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LINEARIZED MODEL FOR WIND TURBINES IN YAW (HORIZONTAL AXIS, STATIC STABILITY).

机译:横摆风力涡轮机的线性化模型(水平轴,静态稳定性)。

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摘要

The analysis of rigid hub, three-bladed horizontal-axis, axisymmetric wind turbines in yaw is made using a linearized, four-degree-of-freedom model. The linearized equations of motion of rotor and nacelle are developed using quasi-steady blade element theory and Lagrange's equations.;The yaw behavior of the system is studied from coefficients of the equations of motion. Analytical results for two wind turbines are presented and studied. The study shows that yaw tracking error is primarily caused by tower shadow. The contribution of the nacelle to the yaw stability is proved to be a destabilizing one. The yaw stability of a wind turbine in a reverse position is investigated and used for verification of the analysis.;The characteristics of yaw static stability are primarily determined by the characteristics of the in-plane force coefficient and the location of the yaw axis relative to the rotor plane. A sensitivity study of the terms in the yaw stiffness coefficient is made. The yaw static stability is strongly affected by a change in the coning angle.;Two Fortran computer programs are developed to compute the numerical values of coefficients of the equations of motion. Program listings and sample outputs are included.
机译:使用线性四自由度模型对偏航中的刚性轮毂,三叶片水平轴,轴对称风力涡轮机进行了分析。利用准稳态叶片单元理论和拉格朗日方程,建立了转子和机舱的线性运动方程。;系统的横摆特性是根据运动方程的系数来研究的。介绍并研究了两个风力涡轮机的分析结果。研究表明,偏航跟踪误差主要是由塔影引起的。机舱对偏航稳定性的贡献被证明是不稳定的。研究了风力涡轮机在反向位置时的偏航稳定性,并将其用于分析验证。;偏航静态稳定性的特性主要取决于平面内力系数的特性以及相对于偏航轴的位置转子平面。进行了偏航刚度系数项的敏感性研究。锥角的变化强烈影响偏航静态稳定性。;开发了两个Fortran计算机程序来计算运动方程系数的数值。包括程序清单和示例输出。

著录项

  • 作者

    CHAIYAPINUNT, SOMSAK.;

  • 作者单位

    Oregon State University.;

  • 授予单位 Oregon State University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1984
  • 页码 222 p.
  • 总页数 222
  • 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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