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Effect of plastic anisotropy on forming behavior of AA-6061 aluminum alloy sheet

机译:塑性各向异性对AA-6061铝合金薄板成形行为的影响

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摘要

AA-6061 (T6) aluminum alloy sheet is used extensively for structural applications in various automotive and aerospace industries due to its excellent mechanical and physical properties. Due to lower formability of this material in age-hardened (T6) condition, forming of complex-shaped components is a major challenge. Forming behavior of the sheet was studied in T6 condition using limit dome height tests by experiment and finite element method for three different sheet directions (rolling direction, inclined direction (ID) and transverse direction). Strain path diagrams were obtained from the experimental limit dome height tests and finite element method simulations from drawing to stretching region, and the results were compared for all the sheet directions. Forming limit diagrams were plotted using strain localization and fracture criteria from experimental and simulated strain path curves. Effect of plastic anisotropy on crack propagation direction was studied using finite element method, and it has been found that the direction of crack propagation was strongly dependent on plastic anisotropy ratio ("r" value) of the sheet in biaxial strain paths.
机译:AA-6061(T6)铝合金薄板由于其优异的机械和物理性能而广泛用于各种汽车和航空航天工业的结构应用。由于这种材料在时效(T6)条件下的可成型性较低,因此复杂形状零件的成型是一项主要挑战。在T6条件下,通过极限穹顶高度试验和有限元方法,针对三个不同的板材方向(轧制方向,倾斜方向(ID)和横向),研究了板材的成形行为。从实验极限球顶高度测试和从拉伸到拉伸区域的有限元方法模拟获得了应变路径图,并比较了所有板材方向的结果。根据实验和模拟应变路径曲线,使用应变局部化和断裂准则绘制成形极限图。使用有限元方法研究了塑性各向异性对裂纹扩展方向的影响,并且发现裂纹扩展的方向强烈依赖于双轴应变路径中片材的塑性各向异性比(“ r”值)。

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