湍流度与覆冰特性对导线动态气动力影响的数值 研究
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1.国网江苏省电力有限公司无锡供电分公司;2.重庆大学雪峰山能源装备安全国家野外科学观测研究站

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国网江苏省电力公司科技项目


Numerical Study on the Effects of Turbulence Intensity and Ice Accretion Characteristics on Dynamic Aerodynamic Forces of Transmission Line Conductors
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1.Wuxi Power Supply Branch, State Grid Jiangsu Electric Power Co., LTD.;2.Xuefengshan Energy Equipment Safety National Field Scientific Observation and Research Station, Chongqing University

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State Grid Jiangsu Electric Power Company's Science and Technology Projects

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    摘要:

    针对现有覆冰导线气动特性研究多基于静态或均匀流场的局限性,本文旨在揭示实际湍流风场中湍流参数(湍流度、平均风速)、覆冰形态(厚度、攻角)与导线动态气动响应的非线性关联机制,为输电线路防舞动设计提供理论依据。基于Fluent构建动态流场模型,通过脉动风速时程控制模拟不同湍流环境(湍流度0~15%,平均风速1~5 m/s),结合覆冰厚度(5~20 mm)与攻角(0°~45°)变化,系统分析覆冰导线的动态气动力特性。研究表明:湍流度增大会显著增强气动力瞬时波动幅值,但抑制其均值;平均风速超过临界值(2 m/s)后,升力系数均值回升而阻力系数持续降低;覆冰厚度增至15 mm时升力方向发生反转,阻力呈线性增长;攻角增至45°附近时升力突跳反转,阻力持续递增。研究结果为输电线路动态气动失稳机理分析与防舞设计优化提供了理论依据。

    Abstract:

    Due to the limitations of current studies on the aerodynamic characteristics of iced conductors—which are mostly based on static or uniform flow fields—this paper aims to reveal the nonlinear coupling mechanisms among turbulence parameters (turbulence intensity, mean wind speed) in actual turbulent wind fields, icing morphology (thickness, attack angle), and the dynamic aerodynamic response of conductors, thereby providing a theoretical basis for the anti-vibration design of transmission lines. A dynamic flow field model is constructed using Fluent, and different turbulent environments (turbulence intensity from 0 to 15% and mean wind speed from 1 to 5 m/s) are simulated through pulsating wind speed time-series control. Combined with variations in icing thickness (5 to 20 mm) and attack angle (30°to 45°), the dynamic aerodynamic characteristics of iced conductors are systematically analyzed. The study shows that an increase in turbulence intensity significantly enhances the instantaneous amplitude of aerodynamic fluctuations while suppressing their mean value; when the mean wind speed exceeds a critical value (2 m/s), the mean lift coefficient rebounds while the drag coefficient continuously decreases; when the icing thickness increases to 15 mm, the direction of lift reverses and the drag increases linearly; near an attack angle of 45°, the lift coefficient abruptly reverses while the drag continues to increase. These findings provide a theoretical foundation for analyzing the mechanisms of dynamic aerodynamic instability and for optimizing the anti-vibration design of transmission lines.

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  • 收稿日期:2025-04-15
  • 最后修改日期:2025-07-08
  • 录用日期:2025-08-03
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