固定式风机多模态气弹耦合与气动阻尼解析

ANALYTICAL FORMULATION OF MULTI-MODE AEROELASTIC COUPLING AND AERODYNAMIC DAMPING OF BOTTOM-FIXED WIND TURBINES

  • 摘要: 该文解析推导了考虑叶片、塔体多模态气弹耦合的气动阻尼矩阵,用于固定式风机气动阻尼的快速、精准量化。基于多体动力学和模态坐标法,构建了包含塔体高阶模态的14自由度风机系统非线性气弹模型,通过气动荷载线性化,解析推导了该系统的气动阻尼矩阵,用于风机多模态气弹耦合和气动阻尼的评估。研究表明:在引入塔顶转动、多模态耦合和叶片柔性的前提下,该气动阻尼矩阵足够精确。以5 MW标准风机为例,叶片挥舞方向气动阻尼比可达86%,远高于摆振方向的最大值2.3%。塔体顺风向气动阻尼比显著高于横风向,后者最大仅为0.4%。塔体横风向三阶模态气动阻尼比在所有运行点均为负,揭示了潜在的气动失稳风险。

     

    Abstract: This study gives a closed-form expression for the aerodynamic damping matrix, incorporating the multi-mode aeroelastic coupling of blades and tower, to enable rapid and accurate quantification of aerodynamic damping ratios for bottom-fixed wind turbines. A 14-degree-of-freedom nonlinear aero-elastic model of the wind turbine system integrating tower multi-mode dynamics is developed using multibody dynamics and the modal-based formulation. The aerodynamic damping matrix of the system is analytically derived through the linearization of aerodynamic loads, facilitating the evaluation of multi-mode aeroelastic coupling and aerodynamic damping. The findings demonstrate that the aerodynamic damping matrix is accurate when tower top rotation, multi-mode coupling and blade flexibility are accounted for. Analysis of a 5 MW baseline wind turbine reveals that the aerodynamic damping ratio of the blade flap-wise modes can reach 86%, markedly exceeding the maximum value of 2.3% of the edgewise modes. The modal aerodynamic damping ratios of the tower in the fore-aft direction are significantly higher than those in the side-side direction, where the latter exhibits a peak value of only 0.4%. The third side-side modal aerodynamic damping ratios of the tower remain negative across all operational points, suggesting a risk of aeroelastic instability.

     

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