Mechanical fatigue assessment of SAC305 solder joints under harmonic vibrations

J. Libot, L. Arnaud, O. Dalverny, J. Alexis, P. Milesi, F. Dulondel
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引用次数: 10

Abstract

Vibration-induced solder joint fatigue is a main reliability concern for aerospace and military industries whose electronic equipment used in the field is required to remain functional under such loading. Due to the RoHS directive which eventually will prevent lead from being utilized in electronic systems, there is a need for a better understanding of lead-free mechanical behavior under vibration conditions. This study reports the durability of Sn3.0Ag0.5Cu (SAC305) solder joints subjected to harmonic solicitations at three specific temperatures (-55°C, 20°C and 105°C). A test assembly is designed and consists in a single daisy-chained 1152 I/O ball grid array (FBGA1152) package assembled on a flame retardant (FR-4) printed circuit board (PCB). The vibration levels are imposed by a controlled deflection at the center of the board at its natural frequency. The electric continuity is monitored to determine the number of cycles to failure of each sample. Mode shape measurements with a scanning vibrometer are also conducted and correlated with Finite Element Analysis (FEA) to ensure accurate calculation of stress within the critical solder balls at the corners of the component. The failed specimens are then cross-sectioned in order to determine failure modes. A comparison of SAC305 durability with SnPb36Ag2 solder is given, along with a set of lifetime measurements for two complementary assemblies: 68 I/O Leadless Chip Carrier (LCC68) and 324 I/O Plastic Ball Grid Array (PBGA324). It turns out that SAC305 outperforms SnPb36Ag2 and the effect of temperature on the mechanical durability of SAC305 appears to be minor. Failure analysis points out different failure modes such as ductile and brittle cracks at the interface between the solder bulk and the component, along with pad cratering-induced copper trace failures. FEA calculations provide data to estimate the high cycle fatigue (HCF) behavior of SAC305 solder under harmonic vibrations.
SAC305焊点在谐波振动下的机械疲劳评价
振动引起的焊点疲劳是航空航天和军事工业的主要可靠性问题,这些工业中使用的电子设备需要在这种载荷下保持功能。由于RoHS指令最终将防止铅在电子系统中使用,因此需要更好地了解振动条件下的无铅机械行为。本研究报告了Sn3.0Ag0.5Cu (SAC305)焊点在三种特定温度(-55°C, 20°C和105°C)下受谐波影响的耐久性。设计了一个测试组件,由一个单一的菊状链1152 I/O球栅阵列(FBGA1152)封装组成,组装在阻燃(FR-4)印刷电路板(PCB)上。振动水平是由控制偏转在板的中心在其固有频率施加。监测电连续性以确定每个样品失效的循环次数。用扫描式测振仪进行模态振型测量,并与有限元分析(FEA)相关联,以确保精确计算组件角落处关键焊球内的应力。然后对破坏试样进行横截面以确定破坏模式。给出了SAC305耐久性与SnPb36Ag2焊料的比较,以及两种互补组件的一组寿命测量:68 I/O无铅芯片载体(LCC68)和324 I/O塑料球栅阵列(PBGA324)。结果表明,SAC305性能优于SnPb36Ag2,温度对SAC305机械耐久性的影响较小。失效分析指出了钎料块与元件界面处的韧性裂纹和脆性裂纹以及焊盘凹坑引起的铜迹失效等不同的失效模式。有限元计算为估计SAC305焊料在谐波振动下的高周疲劳(HCF)行为提供了数据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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