首页> 外文OA文献 >Passive aeroelastic tailoring of wind turbine blades : a numerical analysis
【2h】

Passive aeroelastic tailoring of wind turbine blades : a numerical analysis

机译:风力涡轮机叶片的被动气动弹性定制:数值分析

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

This research aims to have an impact towards a sustainable energy supply. In wind power generation losses occur at tip speed ratios which the rotor was not designed for. Since the ideal blade shape changes nonlinearly with rising wind speeds currently used pitch control mechanisms can only approach the ideal blade deformation. However aeroelastic effects, which cause additional deformation, are almost unavoidable in flexible blade design and it is desirable to tailor these effects to our advantage by a controlled use of orthotropic material properties and a smart design of the blade structure. The idea of systematic aeroelastic tailoring is not new but research has not yet solved the design challenge partly due to the lack of accurate simulation tools. Passively adaptive rotor blades would enable systematic aeroelastic tailoring and have the potential to reduce the cost of energy by around 6% [1]. Within this thesis a design procedure for passively adaptive rotor blades has been developed. It consists of an aerodynamic simulation and optimization code (based on Blade Element Momentum Theory), a structural simulation (based on Finite Element Analysis) and a fluid structure interaction correction loop (based on CFD and FEM). Using the developed design code passively adaptive rotor blades have been designed for the NREL phase VI test turbine. The results show that an ideal passively adaptive blade could improve the efficiency of the test turbine by 3% to 6%.
机译:这项研究旨在对可持续能源供应产生影响。在风力发电中,损耗是在未设计转子的叶尖速比下发生的。由于理想叶片的形状随风速的增加而非线性地变化,因此目前使用的变桨控制机构只能接近理想叶片的变形。但是,在弹性叶片设计中几乎不可避免地会产生导致额外变形的气弹效应,并且希望通过控制正交各向异性材料特性的使用和叶片结构的智能设计来使这些效应适应我们的优势。系统化气动弹性剪裁的想法并不是什么新鲜事物,但是由于缺少精确的仿真工具,研究尚未部分解决设计难题。被动自适应转子叶片将能够进行系统的气动弹性剪裁,并具有将能源成本降低6%的潜力[1]。在本论文中,已经开发了一种用于被动自适应转子叶片的设计程序。它由空气动力学仿真和优化代码(基于叶片元素动量理论),结构仿真(基于有限元分析)和流体结构相互作用校正环(基于CFD和FEM)组成。使用已开发的设计规范,已为NREL VI期试验涡轮机设计了无源自适应转子叶片。结果表明,理想的被动自适应叶片可以将测试涡轮的效率提高3%至6%。

著录项

  • 作者

    Deilmann Christian;

  • 作者单位
  • 年度 2009
  • 总页数
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号