陈安杰, 王策, 贾娅娅, 刘庆宽. 基于BEM的风力机叶片气动性能计算分析[J]. 工程力学, 2021, 38(S): 264-268. DOI: 10.6052/j.issn.1000-4750.2020.05.S035
引用本文: 陈安杰, 王策, 贾娅娅, 刘庆宽. 基于BEM的风力机叶片气动性能计算分析[J]. 工程力学, 2021, 38(S): 264-268. DOI: 10.6052/j.issn.1000-4750.2020.05.S035
CHEN An-jie, WANG Ce, JIA Ya-ya, LIU Qing-kuan. COMPUTATION AND ANALYSIS OF AERODYNAMIC PERFORMANCE OF WIND TURBINE BLADE BASED ON BEM[J]. Engineering Mechanics, 2021, 38(S): 264-268. DOI: 10.6052/j.issn.1000-4750.2020.05.S035
Citation: CHEN An-jie, WANG Ce, JIA Ya-ya, LIU Qing-kuan. COMPUTATION AND ANALYSIS OF AERODYNAMIC PERFORMANCE OF WIND TURBINE BLADE BASED ON BEM[J]. Engineering Mechanics, 2021, 38(S): 264-268. DOI: 10.6052/j.issn.1000-4750.2020.05.S035

基于BEM的风力机叶片气动性能计算分析

COMPUTATION AND ANALYSIS OF AERODYNAMIC PERFORMANCE OF WIND TURBINE BLADE BASED ON BEM

  • 摘要: 叶片是风力发电机组捕获风能的核心部件,因此叶片的气动性能及可靠性是风力机安全运行的关键。本文以某1.5 MW风力机为研究对象,采用GH Bladed计算软件计算得到风力机叶片气动载荷的分布规律,并分析了风速及叶尖速比对叶片的气动载荷影响特性。结果表明:轴向荷载数值远大于切向荷载数值,轴向荷载数值沿着叶片尖端到叶片根部不断减小,随着风速的增大,轴向荷载沿展向分布曲线愈加平缓;叶根气动载荷中起控制作用的是轴向推力与挥舞方向弯矩,且随着风速增加至额定风速而单调增加;叶尖速比增大至5时,轴向荷载沿展向分布曲线平缓且峰值减小,当叶尖速比从7增大至11时,轴向荷载在叶尖又出现尖点且峰值大幅增加;当叶尖速比增大至7时,切向荷载逐渐增大,当叶尖速比从7增至11时,切向荷载减小;叶根气动载荷中起控制作用的是轴向推力与挥舞方向弯矩,随着叶尖速比的增大而单调增加,摆阵方向弯矩值随叶尖速比的增加呈现出先增大后减小的趋势。

     

    Abstract: Blade is the core component of a wind turbine to capture wind energy, the aerodynamic performance and reliability of blade is thusly the key to the safe operation of a wind turbine. In this paper, a 1.5 MW wind turbine is taken as the research object. The distribution of aerodynamic load on the blade of the wind turbine is computed by GH Bladed computational software, and the influence characteristics of wind speed and tip speed ratio on the aerodynamic load of the blade are analyzed. The analysis results show that: the axial load value is far greater than the tangential load value, the axial load value decreases along the blade tip to the blade root, and the axial load distribution curve becomes more and more gentle along the span with the increase of wind speed; in the aerodynamic load of the blade root, the axial thrust and the bending moment in the swing direction play a controlling role, and increase monotonously as the wind speed increases to the rated wind speed; when the tip speed ratio increases to 5, the axial load distribution curve is gentle and the peak value decreases; when the tip speed ratio increases from 7 to 11, the axial load appears at the tip again and the peak value increases significantly; when the tip speed ratio increases to 7, the tangential load increases gradually; when the tip speed ratio increases from 7 to 11, the tangential load decreases; the axial thrust and the bending moment in the swing direction play a controlling role in the aerodynamic load of the blade root; with the increase of the tip speed ratio, the bending moment in the swing direction increases first and then decreases.

     

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