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Evaluating sources of wind turbine fatigue damage.

机译:评估风力涡轮机疲劳损伤的来源。

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摘要

Designing for fatigue has always been a formidable task for the wind turbine engineer. An integrated approach to wind turbine fatigue design is outlined which interfaces existing computer codes that generate simulated wind turbulence (SNLWIND-3D), model wind turbine dynamics (YawDyn and ADAMS), and estimate fatigue life (LIFE2). This approach is employed to investigate potential sources of fatigue damage to wind turbines. Three wind turbine models are used including a downwind, three-bladed, rigid hub machine, an upwind, three-bladed, rigid hub machine, and a downwind, two-bladed, teetering hub machine. For each model, stress cycles at the blade root are calculated from flap moment cycles. Conversion factors for this task were determined based on assumptions regarding fatigue load levels the blades are designed to tolerate. The load to stress conversion and interface of dynamic analysis and fatigue life programs were expedited by the program Dyn2LIFE developed as part of this project.;Results confirm the necessity for accurate models of both wind turbulence and wind turbine to yield meaningful fatigue analysis results. The importance of a complete fatigue analysis including fatigue damage calculation is demonstrated as a means toward understanding the significance of fatigue design decisions. This project reveals several specific sources of fatigue loads.;Although turbulence is a well-known, yet uncontrollable, source of fatigue cycles, it is shown that resultant fatigue damage may actually be due to controllable machine response. For the three-bladed machines, yaw is found to play a significant role in fatigue damage rates. High yaw rates of the free yaw machine are shown to yield gyroscopic load cycles far larger than most other normal operation load cycles. For the fixed yaw machine, yaw error is shown to be a significant source of fatigue damage. Differences in the response of rigid and teetering hub machines make the latter type of turbine more susceptible to rare, extreme load events, primarily because normal operating loads are reduced by design. Hence, these extreme load events prove to better serve as design drivers for teetered turbines, whereas normal operation loads are found to be the greater concern for rigid hub machines.
机译:疲劳设计一直是风力涡轮机工程师的艰巨任务。概述了一种用于风力涡轮机疲劳设计的集成方法,该方法与现有的计算机代码相连接,这些计算机代码生成模拟的风力湍流(SNLWIND-3D),对风力涡轮机动力学进行建模(YawDyn和ADAMS)并估算疲劳寿命(LIFE2)。该方法用于研究风力涡轮机疲劳损坏的潜在来源。使用了三种风力涡轮机模型,包括顺风,三叶片,刚性轮毂机,逆风,三叶片,刚性轮毂机和顺风,两叶片,颤抖轮毂机。对于每个模型,叶片根部的应力周期是根据襟翼力矩周期计算得出的。该任务的转换系数是根据有关叶片可承受的疲劳载荷水平的假设确定的。该项目的一部分开发的程序Dyn2LIFE加快了应力转换的压力以及动态分析和疲劳寿命程序的接口。结果证实了建立精确的风湍流和风力涡轮机模型以产生有意义的疲劳分析结果的必要性。完整疲劳分析(包括疲劳损伤计算)的重要性被证明是理解疲劳设计决策重要性的一种手段。该项目揭示了疲劳载荷的几种具体来源。尽管湍流是众所周知的但不可控制的疲劳循环源,但它表明,由此引起的疲劳损伤实际上可能是由于可控的机器响应所致。对于三叶机,偏航在疲劳损伤率中起着重要作用。自由偏航机的高偏航率显示出陀螺仪的负载周期远大于大多数其他正常运行的负载周期。对于固定偏航机来说,偏航误差被证明是造成疲劳损伤的重要原因。刚性和摇摆式轮毂机的响应差异使后一种类型的涡轮机更容易发生罕见的极端负载事件,这主要是因为通过设计降低了正常运行负载。因此,这些极端负载事件被证明可以更好地用作摇臂式涡轮机的设计驱动程序,而对于刚性轮毂机器,正常运行负载则更为重要。

著录项

  • 作者

    Laino, David John.;

  • 作者单位

    The University of Utah.;

  • 授予单位 The University of Utah.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 151 p.
  • 总页数 151
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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