首页> 外文期刊>Journal of neurosurgical sciences >Weldability of high-strength aluminium alloy EN AW-7475-T761 sheets for aerospace applications, using refill friction stir spot welding
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Weldability of high-strength aluminium alloy EN AW-7475-T761 sheets for aerospace applications, using refill friction stir spot welding

机译:高强度铝合金en AW-7475-T761用于航空航天应用的焊接性,采用refill摩擦搅拌点焊接

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Refill friction stir spot welding is a solid-state welding process for joining lightweight sheets in the overlap configuration by means of frictional heat and mechanical work. The objective is to investigate refill friction stir spot welding of aluminium alloy EN AW-7475-T761, since fusion welding of such high-strength alloys is problematic due to solidification and liquation cracking. This alloy is used in highly stressed structural parts in aerospace applications, because of its low weight, superior strength, high corrosion resistance and corrosion fatigue behaviour. The process parameter optimization and the effect of the parameters on the weld characteristics were examined. The dwell time, the plunge depth and the rotational speed were varied according to a multi-level factorial design. An increase of the dwell time resulted in a larger stir zone area and smaller amount of defects. The width of the central coarse-grained band became smaller, containing a more refined grain size. An increase of the rotational speed lead to a smaller stir zone area, a discontinuous joint line remnant and a larger width of the central coarse-grained band. An increase of the plunge depth lead to a larger stir zone area. Welds produced with a high heat input exhibited a lower average hardness and a higher hardness drop, compared to welds with a low high heat input. Analysis of variance has shown that the dwell time, the plunge depth and their interaction have a statistically significant effect on the lap shear strength: a longer dwell time, a higher plunge depth and their interaction resulted into a higher lap shear strength.
机译:再填充摩擦搅拌点焊是一种固态焊接过程,用于通过摩擦热和机械工作加入重叠配置中的轻质片材。目的是研究铝合金钢合金钢合金的补充摩擦搅拌点焊,因为由于凝固和液化裂解,这种高强度合金的熔接焊接是有问题的。这种合金用于航空航天应用中高压结构部件,由于其重量低,优异的强度,高耐腐蚀性和腐蚀疲劳行为。研究了研究参数优化和参数对焊接特性的影响。停留时间,平面深度和转速根据多级因子设计而变化。停留时间的增加导致更大的搅拌区面积和较小的缺陷。中央粗粒带的宽度变小,含有更精细的晶粒尺寸。转速的增加导致较小的搅拌区区域,不连续的接合线残余和较大的中央粗粒带的宽度。平面深度的增加导致更大的搅拌区区域。与具有低热量输入的焊接相比,用高热输入产生的焊缝表现出较低的平均硬度和更高的硬度下降。方差分析表明,停留时间,暴力深度及其相互作用对膝盖剪切强度有统计学显着的影响:更长的停留时间,更高的暴力深度,它们的相互作用导致更高的杠杆剪切强度。

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