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Experimental Validation of Inertia-Eigenfrequency Emulation for Wind Turbines on System Test Benches

机译:系统试验台上风力涡轮机惯性-本频仿真的实验验证

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Hardware-in-the-loop systems for wind turbine system test benches are prominently used in today’s development process of wind turbine manufacturers to conduct realistic ground-level tests. This contribution presents a state-of-the-art test rig in the multi-megawatt regime equipped with an innovative hardware-in-the-loop (HiL) system which enables ground-based testing of full scale wind turbines. The proposed system consists of a state estimator, an internal wind turbine model comprising an aeroelastic rotor model for reference generation as well as control loops for setpoint tracking and active drivetrain damping purposes. The introduced HiL system is validated experimentally in detail at a test rig with a mounted state-of-the art 3 MW full scale wind turbine. Experiments prove the system’s ability to emulate the nacelles drivetrain dynamics on ground-level while guaranteeing stable operation over the full wind speed range and in demanding instationary design load cases such as gust events. Experimental results show wind turbine related frequency shares originated in the dynamics of the physically not present rotor, e.g. per-revolution frequencies, tower shadow as well as the first torsional drivetrain eigenfrequency are induced. In addition to this, experiments in power production prove the ability of reproducing the nacelle’s power curve with a maximum error of 10 % in the transition of partial and full load operation and less than 3 % over the full operational range.
机译:在当今风力涡轮机制造商的开发过程中,风力涡轮机系统测试台的硬件在环系统得到了显着的应用,以进行实际的地面测试。该成果展示了在数兆瓦级状态下的最新测试设备,该设备配备了创新的硬件在环(HiL)系统,可对大型风力涡轮机进行基于地面的测试。所提出的系统由状态估计器,内部风力涡轮机模型组成,该模型包括用于参考生成的气动弹性转子模型以及用于设定值跟踪和主动动力传动系统阻尼目的的控制环。引入的HiL系统在安装了最新3 MW全尺寸风力涡轮机的试验台上进行了实验性的详细验证。实验证明,该系统能够在地面上模拟机舱动力传动系统的动力学特性,同时确保在整个风速范围内以及在阵风等恶劣的平稳设计载荷情况下均能稳定运行。实验结果表明,与风力涡轮机相关的频率份额源自物理上不存在的转子(例如,转子)的动力学。每转频率,塔影以及第一个扭转动力传动系统的本征频率都会被感应出来。除此之外,电力生产实验证明,能够再现机舱的功率曲线,在部分和满负荷运行的过渡过程中,最大误差为10%,而在整个运行范围内,误差均小于3%。

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