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Wake Deflection in Long Distance from a Yawed Wind Turbine

机译:偏航风力涡轮机的远距离尾迹偏转

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摘要

Since it is important to prevent the wake produced by upstream wind turbines from interfering with downstream wind turbines, a method of deflecting such wakes is desired. In this paper, we present the coupled analysis results of a computational fluid dynamics (CFD) simulation involving a three-bladed rigid wind turbine with a yaw control system that utilizes rFlow3D CFD code, which was developed by the Japan Aerospace Exploration Agency (JAXA), primarily for rotorcraft use. Herein, a three-dimensional (3D), compressible, and unsteady Reynolds-averaged Navier-Stokes (RANS) equation with a Spalart-Allmaras turbulence model is adopted as the governing equation. In this study, wind turbine computations using various wind turbine yaw angles are performed while focusing on the resulting wake velocity distribution and aerodynamic loads, after which the influences of the yaw angle are discussed. Next, based on the wake velocity distribution results for each yaw angle, we move on to a wake interference avoidance simulation for downstream wind turbines that utilizes two prepared wind turbines. Through this study, the following characteristics were confirmed. The results show wake deflection produced by adding yaw angle can provide a sufficient wake skew angle even in far-wake events. Furthermore, the yaw angle introduction accelerates the progression of vortex dissipation and brings about early velocity recovery in the wake region. Simultaneously, the introduction decreases the power generation amount of the yawed upstream wind turbine and increases the fatigue load of flapwise moment added to the blade root. In this paper, the details of flow field, oscillation, and the yawed wind turbine performance characteristics will also be described.
机译:由于重要的是防止上游风力涡轮机产生的尾流干扰下游风力涡轮机,因此需要一种使这种尾流偏转的方法。在本文中,我们介绍了由日本航空航天局(JAXA)开发的,包含三叶片刚性风力涡轮机和偏航控制系统的耦合流体动力学分析的耦合分析结果,该偏航控制系统利用了rFlow3D CFD代码。 ,主要用于旋翼飞机。在此,采用具有Spalart-Allmaras湍流模型的三维(3D),可压缩且不稳定的雷诺平均Navier-Stokes(RANS)方程作为控制方程。在这项研究中,在着重于产生的尾流速度分布和空气动力学载荷的同时,使用各种风力涡轮机偏航角进行了风​​力涡轮机计算,之后讨论了偏航角的影响。接下来,基于每个偏航角的尾流速度分布结果,我们继续进行下游干扰机的尾流干扰避免仿真,该仿真利用了两个准备好的风力涡轮机。通过本研究,确认了以下特征。结果表明,通过增加偏航角产生的尾流偏转即使在远尾事件中也可以提供足够的尾流偏斜角。此外,偏航角的引入加快了涡流消散的进程,并在尾流区域实现了早期速度恢复。同时,引入减少了偏航的上游风力涡轮机的发电量,并增加了加在叶片根部的襟翼力矩的疲劳负荷。在本文中,还将详细介绍流场,振荡和偏航风力发电机的性能特征。

著录项

  • 来源
    《Journal of Energy Resources Technology》 |2017年第5期|051212.1-051212.9|共9页
  • 作者单位

    Graduate School of Mechanical Engineering, Tokyo University of Science, 6-3-1 Niijuku, Katsushika-ku, Tokyo, Japan;

    Japan Aerospace Exploration Agency (JAXA), 6-13-1 Osawa, Mitaka-shi, Tokyo, Japan;

    Graduate School of Mechanical Engineering, Tokyo University of Science, 6-3-1 Niijuku, Katsushika-ku, Tokyo, Japan;

    Graduate School of Mechanical Engineering, Tokyo University of Science, 6-3-1 Niijuku, Katsushika-ku, Tokyo, Japan;

    Graduate School of Mechanical Engineering, Tokyo University of Science, 6-3-1 Niijuku, Katsushika-ku, Tokyo, Japan;

  • 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

  • 入库时间 2022-08-18 00:26:54

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