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Mechanical behaviour and microstructural evolution in fine grain Ti-6Al-4V alloy under superplastic conditions

机译:超塑性条件下细粒Ti-6Al-4V合金中的力学行为和微观结构演化

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Ti-6Al-4V is able to support high level of deformations like superplastic deformation for aeronautical structural applications. However, the applied temperature during forming induces changes in phase fraction, which may have an impact on the mechanisms of deformation involved and the final part. Mechanisms described in the literature, like dislocation glide, diffusional creep. Grain Boundary Sliding (GBS) accommodated by dislocation or diffusion, are still controversial as there are mainly based on post mortem analysis or on stress-strain data. The purpose of this work was to combine interrupted tensile tests and heat treatments to improve the understanding of the mechanisms of deformation on each stage of deformation. The chosen test temperatures were 750°C and 920°C which correspond to different β phase fractions. The microstructural features like grain size and phase fraction were studied by Scanning Electron Microscope (SEM) combined with image analysis. Moreover, EBSD was used to follow the change of crystalline orientation of α grains to distinguish the involved mechanisms as a function of the deformation. Indeed, it would appears that several mechanisms could be activated depending on the deformation stage and on the temperature.
机译:TI-6AL-4V能够支持高水平的变形,如用于航空结构应用的超塑性变形。然而,在形成过程中施加的温度诱导相级分的变化,这可能对所涉及的变形机制和最终部分产生影响。文献中描述的机制,如位错滑动,扩散蠕变。通过位错或扩散容纳的晶界滑动(GBS)仍然存在争议,因为主要基于验尸分析或应力 - 应变数据。这项工作的目的是将中断的拉伸试验和热处理结合,以改善对每个变形阶段变形机制的理解。所选择的测试温度为750℃和920℃,对应于不同的β相级分。通过扫描电子显微镜(SEM)与图像分析相结合研究了晶粒尺寸和相位级分的微观结构特征。此外,EBSD用于遵循α颗粒的晶体取向的变化,以将所涉及的机制与变形的函数区分开。实际上,似乎可以根据变形阶段和温度来激活若干机制。

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