韩兴波, 孙鹏, 王杰, 陈孜铭, 蒋兴良. 大型风机迎风面覆冰增长规律及气动特性[J]. 高电压技术, 2025, 51(3): 1169-1179. DOI: 10.13336/j.1003-6520.hve.20240548
引用本文: 韩兴波, 孙鹏, 王杰, 陈孜铭, 蒋兴良. 大型风机迎风面覆冰增长规律及气动特性[J]. 高电压技术, 2025, 51(3): 1169-1179. DOI: 10.13336/j.1003-6520.hve.20240548
HAN Xingbo, SUN Peng, WANG Jie, CHEN Ziming, JIANG Xingliang. Growth Law and Aerodynamic Characteristics of Icing on the Windward Side of Large Wind Turbines[J]. High Voltage Engineering, 2025, 51(3): 1169-1179. DOI: 10.13336/j.1003-6520.hve.20240548
Citation: HAN Xingbo, SUN Peng, WANG Jie, CHEN Ziming, JIANG Xingliang. Growth Law and Aerodynamic Characteristics of Icing on the Windward Side of Large Wind Turbines[J]. High Voltage Engineering, 2025, 51(3): 1169-1179. DOI: 10.13336/j.1003-6520.hve.20240548

大型风机迎风面覆冰增长规律及气动特性

Growth Law and Aerodynamic Characteristics of Icing on the Windward Side of Large Wind Turbines

  • 摘要: 风力发电机叶片在复杂低温气象条件下极易覆冰,覆冰造成的风机停运或结构损坏等问题一直困扰着风电行业的发展。为此模拟了不同环境条件的风机表面的水滴撞击特性,分析了叶片积冰增长对其气动特性的影响规律,并结合野外风机覆冰观测实验进行对比验证。结果表明:水滴中值直径为20~40 µm之间时,叶片水滴碰撞率变化较大,风速为8~10 m/s时,水滴碰撞率的增长率减小;翼型厚度减小会导致水滴的碰撞范围减小,驻点处的局部碰撞率却逐渐增大。洁净翼型和流线冰翼型的最大升阻比较为接近,流线冰翼型升阻比达到最大值后(临界攻角)随着攻角的增大而减小,而角状冰翼型升阻比达到最大值的临界攻角相对更小。相对于无冰状态,带冰后翼型的失速攻角减小;相对于洁净翼型,流线冰翼型在覆冰2.8 h后功率降低18.5%,角状冰翼型覆冰情况下输出功率降低达76.8%。该研究结果可为风机覆冰条件下的性能分析提供数据积累和技术参考。

     

    Abstract: Wind turbine blades are highly susceptible to ice overlay under complex low-temperature meteorological conditions, and problems such as wind turbine shutdown or structural damage caused by ice overlay have been troubling the development of the wind power industry. This paper simulates the water droplet impact characteristics on the wind turbine surface under different environmental conditions, analyses the influence of the growth of blade ice accumulation on its aerodynamic characteristics, and combines the field wind turbine ice-covering observation experiments for comparative verification. The results show that, when the median diameter of water droplets is between 20 µm and 40 µm, the variation of water droplet collision rate of the blade is larger, and the growth rate of water droplet collision rate decreases when the wind speed is between 8 m/s and 10 m/s; the reduction of the airfoil thickness leads to the reduction of the collision range of the water droplets, while the local collision rate at the stationary point gradually increases. The maximum lift-resistance ratios of the clean and streamlined ice airfoils are very close to each other; after reaching the maximum value of the lift-resistance ratio of the streamlined ice airfoil (critical angle of attack), the ratio decreases with the increase of the angle of attack, whereas the angular ice airfoil lift-resistance ratio reaches its maximum value at a relatively smaller critical angle of attack. The stall angle of attack of the airfoil with ice decreases relative to the ice-free condition; relative to the clean airfoil, the streamlined ice airfoil has a power reduction of 18.5% after 2.8 h of ice cover, and the angular ice airfoil has a power reduction of up to 76.8% in the case of ice cover. The results of this paper can provide data accumulation and technical reference for the performance analysis of wind turbines under ice-covered conditions.

     

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