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Full-scale test of trailing edge flaps on a Vestas V27 wind turbine: active load reduction and system identification

机译:Vestas V27风力发电机的后缘襟翼的全面测试:主动负载减少和系统识别

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A full-scale test was performed on a Vestas V27 wind turbine equipped with one active 70 cm long trailing edge flap on one of its 13m long blades. Active load reduction could be observed in spite of the limited spanwise coverage of the single active trailing edge flap. A frequency-weighted model predictive control was tested successfully on this demonstrator turbine. An average flapwise blade root load reduction of 14% was achieved during a 38 minute test, and a reduction of 20% of the amplitude of the 1P loads was measured. A system identification test was also performed, and an identified linear model, from trailing edge flap angle to flapwise blade root moment, was derived and compared with the linear analytical model used in the model predictive control design model. Flex5 simulations run with the same model predictive control showed a good correlation between the simulations and the measurements in terms of flapwise blade root moment spectral densities, in spite of significant differences between the identified linear model and the model predictive control design model.
机译:在Vestas V27风力涡轮机上进行了全面测试,该风力涡轮机在其13m长的叶片之一上配备了一个有效的70 cm长的后缘襟翼。尽管单个主动后缘襟翼的翼展方向覆盖范围有限,但仍可以观察到主动载荷降低。在该演示涡轮机上成功测试了频率加权模型的预测控制。在38分钟的测试中,平均襟翼叶片根部负载减少了14%,并测量了1P负载幅度减少了20%。还进行了系统识别测试,得出了从后缘襟翼角度到襟翼方向叶片根部力矩的已识别线性模型,并将其与模型预测控制设计模型中使用的线性分析模型进行了比较。尽管所识别的线性模型与模型预测控制设计模型之间存在显着差异,但使用相同模型预测控制进行的Flex5仿真在襟翼叶片根部力矩谱密度方面显示出仿真与测量之间的良好相关性。

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