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Life Expectancies of Ni-doped SAC Solder Alloy Subjected to Drop Test Loading

机译:Ni掺杂SAC焊料合金的跌落试验寿命

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In this research, the mechanical behavior of novel Ni-doped Sn-1.2Ag-0.5Cu (SAC 1205) solder alloy, characterized by a high strain rate, was investigated in order to improve the drop test simulation model accuracy. Most researches focused on the elastic behavior of solder joint in simulation modeling. However, the sensitive strain rate of solder joint was important to take it into consideration since the solder joint was suffered the impact pulse during the drop test. In line with the drop test standard (JEDEC condition B), the test vehicle was subjected to impact loading with the peak acceleration of 1500 G for a period of 0.5 ms. This scenario ensured that the solder joint connecting the package and the test board was subjected to the impact loading for a very short time. In this study, the focus was on Thin Fine-pitch Ball Grid Array (TFBGA) package and the 11 mm × 10.6 mm, 9.4 mm × 9.4 mm, 12.6 mm × 12.6 mm, and 13.1 mm × 13.1 mm package sizes were investigated. The aim was to calculate the solder joint fatigue life by combining the results of finite element modeling with those obtained by experimental testing. The finite element model was used to analyze the stress and strain of the solder joint during the drop test. The model was developed using ANSYS/LS-DYNA and yielded a dynamic explicit solution. In order to investigate the performance of Ni-doped SAC 1205 solder alloy under the drop test conditions, the prediction model of solder alloy fatigue life was developed based on the Physics of Failure (PoF). The purpose of this research is to establish the fatigue life of SAC 1205N solder alloy with considering the sensitivity of strain rate for solder material.
机译:在这项研究中,研究了以高应变速率为特征的新型Ni掺杂Sn-1.2Ag-0.5Cu(SAC 1205)焊料合金的力学行为,以提高跌落试验仿真模型的准确性。大多数研究集中在模拟建模中焊点的弹性行为。但是,考虑到焊点的敏感应变率很重要,因为在跌落测试期间焊点会受到冲击脉冲的影响。根据跌落测试标准(JEDEC条件B),测试车辆承受的冲击载荷为1500 G,峰值加速度为0.5 ms。这种情况确保了连接封装和测试板的焊点在很短的时间内承受冲击载荷。在这项研究中,重点是薄型细间距球栅阵列(TFBGA)封装,并研究了11 mm×10.6 mm,9.4 mm×9.4 mm,12.6 mm×12.6 mm和13.1 mm×13.1 mm的封装尺寸。目的是通过将有限元建模的结果与通过实验测试获得的结果相结合来计算焊点疲劳寿命。有限元模型用于分析跌落测试过程中焊点的应力和应变。该模型是使用ANSYS / LS-DYNA开发的,并提供了动态显式解决方案。为了研究跌落测试条件下掺镍SAC 1205焊料合金的性能,基于失效物理(PoF)建立了焊料合金疲劳寿命的预测模型。这项研究的目的是考虑到应变率对焊锡材料的敏感性来建立SAC 1205N焊锡合金的疲劳寿命。

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