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Wind tunnel testing of scaled wind turbine models: Beyond aerodynamics

机译:比例缩放的风力涡轮机模型的风洞测试:超越空气动力学

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摘要

An aeroelastically scaled model of a wind turbine is described, featuring active individual blade pitch and torque control. The model, governed by supervision and control systems similar to those of a real wind turbine, is capable of simulating steady conditions and transient maneuvers in the boundary layer test section of the wind tunnel of the Politecnico di Milano. Expanding the classical scope of wind tunnel models, the present experimental facility enables applications ranging from aerodynamics to aeroelasticity and control. After a description of the model design and of its main characteristics, several applications are presented. Results are shown for the validation of a wind misalignment observer, for the optimization of the open-loop pitch profile used during emergency shutdowns, for the control in wake interference conditions of two models, and for active load alleviation by higher harmonic individual blade pitch control. Results demonstrate the potential of the proposed experimental facility to enable non-standard observations in the controlled environment of the wind tunnel, beyond the classical purely aerodynamic ones.
机译:描述了风力涡轮机的气动弹性比例模型,其特征在于主动的单个叶片螺距和扭矩控制。该模型由类似于真实风力涡轮机的监督和控制系统控制,能够模拟米兰理工大学风洞边界层测试段中的稳定条件和瞬态操纵。目前的实验设备扩展了风洞模型的经典范围,可实现从空气动力学到空气弹性和控制的各种应用。在描述了模型设计及其主要特征之后,提出了几种应用。显示的结果用于验证风偏心观测器,优化紧急停机期间使用的开环螺距曲线,两种模型的尾流干扰条件下的控制以及通过高次谐波单个叶片螺距控制来减轻主动载荷。结果证明了拟议的实验设施在风洞的受控环境中实现非标准观测的潜力,超越了传统的纯空气动力学观测。

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