Prediction of fatigue crack initiation between underfill epoxy and substrate

D. Wu, B. Su, Y.C. Lee, M. Dunn
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引用次数: 4

Abstract

Delamination between underfill epoxy and a substrate is a critical reliability concern for flip-chip assemblies. Delamination often initiates from multimaterial interface corners, which are sites of elevated stresses, under cyclic loads during testing or operation. Most existing studies of delamination have focused on crack propagation; the presence of an existing crack is assumed, and the conditions under which it will propagate are studied. The related, but different, issue of crack initiation has received far less study. To date, no widely-accepted models of crack initiation from multimaterial interface corners under fatigue loading exist. Here we propose a first step toward establishing such a model. In this study we have used interface corner stress intensities under cyclic loading (/spl Delta/K) to correlate fatigue crack initiation at bimaterial interface corners with different far-field loadings and geometries. Fracture under cyclic loads usually initiates at the interface corner and propagates along an interface. The stress states at the interface corner drives the fatigue crack initiation process. In certain cases, crack initiation can be correlated using a critical value of the stress intensity that exists at the bimaterial interface corner in the context of a linear elastic stress analysis. The stress intensities uniquely characterize the stress state in an annular region surrounding the interface corner with a singular stress field. In order to demonstrate the use of critical stress intensities to correlate fracture initiation, we measured the number of cycles required to initiate a fatigue crack from an epoxy/steel interface corner. The preliminary results suggest that fatigue crack initiation can be correlated with critical values of the stress intensities. Furthermore, the proposed approach to correlate fatigue crack initiation can be coupled with existing approaches to correlate fatigue crack propagation, thus resulting in a tool for complete lifecycle analysis.
底填环氧树脂与基体之间疲劳裂纹萌生的预测
下填充环氧树脂和衬底之间的分层是倒装芯片组件的关键可靠性问题。在测试或运行过程中,在循环载荷作用下,多材料界面角处的应力升高,往往引发分层。现有的分层研究大多集中在裂纹扩展上;假设存在裂纹,并对裂纹扩展的条件进行了研究。与之相关但不同的裂纹起裂问题得到的研究要少得多。迄今为止,还没有广泛接受的疲劳载荷下多材料界面角裂纹起裂模型。在这里,我们提出建立这样一个模型的第一步。在这项研究中,我们使用循环载荷下的界面角应力强度(/spl Delta/K)来将双材料界面角处的疲劳裂纹萌生与不同的远场载荷和几何形状联系起来。循环荷载作用下的断裂通常从界面角处开始,沿界面扩展。界面角处的应力状态驱动疲劳裂纹萌生过程。在某些情况下,在线性弹性应力分析的背景下,裂纹起裂可以使用存在于双材料界面角处的应力强度临界值进行关联。应力强度独特地表征了界面角周围具有单一应力场的环形区域的应力状态。为了证明使用临界应力强度来关联断裂起裂,我们测量了从环氧树脂/钢界面角开始疲劳裂纹所需的循环次数。初步结果表明,疲劳裂纹萌生与应力强度临界值之间存在相关性。此外,所提出的疲劳裂纹起裂关联方法可以与现有的疲劳裂纹扩展关联方法相结合,从而形成一个完整的生命周期分析工具。
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