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Microstructural evolutions of Sn-3.0Ag-0.5Cu solder joints during thermal cycling

机译:Sn-3.0Ag-0.5Cu焊点在热循环过程中的组织演变

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Temperature-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 harsh loadings. 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 thermomechanical behavior when subjected to temperature variations. As solder joints mechanical properties are dependent of their microstructural characteristics, developing accurate solder joint fatigue models means to correctly capture the microstructural changes that undergo the solder alloy during thermal cycling. This study reports the Sn3.0Ag0.5Cu (SAC305) solder joints microstructural evolution during damaging temperature cycles. Electron BackScatter Diffraction (EBSD) analysis was conducted to assess the SAC305 microstructure corresponding to a specific damage level. Investigated microstructural features included the beta-Sn grain size and crystallographic orientation, as well as the grain boundary misorientation and Ag3Sn intermetallic compound (IMC) size. As-refiowed and damaged components were also mechanically characterized using nanoindentation technique. The microstructural analysis of SAC305 solder joints prior to thermal cycling showed a highly textured microstructure characteristic of hexa-cyclic twinning with two beta-Sn morphologies consisting of preferentially orientated macrograins known as Kara's beach ball, along with smaller interlaced grains. The main observation is that recrystallization systematically occurred in SAC305 solder joints during thermal cycling, creating a high population of misoriented grain boundaries leading to intergranular crack initiation and propagation in the high strain regions. The recrystallization process is accompanied with a progressive loss of crystallographic texture and twinning structure. Ag3Sn IMCs coalescence is another strong indicator of SAC305 solder damage since the bigger and more spaced the IMCs are the less dislocation pinning can prevent recrystallization from occurring.
机译:对于航空航天和军事工业来说,温度引起的焊点疲劳是主要的可靠性问题,因为在航空航天和军事工业中,需要在现场使用的电子设备在苛刻的负载下保持功能正常。由于RoHS指令最终将阻止铅在电子系统中的使用,因此需要更好地了解温度变化时无铅热机械行为。由于焊点的机械性能取决于它们的微结构特征,因此开发精确的焊点疲劳模型意味着可以正确捕获在热循环过程中经历焊锡合金的微结构变化。这项研究报告了在破坏性温度循环过程中Sn3.0Ag0.5Cu(SAC305)焊点的微观结构演变。进行了电子背散射衍射(EBSD)分析,以评估对应于特定损伤水平的SAC305微观结构。研究的微观结构特征包括β-Sn晶粒尺寸和晶体学取向,以及晶界取向错误和Ag3Sn金属间化合物(IMC)尺寸。使用纳米压痕技术还可以对送出和损坏的部件进行机械表征。热循环之前SAC305焊点的微观结构分析显示,六环孪晶具有高度织构化的微观结构特征,具有两个β-Sn形态,包括优先取向的大晶粒(称为Kara的沙滩球)以及较小的交错晶粒。主要观察结果是,SAC305焊点在热循环过程中会系统地发生重结晶,从而产生大量取向错误的晶界,从而导致晶间裂纹在高应变区发生并扩展。重结晶过程伴随晶体结构和孪晶结构的逐渐丧失。 Ag3Sn IMC的聚结是SAC305焊料损坏的另一个有力指标,因为IMC越大且间距越大,位错钉扎越少,就可以防止重结晶的发生。

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