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浮式垂直轴风机的动力学建模、仿真与实验研究

刘利琴 郭颖 赵海祥 唐友刚

刘利琴, 郭颖, 赵海祥, 唐友刚. 浮式垂直轴风机的动力学建模、仿真与实验研究[J]. 力学学报, 2017, 49(2): 299-307. doi: 10.6052/0459-1879-16-264
引用本文: 刘利琴, 郭颖, 赵海祥, 唐友刚. 浮式垂直轴风机的动力学建模、仿真与实验研究[J]. 力学学报, 2017, 49(2): 299-307. doi: 10.6052/0459-1879-16-264
Liu Liqin, Guo Ying, Zhao Haixiang, Tang Yougang. DYNAMIC MODELING, SIMULATION AND MODEL TESTS RESEARCH ON THE FLOATING VAWT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2017, 49(2): 299-307. doi: 10.6052/0459-1879-16-264
Citation: Liu Liqin, Guo Ying, Zhao Haixiang, Tang Yougang. DYNAMIC MODELING, SIMULATION AND MODEL TESTS RESEARCH ON THE FLOATING VAWT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2017, 49(2): 299-307. doi: 10.6052/0459-1879-16-264

浮式垂直轴风机的动力学建模、仿真与实验研究

doi: 10.6052/0459-1879-16-264
基金项目: 

国家自然科学基金 51579176

上海交通大学海洋工程重点试验室开放基金 1501

天津市自然科学基金 16JCYBJC21200

详细信息
    通讯作者:

    2) 刘利琴, 副教授, 主要研究方向:船舶与海洋工程动力学, 海洋可再生能源.E-mail:liuliqin@tju.edu.cn

  • 中图分类号: P75;TK81

DYNAMIC MODELING, SIMULATION AND MODEL TESTS RESEARCH ON THE FLOATING VAWT

  • 摘要: 考虑气动力和水动力的耦合研究浮式垂直轴风机系统的运动响应,将固定式垂直轴风机的气动载荷计算方法进一步推广到海上浮式垂直轴风机的气动载荷计算.考虑阻尼力、波浪力、风载荷、系泊力等,建立了浮式垂直轴风机系统的纵荡-垂荡-纵摇运动方程.考虑动态失速和浮式基础运动,基于双致动盘多流管理论,推导了风机叶片气动载荷计算公式,编制了数值计算程序.以Sandia 17 m风机为例,验证了气动载荷计算程序的正确性.最后进行了模型实验,其中模型的风机为Φ型达里厄垂直轴风机,支撑基础为桁架式Spar型浮式基础,将模型实验结果与数值计算结果进行了对比,验证了耦合计算程序.结果表明,数值计算得到的风机系统的垂荡、纵摇运动的RAO(幅值响应算子)曲线与模型实验结果吻合较好,验证了耦合程序的正确性.然而,由于数值计算与模型实验在运动自由度、阻尼、风载荷等方面存在差别,数值计算结果与模型实验结果仍有一定的差异.

     

  • 图  1  风机系统坐标和速度矢量关系图

    Figure  1.  Coordinate system and vector relation of the wind turbine

    图  2  计算流程图

    Figure  2.  Computing process

    图  3  气动载荷计算程序验证

    Figure  3.  Validation of the aerodynamics computing code

    图  4  浮式风机

    Figure  4.  The floating VAWT

    图  5  实验布置图

    Figure  5.  The test layout

    图  6  浮式风机垂荡、纵摇RAO曲线

    Figure  6.  RAO curves of heave and pitch of the floating VAWT

    表  1  模型参数

    Table  1.   Parameter of model

    表  2  浮式风机阻尼系数

    Table  2.   Damping coefficient of the floating VAWT

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出版历程
  • 收稿日期:  2016-09-20
  • 网络出版日期:  2016-12-15
  • 刊出日期:  2017-03-18

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