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Application of Structural Similitude Theory in Subcomponent Testing of Wind Turbine Blades

机译:结构相似理论在风力涡轮机叶片子组件测试中的应用

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Currently material selection for wind turbine blades is based upon initial coupon testing to evaluate mechanical properties (e.g. stiffness, delamination strength, fatigue durability) and also full-scale tests to benchmark the final design. However, the coupon testing is often not representative of the mechanical performance in full-scale blades, so time-consuming and very expensive full-scale tests are required to quantify the blade durability. Appropriate sub-component testing has the potential to bridge the gap between coupon and full-scale tests and to expedite the material characterization and structural optimization saving both time and money. In this study, the similarity conditions of an analytical model of a simply-supported plate analogous to the spar cap of a wind turbine blade are investigated with the objective of designing an applicable scaled down subcomponent. Based on direct use of the governing equations, bending of a specially orthotropic rectangular laminated plate under transverse loads is analyzed to extract the scaling laws. Theoretical maximum deflection of the subcomponent is mapped to the deflection of spar cap using scaling laws. Accuracy of the scaling laws in mapping the data is then used as a subcomponent design criteria and the effect of the ply stack up scheme and size of subcomponent are investigated by applying complete and partial similarity conditions. The results indicate that subcomponents with distortion in ply stack up can predict the maximum deflection of the prototype with good accuracy. However, using subcomponents with different aspect ratios than the prototype yield an inaccurate prediction of prototype response.
机译:目前用于风力涡轮机叶片的材料选择基于初始优惠券测试,以评估机械性能(例如刚度,分层强度,疲劳耐久性)以及全规模测试以基准最终设计。然而,优惠券测试通常不代表全级刀片中的机械性能,因此需要耗时和非常昂贵的全尺度测试来量化叶片耐久性。适当的子组件测试有可能弥合优惠券和全尺度测试之间的差距,并加快储蓄的材料表征和结构优化,节省时间和金钱。在该研究中,通过设计适用的缩小子组件的目的研究了类似于风力涡轮机叶片的翼梁帽的简单支撑板的分析模型的相似性条件。基于直接使用控制方程,分析了横向载荷下的特殊正式矩形层压板的弯曲,以提取缩放法。子组件的理论最大偏转是使用缩放法律映射到翼梁帽的偏转。然后,使用综合和部分相似性条件,研究了映射数据的缩放规律的准确性,作为子组件设计标准,并通过应用完整和部分相似性条件来研究层次堆叠方案和子组件尺寸的效果。结果表明,层叠层中的失真子组件可以预测原型的最大偏转,精度良好。然而,使用具有不同纵横比的子组件比原型产生的原型响应的不准确预测。

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