α-β or near α titanium alloys with various microstructure were subjected to fatigue test in liquid nitrogen. The internal crack initiation occurred longer than 10^5 cycles at 77 K. The initiation site was a facet or its aggregate which originated from α grain transgranular cracking in each material. In equiaxed α structures, the location of initiation site was obviously restricted to near the specimen surface (i.e. 10-200μm deep from the specimen surface). In acicular α structures, the location was more or less near the specimen surface and more interior cases were also seen, which were associated with a larger initiation site size. In elongated α structure, on the contrary, the location was scattered from the vicinity of specimen surface to the center in fracture surface. The size of the internal crack initiation sites was evaluated, and the location of the sites was discussed from the viewpoints of the cyclic stress and their size.
机译:为了阐明在高周疲劳中内部裂纹萌生部位是如何根据微观结构分布的,对具有各种微观结构的α-β或近α钛合金在液氮中进行了疲劳测试。内部裂纹的萌生在77 K处发生的时间超过10 ^ 5个周期。该萌生点是一个小面或其聚集体,其起源于每种材料中的α晶粒跨晶裂纹。在等轴α结构中,起始点的位置明显限于样品表面附近(即距样品表面深10-200μm)。在针状α结构中,该位置或多或少地靠近样品表面,并且还观察到更多内部情况,这与较大的起始位点大小有关。相反,在细长的α结构中,该位置从试样表面附近到断裂表面的中心分散。评估内部裂纹萌生部位的尺寸,并从循环应力及其尺寸的角度讨论部位的位置。

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