首页> 外文OA文献 >A direct approach of design optimization for small horizontal axis wind turbine blades
【2h】

A direct approach of design optimization for small horizontal axis wind turbine blades

机译:小型水平轴风力涡轮机叶片设计优化的直接方法

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

The performance of a wind turbine rotor depends on the wind characteristics of the site and the aerodynamic shape of the blades. The blade geometry determines the torque and the power generated by the rotor. From aerodynamic point of view, an economic and efficient blade design is attained by the maximization of rotor power coefficient. For small wind turbine blade design, there are some factors different from large blade. Such as, the small ones experience much lower Reynolds number flow than the large ones, thus large wind turbine airfoils may perform very poorly in small applications. The small turbines are self-started at lower wind speed, thus the hub and tip parts are vital for the starting-up torque which should be able to conquer the resistance of the generator and the mechanical system. This paper presents a direct method for small wind turbine blade design and optimization. A unique aerodynamic mathematical model was developed to obtain the optimal blade chord and twist angle distributions along the blade span. The airfoil profile analysis was integrated in this approach. The Reynolds number effects, tip and hub effects, and drag effects were all considered in the design optimization. The optimal chords and twist angles were provided with series of splines and points and three-dimensional blade models. This approach integrates blade design and airfoil analysis process, and enables seamless link with computational fluid dynamics analysis and CNC manufacturing.
机译:风力涡轮机转子的性能取决于现场的风特性和叶片的空气动力学形状。叶片的几何形状决定了转子产生的扭矩和功率。从空气动力学的角度来看,通过使转子功率系数最大化可以实现经济有效的叶片设计。对于小型风力涡轮机叶片设计,有一些因素与大型叶片不同。例如,小型飞机的雷诺数流比大型飞机的雷诺数流低得多,因此大型风力涡轮机翼型在小型应用中的性能可能非常差。小型涡轮机以较低的风速自动启动,因此轮毂和叶尖部件对于启动扭矩至关重要,该扭矩应能够克服发电机和机械系统的阻力。本文提出了一种用于小型风力涡轮机叶片设计和优化的直接方法。开发了独特的空气动力学数学模型,以获得沿叶片跨度的最佳叶片弦和扭转角分布。机翼轮廓分析已整合到该方法中。设计优化中考虑了雷诺数效应,叶尖和轮毂效应以及阻力效应。通过一系列花键和点以及三维叶片模型提供了最佳的弦和扭转角。这种方法将叶片设计和机翼分析过程集成在一起,并且可以与计算流体动力学分析和CNC制造无缝连接。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

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