Airfoil design for large horizontal axis wind turbines in low wind speed regions

被引:24
|
作者
Li, Xingxing [1 ,2 ]
Zhang, Lei [1 ,2 ]
Song, Juanjuan [1 ,2 ]
Bian, Fengjiao [3 ]
Yang, Ke [1 ,2 ,4 ]
机构
[1] Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
[2] Chinese Acad Sci, Key Lab Wind Energy Utilizat, Beijing 100190, Peoples R China
[3] Goldwind Sci & Technol Co Ltd, Syst Control & Simulat Dept, Beijing 100176, Peoples R China
[4] Chinese Acad Sci, Dalian Natl Lab Clean Energy, Dalian 116023, Peoples R China
基金
中国国家自然科学基金;
关键词
low wind speed site; Horizontal axis wind turbine; High inflow turbulence; Noise; Special airfoil; Extended airfoil design optimization framework; REYNOLDS-NUMBERS; OPTIMIZATION; PERFORMANCE; METHODOLOGY;
D O I
10.1016/j.renene.2019.07.163
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
Low wind speed technology helps to reduce the cost of energy, but also creates huge challenge on the wind turbine blade design. To essentially address the particular blade requirements in low wind speed regions with high inflow turbulence, this study extends previous airfoil design optimization methods. Firstly, special design criteria were proposed besides traditional considerations, concerning efficiency, loads, noise and in particular the high inflow turbulence effects on the enlarged blades. Then through improved mathematic models and modified auto optimization platform, an extended airfoil design optimization framework dedicated to low wind speed sites was established. The case design results show that key features of the new airfoil tailed to low wind speed sites are effectively enhanced: the design lift coefficient and lift-to-drag ratio are fairly increased, and the maximum lift coefficient is well constrained. In addition, the acoustic parameter of the new airfoil is successfully reduced. More important is that the airfoil performance sensitivity to surface roughness and inflow turbulence intensity are evidently eliminated. These finally contribute to an improved overall performance. The rotor blade performance evaluation with the new design airfoil in further verified the case design. Results indicate the proposed framework is able to design special airfoils suited for site-specific blade requirements, contributed by the customized considerations, parameterization model, robust calculation method and global algorithms. (c) 2019 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2345 / 2357
页数:13
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