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Structural investigation of composite wind turbine blade considering various load cases and fatigue life

机译:考虑各种载荷工况和疲劳寿命的复合材料风力涡轮机叶片的结构研究

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摘要

This study proposes a structural design for developing a medium scale composite wind turbine blade made of E-gLass/epoxy for a 750 kW class horizontal axis wind turbine system. The design loads were determined from various load cases specified at the IEC61400-1 international specification and GL regulations for the wind energy conversion system. A specific composite structure configuration, which can effectively endure various loads such as aerodynamic loads and loads due to accumulation of ice, hygro-thermal and mechanical loads, was proposed. To evaluate the proposed composite wind turbine blade, structural analysis was performed by using the finite element method. Parametric studies were carried out to determine an acceptable blade structural design, and the most dominant design parameters were confirmed. In this study, the proposed blade structure was confirmed to be safe and stable under various load conditions, including the extreme load conditions. Moreover, the blade adapted a new blade root joint with insert bolts, and its safety was verified at design loads including fatigue loads. The fatigue life of a blade that has to endure for more than 20 years was estimated by using the well-known S-N linear damage theory, the service load spectrum, and the Spera's empirical equations. With the results obtained from all the structural design and analysis, prototype composite blades were manufactured. A specific construction process including the lay-up molding method was applied to manufacturing blades. Full-scale static structural test was performed with the simulated aerodynamic loads. From the experimental results, it was found that the designed blade had structural integrity. In addition, the measured results of deflections, strains, mass, and radial center of gravity agreed well with the analytical results. The prototype blade was successfully certified by an international certification institute, GL (Germanisher Lloyd) in Germany.
机译:这项研究提出了一种结构设计,用于开发适用于750 kW级水平轴风力涡轮机系统的,由E-gLass /环氧树脂制成的中型复合风力涡轮机叶片。设计载荷是根据IEC61400-1国际规范和GL规例针对风能转换系统指定的各种载荷工况确定的。提出了一种特定的复合结构构造,该构造可以有效地承受各种载荷,例如空气动力学载荷和由于冰的积累引起的载荷,湿热载荷和机械载荷。为了评估建议的复合材料风力涡轮机叶片,使用有限元方法进行了结构分析。进行了参数研究以确定可接受的叶片结构设计,并确定了最主要的设计参数。在这项研究中,所提出的叶片结构在各种负载条件(包括极端负载条件)下被证实是安全且稳定的。此外,该叶片还采用了带有插入螺栓的新型叶片根部接头,并且在包括疲劳负荷在内的设计负荷下都经过了安全性验证。通过使用众所周知的S-N线性损伤理论,使用载荷谱和Spera的经验公式,估算了必须承受20年以上的叶片的疲劳寿命。通过所有结构设计和分析获得的结果,制造了复合材料原型叶片。将包括叠层成型法的特定构造过程应用于叶片制造。在模拟的空气动力载荷下进行了全面的静态结构测试。根据实验结果,发现设计的叶片具有结构完整性。另外,挠度,应变,质量和径向重心的测量结果与分析结果非常吻合。叶片原型已通过德国国际认证机构GL(德国劳埃德船级社)的成功认证。

著录项

  • 来源
    《Energy》 |2005年第12期|p.2101-2114|共14页
  • 作者

    C. Kong; J. Bang; Y. Sugiyama;

  • 作者单位

    Division of Aerospace and Naval Architectural Engineering, Chosun University, Gwangju, South Korea;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 能源与动力工程;
  • 关键词

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