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S型叶尖小翼对风力机流场特性影响的研究
引用本文:张立茹,汪建文,于海鹏,由志刚,高志鹰.S型叶尖小翼对风力机流场特性影响的研究[J].工程热物理学报,2012(5):788-791.
作者姓名:张立茹  汪建文  于海鹏  由志刚  高志鹰
作者单位:内蒙古工业大学能源与动力工程学院;风能太阳能利用技术省部共建教育部重点实验室
基金项目:教育部博士学科点专项科研基金(No.20091514110001);内蒙古自治区高等学校科学研究项目(No.NJ09072)
摘    要:在额定尖速比下,结合滑移网格的大涡模拟方法,对有无叶尖S型小翼的三叶片水平轴风力机流场特性进行了数值研究,结果表明:加装S型小翼后,改善了风轮上游的速度及压力分布情况,汲取了更多的风能;风轮压力面及吸力面的最大压差由1359 Pa提高到1756 Pa,使风轮功率放大;叶尖涡结构扩展规律与PIV(Particle Image Velocimetry)实验结果一致,叶尖涡轴向速度由15.6 m/s降低到了13.3 m/s,涡漩能量减少,叶尖涡涡量强度减弱,降低了气动噪声。

关 键 词:水平轴风力机  S型小翼  流场特性  影响

Research on Characteristics of the Flow Field of Wind Turbine With the S-Type Tip Vane
ZHANG Li-Ru,WANG Jian-Wen,YU Hai-Peng,YOU Zhi-Gang,GAO Zhi-Ying.Research on Characteristics of the Flow Field of Wind Turbine With the S-Type Tip Vane[J].Journal of Engineering Thermophysics,2012(5):788-791.
Authors:ZHANG Li-Ru  WANG Jian-Wen  YU Hai-Peng  YOU Zhi-Gang  GAO Zhi-Ying
Institution:1,2) (1.College of Energy and Power Engineering Inner Mongolia University of Technology,Hohhot,Inner Mongolia 010051,China; 2.Key Laboratory of Wind Energy and Solar Energy of the Ministry of Education,Hohhot,Inner Mongolia 010051,China)
Abstract:With the given tip speed ratio,combined with the large eddy simulation method of sliding mesh,this paper did numerical studies on the characteristics of the flow field of the three-blade horizontal axis wind turbine with and without the S-type tip vane.Results showed that:With the S-type tip vane,the speed and pressure distribution of upstream of the wind turbine were improved and more wind energy were absorbed.The differential pressure of the wind turbine between pressure surface and suction surface increased from 1359 Pa to 1756 Pa,which made the power of the wind turbine amplify.The law of tip vortex was consistent to the experimental results of the PIV. Meanwhile,axial velocity of the tip vortex reduced from 15.6 m/s to 13.3 m/s,the energy of vortex and intensity were reduced and the aerodynamic noise was reduced.
Keywords:horizontal axis wind turbine  S-type tip vane  characteristics of flow field  effects
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