首页|基于风力发电机组偏航控制策略关键参数的测试与分析

基于风力发电机组偏航控制策略关键参数的测试与分析

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风电机组偏航控制策略中,各偏航动作之间状态的切换需依靠液压夹钳、电磁刹车与偏航驱动电机共同控制实现,所需4个关键时间点需通过样机测试得出.针对此,以某机型液压系统厂内测试为例,获取液压系统泄压-建压测试曲线;并增设多组对比测试,深入分析影响系统性能的因素;通过多领域融合的系统仿真软件进行仿真分析,为系统快速优化提供更多途径.结果表明:3台液压站所测泄压-建压曲线一致性较高,可准确得到4个时间点;单、双蓄能器对系统泄压-建压速度影响不大;不同回路背压值对系统建压时长影响较大,对泄压时长影响较小;串联制动器总出口压力响应滞后于总入口响应.可利用仿真手段设置更多系统变量组合,进一步快速优化系统策略,降低机组运行故障率.
Test and Analysis of Key Parameters Based on Yaw Control Strategy of Wind Turbine
In the yaw control strategy of the wind turbine,the state switching between each yaw action needs to be realized by the joint control of hydraulic clamp,electromagnetic brake and yaw drive motor,and the required four time points need to be obtained through prototype testing.In view of this,the in-plant test of a certain model hydraulic system was taken as an example to obtain the pressure relief-pressure construction test curves.Multiple sets comparative tests were added to deeply analyze the factors affecting sys-tem performance.The simulation analyses were performed through AMESim to provide more ways for system rapid optimization.The re-sults show that the pressure relief-pressure construction curves measured by the three hydraulic stations have high consistency,and the four time points can be accurately obtained;the single accumulator and dual accumulator have little effect on the pressure relief-pres-sure construction velocity of the system;the different loop pressure values have greater influence on the system pressure construction time and less influence on the pressure relief time;the total outlet pressure response of multiple series brakes lag behind the total inlet pressure response.Simulation means can be used to set more system variables to further optimize the system strategy and reduce the fail-ure rate of unit operation.

wind turbineyaw control strategysystem simulation

许敏影、何先照、陈通、李亚、何俊尉

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浙江运达风电股份有限公司,浙江杭州 310012

浙江省风力发电技术重点实验室,浙江杭州 310012

风力发电机 偏航策略 系统仿真

浙江省"尖兵领雁"研发攻关计划

2022C01178

2024

机床与液压
中国机械工程学会 广州机械科学研究院有限公司

机床与液压

CSTPCD北大核心
影响因子:0.32
ISSN:1001-3881
年,卷(期):2024.52(8)