首页> 外文会议>2007 international conference on electronic materials and packaging >Thermal Cycling Reliability of Cu/SnAg Double-Bump Flip-chip Assemblies for 100um Pitch Applications
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Thermal Cycling Reliability of Cu/SnAg Double-Bump Flip-chip Assemblies for 100um Pitch Applications

机译:用于100um间距应用的Cu / SnAg双凸块倒装芯片组件的热循环可靠性

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Thick Cu column based double-bump flip-chip structure is one of the promising alternatives for fine pitch flip-chip applications. In this study, the thermal cycling (T/C) reliability of Cu/SnAg double-bump flip-chip assemblies was mainly investigated and the failure mechanism was analyzed through the correlation of T/C test results and the finite element analysis (FEA). T/C failures occurred from the outmost Cu/SnAg flip-chip joints with largest distance of the neutral point (DNP) of a chip. After 1000 cycles, all of the failures occurred at about 4~7 Cu/SnAg joints located at the edge and corner of a chip. SAM (scanning acoustic microscope) analysis and SEM (scanning electron microscope) observation indicated that the failure site was Cu column/Si chip interface and the displacement of Al and Ti layer of Cu/Si interface due to large compressive stress. From the FEA, the maximum stress was concentrated at Cu column/Si chip interface during thermal cycling. From the low cycle fatigue model, the accumulation of the equivalent plastic strain resulted in the thermal fatigue deformation of Cu column bumps and finally reduced the thermal cycling lifetime. As the number of thermal cycles increased, the maximum equivalent plastic strains of each joint increased at from the outmost joints to the 4th ~ 7th joints which showed T/C failures after 1000 cycles. However, equivalent plastic strains did not increase regardless of thermal cycles. In addition, a normal stress of y-direction, S_(22) was a dominant component determining overall stress of Cu/SnAg flip-chip joints and it was compressive. During thermal cycling, the compressive normal stress in low temperature region was mainly inflicted on Cu column bumps in perpendicular direction (y-direction in 2-D FEA) to a chip and Cu column bumps. As a result, the displacement failure of Al and Ti layer, the main T/C failure mode of Cu/SnAg flip-chip assembly, occurred between Si chip and Cu column interface by the compressive normal stress.
机译:基于厚铜柱的双凸点倒装芯片结构是用于小间距倒装芯片应用的有前途的替代产品之一。本研究主要研究Cu / SnAg双凸块倒装芯片组件的热循环(T / C)可靠性,并通过T / C测试结果与有限元分析(FEA)的相关性分析失效机理。 。 T / C故障发生在最远的Cu / SnAg倒装芯片接头处,其芯片中性点(DNP)的距离最大。经过1000次循环后,所有故障都发生在位于芯片边缘和角落的大约4〜7个Cu / SnAg接头处。 SAM(扫描声显微镜)分析和SEM(扫描电子显微镜)观察表明,破坏点是Cu柱/ Si芯片界面,并且由于较大的压应力导致Cu / Si界面的Al和Ti层位移。从FEA,最大应力集中在热循环过程中的Cu柱/ Si芯片界面。根据低循环疲劳模型,等效塑性应变的累积导致铜柱凸块的热疲劳变形,并最终缩短了热循环寿命。随着热循环次数的增加,每个接头的最大等效塑性应变在从最外侧的接头到第4〜7个接头处增加,这表明在1000次循环后T / C失效。但是,无论热循环如何,等效塑性应变均不会增加。此外,y方向的法向应力S_(22)是决定Cu / SnAg倒装芯片接头整体应力的主要成分,它是压缩性的。在热循环过程中,低温区域的压缩法向应力主要施加在垂直于芯片和Cu柱凸点的方向(二维FEA中的y方向)上的Cu柱凸点上。结果,Al和Ti层的位移破坏,即Cu / SnAg倒装芯片组件的主要T / C破坏模式,在硅片和Cu柱界面之间由于压缩法向应力而发生。

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