...
首页> 外文期刊>Applied Ocean Research >Comparative study of short-term extreme responses and fatigue damages of a floating wind turbine using two different blade models
【24h】

Comparative study of short-term extreme responses and fatigue damages of a floating wind turbine using two different blade models

机译:使用两种不同的刀片模型的浮动风力涡轮机短期极端反应和疲劳损坏的比较研究

获取原文
获取原文并翻译 | 示例

摘要

In this work, two different blade structural models are used to estimate the blade deformations and the global structural responses of a 10MW floating offshore wind turbine (FOWT). One model is based on the EulerBernoulli beam theory and it is solved by the linear normal mode superposition method. The other model is based on the geometry exact beam theory (GEBT) which can consider the full geometric nonlinearity and large deformation. The control equations of GEBT are discretized by Legendre spectral finite elements. The aero-hydro-servo-elastic fully coupled numerical simulations are conducted in the open-source analysis tool OpenFAST to explore the feasibility of the two different structural models for modeling large scale wind turbine blades. Both the steady-state and dynamic results show that power generation and thrust on rotor are similar for the different blade models. There is a small difference in the results of the blade pitch angle and flapwise and edgewise blade root bending moment at high wind speeds due to the lack of torsion degree of freedom in the mode-based method. The difference between the two models is mainly reflected in the prediction of blade tip deformations. The one-hour short-term extreme blade root bending moments and the damage equivalent fatigue loads at blade root are both compared based on the two models. For edgewise bending moment, the extreme value of GEBT model is found at cut-out wind speed, whereas the linear beam model predicts the extreme value around rated wind speed. For the flapwise bending moment, the extreme value is captured around the rated wind speed for both of the two models, but GEBT model presents a larger value. As for fatigue loads, the shortterm 1 Hz damage equivalent loads calculated based on the linear beam model are smaller than GEBT model at almost all load cases for both edgewise and flapwise root bending moment, which implies that the linear beam model may underestimate the life time fatigue damage at blade root.
机译:在这项工作中,两种不同的刀片结构模型用于估计10MW浮动海上风力涡轮机(家禽)的叶片变形和全球结构响应。一种模型基于Eulerbernoulli光束理论,并且通过线性正常模式叠加方法解决。另一个模型基于几何精确光束理论(GEBT),其可以考虑完整的几何非线性和大变形。 GEBT的控制方程由Legendre谱有限元离散化。 Aero-Hydro-Servo-Elastic完全耦合数值模拟在开源分析工具中进行,探讨了两个不同结构模型的可行性,用于建模大型风力涡轮机叶片。稳态和动态结果都表明,转子上的发电和推力与不同的刀片模型相似。由于基于模式的方法中的缺乏自由度,叶片桨距角和浮动角度和脉冲和边缘叶片根部弯曲力矩的较小差异很小。两种模型之间的差异主要反映在叶片尖端变形的预测中。刀片根的一小时短期极端叶片根弯矩和损坏等效疲劳负载基于两种型号比较。对于EdgeWise弯曲时刻,GeBT模型的极值在切换风速下发现,而线性光束模型预测额定风速周围的极值。对于刷新弯曲时刻,对于两个模型的额定风速捕获极值,但GeBT模型呈现更大的值。对于疲劳负载,基于线性光束模型计算的短期1 Hz损伤等效负载在几乎所有负载箱中都小于GeBT模型,用于边缘和刷装根弯矩,这意味着线性光束模型可能低估了寿命刀片根的疲劳损坏。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号