赵元星, 汪建文, 张立茹, 刘珍, 白叶飞. 气动力和离心力对风力机叶片应力影响研究[J]. 太阳能学报, 2021, 42(2): 225-232. DOI: 10.19912/j.0254-0096.tynxb.2020-1004
引用本文: 赵元星, 汪建文, 张立茹, 刘珍, 白叶飞. 气动力和离心力对风力机叶片应力影响研究[J]. 太阳能学报, 2021, 42(2): 225-232. DOI: 10.19912/j.0254-0096.tynxb.2020-1004
Zhao Yuanxing, Wang Jianwen, Zhang Liru, Liu Zhen, Bai Yefei. RESEARCH ON INFLUENCE OF AERODYNAMIC LOAD AND CENTRIFUGAL LOAD ON WIND-TURBINE-BLADE STRESS[J]. Acta Energiae Solaris Sinica, 2021, 42(2): 225-232. DOI: 10.19912/j.0254-0096.tynxb.2020-1004
Citation: Zhao Yuanxing, Wang Jianwen, Zhang Liru, Liu Zhen, Bai Yefei. RESEARCH ON INFLUENCE OF AERODYNAMIC LOAD AND CENTRIFUGAL LOAD ON WIND-TURBINE-BLADE STRESS[J]. Acta Energiae Solaris Sinica, 2021, 42(2): 225-232. DOI: 10.19912/j.0254-0096.tynxb.2020-1004

气动力和离心力对风力机叶片应力影响研究

RESEARCH ON INFLUENCE OF AERODYNAMIC LOAD AND CENTRIFUGAL LOAD ON WIND-TURBINE-BLADE STRESS

  • 摘要: 针对自行研制的NACA4415翼型水平轴风力机,通过流固耦合的数值模拟计算方法,考虑气动力和离心力以及两者耦合作用,选取叶片最大弦长、中部弦长、气动中心线展向以及最大应力点位置,分析风力机叶片在不同工况下的应力特性分布规律。结果表明:在气动力作用下,叶片相同弦长位置处迎风面应力小于背风面应力,且随尖速比和入流风速增大而增大,最大应力点位置随着尖速比增大沿翼展向外且靠近叶片前缘方向延伸;在离心力作用下,叶片相同弦长位置处迎风面应力大于背风面应力,且随尖速比增大而增大,而最大应力点均在叶根最大弦长位置(9.93 mm,10.80 mm,-126.33 mm);在耦合作用下,叶片相同弦长位置处迎风面应力大于背风面应力,随尖速比和入流风速增大而增大,且依次大于气动力和离心力产生的应力,而最大应力点均在叶根最大弦长位置。仿真结果对于风力机翼型的选择及优化设计具有重要的理论意义及参考价值。

     

    Abstract: Useing the NACA 4415 horizontal-axis wind turbine as a case study and through the numerical simulation calculation method of fluid-solid coupling,considering the aerodynamic load and centrifugal load as well as their coupling effect,the maximum chord length,middle chord length,aerodynamic center line spanwise direction and the position of the maximum stress point are selected to analyze the stress characteristics of wind turbine blade under different working conditions in this paper.The study indicates that under aerodynamic load,the windward surface stress at the same chord length of the blade is less than the leeward stress,which increases with the tip speed ratio and the inflow wind speed.As the tip speed ratio increases,the maximum stress point position extends outward along the wingspan and near the leading edge of the blade.Under the action of centrifugal load,the windward surface stress at the same chord length of the blade is greater than the leeward surface stress,which increases with the tip speed ratio,the maximum stress point is at the maximum chord length of the blade(9.93 mm,10.80 mm,-126.33 mm).Under the coupling action,the windward surface stress at the same chord length of the blade is greater than the leeward surface stress,which increases with the increase of the tip speed ratio and the inflow wind speed.Also,the windward surface stress is in turn greater than the stress generated by aerodynamic load and centrifugal load.The maximum stress point is at the maximum chord length of the blade.The simulation results have important theoretical significance and reference value for the selection and optimization design of wind turbine airfoil.

     

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