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Interfacial Reaction and Failure Mechanism of SAC/Co-P Solder Joint under Rapid Thermal Fatigue

机译:SAC / Co-P焊点在快速热疲劳下的界面反应和破坏机理

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In this paper, the interfacial reaction and failure mechanism of SAC305/Co-P solder joint under rapid thermal fatigue loading was studied. The Co-P UBM with P (phosphorus) concentrations of 3% and 6% were prepared on BGA substrate by ultrasonic assisted electro-deposition process. Sn3.0wt.%Ag-0.5%Cu (SAC305) BGA solder ball were reflowed on Co-P finishes to form SAC/Co-P solder joints. This solder joints were used to conduct rapid thermal shock test, With the application of electromagnetic induced heating and cooling circulation system, the solder joints were rapidly heated and cooled. After 4500 cycles of rapid thermal shock, the average thickness of the interfacial intermetallic compound (IMC) of SAC/Co-3% P increased from 2.012μm to 2.953μm. While the IMC of SAC/Co-6% P increases from 2.075μm to 2.377μm. The thickness of IMC increased slightly. The morphology of IMC changes due to the difference of P concentrations in Co-P UBM. As the number of shock cycles increases, the thickness of interfacal IMCs with higher P concentration is relatively stable. Through the comparative analysis of SAC/Co-6% P solder joints at different cycles, it was found that the cracks began to emerge at the outermost root of the solder joints. With the rapid thermal shock, the crack propagates between solder and interface. and the main direction of the propagation is horizontal with the direction of pad. The ultimate failure form is fatigue toughness failure. Experiments show that the solder joints still show regular fatigue failure mechanism under rapid thermal fatigue loading. Therefore, this establishes an important theoretical date for the failure mechanism of the new Co-P UBM interface under the rapid thermal fatigue system.
机译:本文研究了SAC305 / Co-P焊点在快速热疲劳载荷下的界面反应及破坏机理。通过超声辅助电沉积工艺在BGA衬底上制备了P(磷)浓度分别为3%和6%的Co-P UBM。将Sn3.0wt。%Ag-0.5%Cu(SAC305)BGA焊球回流到Co-P精加工上以形成SAC / Co-P焊点。该焊点用于进行快速的热冲击试验,在电磁感应加热和冷却循环系统的应用下,焊点被快速加热和冷却。经过4500次快速热冲击后,SAC / Co-3%P的界面金属间化合物(IMC)的平均厚度从2.012μm增加到2.953μm。而SAC / Co-6%P的IMC从2.075μm增加到2.377μm。 IMC的厚度略有增加。由于Co-P UBM中P浓度的差异,IMC的形态发生了变化。随着电击次数的增加,P浓度较高的界面IMC的厚度相对稳定。通过对SAC / Co-6%P焊点在不同周期下的比较分析,发现裂纹开始出现在焊点的最外层根部。随着快速的热冲击,裂纹在焊料和界面之间传播。传播的主要方向与垫的方向成水平。最终的破坏形式是疲劳韧性破坏。实验表明,在快速热疲劳载荷下,焊点仍显示出规则的疲劳破坏机理。因此,这为快速热疲劳系统下新型Co-P UBM界面的失效机理建立了重要的理论依据。

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