• CN:11-2187/TH
  • ISSN:0577-6686

›› 2011, Vol. 47 ›› Issue (10): 113-118.

• 论文 • 上一篇    下一篇

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水平轴风力机的功率极限

姜海波;曹树良;阳平   

  1. 海军工程大学后勤指挥与工程系;清华大学热能工程系
  • 发布日期:2011-05-20

Power Limit of Horizontal Axis Wind Turbine

JIANG Haibo;CAO Shuliang;YANG Ping   

  1. Department of Logistics Command and Engineering, Naval University of Engineering Department of Thermal Engineering, Tsinghua University
  • Published:2011-05-20

摘要: 为求得理想风力机的功率系数随尖速比和翼型升阻比变化的表达式,作为实际风力机功率系数的理论极值,采用叶素—动量理论,推导出理想叶片弦长公式;沿理想叶片翼展积分,得到功率系数表达式。在该表达式中令阻力系数为0,得到与尖速比关联的功率系数极限公式;进一步令尖速比趋近于无穷大,得到贝兹极限(16/27)。为给出实际风力机功率系数极限值,以及为便于理论分析,对升阻比在10~1 000和尖速比在1~10范围内的理想风力机的功率系数进行详细计算,给出了数据表格。研究结果表明,理想风力机的功率系数仅是尖速比和升阻比的函数,只有当尖速比和升阻比都趋近于无穷大时功率系数才趋近于贝兹极限。研究还表明,升阻比小于100的实际风力机的功率系数不可能超过0.538,如果考虑有限叶片数和叶片形状的影响,实际风力机的功率系数难以超过0.500

关键词: 贝兹极限, 风能利用, 功率系数极限, 尖速比, 气动效率, 升阻比, 水平轴理想风力机, 共同空间模式, 康复训练, 脑电信号, 上肢外骨骼

Abstract: In order to obtain the expression of the ideal horizontal axis wind turbine power coefficient with tip-speed ratio and airfoil lift-drag ratio changes, as the theoretical extreme value of an actual wind turbine power coefficient, the ideal blade chord expression is deduced by blade element-momentum (BEM) theory, and the ideal wind turbine power coefficient is obtained by integrating along the ideal blade span. Let the drag coefficient in the power coefficient expression equal to 0, the power coefficient limit formula associated with the tip-speed ratio is obtained; and further let the tip-speed ratio approach to infinity, Betz limit (16/27) is obtained. To find the actual wind turbine power coefficient limit, and to facilitate theoretical analysis, ideal wind turbine power coefficient for lift-drag ratio in the range of 10 to 1 000 and tip-speed ratio of 1 to 10 is calculated in detail, and the corresponding data form is given. The research shows that the ideal wind turbine power coefficient is only the function of tip-speed ratio and the lift-drag ratio, and the power coefficient approaches Betz limit only when both the tip-speed ratio and the lift-drag ratio is close to infinity. The results also show that the actual wind turbine power coefficient is impossible to exceed 0.538 if the lift-drag ratio is less than 100, and is difficult to exceed 0.500 if the effects of limited blade number and blade shape are considered.

Key words: Aerodynamic efficiency, Betz limit, Ideal horizontal axis wind turbine(IHAWT), Lift-drag ratio, Power coefficient limit, Tip-speed ratio, Wind energy utilization, CSP, EEG, Rehabilitation training, Upper-limb exoskeleton

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