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Influence of Microstructure and Notch on Low-Cycle Fatigue Behavior of Ti-6Al-4V Alloy at Elevated Temperature

机译:微观结构和缺口对升高温度下Ti-6Al-4V合金的低循环疲劳行为的影响

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摘要

The influences of micro structure and notch on the low-cycle fatigue behavior of Ti-6Al-4V alloy at elevated temperature were studied. Three kinds of microstructures in Ti-6Al-4V alloy were prepared under different heat treatment conditions; eqiaxed #alpha# structure, lenticular #alpha# structure and bimodal (mixed structure of equiaxed Cr and lenticular Cr) structure. Low-cycle fatigue tests were performed at 773K in air under a stress controlled triangular wave form for the smooth and circumferentially notched specimens. The following conclusions were obtained.(1)The low-cycle fatigue strength of the smooth specimen depended upon the microstructure. The highest was the bimodal structure and the lowest the lenticular Cr structure. However, the difference in low-cycle fatigue life among the specimens with different microstructures was not observed for the notched specimens with stress concentration factors of 2.5 and 6.0.(2)The crack initiation of the smooth specimen was affected by the microstructure, but for the notched specimen the crack initiation occurred at the stress concentrated region and the fatigue life did not depend on the microstructure.(3)The crack initiation lifetime of the notched specimen was predicted from the stress distribution around notch root obtained from the finite element method.
机译:研究了微结构和缺口对升高温度下Ti-6Al-4V合金的低循环疲劳行为的影响。在不同热处理条件下制备Ti-6Al-4V合金中的三种微观结构; EQIAXED#ALPHA#结构,透镜#alpha#结构和双峰(均匀CR和透镜CR的混合结构)结构。低循环疲劳试验在773K在空气中以应力控制的三角形波形,用于光滑和周向的缺口样本。获得了以下结论。(1)平滑试样的低循环疲劳强度依赖于微观结构。最高的是双峰结构和最低的透镜Cr结构。然而,对于具有2.5和6.0的应力浓度因子的缺口样品,未观察到具有不同微结构的试样之间的低周期疲劳寿命的差异。(2)平滑样品的裂纹引发受微观结构的影响,但是对于缺口样品在应力集中区域发生裂纹引发,疲劳寿命不依赖于微观结构。(3)从来自有限元法获得的凹口根系周围的应力分布预测出缺口标本的裂纹启动寿命。

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