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Experimental study and life prediction on high cycle vibration fatigue in BGA packages

机译:BGA封装中高周振动疲劳的实验研究和寿命预测

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摘要

A technique and loading apparatus have been developed which allow ball grid array (BGA) packages to be visually inspected during high cycle vibration testing. This system provides controls for varying the cycling frequency and magnitude of the applied load. The failures of solder interconnects in BGA specimens were recorded by a direct visual monitoring method. Stroboscopic video was employed to freeze the motion of the vibrating solder interconnects while showing the real-time evolution of failure. In all test cases, BGA interconnect failure was observed to be the result of crack initiation and propagation along the nickel/solder interface. A primary crack developed at one edge of the interconnect and progressed stably until a secondary crack initiated from the opposite edge. The crack growth accelerated until these cracks coalesced, resulting in complete separation of the interconnect. The percentages of time spent in crack initiation, stable propagation and accelerated propagation are, on the order of 15%, 60% and 25%, respectively. Vibration tests at frequencies ranging from 50 to 100 Hz were performed and the number of cycles to failure was found to be frequency-independent in this range. Several commonly used damage mechanics and fracture mechanics fatigue life-prediction models are examined based on failure parameters computed from a nonlinear finite element analysis. It was found that while the damage models examined show large discrepancies between predicted and actual cycles-to-failure, the fracture model correlates with the test data within a factor of 1.5.
机译:已经开发出一种技术和装载设备,其允许在高周期振动测试期间目测检查球栅阵列(BGA)封装。该系统提供了用于更改循环频率和所施加负载大小的控件。通过直接的视觉监控方法记录了BGA样品中焊料互连的故障。频闪视频被用来冻结振动的焊料互连的运动,同时显示故障的实时演变。在所有测试案例中,观察到BGA互连故障是裂纹萌生和沿镍/焊料界面扩展的结果。一次裂纹在互连的一个边缘处发展并稳定地发展,直到从相对边缘开始产生二次裂纹为止。裂纹增长加速,直到这些裂纹合并,导致互连完全分离。裂纹萌生,稳定扩展和加速扩展所花费的时间百分比分别约为15%,60%和25%。在50至100 Hz的频率范围内进行了振动测试,发现在该范围内,故障循环的次数与频率无关。基于非线性有限元分析计算出的失效参数,研究了几种常用的损伤力学和断裂力学疲劳寿命预测模型。结果发现,虽然所检查的损伤模型在预测的和实际的失效周期之间显示出很大的差异,但断裂模型与测试数据的相关性在1.5倍之内。

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