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Comparison of numerical modelling techniques for impact investigation on a wind turbine blade

机译:风力涡轮机叶片冲击研究数值建模技术的比较

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摘要

Wind turbine blades are exposed to numerous impact risks throughout their lifetimes. The impact risks range from bird collisions during operation to impacts with surrounding structures at the time of transportation and installation. Impact loads on the fibre composite blades can induce several complex, simultaneously interacting and visually undetectable damage modes and have a high potential to reduce the local and global blade stiffness. An assessment of such impact-induced damages is therefore necessary and usually involves high computational costs using numerical procedures, especially when analysing large composite components. To minimise this computational expense, different numerical impact modelling techniques are utilised, primarily shell-elementbased approaches and multiscale-modelling-based global-local approaches. In this article, a comparison between (1) pure shell, (2) shell-to-solid coupling, and (3) submodelling finite element modelling techniques using Abaqus/Explicit is presented for a case where an impactor hits the leading edge of a blade. A high-fidelity local solid finite element model is developed for the leading edge of a DTU 10 MW blade at the region of impact and its stiffness is compared with baseline. A user material subroutine VUMAT for the intralaminar damage mode based on the Hashin failure criterion is formulated and then validated via an experiment from the literature. Finally, based on different numerical modelling techniques, impact investigations are performed, and the impact responses, damage to the blade and computational analysis durations are compared. It is found that the submodelling-based global-local approach is the most efficient analysis technique for this case, capturing failure modes including delamination, core crushing and local surface indentation in the blade. The findings of this study can be used to develop accurate and computationally efficient tools for modelling impact-induced damage to a blade.
机译:风力涡轮机叶片在其整个生命周期中都面临着许多撞击风险。撞击风险的范围从操作过程中的鸟类碰撞到运输和安装时对周围结构的撞击。纤维复合材料叶片上的冲击载荷会引起几种复杂的,同时相互作用的和视觉上无法检测到的破坏模式,并且具有降低局部和整体叶片刚度的巨大潜力。因此,对这种冲击造成的损坏进行评估是必要的,并且通常涉及使用数值程序的高计算成本,尤其是在分析大型复合部件时。为了使这种计算费用最小化,使用了不同的数值影响建模技术,主要是基于壳单元的方法和基于多尺度建模的全局局部方法。本文比较了(1)纯壳,(2)壳固耦合和(3)使用Abaqus / Explicit进行子建模的有限元建模技术,以比较撞击器撞到前缘的情况。刀。针对DTU 10 MW叶片在撞击区域的前缘开发了高保真局部实体有限元模型,并将其刚度与基线进行了比较。制定了基于Hashin破坏准则的层内损伤模式用户材料子例程VUMAT,然后通过文献中的实验对其进行验证。最后,基于不同的数值建模技术,进行了冲击研究,并对冲击响应,叶片损坏和计算分析持续时间进行了比较。发现基于子模型的全局局部方法是这种情况下最有效的分析技术,可捕获包括脱层,型芯破碎和叶片局部表面压痕在内的故障模式。这项研究的发现可用于开发精确且计算效率高的工具,以建模冲击引起的叶片损坏。

著录项

  • 来源
    《Composite Structures》 |2019年第2期|856-878|共23页
  • 作者单位

    Norwegian Univ Sci & Technol, Dept Marine Technol, Trondheim, Norway|NTNU, Ctr Marine Operat Virtual Environm SFI MOVE, Trondheim, Norway;

    Norwegian Univ Sci & Technol, Dept Mech & Ind Engn, Trondheim, Norway;

    Tech Univ Denmark, Dept Wind Energy, Kongens Lyngby, Denmark;

    Norwegian Univ Sci & Technol, Dept Marine Technol, Trondheim, Norway|NTNU, Ctr Marine Operat Virtual Environm SFI MOVE, Trondheim, Norway;

    NTNU, Ctr Marine Operat Virtual Environm SFI MOVE, Trondheim, Norway|Univ Adger, Dept Engn Sci, N-4879 Grimstad, Norway;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Wind turbine blade; Impact; Finite element method; Global-local method; Progressive failure analysis;

    机译:风力涡轮机叶片;冲击;有限元法;全局局部法;渐进式失效分析;

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