Studies on the thermal cycling reliability of fine pitch Cu/SnAg double-bump flip chip assemblies on organic substrates: Experimental results and numerical analysis

H.-Y Son, K. Paik, Il-ho Kim, Jin-Hyoung Park, Soon-Bok Lee, Gi-Jo Jung, Byung-Jin Park, Kwang-yoo Byun
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引用次数: 2

Abstract

A 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 firstly investigated and the failure mechanism was analyzed through correlation of T/C test and the finite element analysis (FEA) results. After 1000 thermal cycles, the T/C failure site was the Cu column/Si chip interface, where was identified via a FEA as the location of the maximum stress concentration during thermal cycling. During thermal cycling, the Al pad and Ti layer between the Si chip and Cu column bumps were displaced due to thermo-mechanical stress. Based on the low cycle fatigue model, the accumulation of equivalent plastic strain resulted in thermal fatigue deformation of the Cu column bumps, and ultimately reduced the thermal cycling lifetime. In addition, the normal plastic strain of the y-direction, 822, was determined to be compressive and was a dominant component in relation to the plastic deformation of Cu/SnAg double-bumps. As the number of thermal cycles increased, normal plastic strains in the perpendicular direction to the Si chip were accumulated on the Cu column bumps at the chip edge in the low temperature region. Thus it was found that displacement failure of the Al pad and Ti layer, the main T/C failure mode of the Cu/SnAg flip-chip assembly, occurred at the Si chip/Cu column interface by compressive normal deformation during thermal cycling. Next, the effect of Cu column height was investigated for the enhancement T/C reliability. As results of T/C test for 60 um and 85 um Cu column heights, flip chip assemblies with thicker Cu column height showed better T/C reliability. In the real time moire interferomerry, shear strain and normal strain of the x-direction was almost same regardless of Cu column height. On the other hand, the normal strain of y-direction (perpendicular direction to the Si chip) at Si chip/Cu column interface for 85 um-thick Cu samples shows significantly reduced value compared with 60 um-thick Cu samples. This relaxation of the normal plastic strain of the y-direction is the origin that thicker Cu column height guarantees better T/C reliability.
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有机基板上细间距Cu/SnAg双凸块倒装芯片热循环可靠性研究:实验结果与数值分析
基于厚铜柱的双凸点倒装芯片结构是一种很有前途的小间距倒装芯片应用方案。本研究首先对Cu/SnAg双碰撞倒装芯片组件的热循环可靠性进行了研究,并通过热循环试验与有限元分析(FEA)结果的相关性分析了其失效机理。经过1000次热循环后,T/C破坏部位为Cu柱/Si芯片界面,通过有限元分析确定该界面为热循环过程中最大应力集中的位置。在热循环过程中,由于热机械应力的作用,硅片和Cu柱凸起之间的Al衬垫和Ti层发生了位移。基于低周疲劳模型,等效塑性应变的积累导致铜柱凸点产生热疲劳变形,最终导致热循环寿命降低。此外,y方向的法向塑性应变为压缩应变822,是Cu/SnAg双凸点塑性变形的主导分量。随着热循环次数的增加,在低温区,垂直于硅片方向的正常塑性应变在芯片边缘的Cu柱凸起处积累。结果表明,在热循环过程中,Al衬垫和Ti层的位移破坏主要发生在Si片/Cu柱界面处,这是Cu/SnAg倒装芯片的主要T/C破坏模式。其次,研究了铜柱高度对提高T/C可靠性的影响。在铜柱高度为60 um和85 um时的T/C测试结果表明,铜柱高度越厚的倒装芯片具有更好的T/C可靠性。在实时云纹干涉测量中,无论铜柱高度如何,x方向的剪切应变和法向应变几乎相同。另一方面,与60 um-厚Cu试样相比,85 um-厚Cu试样的Si - chip/Cu柱界面y方向(垂直于Si - chip方向)法向应变明显减小。这种y向法向塑性应变的松弛是Cu柱高度越厚保证T/C可靠性越好的原因。
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