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Crack surface morphology and grain misorientation in fatigued aluminium alloy AA7050 samples after interrupted ageing and retrogression-reageing treatments

机译:疲劳铝合金AA7050中断后衰老和倒退的治疗后裂缝表面形态和晶粒杂散

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We present the investigation of fatigue crack surface morphology and crystallographic grain orientation in samples of aluminium alloy AA7050 that had been subjected to interrupted ageing (T6I4-65) and retrogression-reageing (RRA) heat treatments. Both T6I4-65 and RRA ageing treatments generate bimodal (particle size) microstructural features. A single tensile overload was applied and its influence on the crystallographic grain orientation was evaluated using electron backscatter diffraction (EBSD). The results reveal that T6I4-65 and RRA heat treatments contribute to the increased occurrence of planar slip features in the form of small and large flat facets, respectively. T6I4-65 condition leads to a greater degree of lattice misorientation in the vicinity of fatigue crack tip than the RRA condition which is likely to be the evidence of increased plastic deformation due to the overload.
机译:我们介绍了在已经进行中断老化的铝合金AA7050样品中疲劳裂纹表面形态和晶粒晶型的调查,其进行中断(T6I4-65)和倒置引发(RRA)热处理。 T6I4-65和RRA老化治疗均产生双峰(粒径)微观结构特征。应用单个拉伸过载,并使用电子反向散射衍射(EBSD)评估其对晶粒取向的影响。结果表明,T6I4-65和RRA热处理有助于分别增加小型和大平面形式的平面滑移特征的发生。 T6I4-65条件导致疲劳裂纹尖端附近的晶格误报比RRA条件,这可能是由于过载引起的塑性变形增加的证据。

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