首页> 外文会议>Proceedings of the American Society for Composites Twenty-Ninth technical conference, Proceedings of the 16th US-JAPAN conference on composite materials ASTM-D30 meeting >Evaluation of the Thermal Damage in Glass Fiber Polymer-Matrix Composites in Wind Turbine Blades Subjected to Lightning Strike
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Evaluation of the Thermal Damage in Glass Fiber Polymer-Matrix Composites in Wind Turbine Blades Subjected to Lightning Strike

机译:雷击对风力涡轮机叶片中玻璃纤维聚合物基复合材料热损伤的评估

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摘要

A primary motivation for this study comes from the need to improve the ability ofrnpolymer matrix composites to withstand lightning strikes. In particular, we arernconcerned with lightning strike damage in composite wind turbine blades. Thernproblem is essentially multiphysic, as the electric-current-induced temperature in therncomposite blade subjected to a lightning strike may reach up to 1,200 ℃, leading tornextensive thermal damage including surface damage, delamination, cracks, matrixrndecomposition, fiber breakage and sublimation, and abrupt failure of the blade.rnIn this work, the thermal response of the polymer-matrix composite laminate usedrnin a Sandia 100-meter All-glass Baseline Wind Turbine Blade (SNL 100-00) subjectedrnto lightning strike is studied. The tip region composite panel is considered, as it hasrnbeen reported in the literature that the blade tip is more susceptible to lightning strike than the remaining parts of the blade.rnA physical model to show the surface interaction between the lightning arc and therncomposite structure has been developed. The model provides time- and electriccurrent-rndependent variation of the lightning arc radius and lightning-current-inducedrnheat flux generated at the composite surface. The temperature-dependent thermalrnproperties of the VectorPly E-LT 5500 unidirectional [0]_2 E-glass fiber vinyl esterrnresin matrix fabric and SNL triaxial [±45]_2[0]_2 E-glass fiber vinyl ester resin matrixrnfabric used in the wind blade tip composite panel were derived using availablernexperimental data. The formulated nonlinear transient heat transfer problem withrnmoving boundary is solved using the finite element method. The solution procedurernaccounts for phase transitions in the materials, and the obtained results includerntemperature field profiles and evolution of the thermal damage.
机译:这项研究的主要动机是需要提高聚合物基复合材料承受雷击的能力。特别是,我们对复合材料风力涡轮机叶片中的雷击损坏感到担忧。该问题本质上是多物理场的,因为受到雷击的电流在复合刀片中产生的温度可能高达1200℃,从而导致广泛的热损伤,包括表面损伤,分层,裂纹,基体分解,纤维断裂和升华以及突然失效。在这项工作中,研究了经受雷击的Sandia 100米全玻璃基线风力涡轮机叶片(SNL 100-00)中使用的聚合物基复合材料层压板的热响应。考虑到尖端区域复合板,因为在文献中已经报道了叶片尖端比叶片的其余部分更容易受到雷击。物理模型表明了雷电弧与复合结构之间的表面相互作用发达。该模型提供了在复合表面产生的雷电半径和雷电流引起的热通量随时间和电流的变化。叶片中使用的VectorPly E-LT 5500单向[0] _2电子玻璃纤维乙烯基酯树脂基布和SNL三轴[±45] _2 [0] _2电子玻璃纤维乙烯基酯树脂基布的随温度变化的热性能尖端复合板是使用可用的实验数据得出的。用有限元方法解决了边界不固定的非线性瞬态传热问题。求解过程考虑了材料中的相变,获得的结果包括温度场分布和热损伤的演变。

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