不同倾角下漂浮式风力涡轮机转子的空气动力和结构评估

H. H. Mian, M. S. Siddiqui, N. Franchina, O. Kouaissah, G. Wang, T. A. Nygaard
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引用次数: 0

摘要

由于波浪引起的平台运动,预测浮式海上风力涡轮机(FOWT)的空气动力性能具有挑战性。风浪的影响导致平台产生六自由度运动,直接影响涡轮机的性能。了解特定自由度(DOF)运动对空气动力学和结构响应的影响对于有效的风机设计至关重要。本研究探讨了转子倾斜对空气动力性能和结构响应的影响。研究采用计算流体动力学(CFD)分析,并将空气动力载荷映射到有限元(FE)网格上进行结构分析。研究采用了全面的三维模拟,利用移动参考框架 (MRF) 方法对 NREL 5 兆瓦参考风力涡轮机进行 CFD 模拟。它探讨了海上结构在运行过程中遇到的不同转子倾斜角度(5°、10°、15° 和 20°),并研究了它们对空气动力性能的影响。使用径向基函数 (RBF) 插值技术将预测的空气动力载荷映射到叶片 FE 网格上,并使用开源 FE 求解器 CalculiX 进行求解。分析结果表明,涡轮机的性能在倾角为 10° 时相对不受影响。然而,进一步增大转子倾角会对涡轮机性能产生不利影响,导致推力和功率输出明显下降。流体-结构耦合分析深入揭示了涡轮叶片所经历的变形和应力,表明倾角越大,襟翼位移明显增加,而边缘位移受到的影响并不明显。叶片上的最大应力位置与实际观测结果基本吻合。
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Aerodynamic and Structural Assessment of Floating Wind Turbine Rotor Under Varying Tilt Angle
Predicting the aerodynamic performance of floating offshore wind turbines (FOWTs) proves challenging due to platform motion induced by waves. The effect of wind and waves results in a six-degree-of-freedom motion of the platform, directly influencing turbine performance. Understanding the impact of specific degrees of freedom (DOF) motions on aerodynamics and structural response is crucial for effective wind turbine design. This research examines the impact of rotor tilt on both aerodynamic performance and structural response. The investigation employs computational fluid dynamics (CFD) analysis and mapping aerodynamic loads onto the finite element (FE) mesh for structural analysis. The study employs a comprehensive 3D simulation, utilizing the moving reference frame (MRF) method for the NREL 5 MW reference wind turbine CFD simulations. It explores different rotor tilt angles (5°, 10°, 15°, and 20°) encountered by offshore structures during their operation and examines their impact on aerodynamic performance. Predicted aerodynamic loads were mapped onto the blade FE mesh using the radial basis function (RBF) interpolation technique and solved using the open-source FE solver CalculiX. The analysis shows that the turbine performance is relatively unaffected up to a tilt angle of 10°. However, further increase in rotor tilt angle adversely impacts turbine performance, leading to notable reductions in thrust and power output. The fluid-structure coupled analysis provided insights into the deformations and stresses experienced by the turbine blade, indicating a notable increase in flap-wise displacement for larger tilt angles, while edge-wise displacement is not as significantly affected. The maximum stress location on the blade generally correlates well with actual observations.
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