首页> 外文期刊>Journal of Electronic Materials >Modeling solder joint fatigue life for gull-wing leaded packages: part I -- elastic plastic stress model
【24h】

Modeling solder joint fatigue life for gull-wing leaded packages: part I -- elastic plastic stress model

机译:鸥翼式引线封装焊点疲劳寿命建模:第一部分-弹性塑性应力模型

获取原文
获取原文并翻译 | 示例
           

摘要

It is a challenge to assess solder joint fatigue life in the modern electronics industry because of complex geometries, complex non-linear viscoplastic material properties, and the frequently changing environmental conditions. The first step inthe fatigue life assessment process is to find the stress distribution in the solder. Traditionally, this has been done using numerical tools like finite element methods. The finite element approach requires a highly trained and experienced analyst andhuge computing resources, while the accuracy is always questioned. This study aims to develop a more accurate analytical-cum-empirical model to predict critical stresses in the solder joint so as to avoid the necessity of finite element simulation. Thispaper presents a generic elastic-plastic stress model that is obtained based on theoretical stress analysis solutions that is tweaked by using a design of experiments technique with FEA simulations.
机译:由于复杂的几何形状,复杂的非线性粘塑性材料特性以及经常变化的环境条件,评估现代电子工业中的焊点疲劳寿命是一项挑战。疲劳寿命评估过程的第一步是找到焊料中的应力分布。传统上,这是使用数值工具(例如有限元方法)完成的。有限元方法需要训练有素,经验丰富的分析人员和庞大的计算资源,而准确性始终受到质疑。这项研究旨在建立一个更准确的分析和经验模型来预测焊点中的临界应力,从而避免了有限元模拟的必要性。本文介绍了一个通用的弹塑性应力模型,该模型是基于理论应力分析解决方案而获得的,该解决方案通过使用具有FEA仿真的实验技术的设计进行了调整。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号