实验验证了球栅阵列焊点振动疲劳寿命预测模型

T. E. Wong, F. Palmieri, L. Kachatorian
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引用次数: 4

摘要

采用一种新的方法支持球栅阵列(BGA)焊点振动疲劳寿命预测模型的试验验证。该模型是根据29种不同金属材料的高周疲劳试验数据,采用曲线拟合技术推导出的通用斜率经验公式发展而来的。为了建立BGA焊点振动疲劳寿命预测模型,首先设计、制造了不同尺寸的BGA菊链封装焊接试验车(TV),并在连续监测焊点完整性的情况下进行了随机振动试验。基于测量结果,进行了破坏性物理分析,进一步验证了焊点的失效位置和裂纹路径。接下来,开发了一种方法来确定由于TV暴露于随机振动环境而导致的BGA焊点的应力/应变。该方法采用三维建模技术对BGA封装的振动响应进行仿真。利用MSC/NASTRAN™计算机代码进行线性静态和动态有限元分析,结合体积加权平均技术,计算焊点的有效应变。在计算过程中,几个内部开发的Fortran程序,结合从MSC/NASTRAN™静态和频率响应分析中获得的输出,用于执行所需的计算。最后,建立了包含两个未知参数的振动疲劳寿命模型,该模型可以通过将导出的焊料有效应变与试验数据相关联来确定。这个测试校准的模型然后被推荐作为一个有效的工具来确定BGA焊点在振动过程中的完整性。还建议选择更多具有各种封装尺寸,焊接球配置,振动轮廓的研究案例,以进一步校准该模型。本文给出了一个313针塑料和304针陶瓷BGAs的例子。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimentally Validated Vibration Fatigue Life Prediction Model for Ball Grid Array Solder Joint
A newly developed methodology is used to support test validation of ball grid array (BGA) solder joint vibration fatigue life prediction model. This model is evolved from an empirical formula of universal slopes, which is derived from high-cycle fatigue test data using a curve fitting technique over 29 different materials of metals. To develop the BGA solder joint vibration fatigue life prediction model, a test vehicles (TV), on which various sizes of BGA daisy-chained packages are soldered, is first designed, fabricated and subjected to random vibration tests with continuously monitoring the solder joint integrity. Based on the measurement results, a destructive physical analysis is then conducted to further verify the failure locations and crack paths of the solder joints. Next, a method to determine the stresses/strains of BGA solder joints resulting from exposure of the TV to random vibration environments is developed. In this method, a 3-D modeling technique is used to simulate the vibration responses of the BGA packages. Linear static and dynamic finite element analyses with MSC/NASTRAN™ computer code, combined with a volume-weighted average technique, are conducted to calculate the effective strains of the solder joints. In the calculation process, several in-house developed Fortran programs, in conjunction with the outputs obtained from MSC/NASTRAN™ static and frequency response analyses, are used to perform the required computations. Finally, a vibration fatigue life model is established with two unknown parameters, which can be determined by correlating the derived solder effective strains to the test data. This test-calibrated model is then recommended to serve as an effective tool to determine the integrity of the BGA solder joints during vibration. Selecting more study cases with various package sizes, solder ball configurations, vibration profiles to further calibrate this model is also recommended. An example of a 313-pin plastic and 304-pin ceramic BGAs is illustrated in the present study.
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