研究环境温度对基于振动的SHM特征一致性的影响

T. Dardeno, M. Haywood-Alexander, R. Mills, L. Bull, N. Dervilis, K. Worden
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引用次数: 3

摘要

结构健康监测(SHM)系统已经在多个工程应用中实施,并且SHM仍然是一个活跃的研究领域,旨在提高这些结构的安全性、可靠性和管理。然而,一些挑战限制了SHM技术的实际实施和推广,例如操作和环境波动、可重复性问题以及边界条件的变化。这些不一致对于基于机器学习的SHM来说可能是有问题的,因为健康状态可能被错误地标记为损坏,或者损坏状态可能被错误地分类为正常变化。同样,制造差异也会导致相似结构之间的差异。考虑这些变化对于基于种群的SHM方法(PBSHM)尤其重要,PBSHM寻求在类似结构中传递有价值的信息,包括正常操作条件和损坏状态。这项工作旨在量化这种可变性,并评估当这些偏差发生时SHM的适用性。本文讨论了在一组全尺寸复合材料滑翔机机翼上通过一系列测试收集振动数据的实验活动。测试在多种环境温度下进行,并在真实和模拟的损伤条件下进行。检查机翼的频率响应函数以确定固有频率的变化。
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INVESTIGATING THE EFFECTS OF AMBIENT TEMPERATURE ON FEATURE CONSISTENCY IN VIBRATION-BASED SHM
Structural health monitoring (SHM) systems have been implemented across multiple engineering applications, and SHM remains an active area of research addressing the improved safety, reliability, and management of these structures. Several challenges, however, have limited the practical implementation and generalisation of SHM technologies, such as operational and environmental fluctuations, repeatability issues, and changes in boundary conditions. These inconsistencies can be problematic for SHM based on machine learning, as healthy states may be incorrectly flagged as damaged, or damaged states may be misclassified as normal variations. Likewise, manufacturing differences can result in variation among similar structures. Accounting for these variations is especially important for a population-based approach to SHM (PBSHM), which seeks to transfer valuable information, including normal operating conditions and damage states, across similar structures. This work aims to quantify this variability, and evaluate the applicability of SHM when these deviations occur. In this paper, an experimental campaign is discussed, in which vibration data were collected over a series of tests on a set of full-scale, composite glider wings. Tests were performed at multiple ambient temperatures, and with real and simulated damage conditions. The frequency response functions of the wings are examined to identify changes in natural frequency.
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