Modelling of health monitoring signals and detection areas for aerospace structures

Jan Šplíchal, J. Hlinka
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Abstract

This paper is focused on Structural Health Monitoring (SHM) for aerospace use. It analyses the performance of commercially available finite element (FE) software packages for the simulation of propagation of ultrasonic guided waves (UGW) in typical aerospace structures. The purpose of the research is to support activities leading to the introduction of UGW based health monitoring on aerospace structures, as well as to support the design of future structures with integrated health monitoring. Activities are demonstrated on panels with growing complexity (adding different materials, sensors, damage types etc.). FE simulations are used to identify “detection areas” of UGW sensors. This output can be directly applied to the design of future aerospace structures with an integrated SHM system (to ensure the proper planning of the placement of UGW sensors).
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航空航天结构健康监测信号和探测区域的建模
本文主要研究航空航天结构健康监测(SHM)。分析了市售的超声导波在典型航空结构中传播仿真有限元软件包的性能。这项研究的目的是支持导致在航空航天结构上引入基于超重力重力的健康监测的活动,以及支持设计具有综合健康监测的未来结构。活动在越来越复杂的面板上进行演示(添加不同的材料、传感器、损坏类型等)。利用有限元模拟来识别超重力波传感器的“探测区域”。该输出可以直接应用于未来航空航天结构的集成SHM系统的设计(以确保正确规划UGW传感器的放置)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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