疲劳载荷和持续高温下芯片- uf FCBGA界面分层倾向的演变

P. Lall, A. Pandurangan, J. Williamson
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引用次数: 0

摘要

汽车引擎盖的应用越来越多地使用电子系统来实现安全和关键功能。在倒装芯片球栅阵列(FCBGA)封装中,下填充层(UF)在基板和晶片之间形成完整的机械支撑。此外,底部填充物保护芯片免受冲击、振动、湿气和辐射。下填充为焊料互连提供了巨大的机械支撑,并在温度漂移期间限制了塑料工作的数量。分层是在芯片- uf界面观察到的重要失效模式之一。Chip-UF界面在持续高温循环疲劳载荷下的研究尚未广泛开展。制备Chip-UF双材料样品,在100℃下进行长期高温时效,然后在四点弯曲疲劳载荷下进行测试。试件分别进行了30天、60天、90天、120天、180天的等温老化。通过试验确定了界面裂纹扩展速率与疲劳循环次数的关系。计算了每个试验条件下的稳态能量释放率和i型应力强度值的范围(ΔKI)。利用Paris幂律建立了裂纹扩展速率与应力强度因子范围的关系。根据关系确定Paris指数(A,n),以了解疲劳载荷下界面断裂韧性随老化天数的变化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Evolution of Propensity for Chip-UF FCBGA Interface Delamination Under Fatigue-Loading and Sustained High Automotive Temperatures
Underhood applications in automotive are increasingly using electronics systems for safety and critical functions. In flip-chip ball grid array (FCBGA) packages, underfill (UF) forms the integral mechanical support between the substrate and die. In addition, underfills protect the chip against shock, vibration, moisture, and radiation. Underfills provide great mechanical support to the solder interconnects and limit the amount of plastic work during temperature excursions. Delamination is of the significant failure modes observed at chip-UF interfaces. Chip-UF interfaces have not been studied widely under cyclic fatigue loading with sustained high-temperature exposure. Chip-UF bi-material samples are prepared and subjected to long-term high-temperature aging at 100°C and then tested under four-point bend fatigue loading. The specimens have been exposed to isothermal aging for 30 days, 60 days, 90 days, 120 days, and 180 days. The interfacial crack growth rate with respect to the number of fatigue cycles has been determined from the experiment. The steady-state energy release rate and range of mode-I stress intensity values (ΔKI) have been computed for each of the test conditions. Paris power law has been used to establish the relationship between the crack growth rate and the range of stress intensity factors. Paris exponents (A,n) are determined from the relationship to understand the evolution in interfacial fracture toughness with respect number of days of aging under fatigue loading.
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