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Effects of defects in composite wind turbine blades – Part 2: Progressive damage modeling of fiberglass-reinforced epoxy composites with manufacturing-induced waves

机译:复合材料风力涡轮机叶片中缺陷的影响–第2部分:制造波引起的玻璃纤维增​​强环氧复合材料的渐进式损伤建模

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Composite wind turbine blades are typically reliable; however, premature failures are often in regions of manufacturing defects. While the use of damage modeling has increased with improved computational capabilities, they are often performed for worst-case scenarios in which damage or defects are replaced with notches or holes. To better understand and predict these effects, an effects-of-defects study has been undertaken. As a portion of this study, various progressive damage modeling approaches were investigated to determine if proven modeling capabilities could be adapted to predict damage progression of composite laminates with typical manufacturing flaws commonly found in wind turbine blades. Models were constructed to match the coupons from, and compare the results to, the characterization and material testing study presented as a companion. Modeling methods were chosen from established methodologies and included continuum damage models (linear elastic with Hashin failure criteria, user-defined failure criteria, nonlinear shear criteria), a discrete damage model (cohesive elements), and a combined damage model (nonlinear shear with cohesive elements). A systematic, combined qualitative–quantitative approach was used to compare consistency, accuracy, and predictive capability for each model to responses found experimentally. Results indicated that the Hashin and combined models were best able to predict material response to be within 10?% of the strain at peak stress and within 10?% of the peak stress. In both cases, the correlation was not as accurate as the wave shapes were changed in the model; correlation was still within 20?% in many cases. The other modeling approaches did not correlate well within the comparative framework. Overall, the results indicate that this combined approach may provide insight into blade performance with known defects when used in conjunction with a probabilistic flaw framework.
机译:复合风力涡轮机叶片通常是可靠的;但是,过早的故障通常发生在制造缺陷的区域。尽管通过改进的计算能力增加了损坏建模的使用,但通常在最坏情况下使用缺口或孔代替损坏或缺陷来执行损坏建模。为了更好地理解和预测这些影响,已经进行了缺陷影响研究。作为这项研究的一部分,对各种渐进式损伤建模方法进行了研究,以确定确定的建模能力是否可用于预测复合材料层压板的损坏进展,而复合材料层压板通常具有风力涡轮机叶片中常见的制造缺陷。构建模型以匹配来自作为伴侣的表征和材料测试研究中的试样,并将结果进行比较。建模方法是从已建立的方法中选择的,包括连续损伤模型(具有Hashin破坏准则的线性弹性,用户定义的破坏准则,非线性剪切准则),离散损伤模型(内聚元素)和组合损伤模型(具有内聚力的非线性剪切)元素)。一种系统的,定性-定量相结合的方法用于比较每个模型与实验发现的响应的一致性,准确性和预测能力。结果表明,Hashin模型和组合模型最能预测材料在峰值应力下的应变在10%之内,在峰值应力的10%之内。在这两种情况下,相关性均不如模型中的波形变化那样准确。在许多情况下,相关性仍在20%以内。在比较框架内,其他建模方法之间没有很好的相关性。总体而言,结果表明,与概率缺陷框架结合使用时,这种组合方法可以深入了解具有已知缺陷的刀片性能。

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