环氧树脂与铜的界面裂纹扩展

Weihai Zhang, Daoguo Yang, L. Ernst, Bingbing Zhang, Wenbo Yang, M. Cai
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引用次数: 3

摘要

在前面[1-6]讨论的CU-EMC界面上的MMB分层实验中,界面断裂表现为“脆性界面”特征。这是因为实际的断裂出现在易碎的EMC和易碎的CU氧化物(存在于CU引线框架上)之间。一般认为“脆性界面”在循环载荷条件下不会发生低周疲劳断裂或亚临界断裂。因此,在[7]中,CU-EMC界面出现疲劳断裂的报道有些令人惊讶。这种令人惊讶的行为的原因可能是CU衬底的过载超过其屈服极限,或者仅仅是由于CU在裂纹尖端附近的局部塑性现象。在这种情况下,即使在非渐进循环加载下,裂纹尖端的j积分值也可能上升。为了在[1-6]的MMB试验中研究这一现象,我们采用了大量的循环变形模拟来探索CU-lead-frame在其屈服极限弯曲情况下的j积分值。本文将讨论以下步骤:由于在非渐进式循环加载期间,预计j -积分值会发生极小的变化,并且这些变化应该被很好地记录下来,因此首先讨论了3种不同FEM软件包(ANSYS, ABAQUS, MARC)的MMB试验的j -积分评估的单独比较。对室温下非渐进式循环加载(电磁兼容的玻璃态)的j积分值进行了仿真计算。在第一个周期之后,会发生摇降到弹性的动作。因此,根据室温下的模拟结果,不太可能发生亚临界断裂。预计在高温下(= EMC的橡胶状态),在最初的几个循环之后,将再次发生摇降到弹性的动作。因此,CU中的塑性行为不被认为是亚临界断裂的根本原因。另一方面,在包括高温在内的循环载荷下的封装,在高温下的暴露会伴随着EMC的持续老化。并行研究[15]发现,由于电磁兼容的老化,封装的变形和应力状态随着时间的推移发生了巨大的变化。这种急剧变化的状态很可能是先前观察到的亚临界断裂的起源。这方面需要进一步的研究。
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Interface crack propagation between epoxy moulding compound and copper
For the MMB delamination experiments on CU-EMC interfaces as previously discussed in [1-6], the interface fracture shows the characteristics of a "brittle interface". This is because of the fact that the actual fracture appears between the brittle EMC and the brittle CU-oxides (being present on the CU lead-frame). Low cycle fatigue fracture or sub-critical fracture under cyclic loading conditions is generally considered not to be occurring for "brittle interfaces". Therefore, it was somewhat surprising that in [7] fatigue fracture was reported to occur for CU-EMC interfaces. The reason for this surprising behaviour could possibly be found in the overloading of the CU-substrate above its yield limit or just due to local plastic phenomena in the CU near the crack tip. In such a case the J-Integral value at the crack tip could possibly rise even under non-progressive cyclic loading. In order to research this phenomena for the MMB test of [1-6], a number of cyclic deformation simulations is applied to explore the J-Integral value for the case that the CU-lead-frame is being bend above its yield limit. In this paper following steps will be discussed: As during non-progressive cyclic loading extremely small changes of the J-Integral value are expected to occur and these should be well registered, first a separate comparison of the J-Integral evaluation of the MMB test for 3 different FEM packages is discussed (ANSYS, ABAQUS, MARC). The simulation results for the J-Integral values during non-progressive cyclic loading at room temperature (=Glassy state of the EMC), are evaluated. It occurs that Shake down to Elastic action occurs after the first cycles. As a result, based on the simulation results at room temperature, sub-critical fracture is not likely to occur. It is expected that at high temperatures (=Rubbery state of the EMC) again Shake down to Elastic action will occur after the first few cycles. Consequently, plastic behaviour in the CU is not considered as the root cause of sub-critical fracture. On the other hand, in packages under cyclic loading including high temperature, the exposure at high temperature will be accompanied by continuing aging of the EMC. In parallel research [15] it was found that due to aging of the EMC the deformation and stress state of a package is dramatically changing with time. This dramatically changing state could well be the origin of previously observed sub-critical fracture. Here further research will be required.
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