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首页> 外文期刊>International Journal of Fatigue >Faceted crack initiation characteristics for high-cycle and very-high-cycle fatigue of a titanium alloy under different stress ratios
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Faceted crack initiation characteristics for high-cycle and very-high-cycle fatigue of a titanium alloy under different stress ratios

机译:钛合金在不同应力比下的高周疲劳和超高周疲劳的刻面裂纹萌生特性

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摘要

Ultrasonic fatigue tests were conducted at the stress ratios of -1, -0.5, -0.1, 0.1 and 0.5 for a Ti-6Al-4V alloy in high-cycle and very-high-cycle fatigue regimes. Experimental results showed that faceted crack initiation was the main failure mode for specimens at the stress ratios of -0.1,0.1 and 0.5, and multi-site faceted crack initiation was observed at the stress ratios of 0.1 and 0.5. The measurements indicated that the number of facets increased with the increase of stress ratio. Based on the observations, the mechanism of faceted crack initiation was proposed, i.e., (ⅰ) cleavage of isolated primary α grains in cluster; (ⅱ) gradual growth of originated cracks (facets), and the coalescence of adjacent facets; and (ⅲ) coalesced facets forming a main crack in the cluster. Moreover, a model based on Poisson defect distribution is proposed to describe the effects of stress ratio on faceted crack initiation, which is in agreement with the experimental results.
机译:对于Ti-6Al-4V合金,在高循环和超高循环疲劳状态下,以-1,-0.5,-0.1、0.1和0.5的应力比进行了超声波疲劳测试。实验结果表明,在应力比为-0.1、0.1和0.5的情况下,多面裂纹萌生是试样的主要破坏方式,在应力比为0.1和0.5时观察到多点多面裂纹萌生。测量表明,小面的数量随着应力比的增加而增加。在此基础上,提出了多面裂纹萌生的机理,即(ⅰ)分裂了簇中分离的初生α晶粒。 (ⅱ)产生的裂纹(小平面)逐渐增长,相邻小平面的合并; (ⅲ)聚结的小面在簇中形成主要裂缝。此外,提出了一种基于泊松缺陷分布的模型来描述应力比对刻面裂纹萌生的影响,与实验结果相吻合。

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