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Investigating strain transfer in polymer coated structures for the health monitoring of aerospace vehicles using polymer photonic waveguides

机译:研究使用聚合物光子波导的聚合物涂层结构中的应变传递,以监测航空航天器的健康状况

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In this work, we present the concept of planar polymer photonic waveguides for the health monitoring of aerospace structures. Here a polymer layer is deposited onto the material/structure to be monitored. Within the polymer layer, waveguides are created after deposition. These waveguides can then be used as “optical fibres” for optical fibre sensing methodologies. In investigating the use of polymer photonic waveguides the question to be answered is: does the strain in the test material transfer to the polymer layer, such that the value to be measured optically is reliable and indicative of the true strain in the test structure? To answer this question we have conducted a preliminary structural analysis with finite element analysis, utilising ANSYS. A simple aluminium cantilever was used as the test structure, and layers of polyethylene with different thicknesses were added to this. Result show that the thinner the layer of polymer, the more accurate the measured strain will be. For a 100um coating, the difference is strain was observed to be on the order of 3.3%.
机译:在这项工作中,我们提出了用于航空航天结构健康监测的平面聚合物光子波导的概念。此处,聚合物层沉积在要监控的材料/结构上。在聚合物层内,沉积后会形成波导。这些波导然后可以用作光纤传感方法的“光纤”。在研究聚合物光子波导的使用时,需要回答的问题是:测试材料中的应变是否会转移到聚合物层上,从而使要进行光学测量的值可靠并指示测试结构中的真实应变?为了回答这个问题,我们利用ANSYS进行了带有有限元分析的初步结构分析。一个简单的铝悬臂用作测试结构,并向其中添加了不同厚度的聚乙烯层。结果表明,聚合物层越薄,测得的应变越准确。对于100um的涂层,差异是观察到的应变约为3.3%。

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