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首页> 外文期刊>Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology >Microstructure and fatigue damage mechanism of Fe Co-Ni-Al-Ti-Zr high-entropy alloy film by nanoscale dynamic mechanical analysis
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Microstructure and fatigue damage mechanism of Fe Co-Ni-Al-Ti-Zr high-entropy alloy film by nanoscale dynamic mechanical analysis

机译:Fe Co-Ni-Al-Ti-ZR高熵合金膜的微观结构和疲劳损伤机理通过纳米级动态力学分析

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摘要

Micro-electromechanical system (MEMS) films are subjected to a large number of impact during the working process. The fatigue life of the films need be measured to evaluate the reliability of the film's impact resistance. In this work, a new kind of MEMS soft magnetic non-equimolar high-entropy alloy (HEA) film (Fe-Co-Ni)(25)(Ti-Zr-Al)(75) was prepared by magnetron sputtering. The fatigue damage behaviors of the HEA film was investigated by nanoscale dynamic mechanical analysis (nanoDMA) technique. Scanning electron microscopy (SEM), X-ray diffraction (XRD) and transmission electron microscopy (TEM) were adopted to analyze the microstructure and damage surfaces pattern. The results showed that the HEA film displayed a polycrystalline structure with the fcc solid solution uniformly distributed in the amorphous phase. There were three stages during the process of fatigue damage, the compressional deformation stage, the buckling and layering stage, and the edge crack propagation leads to the delamination stage. The contact stiffness suddenly decreased at the moment of fatigue damage happening.
机译:微机电系统(MEMS)薄膜在工作过程中受到大量影响。需要测量薄膜的疲劳寿命以评估薄膜的抗冲击性的可靠性。在这项工作中,通过磁控溅射制备了一种新的MEMS软磁非等摩尔高熵高熵合金(HEA)膜(Fe-Co-Ni)(25)(Ti-Zr-Al)(75)。纳米级动态机械分析(纳米摩根)技术研究了HEA膜的疲劳损伤行为。采用扫描电子显微镜(SEM),X射线衍射(XRD)和透射电子显微镜(TEM)来分析微观结构和损坏表面图案。结果表明,HEA膜显示出具有在非晶相中均匀分布的FCC固溶体的多晶结构。在疲劳损伤过程中有三个阶段,压缩变形阶段,屈曲和分层阶段,并且边缘裂纹传播导致分层阶段。在发生疲劳损伤时,接触刚度突然下降。

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