首页|期刊导航|航空材料学报|铝合金搅拌摩擦焊缝和母材疲劳裂纹扩展行为

铝合金搅拌摩擦焊缝和母材疲劳裂纹扩展行为OA北大核心CSCDCSTPCD

Performances of Fatigue Crack Growth for Aluminum Friction Stir Welds and Base Materials

中文摘要英文摘要

对7075-T6和LC4CS两种铝合金搅拌摩擦焊缝的疲劳裂纹扩展(da/dN)行为进行实验研究,并与7075-T6母材疲劳性能进行对比分析.结果表明:沿焊缝中心、前进和后退边方向,7075-T6搅拌摩擦焊疲劳裂纹扩展速率da/dN均低于LC4CS的da/dN;但沿垂直于焊缝方向两者da/dN基本一致;同种材料焊缝中心da/dN为最低,其次是后退边和前进边,而沿垂直焊缝方向da/dN为最高;7075-T6焊缝中心da/dN与其母材比较,低载荷 ΔK…查看全部>>

The fatigue crack propagation performances for friction stir welded AA7075-T6 and LC4CS (a Chinese brand aluminum alloy similar to AA7075-T6)joints and their corresponding base materials have been investigated.It was found that the fatigue crack growth rates (da/dN)for AA7075-T6 welded joints along the weld center line,advanced and retracted side regions are all slower than that of LC4CS alloy,but the da/dN values along the perpendicular direction of weld fo…查看全部>>

秦红珊;杨新岐

天津大学 理学院,天津 300354天津大学 材料科学与工程学院,天津 300354

矿业与冶金

搅拌摩擦焊7075-T6和LC4CS铝合金疲劳裂纹扩展疲劳断口

Friction stir weldsAA7075-T6 and LC4CS alloyfatigue crack propagationfatigue fracture surface

《航空材料学报》 2017 (5)

搅拌摩擦焊中“弱连接”机制及对疲劳行为的影响研究

41-47,7

国家自然科学基金(50775159)

10.11868/j.issn.1005-5053.2016.000125

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