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Load mitigation of wind turbine blade by aeroelastic tailoring via unbalanced laminates composites

机译:通过不平衡层压复合材料的气动弹性剪裁来减轻风力涡轮机叶片的负荷

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The parametric study of unbalanced tri-axial non-crimp fabrics laminates, typically used in the blade skin layup, showed that the highest bend-twist coupling up to 0.56 was achieved when all three kinds of unbalances (i.e. ply-angle, ply-material and ply-thickness unbalances) were simultaneously present in the laminates. Based on aeroelastic tailoring via unbalanced laminates, the bend-twist coupling towards feather of various degrees was implanted to the skin layup of a variable-speed collective-pitch controlled 5 MW wind turbine rotor blades and fully-coupled aero-servo-elastic analyses were performed. The results showed that when the ply-thickness unbalance is added in the skin layup, in addition to already existing ply-angle and ply-material unbalances, an average increase in the coupling magnitude by approximately 51% along the blade length and a reduction in fatigue load and collective-pitch demand by approximately 1.6-2.9% and 5.5-19.9% across the range of applied stochastic winds ranging from 7 m/s to 23 m/s. (C) 2015 Elsevier Ltd. All rights reserved.
机译:对不平衡三轴非卷曲织物层压板的参数研究表明,通常在叶片蒙皮叠层中使用该层压板,当所有三种不平衡(即帘布层角度,帘布层材料)均达到最高0.56的弯曲扭曲耦合时和层厚度不平衡)同时出现在层压板中。基于通过不平衡层压材料进行的气动弹性剪裁,将向不同角度的羽毛弯曲弯曲耦合植入到变速集体螺距控制的5 MW风力涡轮机转子叶片的蒙皮层上,并进行了完全耦合的航空伺服弹性分析执行。结果表明,当在皮肤铺层中添加层厚不平衡时,除了已经存在的层角和层材料不平衡外,沿叶片长度的耦合强度平均增加了约51%,并且减少了在从7 m / s到23 m / s的随机风范围内,疲劳载荷和总螺距要求分别约为1.6-2.9%和5.5-19.9%。 (C)2015 Elsevier Ltd.保留所有权利。

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