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Dissimilar ultrasonic spot welding of aerospace aluminum alloy AA2139 to titanium alloy TiAl6V4

机译:航空铝合金aa2139与钛合金Tial6V4的异种超声波点焊

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摘要

The microstructure, hardness, lap shear strength and fracture energy of AA2139–TiAl6V4 spot joints produced by ultrasonic welding were investigated and related to the weld thermal cycle. No obvious intermetallic reaction layer was observed in the AA2139–TiAl6V4 welds, even using transmission electron microscopy. The hardness profile of AA2139 side after welding was studied, demonstrating that the heat introduced by the welding process leads to some softening with partial hardness recovery after natural aging. The effects of welding time on peak load and fracture energy were investigated. The peak load and fracture energy of welds increased with an increase in welding time and then reached a plateau, i.e., maximum peak load 5.3 kN and maximum fracture energy 3.7 kN mm. In all cases, failure occurred by fracture at the weld interface.
机译:研究了超声波焊接制备的AA2139-TiAl6V4点焊接头的组织,硬度,搭接剪切强度和断裂能,并与焊接热循环有关。即使使用透射电子显微镜,在AA2139-TiAl6V4焊缝中也没有观察到明显的金属间反应层。研究了焊接后AA2139侧的硬度分布,表明焊接过程中引入的热量导致一些软化,自然老化后部分硬度得以恢复。研究了焊接时间对峰值载荷和断裂能的影响。焊接的峰值载荷和断裂能随着焊接时间的增加而增加,然后达到一个平台,即最大峰值载荷为5.3 kN,最大断裂能为3.7 kN mm。在所有情况下,焊接界面处的断裂都会导致失效。

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