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Structural Optimization of 3 MW Wind Turbine Blades Using a Two- Step Procedure

机译:使用两步过程优化3 MW风力涡轮机叶片的结构

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Modern large wind turbines, utilized to harness the kinetic energy of the wind, are rated at megawatts in output power. The design of large wind turbine blades must consider both their aerodynamic efficiency and structural robustness. This paper presents a two-step procedure for the optimum design of composite wind turbine blades. The results of the first step are the aerodynamically optimal cord lengths and twist angles of airfoils for the blade cross-sections along the blade spanwise direction. The second step yields optimal material distribution for the composite blade. A 3 MW wind turbine with blades having cross-sections of NREL S818, S82S and S826 airfoil types is demonstrated as the design example. Loaded by maximum forces and moments extracted from simulated time series, a parameterized finite element model of the aerodynamically optimized blade is created using the ANSYS software. The optimization results show that the initial blade model is an infeasible design due to a high level of the maximum stress, exceeding the upper limit of the stress constraint, but eventually the process converges to a feasible solution with the expense of increased total mass of the blade.
机译:用于利用风的动能的现代大型风力涡轮机的额定输出功率为兆瓦。大型风力涡轮机叶片的设计必须同时考虑其空气动力学效率和结构坚固性。本文提出了两步过程,以优化复合材料风力涡轮机叶片的设计。第一步的结果是沿叶片翼展方向的叶片横截面的空气动力学最佳绳索长度和翼型的扭转角。第二步为复合材料叶片产生最佳的材料分布。作为设计示例,演示了一种3 MW风力发电机,其叶片的横截面为NREL S818,S82S和S826型。通过从模拟时间序列中提取最大力和力矩来加载,使用ANSYS软件创建了空气动力学优化叶片的参数化有限元模型。优化结果表明,由于最大应力水平高,超过了应力约束的上限,因此初始叶片模型是不可行的设计,但最终该过程收敛到了可行的解决方案,但增加了叶片的总质量刀。

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