超大2.5D基板上模制中间层(MIoS)封装集成-翘曲和可靠性

S. Nam, Younglyong Kim, Aeni Jang, I. Hwang, Sung-Pae Park, Su-chang Lee, Dae-woo Kim
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引用次数: 2

摘要

为了满足人工智能、数据中心等高端应用的需求,先进的封装技术得到了迅速发展。2.5D硅中间体技术一直是高端应用的解决方案,因为它具有异构器件集成兼容性:高带宽存储器(HBMs),逻辑器件或功能小芯片。在本研究中,成功展示了一种名为基板上模制中间层(MIoS)的2.5D结构封装,该封装具有超大硅中间层(>2800mm2),尺寸为85\ × 85\text{mm}^{2}$,由2个asic和8个hbm组装而成,具有更高的芯片集成能力。此外,还研究了超大尺寸2.5D MIoS封装的关键挑战,如模制中间层(MIP)模块的翘曲和受热机械应力影响的高可靠性。采用有限元法模拟了MIP的翘曲过程,在焊料熔化温度下,将MIP与衬底之间的翘曲差控制在50um以下。结果表明,60K的凸点数量在回流焊过程中获得了良好的连接质量。在热循环测试(- 55 ~ 125°C)下评估封装可靠性,以优化由组件热膨胀(CTE)不匹配引起的应力:衬底,下填料,环框架材料和环氧模具化合物(EMC)。早期的失效模式主要为下充填体裂纹和器件角部电磁兼容裂纹,但通过对元器件材料特性的研究,提高了封装级可靠性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Extremely Large 2.5D Molded Interposer on Substrate (MIoS) Package Integration - Warpage and Reliability
Advanced package technology has been developed rapidly to meet a demand of the high end application such as AI and datacenter. 2.5D silicon interposer technology has been focused as the solution, for high end applications because of its heterogeneous device integration compatibility: high bandwidth memories (HBMs), logic devices or functional chiplets. In this study, a 2.5D structure package called Molded Interposer on Substrate (MIoS) with an extremely large silicon interposer (>2800mm2) on the $85\times 85\text{mm}^{2}$ body size assembled with 2-ASICs and 8-HBMs was demonstrated successfully for higher chip integration capability. Also, the key challenges of extremely large size 2.5D MIoS package such as warpage of the molded interposer (MIP) module and high level of reliability subjected to thermo-mechanical stress were investigated. MIP warpage was simulated by finite element method (FEM) and controlled the warpage difference between MIP and substrate below 50um at solder melting temperature. As a result, the number of 60K bumps obtained the good joint quality during reflow bonding process. The package reliability was evaluated under thermal cycle test (−55∼125°C) for optimizing the stress induced by the mismatch of thermal expansion (CTE) of components: substrate, underfill, ring frame materials and epoxy mold compound (EMC). The primary failure modes were underfill crack and EMC crack at the corner of devices at the early stage but, through a study on components material properties, package level reliability was improved.
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