MEMS悬臂梁对金属薄膜高周疲劳试验的影响

N. Jöhrmann, C. Stöckel, B. Wunderle
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引用次数: 0

摘要

铝仍然是像mosfet或igbt这样的电力电子芯片最重要的接触金属化之一。由于铝和硅或碳化硅之间的热膨胀系数(CTEs)差异很大,并且在高功率瞬态时热点产生的温度,这些层容易因热机械疲劳而失效。通常,寿命评估是通过将专用测试样品进行标准化压力测试(例如热循环)来完成的。本文建立在先前的工作基础上,通过等温机械载荷,使用Si MEMS悬臂梁作为样品载体,对高周疲劳状态下的铝薄膜进行加速应力测试和寿命建模。疲劳膜的表面粗糙度先前通过原子力显微镜(AFM)和扫描电子显微镜(SEM)作为失效参数进行测量。通过与从有限元模拟中获得的等效塑性应变进行比较,得出了基于失效物理的可靠性范式,该范式显示了表面粗糙度与累积塑性应变之间的关系。通过使用包含两个AlN压电的新设计,现在可以实现闭环控制,而无需外部激振器和光学装置来测量疲劳期间的悬臂幅值。这也使得原位应力测试更容易,例如在SEM内或光学显微镜下,以进一步了解薄铝随着时间的推移降解的发展。采用新设计进行了107次加速应力试验,并将光学显微镜测得的表面粗糙度与有限元模拟结果进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
MEMS Cantilever on High-Cycle Fatigue Testing of thin Metal Films
Aluminium is still one of the most important contact metallisation for power electronic chips like MOSFETs or IGBTs. With a large difference in thermal expansion coefficients (CTEs) between aluminium and silicon or silicon carbide, and the temperatures generated in hot-spots during high power transients, these layers are prone to failure due to thermo-mechanical fatigue. Usually lifetime assessment is done by subjecting dedicated test specimens to standardised stress tests as e.g. thermal cycling. This paper builds on previous work about a method for accelerated stress testing and lifetime modelling of thin aluminium films in the high-cycle fatigue regime by isothermal mechanical loads using Si MEMS cantilevers as sample carriers. Surface roughness of the fatigued films was previously measured as a failure parameter, both via atomic force microscopy (AFM) and scanning electron microscopy (SEM). This was motivated within a physics-of-failure based reliability paradigm by comparison with equivalent plastic strain obtained from finite element simulations, which show a relation between surface roughness and the cumulated plastic strain. By using a new design including two AlN piezos, it is now possible to realize a closed loop control without the need for an external shaker and an optical setup to measure the cantilever amplitude during the fatiguing. This also enables easier Insitu stress testing, e.g. inside a SEM or below an optical microscope, to gain further insight into the development of degradation of the thin aluminium over time. An accelerated stress test with 107 cycles using the new design is presented, and surface roughness obtained via optical microscopy is compared with finite element simulations.
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