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Gull-wing solder joint fatigue life sensitivity evaluation

机译:鸥翼式焊点疲劳寿命敏感性评估

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摘要

A Taguchi design of experiment approach was applied to thermostructural analyses of a gull-wing solder joint assembly. This approach uses a minimum number of finite element analyses to evaluate the impact of solder joint assembly parameters onfatigue life of the assembly. To avoid costly complex modeling efforts for each parametric case study, a commercially available program, MSC/PATRAN's PATRAN Command Language, was used to automatically create finite element models of a two-dimensionalgull-wing solder joint assembly based on nine parameters. Modeling time was dramatically reduced from days to a few minutes for each detailed lead/ solder model. Two sets of parametric studies were conducted to evaluate the impact of variation of the sixparameters. The analysis results indicate that lead ankle radius is the most critical parameter affecting solder joint total fatigue life, and lead and minimum solder thicknesses are the next most critical ones. Therefore, to effectively improve thesolder joint fatigue life margin, it is recommended to: (1) increase the minimum solder thickness; (2) use thinner lead; and (3) use a larger lead ankle radius, even though this may require reducing lead shin length. By implementing only the lastrecommendation to modify the current solder joint assembly, the fatigue life margin in this design could, in general, be improved by 27 percent or more.
机译:Taguchi设计的实验方法被应用于鸥翼式焊点组件的热结构分析。该方法使用最少数量的有限元分析来评估焊点装配参数对装配疲劳寿命的影响。为了避免每个参数案例研究花费昂贵的复杂建模工作,使用了商用程序MSC / PATRAN的PATRAN命令语言,该程序基于九个参数自动创建二维鸥翼式焊点组件的有限元模型。每个详细的引线/焊料模型的建模时间从几天大大减少到几分钟。进行了两组参数研究,以评估六个参数变化的影响。分析结果表明,铅脚踝半径是影响焊点总疲劳寿命的最关键参数,而铅和最小焊锡厚度是次要的关键参数。因此,为有效提高焊点疲劳寿命,建议:(1)增加最小焊锡厚度; (2)使用较细的铅; (3)使用较大的铅踝半径,即使这可能需要减小铅胫长度。通过仅执行最新的建议来修改当前的焊点组件,通常可以将这种设计的疲劳寿命裕度提高27%或更多。

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