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Reliability-based fatigue life investigation for a medium-scale composite hydrokinetic turbine blade

机译:中型复合动力动叶片的基于可靠性的疲劳寿命研究

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摘要

As the most important, expensive component of a hydrokinetic turbine system, the composite turbine blade must achieve a long operating life (10-20 years). The investigation of fatigue life for the composite turbine blade is essential when designing a cost-effective hydrokinetic composite turbine system. A reliability-based fatigue life analysis methodology was developed for a medium-scale, horizontal axis, hydrokinetic turbine blade. Finite element method, coupled with the blade element momentum theory, was used to find the stress response on the turbine blade. The fatigue behavior of the blade was studied in stress-critical zones. A metamodel was constructed for the stress response according to simulations at specified design points. Accounting for uncertainties in material properties and the material S-N curve, the reliability analysis method was employed to estimate the fatigue life distribution of the hydrokinetic turbine blade. The effect of river velocity models on the fatigue life of turbine blades was also studied. The fatigue life of the composite blade was sensitive to composite material properties. Transverse strain E_(22) is particularly dominant which is related to the matrix cracking as the fatigue failure mode. The statistical distribution of S-N data implies a significant dependence of fatigue life on composite S-N data.
机译:复合动力涡轮叶片作为动水涡轮系统中最重要,最昂贵的组件,必须具有较长的使用寿命(10-20年)。在设计经济高效的流体动力学复合材料涡轮机系统时,研究复合材料涡轮机叶片的疲劳寿命至关重要。基于可靠性的疲劳寿命分析方法是针对中等规模的水平轴流体动力学涡轮机叶片开发的。结合叶片单元动量理论,使用有限元方法来寻找涡轮叶片上的应力响应。在应力关键区域研究了叶片的疲劳行为。根据指定设计点上的仿真,构建了用于应力响应的元模型。考虑到材料特性和材料S-N曲线的不确定性,采用可靠性分析方法来估算流体动力涡轮叶片的疲劳寿命分布。还研究了流速模型对涡轮叶片疲劳寿命的影响。复合材料叶片的疲劳寿命对复合材料的性能敏感。横向应变E_(22)是特别重要的,这与作为疲劳破坏模式的基体开裂有关。 S-N数据的统计分布意味着疲劳寿命对复合S-N数据的显着依赖。

著录项

  • 来源
    《Ocean Engineering 》 |2014年第1期| 230-242| 共13页
  • 作者单位

    Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology, Rolla, MO 65409, USA;

    Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology, Rolla, MO 65409, USA;

    Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology, Rolla, MO 65409, USA;

    Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology, Rolla, MO 65409, USA;

    Department of Materials Science and Engineering, University of North Texas, Denton, TX 76203, USA;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Fatigue; Reliability; Blade element momentum; Finite element method; Hydrokinetic; Composite blade;

    机译:疲劳;可靠性;叶片元素动量;有限元法;流体动力学复合刀片;

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