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风电叶片两点疲劳试验系统激振器加载控制
引用本文:廖高华,乌建中. 风电叶片两点疲劳试验系统激振器加载控制[J]. 同济大学学报(自然科学版), 2018, 46(11): 1562-1567
作者姓名:廖高华  乌建中
作者单位:同济大学 机械与能源工程学院,上海 201804;南昌工程学院 江西省精密驱动与控制重点实验室,江西 南昌 330099,同济大学 机械与能源工程学院,上海 201804
基金项目:江西省精密驱动与控制重点实验室开放基金项目(PLPDC-KFKT-201622)
摘    要:基于电驱动惯性式激振装置,构建了一种风电叶片两点激振疲劳试验系统,并提出了虚拟主令同步控制算法.以PID算法设计误差补偿器,利用李雅普诺夫函数证明虚拟主令同步控制算法的稳定性,并建立控制仿真模型,数值仿真分析虚拟主令同步控制算法的收敛性及鲁棒性.最后,试验验证了耦合下虚拟主令同步控制算法的有效性.结果表明:虚拟主令同步控制算法能使激振器快速跟随,激振器之间相位差的波动很小,叶片振幅稳定,实现了风电叶片的平稳有效加载.

关 键 词:多激振器;协同控制;机电耦合;疲劳加载
收稿时间:2017-11-15
修稿时间:2018-10-14

Load Control of Vibration Exciter in Two point Fatigue Test System of Wind Turbine Blade
LIAO Gaohua and WU Jianzhong. Load Control of Vibration Exciter in Two point Fatigue Test System of Wind Turbine Blade[J]. Journal of Tongji University(Natural Science), 2018, 46(11): 1562-1567
Authors:LIAO Gaohua and WU Jianzhong
Affiliation:College of Mechanical Engineering, Tongji University, Shanghai 201804, China; Jiangxi Province Key Laboratory of Precision Drive & Control, Nanchang Institute of Technology, Nanchang 330099, China and College of Mechanical Engineering, Tongji University, Shanghai 201804, China
Abstract:Based on the electrically driven inertial vibration exciter, a two point excitation fatigue test system of wind turbine blade was constructed. The virtual master synchronization control algorithm was put forward. The PID algorithm was used to design the error compensator, then the stability of the control algorithm was proved by using Lyapunov function. The control simulation model was established, and the convergence and the robustness of the control algorithm were analyzed by numerical simulation. Finally, the effectiveness of the control algorithm of electromechanical coupling was verified. The results show that the control algorithm can make the exciter follow quickly, the fluctuation of phase difference between the exciters is very small, the blade amplitude is stable, and the stable and effective loading of wind turbine blades is realized.
Keywords:multi-exciter   cooperative control   electromechanical coupling   fatigue loading
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