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Damage tolerant design and condition monitoring of composite material and bondlines in wind turbine blades: Failure and crack propagation

机译:风力涡轮机叶片中复合材料和粘合层的耐损伤设计和状态监测:失效和裂纹扩展

摘要

This research presents a novel method to asses a crack growing/damage event in composite material, in polymer, or in structural adhesive using Fibre Bragg Grating (FBG) sensors embedded in the host material, and its application in to a composite material structure: Wind Turbine Trailing Edge. A Structure-Material-Sensor Finite Element Method (FEM) model was developed to simulate the Fibre Bragg Grating sensor output response, when embedded in a host material (Composite material, polymer or adhesive), during a crack growing/damage event. This Structure-Material-Sensor model provides a tool to analyse the application of this monitoring technique in other locations/structures, by predicting the sensor output and deciding, based on this, the optimal sensor distribution/configuration.
机译:这项研究提出了一种使用嵌入主体材料中的光纤布拉格光栅(FBG)传感器评估复合材料,聚合物或结构胶中裂纹扩展/损坏事件的新方法,并将其应用于复合材料结构:风涡轮后缘。开发了一种结构-材料-传感器有限元方法(FEM)模型,以模拟在裂纹扩展/损坏事件中嵌入主体材料(复合材料,聚合物或粘合剂)时的光纤布拉格光栅传感器输出响应。该结构材料传感器模型提供了一种工具,可以通过预测传感器输出并基于此确定最佳传感器分布/配置来分析此监视技术在其他位置/结构中的应用。

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