首页> 外文会议>Conference on smart sensor phenomena, technology, networks, and systems integration >Investigation of a cross-correlation based optical strain measurement technique for detecting radial growth on a rotating disk
【24h】

Investigation of a cross-correlation based optical strain measurement technique for detecting radial growth on a rotating disk

机译:基于互相关的光学应变测量技术的研究,用于检测旋转磁盘上的径向增长

获取原文

摘要

The Aeronautical Sciences Project under NASA's Fundamental Aeronautics Program is extremely interested in the development of novel measurement technologies, such as optical surface measurements in the internal parts of a flow path, for in situ health monitoring of gas turbine engines. In situ health monitoring has the potential to detect flaws, i.e. cracks in key components, such as engine turbine disks, before the flaws lead to catastrophic failure. In the present study, a cross-correlation imaging technique is investigated in a proof-of-concept study as a possible optical technique to measure the radial growth and strain field on an already cracked sub-scale turbine engine disk under loaded conditions in the NASA Glenn Research Center's High Precision Rotordynamics Laboratory. The optical strain measurement technique under investigation offers potential fault detection using an applied high-contrast random speckle pattern and imaging the pattern under unloaded and loaded conditions with a CCD camera. Spinning the cracked disk at high speeds induces an external load, resulting in a radial growth of the disk of approximately 50.0-μm in the flawed region and hence, a localized strain field. When imaging the cracked disk under static conditions, the disk will be undistorted; however, during rotation the cracked region will grow radially, thus causing the applied particle pattern to be 'shifted'. The resulting particle displacements between the two images will then be measured using the two-dimensional cross-correlation algorithms implemented in standard Particle Image Velocimetry (PIV) software to track the disk growth, which facilitates calculation of the localized strain field. In order to develop and validate this optical strain measurement technique an initial proof-of-concept experiment is carried out in a controlled environment. Using PIV optimization principles and guidelines, three potential speckle patterns, for future use on the rotating disk, are developed and investigated in the controlled experiment. A range of known shifts are induced on the patterns; reference and data images are acquired before and after the induced shift, respectively, and the images are processed using the cross-correlation algorithms in order to determine the particle displacements. The effectiveness of each pattern at resolving the known shift is evaluated and discussed in order to choose the most suitable pattern to be implemented onto a rotating disk in the Rotordynamics Lab. Although testing on the rotating disk has not yet been performed, the driving principles behind the development of the present optical technique are based upon critical aspects of the future experiment, such as the amount of expected radial growth, disk analysis, and experimental design and are therefore addressed in the paper.
机译:NASA基础航空计划下的航空科学项目对新型测量技术的发展非常感兴趣,例如用于燃气轮机发动机原位健康监测的流路内部光学表面测量等。在缺陷导致灾难性故障之前,就地健康监测具有检测缺陷的潜力,即关键组件(例如发动机涡轮盘)中的裂纹。在本研究中,在概念验证研究中对互相关成像技术进行了研究,作为一种可能的光学技术,以测量在美国航空航天局(NASA)加载条件下已经破裂的子级涡轮发动机盘上的径向生长和应变场格伦研究中心的高精度转子动力学实验室。正在研究的光学应变测量技术可通过应用高对比度随机散斑图来进行潜在的故障检测,并利用CCD摄像机在空载和空载条件下对该图案进行成像。高速旋转破裂的磁盘会引起外部负载,从而导致磁盘在缺陷区域的径向增长约为50.0μm,因此会产生局部应变场。在静态条件下对破裂的磁盘进行成像时,该磁盘将不会变形。但是,在旋转过程中,裂纹区域将沿径向生长,从而导致所施加的粒子图案“移动”。然后,将使用在标准粒子图像测速(PIV)软件中实现的二维互相关算法来测量两个磁盘之间产生的粒子位移,以跟踪磁盘的生长,这有助于计算局部应变场。为了开发和验证这种光学应变测量技术,在受控环境中进行了初步的概念验证实验。使用PIV优化原则和指南,开发了三种潜在的斑点图案,供以后在旋转磁盘上使用,并在受控实验中进行了研究。图案上会感应出一系列已知的偏移。分别在引起偏移之前和之后获取参考图像和数据图像,并使用互相关算法处理图像以确定粒子位移。在Rotordynamics实验室中,评估并讨论了每种模式在解决已知偏移方面的有效性,以便选择最合适的模式以实施到旋转磁盘上。尽管尚未对旋转盘进行测试,但当前光学技术发展的驱动原理基于未来实验的关键方面,例如预期的径向增长量,盘分析和实验设计,并且因此在本文中讨论。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号