首页> 外文会议>Electronics Manufacturing Technology Symposium, 1997., Twenty-First IEEE/CPMT International >A fracture mechanics analysis of the popcorn cracking in theplastic IC packages
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A fracture mechanics analysis of the popcorn cracking in theplastic IC packages

机译:爆米花裂纹的断裂力学分析。塑料IC封装

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Popcorn cracking phenomenon in surface mounted packages is treatedby assuming an inherent edge crack at the die pad/EMC interface of aTQFP and subsequent interface delamination under thermal and/or vaporpressure loadings. Using the finite element methods and the methods ofinterface fracture mechanics, path independent energy release rate iscalculated and compared to the interface toughness which is assumed tobe a function of the phase angle. Results indicate that the edge crackpropagates toward the center leading to the delamination of the entiredie pad/EMC interface most notably for the vapor pressure loading, thenmixed loading when thermal and vapor pressure loadings are appliedsimultaneously. For the thermal loading, only the cooling process islikely to lead to the entire delamination where both the energy releaserate and interface toughness decrease with the crack length. For thevapor pressure loading, the energy release rate increases parabolicallywith the crack length but proportionally with the vapor pressure whilethe interface toughness remains almost constant. In the case of themixed loading, the energy release rate increases as in the vaporpressure loading, but the interface toughness decreases with the cracklength; Stress states near the crack tip were closer to mode II forthermal loading but to mode I for vapor pressure loading, and changedfrom mode II to mode I with the crack length for the mixed loading
机译:处理表面贴装包装中的爆米花开裂现象 通过假设在芯片的管芯焊盘/ EMC界面处存在固有的边缘裂纹 在热和/或蒸汽下,TQFP和随后的界面分层 压力负荷。使用有限元方法和 界面断裂力学,与路径无关的能量释放速率为 计算并与假定的界面韧性进行比较 是相位角的函数。结果表明边缘裂纹 向中心传播,导致整个分层 芯片垫/ EMC界面最显着的是蒸汽压力加载,然后 施加热和蒸汽压力载荷时的混合载荷 同时。对于热负荷,仅冷却过程为 可能导致整个分层,同时释放能量 裂纹扩展率和界面韧性随裂纹长度的增加而降低。为了 蒸气压加载时,能量释放率呈抛物线形式增加 与裂纹长度成正比,与蒸汽压力成正比 界面韧性几乎保持不变。在这种情况下 混合负载时,能量释放速率随着蒸气的增加而增加 压力载荷,但界面韧性随裂纹而降低 长度;裂纹尖端附近的应力状态更接近于模式II 热负荷,但在模式I下进行蒸汽压力负荷,并进行了更改 从模式II到模式I具有混合载荷的裂纹长度

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