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Structural Design and Analysis of a Segmented Ultralight Morphing Rotor (SUMR) for Extreme-Scale Wind Turbines

机译:分段式超轻型涡轮机超轻型转子的结构设计与分析

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To alleviate the mass-scaling issues associated with conventional upwind rotors of extreme-scale wind turbines (≥ 10MW), a segmented ultralight morphing rotor (SUMR) concept was proposed by Loth et al. (2010, 2012). The concept employs a downwind rotor with segmented blades whose elements are stiff and whose joints can be unlocked to allow for moment-free downstream alignment. Aligning the combination of gravitational, centrifugal and thrust forces along the blade path reduces downwind cantilever loads, reducing to a primarily tensile loading. Herein, the SUMR concept is developed further by fixing the blade curvature and limiting morphing to a downwind coming angle through a single near-hub joint. Between cut-in and rated conditions, this downwind angle varies linearly between 0° (no alignment) to 24° (full alignment). Between rated conditions and cut-out conditions, the blade is fully-aligned, and this results in a decrease in coning angle to a value of 11° just before cut-out. To quantify mass savings, a 10 MW model (based on the NREL 5 MW reference turbine) was created for a conventional rotor blade and the SUMR blade. The morphing blade used an internal structure similar to the Sandia 100-m all-glass blade. The structural stresses were then predicted with a finite element method over a range of operating wind speeds and azimuthal angles. This leads to a net mass savings of 50% through decreased shell, spar, and shear web thicknesses. Furthermore, the ability to stow the morphing blades under extreme wind conditions with a pivot near the hub is found to substantially reduce the high wind constraint, as compared to that for conventional blades.
机译:为了缓解与超大型风力涡轮机(≥10MW)的常规迎风转子相关的质量缩放问题,Loth等人提出了分段超轻变质转子(SUMR)的概念。 (2010年,2012年)。该概念采用了具有分段叶片的顺风转子,其叶片刚性强,并且其接头可以解锁以实现顺畅的下游对准。沿叶片路径对齐重力,离心力和推力的组合可减少顺风悬臂载荷,从而减小至主要为拉力载荷。在此,通过固定叶片曲率并通过单个近轮毂接头将变形限制为顺风来袭角度,进一步发展了SUMR概念。在切入和额定条件之间,该顺风角度在0°(无对准)至24°(完全对准)之间线性变化。在额定条件和切除条件之间,叶片已完全对准,这导致将锥角减小到即将切除之前的11°值。为了量化节省的质量,针对常规转子叶片和SUMR叶片创建了10 MW模型(基于NREL 5 MW参考涡轮机)。变形刀片使用的内部结构类似于Sandia 100-m全玻璃刀片。然后使用有限元方法在一定的工作风速和方位角范围内预测结构应力。通过减少壳体,翼梁和剪切腹板的厚度,可以节省50%的净质量。此外,与常规叶片相比,发现在极端风速条件下利用枢轴在轮毂附近将变型叶片收起的能力大大降低了高风速约束。

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