首页|平台运动对15MW风机气弹性的影响研究

平台运动对15MW风机气弹性的影响研究

Study on the impact of platform forced motions on aeroelasticity of a 15 MW wind turbine

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随着人们对风力发电经济性要求的提高,风机叶片逐渐变得更长、更柔软,风电场也在不断向深远海发展.因此有必要研究气弹性耦合情况下平台运动对风机叶片和风机发电功率的影响.基于弹性致动线模型,研究了纵摇、纵荡运动对浮式风机叶片气弹性的影响,分析了气动功率、气动推力和叶片变形.研究发现:由于强迫运动产生了额外的附加速度,15 MW风机气动功率波动可达3个标准差,风机的平均气动功率也因此而减小;叶片弯曲和扭转变形沿叶片展向呈非线性分布,叶尖挥舞变形最大值可达14 m,在设计塔架、叶片预倾角时应当预留出一定的变形空间;由于平台纵摇运动附加在各截面处的速度不同,叶片的变形会呈现出非对称的波动,这会使风力机叶片产生额外的气动载荷波动和结构响应.
With increasing demands for the economic efficiency of wind power generation,wind turbine blades are becoming longer and more flexible,and offshore wind farms are advancing into deeper seas.Hence,it is necessary to study the effects of platform motions on wind turbine blades and power generation under aeroelastic coupling conditions.Based on the elastic actuator line model,this study investigates the influences of pitch motion and surge motion on the aeroelasticity of floating wind turbine blades,analyzing aerodynamic power,aerodynamic thrust,and blade deformation.It is found that due to the additional velocity induced by forced motions,the fluctuation in aerodynamic power of a 15 MW turbine can reach three standard deviations,thereby reducing the average aerodynamic power of the turbine.Nonlinear distributions of blade bending and twisting deformations along the span are observed,with maximum blade tip flap deformation up to 14 meters,suggesting that sufficient deformation space should be allowed when designing tower structures and blade pre-twist angles.Moreover,asymmetric fluctuations in blade deformation are caused by differential velocities induced by platform pitch motion at various cross-sections,resulting in additional aerodynamic load fluctuations and structural responses on wind turbine blades.

elastic actuator line modelaeroelastic couplingforced motionfloating wind turbine

王魁、赵伟文、万德成

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上海交通大学 船海计算水动力学研究中心(CMHL)船舶海洋与建筑工程学院,上海 200240

弹性致动线模型 气弹性耦合 强迫运动 漂浮式风机

国家自然科学基金资助项目

52131102

2024

海洋工程
中国海洋学会

海洋工程

CSTPCD北大核心
影响因子:0.552
ISSN:1005-9865
年,卷(期):2024.42(5)
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