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Revealing fatigue damage evolution in unidirectional composites for wind turbine blades using x-ray computed tomography

机译:利用X射线计算机断层扫描揭示风力机叶片单向复合材料的疲劳损伤演变

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摘要

Understanding fatigue damage evolution in the load carrying laminates of wind turbine blade play an important role designing longer and lighter turbine blades. Turbine blades which will make it possible to increase the size of wind turbines or to upgrade existing turbines for lower wind classes’. Thereby, it will be possible to lower the cost of energy for wind energy based electricity. In the presented work, a lab-source x-ray computed tomography equipment (Zeiss Xradia 520Versa) has been used in connection with ex-situ fatigue testing of uni-directional composites in order to identify fibre failure during the fatigue loading. The load carrying laminates in wind turbine blades is typically based on a number of non-crimp fabrics in where the load carrying fibres are oriented in the axial direction of the blades. In order to ease the handling of the fabric during the dry fabric layup and to ensure a good alignment of the final laminates, approximately 10% of the fibres are oriented in secondary directions as so-called backing bundles and stitched to the uni-directionally oriented bundles. Due to the coarse structure of the non-crimp fabric, test samples with a larger cross-section (compared to other comparable x-ray studies) have been used in order to ensure a representative test volume during the ex-situ fatigue testing. Using the ability of the x-ray computed tomography to zoom into regions of interest, non-destructive, the fatiguedamage evolution in a repeating ex-situ fatigue loaded test sample has be explored. Thereby, the fatigue failure mechanism has been uncovered showing fibre breakage regions growing from cross-over regions of the backing bundles. Based on those observations, more realistic micromechanical based fatigue damage models as well as suggestions on bundle arrangement improving the fatigue resistance of non-crimp fabric used in the wind turbine industry can be made.
机译:了解风力涡轮机叶片承重层压板中的疲劳损伤演变在设计更长更轻的涡轮机叶片方面起着重要作用。涡轮叶片,这将有可能增加风力涡轮机的尺寸或升级现有涡轮机,以降低风向。因此,将有可能降低基于风能的电力的能源成本。在提出的工作中,实验室源X射线计算机断层扫描设备(Zeiss Xradia 520Versa)已与单向复合材料的异位疲劳测试结合使用,以识别疲劳载荷期间的纤维破坏。风力涡轮机叶片中的承重层压板通常基于许多非卷曲织物,其中承重纤维沿叶片的轴向取向。为了在干织物铺叠过程中减轻织物的处理并确保最终层压板的良好对齐,大约10%的纤维在所谓的衬布束的辅助方向上定向并缝合到单向定向捆绑。由于非卷曲织物的粗糙结构,已使用横截面较大的测试样品(与其他可比较的X射线研究相比),以确保在异位疲劳测试过程中具有代表性的测试体积。利用X射线计算机断层摄影技术放大非破坏性的目标区域的能力,已经研究了重复的异位疲劳载荷测试样品中疲劳损伤的演变。从而,已经发现了疲劳破坏机理,该疲劳破坏机理显示出纤维断裂区域从背衬束的交叉区域增长。基于这些观察结果,可以得出更实际的基于微机械的疲劳损伤模型,以及有关提高风轮机行业中使用的非卷曲织物的疲劳强度的线束排列建议。

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    Mikkelsen Lars Pilgaard;

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  • 年度 2017
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  • 正文语种 eng
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