复合材料科学与工程 ›› 2015, Vol. 0 ›› Issue (7): 39-44.

• 基础研究 • 上一篇    下一篇

100kW大厚度钝尾缘叶片的静力实验研究

徐立军1*, 徐蕾1, 杨科2   

  1. 1.新疆工程学院,乌鲁木齐 830000;
    2.中国科学院工程热物理研究所,北京 100190
  • 收稿日期:2015-01-27 出版日期:2015-07-28 发布日期:2021-09-13
  • 作者简介:徐立军(1978-),男,博士,副教授,主要从事风力发电机载荷检测及控制策略方面的研究。
  • 基金资助:
    新疆维吾尔自治区自然科学基金项目资助(2014211A021)

AN EXPERIMENTAL STUDY OF 100kW BLADE WITH FLATBACK AND THICK AIRFOILS UNDER STATIC LOAD

XU Li-jun1*, XU Lei1, YANG Ke2   

  1. 1. Xinjiang Institute of Engineering, Urmqi 830091, China;
    2. Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100080, China
  • Received:2015-01-27 Online:2015-07-28 Published:2021-09-13

摘要: 现代风力机叶片的大型化带来了设计和生产方面的诸多问题,叶片的静力实验是分析叶片结构稳定性的重要基础和验证手段。对中国科学院工程热物理研究所研发的100kW大厚度钝尾缘叶片进行了静力实验研究,分析了叶片在摆振和挥舞方向的屈曲特性和应变特性,通过对静力特性进行分析,探讨了叶片在载荷作用下的刚度及应变等性能特性,比较了叶片相对于传统尖尾缘叶片的结构性能优点。最后,将失效实验结果同设计值相比较,分析了产生误差的原因。

关键词: 钝尾缘, 叶片, 静力实验, 屈曲, 应变

Abstract: Increasingly large-sized wind turbine blade brings many design and production problems, static experimental of blade is the important foundation and verification means, which can be used to analyze the structure stability of the blade. This paper presents the static experimental study of the 100kW experimental blade with flatback and thick airfoils, which was designed by project team. The bucking and strain behavior of flapwise and edgewise are analyzed. Performance of the blade, including buckling and strain under the action of load is investigated, the structural performance advantages are compared with the traditional blade with sharpedge and the blade with flatback. At last, the results of failure experimental are compared with the design value to analyze the error generation causes.

Key words: flatback, blade, static experiment, buckling, strain

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