材料工程

航空用铝合金搅拌摩擦焊拉伸特性

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  • 沈阳航空航天大学 航空航天工程学部(院), 沈阳 110136
陈振中(1963-), 男, 辽宁沈阳人, 教授, 主要研究方向:结构疲劳断裂与可靠性分析, E-mail:zhenzhong_chen@hotmail.com。

收稿日期: 2012-11-21

基金资助

辽宁省教育厅科研基金(项目编号:L2010415);沈阳市人才项目(项目编号:src201101)

Tensile properties of friction stir welded aluminum alloys in aviation

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  • Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136

Received date: 2012-11-21

摘要

对6mm厚的航空用AA7050-T7451、AA2024-T4铝合金进行了同种和异种材料的搅拌摩擦焊接, 并对3种接头的拉伸特性和断口进行了分析。试验结果表明, 同种材料接头的强度极限达到母材的90%以上, 屈服极限达到母材的75%以上, AA7050/AA2024 FSW接头强度分别达到AA7050母材和AA2024母材的60.5%和70.8%, 屈服极限分别达到AA7050母材和AA2024母材的46.2%和75.5%;焊缝焊核区由细小均匀的等轴晶粒组成, 热机影响区颗粒粗化并发生扭曲变形, 热影响区晶粒受循环热影响变得粗大;拉伸试验断裂发生在前进侧热机影响区/热影响区的过渡段, 断口存在明显的韧窝, 整体属于韧性断裂。

本文引用格式

陈振中, 马小革, 肖尧, 李明 . 航空用铝合金搅拌摩擦焊拉伸特性[J]. 沈阳航空航天大学学报, 2013 , 30(5) : 47 -50 . DOI: 10.3969/j.issn.2095-1248.2013.05.010

Abstract

This paper deals with the tensilel properties through jointing AA7050-T7451 and AA2024-T4 aluminum alloys in aviation by friction stir weld and analyzing fracture surfaces.The results show that the ultimate strength can reach 90%, the yield limit can reach 75%, the ultimate strength of AA7050/AA2024 FSW joint can reach 60.5% of AA7050 and 70.8% of AA2024.The yield limit can reach 46.2 % of AA7050 and 75.5% of AA2024.The equi-axial fine grains are found in the weld nugget, the coarse and distorted grains in the thermo-mechanically affected zone, and coarse grains in the heat affected zone.The fractures occur at the advancing side between thermo-mechanically affected zone and heat affected zone.Dimples appear on the fracture surfaces, which means that the fractures are ductile fracture.

参考文献

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