首页> 外文会议>Conference on Smart Materials II, Dec 16-18, 2002, Melbourne, Australia >Finite element modeling to determine thermal residual strain distribution of bonded composite repairs for structural health monitoring design
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Finite element modeling to determine thermal residual strain distribution of bonded composite repairs for structural health monitoring design

机译:有限元建模,以确定粘结复合材料修补物的热残余应变分布,以进行结构健康监测设计

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The economic implication of fleet upgrades, particularly in Australia with military aircraft such as the F-111 and F/A-18, has led to an increasing reliance on composite repair technology to address fatigue and corrosion-affected aircraft components. The increasing use of such repairs has led to a research effort to develop various in―situ health monitoring systems that may be incorporated with a repair. This paper reports on the development of a theoretical methodology that uses finite element analysis (FEA) to model the strain profiles which optical sensors, on or within the patch, will be exposed to under various operational scenarios, including load and disbond. Numerical techniques are then used to predict the fibre Bragg grating (FBG) reflections which occur with these strain profiles. The quality of these reflection are a key consideration when designing FBG based structural health monitoring (SHM) systems. This information can be used to optimise the location of both surface mounted, and embedded sensors, and determine feasibility of SHM system design. Research was conducted into the thermal residual strain (TRS) within the patch. A finite element study revealed the presence of significant thermal residual strain gradients along the surface of the tapered region of the patch. As Bragg gratings are particularly sensitive to strain gradients, (producing a result similar to a chirped grating) the strain gradient on the composite at potential sensor locations both under load, and in the event of disbond was considered. A sufficiently high gradient leads to an altered Bragg reflection. These spurious reflections need to be considered, and theoretically obtained reflections can provide information to allow for load scenarios where the Bragg shift is not a smooth, well defined peak. It can also be shown that embedded fibres offer a higher average thermal residual strain reading, while being subject to a much lower strain gradient. This particularly favors the optical disbond detection system that is being developed. While certification concerns exist with embedding sensors in repairs, this study shows that embedded optical fibre sensors may provide for a health monitoring system with enhanced reliability and sensitivity.
机译:机队升级的经济意义,尤其是在澳大利亚使用F-111和F / A-18等军用飞机的情况下,已导致人们越来越依赖复合材料修复技术来解决疲劳和受腐蚀影响的飞机部件。此类维修的使用日益增加,导致人们进行了研究工作,以开发可能与维修结合在一起的各种现场健康监测系统。本文报告了一种理论方法的发展,该理论方法使用有限元分析(FEA)来建模应变曲线,在包括负载和剥离在内的各种操作场景下,贴片上或贴片内的光学传感器将暴露于其中。然后使用数值技术来预测随这些应变曲线而发生的光纤布拉格光栅(FBG)反射。在设计基于FBG的结构健康监测(SHM)系统时,这些反射的质量是关键考虑因素。该信息可用于优化表面安装传感器和嵌入式传感器的位置,并确定SHM系统设计的可行性。对贴片内的热残余应变(TRS)进行了研究。有限元研究表明,沿着贴片锥形区域的表面存在明显的热残余应变梯度。由于布拉格光栅对应变梯度特别敏感(产生的结果类似于a光栅),因此考虑了在载荷作用下以及在发生剥离时复合材料在潜在传感器位置处的应变梯度。足够高的梯度会导致布拉格反射发生变化。需要考虑这些杂散反射,并且理论上获得的反射可以提供信息,以支持布拉格位移不是平滑且定义明确的峰值的负载情况。还可以表明,包埋的纤维具有更高的平均平均热残余应变读数,同时具有较低的应变梯度。这特别有利于正在开发的光学剥离检测系统。尽管在维修中存在嵌入传感器的认证问题,但这项研究表明,嵌入式光纤传感器可以为健康监控系统提供更高的可靠性和灵敏度。

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