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Reliability of Cu wire bonds in microelectronic packages

机译:微电子封装中铜丝键合的可靠性

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In this study the thermo-mechanical response of 25 mu m Cu wire bonds in an LQFP-EPad (Low Profile Quad Flat Exposed Pad) package was investigated by numerical and experimental means. The aim was to develop a methodology for fast evaluation of the packages, with focus on wire bond fatigue, by combining finite element analysis (FEA) and mechanical fatigue testing. The investigations included the following steps: (i) simulation of the warpage induced displacements in the encapsulated LQFP-176-Epad package due to temperature changes, (ii) reproducing the thermally induced stresses in the wire bond loops in an unmolded (non-encapsulated) LQFP package using an accelerated multiaxial mechanical fatigue testing set-up under the displacement amplitudes determined in case (i) and determination of the loading cycles to failure (N-f), (iii) FEA of the experiments performed in (ii) based on the boundary conditions determined in (i) to calculate the states of stress and strain in the wire bonds subjected to multiaxial mechanical cyclic loading. Our investigations confirm that thermal and mechanical cyclic loading results in occurrence of high plastic strains at the heat affected zone (HAZ) above the nail-head, which may lead to fatigue failure of the wire bonds in the packages. The lifetime of wire bonds show a proportional relation between the location and angle of the wire bond to the direction of loading. The calculated accumulated plastic strain in the HAZ was correlated to the experimentally determined N-f values based on the volume weighted averaging (VWA) approached and presented in a lifetime diagram (Delta d - N-f) for reliability assessment of Cu wire bonds. The described accelerated test method could be used as a rapid qualification test for the determination of the lifetimes of wire bonds at different positions on the chip as well as for related improvements of package design. (C) 2017 Elsevier Ltd. All rights reserved.
机译:在这项研究中,通过数值和实验方法研究了LQFP-EPad(低轮廓四方扁平裸露焊盘)封装中25μm铜丝键合的热机械响应。目的是通过结合有限元分析(FEA)和机械疲劳测试,开发一种用于快速评估封装的方法,重点是引线键合疲劳。研究包括以下步骤:(i)模拟由于温度变化导致的封装的LQFP-176-Epad封装中的翘曲引起的位移,(ii)在未模制(未封装)中重现引线键合环中的热诱发应力。 )LQFP封装,使用加速多轴机械疲劳测试装置,在情况(i)中确定的位移幅度下确定失效的载荷循环(Nf),(iii)在(ii)中基于(i)中确定的边界条件,以计算承受多轴机械循环载荷的引线键合中的应力和应变状态。我们的研究证实,热和机械循环载荷会在钉头上方的热影响区(HAZ)处产生高塑性应变,这可能导致包装中引线键的疲劳失效。焊线的寿命显示焊线的位置和角度与负载方向之间的比例关系。基于接近的体积加权平均数(VWA),将在热影响区中计算出的累积塑性应变与实验确定的N-f值相关,并以寿命图(Delta d-N-f)表示,以评估Cu引线键合的可靠性。所描述的加速测试方法可以用作快速鉴定测试,以确定芯片上不同位置的引线键合的寿命以及封装设计的相关改进。 (C)2017 Elsevier Ltd.保留所有权利。

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