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Structural health monitoring and condition based fatigue damage prognosis of complex metallic structures.

机译:复杂金属结构的结构健康监测和基于条件的疲劳损伤预后。

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摘要

Current practice in fatigue life prediction is based on assumed initial structural flaws regardless of whether these assumed flaws actually occur in service. Furthermore, the model parameters are often estimated empirically based on previous coupon test results. Small deviations of the initial conditions and model parameters may generate large errors in the expected dynamical behavior of fatigue damage growth. Consequently, a large degree of conservatism is incorporated into structural designs due to these expected uncertainties. The current research in the area of Structural Health Monitoring (SHM) and probabilistic fatigue modeling can help in improved fatigue damage modeling and remaining useful life estimation (RULE) techniques. This thesis discusses an integrated approach of SHM and adaptive prognosis model that not only estimates the current health, but can also forecast the future health and calculate RULE of an aerospace structural component with high level of confidence. The approach does not assume any fixed initial condition and model parameters. This dissertation include the following novel contributions. 1) A Bayesian based off-line Gaussian Process (GP) model is developed, which is the core of the present condition based prognosis approach. 2) Different passive and active SHM approaches are used for on-line damage state estimation. Applications of passive sensing are shown to estimate the time-series fatigue damage states both under constant and random fatigue loading. It is found that there is a good correlation between estimated damage states and optically measured damage states. In addition, applications for both narrow and broadband active sensing approaches are presented to estimate smaller incipient damage. It is demonstrated that the active sensing techniques not only can identify smaller incipient damage but also can quantify fatigue damage during all the three stages (stages I , II, and III) of fatigue life. 3) An integrated on-line SHM and off-line GP predictive model is developed for real-time condition based damage state estimation of complex Aluminum structures under fatigue loading. It is found that the proposed technique can forecast the future damage states well before the final failure.
机译:疲劳寿命预测的当前实践是基于假定的初始结构缺陷,而不管这些假定的缺陷是否实际在使用中发生。此外,通常基于先前的试样测试结果凭经验估算模型参数。初始条件和模型参数的小偏差可能会在疲劳损伤增长的预期动力学行为中产生较大的误差。因此,由于这些预期的不确定性,在结构设计中加入了高度的保守性。结构健康监测(SHM)和概率疲劳建模领域的当前研究可以帮助改进疲劳损伤建模和剩余使用寿命估计(RULE)技术。本文讨论了SHM和自适应预测模型的集成方法,该方法不仅可以估计当前的健康状况,还可以预测未来的健康状况,并以高置信度来计算航空航天结构部件的RULE。该方法不假定任何固定的初始条件和模型参数。本论文包括以下新颖的贡献。 1)建立了基于贝叶斯的离线高斯过程(GP)模型,这是当前基于状态的预测方法的核心。 2)不同的被动和主动SHM方法用于在线损伤状态估计。显示了被动感测的应用,以估计恒定和随机疲劳载荷下的时间序列疲劳损伤状态。发现估计的损伤状态与光学测量的损伤状态之间具有良好的相关性。此外,还介绍了窄带和宽带有源传感方法的应用,以估计较小的初期损坏。结果表明,主动传感技术不仅可以识别较小的初期损坏,而且可以量化疲劳寿命的所有三个阶段(第一,第二和第三阶段)的疲劳破坏。 3)建立了基于在线SHM和离线GP的集成预测模型,用于基于复杂工况在疲劳载荷下基于实时条件的损伤状态估计。发现所提出的技术可以在最终失效之前预测未来的损坏状态。

著录项

  • 作者

    Mohanty, Subhasish.;

  • 作者单位

    Arizona State University.;

  • 授予单位 Arizona State University.;
  • 学科 Engineering Aerospace.;Engineering Mechanical.;Engineering Electronics and Electrical.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 208 p.
  • 总页数 208
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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