An experimental study on the aerodynamic loads of a floating offshore wind turbine under imposed motions

F. Taruffi, Felipe Novais, A. Viré
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Abstract

Abstract. The rotor of a floating wind turbine is subject to complex aerodynamics due to changes in relative wind speeds at the blades and potential local interactions between blade sections and the rotor near wake. These complex interactions are not yet fully understood. Lab-scale experiments are highly relevant for capturing these phenomena and provide means for the validation of numerical design tools. This paper presents a new wind tunnel experimental setup able to study the aerodynamic response of a wind turbine rotor when subjected to prescribed motions. The present study uses a 1:148 scale model of the DTU 10 MW reference wind turbine mounted on top of a 6 degrees of freedom parallel kinematic robotic platform. Firstly, the thrust variation of the turbine is investigated when single degree of freedom harmonic motions are imposed by the platform, with surge, pitch and yaw being considered in this study. For reduced frequencies greater than 1.2, it is found that the thrust variation is amplified by up to 150 % compared to the quasi-steady value when the turbine is subject to pitch and surge motions, regardless of the amplitude of motion. A similar behaviour is also noticed under yaw motions. Secondly, realistic 6 degrees of freedom motions are imposed by the platform. The motions are derived from FAST simulations performed on the full-scale turbine coupled with the TripleSpar floater, and the tests aim at exploring the thrust force dynamics for different sea states and wind conditions, obtaining reasonable agreement with the simulations. Finally, the work shows the capabilities of an off-the-shelf hexapod to conduct hybrid testing of floating offshore wind turbines in wind tunnels, as well as its limitations in performing such tests.
浮式海上风力涡轮机在外加运动下的空气动力负荷实验研究
摘要由于叶片处相对风速的变化以及叶片部分与转子近尾流之间潜在的局部相互作用,浮动风力涡轮机的转子受到复杂空气动力学的影响。人们对这些复杂的相互作用尚未完全了解。实验室规模的实验对于捕捉这些现象非常重要,并为验证数值设计工具提供了手段。本文介绍了一种新的风洞实验装置,能够研究风力涡轮机转子在受到规定运动时的气动响应。本研究使用一个 1:148 比例的 DTU 10 兆瓦参考风力涡轮机模型,安装在一个 6 自由度平行运动机器人平台的顶部。首先,研究了平台施加单自由度谐波运动时涡轮机的推力变化,本研究考虑了激波、俯仰和偏航。研究发现,在降低频率大于 1.2 的情况下,当涡轮机受到俯仰和激波运动时,无论运动幅度如何,推力变化与准稳定值相比最多可放大 150%。在偏航运动中也有类似的表现。其次,平台施加了逼真的 6 自由度运动。这些运动来自于对全尺寸涡轮机和 TripleSpar 浮筒进行的 FAST 模拟,测试旨在探索不同海况和风况下的推力动态,并与模拟结果取得合理的一致。最后,这项工作展示了现成的六脚架在风洞中对浮动海上风力涡轮机进行混合测试的能力,以及在进行此类测试时的局限性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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