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Active load reduction by means of trailing edge flaps on a wind turbine blade

机译:通过风力涡轮机叶片上的后缘襟翼减少主动负载

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This paper presents the blade fatigue load reduction achieved with a trailing edge flap during a full scale test on a Vestas V27 wind turbine. A frequency-weighted linear model predictive control (MPC) is tuned to decrease flapwise blade root fatigue loads at the frequencies where most of the blade damage occurs, i.e. the 1P and 2P frequencies (respectively 1 and 2 events per revolution). Frequency-weighted MPC is chosen for its ability to handle constraints on the trailing edge flap deflection and to optimise its actuation in order to decrease wear and tear of the actuator. The controller was first tested in aero-servo-elastic simulations, before being implemented on a Vestas V27 wind turbine. Consistent load reduction is achieved during the full-scale test. An average of 14% flapwise blade root fatigue load reduction is measured.
机译:本文介绍了在Vestas V27风力涡轮机进行全面测试期间,通过后缘襟翼实现的叶片疲劳负载降低。调整了频率加权线性模型预测控制(MPC),以在大多数叶片损坏发生的频率(即1P和2P频率(每转分别发生1和2个事件))下降低翼翼叶片根部疲劳负载。选择频率加权的MPC是因为它具有处理后缘襟翼偏转的约束并优化其致动的能力,以减少致动器的磨损。该控制器首先在航空弹性仿真中进行了测试,然后在Vestas V27风力涡轮机上实现。在满量程测试期间,可以始终如一地减少负载。测得翼片方向叶片根部疲劳负荷平均降低了14%。

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