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Yield Strength and Residual Stress Measurements on Friction-Stir-Welded Aluminum Alloys

机译:搅拌摩擦焊接铝合金的屈服强度和残余应力测量

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摘要

Friction-stir welding is a relatively new joining technology that has great potential for the aerospace industry. Tonuse friction-stir welding tomanufacture an airworthy and damage-tolerant structure, themechanical behaviormustnbe fully understood. This paper presents the experimental results in which the local yield strength and the residualnstress profile for friction-stir-welded AA2024-T3, AA7075-T6, and AA6013-T4 were measured. X-ray diffractionnwas used tomeasure the residual stresses. The residual stress profiles in all three alloys exhibited high tensile stressesnin the center region of the weld. Around the weld the stress levels were reduced to either zero or low-magnitudencompressive stresses. Both AA2024-T3 and AA7075-T6 show comparable residual stress profiles, whereas AA6013-nT4 exhibits lower-magnitude residual stresses. Digital imaging correlation was used to measure the local yieldnstrength in all three alloys with and without welds. The yield strength profiles obtained with this new technologynmatched perfectly with the corresponding hardness profiles of the welds. A relation was found between the yieldnstrength profiles and the residual stress profiles, which resulted in understanding of how the appearance of thenresidual stress profiles is determined by the yield strength profile.
机译:搅拌摩擦焊是一种相对较新的连接技术,在航空航天工业中具有巨大的潜力。要使用搅拌摩擦焊制造适航且耐损伤的结构,必须充分了解其力学性能。本文介绍了实验结果,其中测量了搅拌摩擦焊接AA2024-T3,AA7075-T6和AA6013-T4的局部屈服强度和残余应力轮廓。 X射线衍射用于测量残余应力。所有三种合金中的残余应力轮廓在焊缝的中心区域均表现出较高的拉伸应力。在焊缝周围,应力水平减小到零或低幅压缩应力。 AA2024-T3和AA7075-T6都显示出可比较的残余应力曲线,而AA6013-nT4则显示出较低幅值的残余应力。使用数字成像相关性来测量带有和不带有焊缝的所有三种合金的局部屈服强度。用这种新技术获得的屈服强度曲线与相应的焊缝硬度曲线完美匹配。在屈服强度轮廓和残余应力轮廓之间发现了一种关系,这使人们了解了残余应力轮廓的外观如何由屈服强度轮廓决定。

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