高温长期时效下环氧模塑复合材料疲劳裂纹扩展特性研究

P. Lall, Yunli Zhang, J. Suhling, J. Williamson, P. Thompson
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引用次数: 1

摘要

动态力学分析,如拉力试验,可用于研究高分子材料的疲劳破坏。通过增加动态应变或应力幅值,可以表征材料的疲劳和破坏。二氧化硅填充环氧树脂模塑化合物广泛应用于现代电子工业中,以保护硅片免受机械、化学和热效应的影响。关于能够长时间(10万小时)在高温下存活的塑料封装电子元件的疲劳可靠性的信息不足。本文介绍了疲劳效应测量的具体步骤。断裂韧性试验方法采用Feddersen法。对原始试样进行了低周疲劳试验。研究了几种环氧树脂模塑复合材料在持续高温长期时效作用下的老化效果。两种流行的模塑化合物,EMC-1和EMC-2,在三种老化温度下进行了研究:100℃,低于玻璃化转变温度,150℃,高于玻璃化转变温度,从原始到120天老化。记录和讨论了在恒定或增加应力或应变下的裂纹扩展。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Characterization of Fatigue Crack Growth of Epoxy Molding Compounds Under High-Temperature Long-Term Aging
Dynamic mechanical analysis such as tension test allows for studying the fatigue failure of polymer materials. By increasing the dynamic strain or stress amplitude, the fatigue and failure of material could be characterized. Silica-filled epoxy molding compounds are widely used in modern electronic industry, to protect the silicon chip from mechanical, chemical and thermal effects. There is insufficient information on fatigure reliability of plastic encapsulated electronic components capable of surviving high temperatures for long periods (>100,000 hours). In this paper, the details of the procedure for fatigue effect measurement are described. Feddersen’s approach for fracture toughness test method is applied. Low cycle fatigue is investigated for pristine samples. The aging effects of a number of epoxy molding compounds subjected to sustained high-temperature long-term aging have been studied. Two popular molding compounds, EMC-1 and EMC-2, are studied under three aging temperatures: 100C, below the glass transition temperature, and 150 °C, above the glass transition temperature, from pristine to 120 days aging. The crack propagation under constant or increasing stress or strain has been recorded and discussed.
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