研究大型风力轮机叶片的合模式动参数
1School of Mechanical Engineering, Shandong University of Technology, Zibo, China.
Scientific reports
|June 4, 2024
概括
增加风力轮机叶片大小提高了灵活性,冒着空气动力弹性不稳定性和的风险. 叶片尖区域的参数变化显著影响了飞的特征,增加的刚性通常会增加振动频率和飞速度.
科学领域:
- 空气动力学 在空气动力学.
- 结构动力学 结构动力学
- 风能工程 风能工程
背景情况:
- 较大的风力轮机叶片具有更大的灵活性,使它们在运行过程中容易受到空气动力弹性不稳定性的影响.
- 由曲扭曲效应驱动的合模式飞,在长叶片中构成叶片故障的重大风险.
研究的目的:
- 用欧勒·伯努利束理论和西奥多森空气动力学负荷来建立叶片的特征方程.
- 分析区域参数变化对NREL 5MW风力轮机叶片动特征的影响.
主要方法:
- 欧勒·伯努利束理论和西奥多森非定向空气动力学负荷的应用.
- 有限元法 (FEM) 用于建立叶片的特征方程.
- 对NREL 5MW风力轮机叶片进行参数分析,重点关注不同地区和属性.
主要成果:
- 叶片尖区域的参数变化对飞特征的影响最大.
- 增加的曲和扭曲刚度通常会导致更高的振动频率和的速度.
- 曲刚度的降低会使飞速度稳定,而扭曲刚度的增加会提高飞速度.
结论:
- 旋转半径与的频率和速度成反比例.
- 中心点偏移对飞频率的影响很小,但对尖端区域的飞速度的影响很大.
- 增加扭矩刚度对于防止合模式动至关重要,为叶片设计提供了基础.
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