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首页> 外文期刊>The International Journal of Advanced Manufacturing Technology >Experimental and numerical investigation on forming limit curves of AA6082 aluminum alloy at high strain rates
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Experimental and numerical investigation on forming limit curves of AA6082 aluminum alloy at high strain rates

机译:高应变率AA6082铝合金形成极限曲线的实验性和数值研究

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摘要

The influence of high strain rate on the forming limit curves of AA6082-T6 aluminum alloy sheets, 1 mm in thickness, was investigated by means of dynamic tensile and hemispherical punch tests carried out until the onset of sample failure using a Split Hopkinson Bar (SHB) system, at a punch speed of 7500 and 12000 mm/s. The equipment used was designed according to the standard EN ISO 12004-2 but properly scaled to adapt it to the SHB apparatus. A finite element analysis was performed to quantify the strain rate values reached during tests (around 600 and 1000 s(-1) associated at the punch speeds of about 7500 and 12000 mm/s, respectively). The limit strains were determined on different sample geometries undergoing deformation in the range from the uniaxial and balanced biaxial stress states typical for sheet metal forming processes. The major and minor strain distributions, acquired through an accurate image analysis by analyzing the deformation of a previously imprinted grid on the specimen surface, allowed to plot the dynamic forming limit curves at different high strain rate values. Such forming limit curves were compared with those provided by samples deformed under quasi-static loading condition, using the same equipment and specimen geometries, in order to evaluate the influence of the loading rate on the formability. It was observed that the formability of AA6082-T6 aluminum alloy strongly improves as the strain rate increases from quasi-static to dynamic conditions.
机译:通过动态拉伸和半球形冲头试验,研究了高应变速率对厚度为1mm的AA6082-T6铝合金板材成形极限曲线的影响,直至使用分离式霍普金森杆(SHB)系统的样品失效,冲压速度为7500和12000 mm/s。所用设备根据标准EN ISO 12004-2设计,但适当缩放以适应SHB设备。进行了有限元分析,以量化试验期间达到的应变率值(在大约7500和12000 mm/s的冲压速度下,分别约600和1000 s(-1))。在板材成形过程中典型的单轴和平衡双轴应力状态范围内,在经历变形的不同样品几何形状上确定极限应变。通过分析试样表面上先前压印网格的变形,通过精确的图像分析获得的主应变和次应变分布,可以绘制不同高应变率值下的动态成形极限曲线。使用相同的设备和试样几何形状,将此类成形极限曲线与准静态加载条件下变形试样提供的曲线进行比较,以评估加载速率对成形性的影响。结果表明,随着应变速率从准静态状态增加到动态状态,AA6082-T6铝合金的成形性显著提高。

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