时速600 km磁浮隧道衬砌表面气动载荷特征研究

Aerodynamic Load Characteristics of Tunnel Lining Surfaces Induced by a 600 km/h Maglev Train

  • 摘要: 高速磁浮列车通过隧道时,诱发了较大的气动载荷,是引起隧道衬砌疲劳破坏的主要原因之一。基于一维流动模型,揭示了隧道内压力波的基本特征,分析了隧道内最大正、负压值出现的位置和时刻,归纳了隧道长度、阻塞比和列车速度对气动载荷的影响特征。研究结果表明:隧道内测点压力波动由列车波特征和列车近场特征主导;压力波会呈现出周期性衰减特性,其衰减时间与隧道长度有关;当隧道长度大于0.6 km时,列车在隧道内运行时,取得最大负压值,列车离开隧道后,取得最大正压值。最大正、负压值对应的位置与隧道长度之比为定值0.5和0.667;压力最大值随着隧道长度的增加先增大后减小;压力极值会随着阻塞比的增加而增大;压力最大值与速度的2.51~3.76次方成正比;获得了隧道内气动载荷的分布规律和范围。研究成果可为隧道衬砌气动疲劳强度的设计提供理论支持。

     

    Abstract: The high-speed maglev train induces significant aerodynamic loads when passing through tunnels, which is one of the primary causes of fatigue damage to tunnel linings. Based on a one-dimensional flow mode, the fundamental characteristics of pressure waves inside the tunnel were revealed. The spatial and temporal distributions of the maximum positive and negative pressures were analyzed, and the influence patterns of tunnel length, blockage ratio, and train speed on aerodynamic loads were systematically summarized. The results indicate that the pressure fluctuations at the tunnel monitoring points are primarily governed by the train wave signature (TWS) and the train near-field signature (TNS). The pressure waves exhibit a periodic attenuation behavior, and the attenuation duration is closely related to the tunnel length. When the tunnel length exceeds 0.6 km, the maximum negative pressure occurs while the train is inside the tunnel, whereas the maximum positive pressure is reached after the train exits the tunnel. The positions corresponding to the maximum positive and negative pressures maintain fixed ratios to the tunnel length, at 0.5 and 0.667, respectively. The peak pressure initially increases and then decreases with increasing tunnel length. Both the maximum positive and negative pressures increase with the blockage ratio. In addition, the maximum pressure is proportional to the train speed raised to a power between 2.51 and 3.76. The distribution patterns and magnitude ranges of aerodynamic loads acting on the tunnel lining were quantitatively determined. These findings provide a theoretical reference for the aerodynamic fatigue strength design of tunnel linings.

     

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