D. Goettler, Amit Savkar, K. D. Murphy, Z. Leseman
{"title":"Repair of Stiction Failed MEMS Using Structural Vibrations","authors":"D. Goettler, Amit Savkar, K. D. Murphy, Z. Leseman","doi":"10.1115/IMECE2007-43622","DOIUrl":null,"url":null,"abstract":"It has been shown in recent times that the use of structural vibrations is a viable approach in repairing stiction failed MEMS cantilever beams. It has also been observed that such a technique is sensitive to various parametric values associated with the de-sticking of these beams. In the current paper we present experimental results which characterize the ideal cantilever beam. An analytical model of stiction failed MEMS cantilever beams under electrostatic actuation is presented. Physical parameters such as stiffness, bending rigidity, damping, excitation voltage, etc. are incorporated in terms of Mathieu parameters to study the stability of the system. An experimental characterization of natural frequency, Young’s Modulus, and damping ratio, which form important components of the analysis, is presented. Accompanying these results is a description of the experimental set up used for finding these parameters. Experiments were performed at both atmospheric and vacuum pressures. An interferometric microscope mounted above the glass window of the vacuum chamber was used to determine the crack length of each beam and observe the profiles of the arrays of microcantilevers in-situ. A Laser Doppler Vibrometer was used for determination of characterization parameters. The microcantilevers were fabricated using the SUMMiT IV process of Sandia National Laboratories. Structural vibrations were induced by placing an alternating voltage on a cofabricated actuation pad located under the microcantilevers near their anchor point. Theoretical modeling shows the dependence of physical parameters that lead to stiction repair.Copyright © 2007 by ASME","PeriodicalId":315415,"journal":{"name":"2008 GSW Proceedings","volume":"69 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2008 GSW Proceedings","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/IMECE2007-43622","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2
利用结构振动修复粘滞故障的MEMS
近年来的研究表明,结构振动是修复MEMS悬臂梁的一种可行方法。还观察到,这种技术对与这些梁的脱粘有关的各种参数值很敏感。本文给出了表征理想悬臂梁的实验结果。提出了静电驱动下MEMS悬臂梁的伸缩失效解析模型。将刚度、抗弯刚度、阻尼、励磁电压等物理参数纳入Mathieu参数,研究系统的稳定性。给出了固有频率、杨氏模量和阻尼比的实验表征,这是分析的重要组成部分。随附这些结果是用于寻找这些参数的实验设置的描述。实验是在大气和真空压力下进行的。安装在真空室玻璃窗上方的干涉显微镜测量了每根梁的裂纹长度,并现场观察了微悬臂阵列的轮廓。采用激光多普勒测振仪测定表征参数。微悬臂梁采用桑迪亚国家实验室的SUMMiT IV工艺制造。结构振动是通过在微悬臂下靠近其锚点的共同制造的驱动垫上放置交流电压来诱导的。理论建模表明,导致粘滞修复的物理参数的依赖性。ASME版权所有©2007
本文章由计算机程序翻译,如有差异,请以英文原文为准。