复合材料科学与工程 ›› 2020, Vol. 0 ›› Issue (2): 19-24.

• 基础研究 • 上一篇    下一篇

小型风力机叶片全覆冰仿真和模态试验对比研究

李飞宇, 崔红梅*, 陈红星, 苏宏杰   

  1. 内蒙古农业大学机电工程学院,呼和浩特010018
  • 收稿日期:2019-05-30 出版日期:2020-02-28 发布日期:2020-02-28
  • 通讯作者: 崔红梅(1978-),女,副教授,硕士生导师,博士,主要研究方向为工程测试与控制,chm123m@126.com。
  • 作者简介:李飞宇(1990-),男,工程师,硕士,主要从事风力发电机叶片测试技术方面的研究。
  • 基金资助:
    国家自然科学基金项目(11262015);内蒙古农业大学优秀青年科学基金项目(2014XYQ-9)

A COMPARATIVE STUDY OF SIMULATION AND MODAL TEST FORA SMALL ICING WIND TURINE BLADE

LI Fei-yu, CUI Hong-mei*, CHEN Hong-xing, SU Hong-jie   

  1. The College of Electromechanical Engineering, Inner Mongolia Agricultural University, Hohhot 010018, China
  • Received:2019-05-30 Online:2020-02-28 Published:2020-02-28

摘要: 风力机叶片覆冰后会影响风力发电机组正常工作,甚至会使风力机过载、叶片折断,进而造成安全事故和资源浪费。应用ANSYS模态仿真和模态试验两种研究方法,探究风力机叶片在不同覆冰厚度下模态参数的变化,得到叶片前四阶振型和固有频率。结果表明,仿真和试验模态测试结果接近,振型相符,基频的误差在3%以内。覆冰后叶片一阶固有频率振型为挥舞,从第二阶开始,出现挥舞和摆振方向的耦合模态振型。前四阶振型随着覆冰厚度增加振动形式保持不变,主要振动形式为挥舞摆动,叶尖处的振幅逐渐变小。随着覆冰厚度的增加,叶片固有频率逐渐降低,在覆冰厚度为30 mm时,叶片基频比不覆冰降低28.7%。

关键词: 风力机叶片, 仿真模态, 试验模态, 覆冰, 振型, 固有频率

Abstract: After the wind turbine blades are covered with ice, the normal operation of wind turbine generator system is affected, the wind turbine will be overloaded and the blades will be broken, which will cause safety accidents and waste of resources. Therefore, it is very important to detect the icing condition of wind turbine blades by the modal parameters. In this paper, the modal parameters of wind turbine blade under different icing thickness were measured by modal testing system and calculated by the finite element software ANSYS, and the first four vibration modes and natural frequencies of the blades are obtained. The results show that the results of simulation modal and experimental modal are close, the vibration characteristics are consistent, and the error of fundamental frequency is within 3%. The first-order natural frequency vibration mode of the blade after icing is flap-wise. Starting from the two-order natural frequency vibration mode of the blade, the coupled mode of flap-wise and edge-wise directions appears. The first four-order vibration modes of the blade remain unchanged as the increasing of ice thickness, the main vibration mode is flap-wise, and the amplitude at the tip of the blade decreases gradually. When the ice thickness is 30 mm, the fundamental frequency of the blade decreases by 28.7% compared with that without icing. These results have certain guidance on design of blade icing state detection system based on vibration detection technology.

Key words: wind turbine blade, simulation modal, experimental modal, icing, vibration mode, natural frequency

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