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INVESTIGATIONS ON THE FATIGUE LOAD REDUCTION POTENTIAL OF ADVANCED CONTROL STRATEGIES FOR MULTI-MW WIND TURBINES USING A FREE VORTEX WAKE MODEL

机译:利用自由涡旋模型研究多兆瓦风力发电机组高级控制策略的疲劳负荷减小潜力

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This paper presents the results of a fatigue load evaluation from aeroelastic simulations of a multi-megawatt wind turbine. Both the Blade Element Momentum (BEM) and the Lifting Line Free Vortex Wake (LLFVW) methods were used to compute the aerodynamic forces. The loads in selected turbine components, calculated from NREL's FAST v8 using the aerodynamic solver AeroDyn, are compared to the loads obtained using the LLFVW aerodynamics formulation in QBlade. The DTU 10 MW Reference Wind Turbine is simulated in power production load cases at several wind speeds under idealized conditions. The aerodynamic forces and turbine loads are evaluated in detail, showing very good agreement between both codes. Additionally, the turbine is simulated under realistic conditions according to the current design standards. Fatigue loads derived from load calculations using both codes are compared when the turbine is controlled with a basic pitch and torque controller. It is found that the simulations performed with the BEM method generally predict higher fatigue loading in the turbine components. A higher pitch activity is also predicted with the BEM simulations. The differences are larger for wind speeds around rated wind speed. Furthermore, the fatigue reduction potential of the individual pitch control (IPC) strategy is examined and compared when using the two different codes. The IPC strategy shows a higher load reduction of the out-of-plane blade root bending moments when simulated with the LLFVW method. This is accompanied with higher pitch activity at the actuation frequency of the IPC strategy.
机译:本文介绍了多兆瓦级风力涡轮机的气动弹性仿真得出的疲劳载荷评估结果。叶片要素动量(BEM)和举升自由涡旋唤醒(LLFVW)方法均用于计算空气动力。将使用空气动力求解器AeroDyn根据NREL的FAST v8计算出的选定涡轮机组件中的载荷与使用QBlade中的LLFVW空气动力学公式获得的载荷进行比较。 DTU 10 MW参考风力涡轮机是在理想条件下以多种风速在发电负荷情况下进行模拟的。详细评估了空气动力和涡轮机负载,显示了两个规范之间的良好一致性。此外,根据当前设计标准在实际条件下对涡轮进行了仿真。当使用基本螺距和扭矩控制器控制涡轮时,将比较使用这两个代码进行载荷计算得出的疲劳载荷。发现使用BEM方法执行的模拟通常预测涡轮机部件中的较高疲劳载荷。通过BEM仿真还可以预测更高的音调活动。对于额定风速附近的风速,差异更大。此外,当使用两个不同的代码时,将检查并比较单个变桨控制(IPC)策略的疲劳降低潜力。当使用LLFVW方法进行仿真时,IPC策略显示出了更高的平面外叶片根部弯矩弯矩的负荷降低。在IPC策略的启动频率上伴随着更高的音调活动。

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