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Fatigue crack growth behavior in Sn-Pb eutectic solder/copper joint under mode I loading

机译:I型加载下Sn-Pb共晶焊料/铜接头的疲劳裂纹扩展行为

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摘要

Fatigue crack growth (FCG) behavior along 63Sn-37Pb solder/copper interface was investigated using a solder-jointed plate specimen with a single-edge crack under opening tensile loading (mode I). Finite element analysis was conducted for evaluating stress intensity factor (K) and/-integral (J) of the crack tip. Under frequency of 10 Hz and stress ratio of 0.1, the fatigue crack propagation rate could be characterized successfully by either stress intensity factor range (△K) or/-integral range (△J). A fatigue crack propagated in transgranular manner through Pb-rich phases and Sn-rich phases near the solder-copper interface. With increasing crack length, the size of plastic zone at the crack tip and the von Mises stress along the solder-copper interface increased, which resulted in the interfacial debonding near the crack tip. The critical crack length (a/W) and adhesive strength for interfacial debonding were 0.46 and 20.2 MPa, respectively.
机译:使用在开放拉伸载荷下(模式I)具有单边缘裂纹的焊点板样品,研究了沿63Sn-37Pb焊料/铜界面的疲劳裂纹扩展(FCG)行为。进行了有限元分析,以评估裂纹尖端的应力强度因子(K)和/积分(J)。在10 Hz的频率和0.1的应力比下,可以通过应力强度因子范围(△K)或/积分范围(△J)来成功表征疲劳裂纹扩展速率。疲劳裂纹以晶间方式通过焊料-铜界面附近的富Pb相和富Sn相传播。随着裂纹长度的增加,裂纹尖端的塑性区的尺寸和沿焊料-铜界面的冯·米塞斯应力增加,这导致裂纹尖端附近的界面剥离。界面剥离的临界裂纹长度(a / W)和粘合强度分别为0.46和20.2 MPa。

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