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低真空管道超高速磁浮模型车系统边界条件影响分析

牟瀚林 颜佳海 欧阳萍萍 张卫华 马卫华

牟瀚林, 颜佳海, 欧阳萍萍, 张卫华, 马卫华. 低真空管道超高速磁浮模型车系统边界条件影响分析[J]. 西南交通大学学报. doi: 10.3969/j.issn.0258-2724.20250335
引用本文: 牟瀚林, 颜佳海, 欧阳萍萍, 张卫华, 马卫华. 低真空管道超高速磁浮模型车系统边界条件影响分析[J]. 西南交通大学学报. doi: 10.3969/j.issn.0258-2724.20250335
MU Hanlin, YAN Jiahai, OUYANG Pingping, ZHANG Weihua, MA Weihua. Analysis of Influence of Boundary Conditions on Ultra-High-Speed Maglev Model Vehicle System in Low-Vacuum Pipeline[J]. Journal of Southwest Jiaotong University. doi: 10.3969/j.issn.0258-2724.20250335
Citation: MU Hanlin, YAN Jiahai, OUYANG Pingping, ZHANG Weihua, MA Weihua. Analysis of Influence of Boundary Conditions on Ultra-High-Speed Maglev Model Vehicle System in Low-Vacuum Pipeline[J]. Journal of Southwest Jiaotong University. doi: 10.3969/j.issn.0258-2724.20250335

低真空管道超高速磁浮模型车系统边界条件影响分析

doi: 10.3969/j.issn.0258-2724.20250335
基金项目: 国家重点研发计划(2024YFB4303205)
详细信息
    作者简介:

    牟瀚林(1982—),男,正高级工程师,博士研究生,研究方向为磁浮列车系统动力学,E-mail:004308@crfsdi.com

    通讯作者:

    欧阳萍萍(1982—),女,博士研究生,研究方向为磁浮列车系统动力学,E-mail:oypp@swjtu.edu.cn

  • 中图分类号: TH212;TH213.3

Analysis of Influence of Boundary Conditions on Ultra-High-Speed Maglev Model Vehicle System in Low-Vacuum Pipeline

  • 摘要:

    当磁浮车辆超高速运行时,轨道不平顺、空气阻力等边界条件将会显著影响车辆运行安全性与稳定性. 本文基于多态耦合轨道交通动模试验平台,建立考虑超导钉扎悬浮与导向力特性、空气阻力及轨道不平顺等条件的超高速磁浮模型车系统动力学模型,模拟在1.6 km试验线上实现最高速度(1 500 km/h)的牵引-惰行-制动工况;基于该动力学模型,仿真分析模型车系统在不同轨道不平顺幅值倍数、不同速度、不同限位间隙下运行的振动响应情况. 研究结果表明:低真空环境下,轨道不平顺幅值为0.15 mm时,最高速度工况下,动子在运行过程中呈左右摆动的振动形式,杜瓦垂向位移最大值达4.88 mm;随着模型车系统运行速度增大,系统振动增强,各动力学指标幅值呈上升趋势;横向限位间隙增大有利于减弱模型车系统横向振动,垂向限位间隙增大会加剧模型车系统垂向振动.

     

  • 图 1  模型车系统结构示意

    Figure 1.  Schematic diagram of model vehicle system structure

    图 2  动子运行里程、速度和加速度随运行时间变化示意

    Figure 2.  Schematic diagram of variation of operating mileage, speed, and acceleration of mover with running time

    图 3  悬浮力-高度变化

    Figure 3.  Suspension force–height variation

    图 4  导向力-横移变化

    Figure 4.  Guiding force–lateral displacement variation

    图 5  轨道不平顺数据

    Figure 5.  Track irregularity data

    图 6  动力学模型示意

    Figure 6.  Schematic diagram of dynamic model

    图 7  动子动力学响应

    Figure 7.  Dynamic response of mover

    图 8  杜瓦动力学响应

    Figure 8.  Dynamic response of Dewar

    图 9  横向垂向滑块受力

    Figure 9.  Forces on lateral and vertical sliders

    图 10  杜瓦动力学响应

    Figure 10.  Dynamic response of Dewar

    图 11  动子横向位移

    Figure 11.  Lateral displacement of mover

    图 12  不同速度下杜瓦动力学响应

    Figure 12.  Dynamic response of Dewar at different speeds

    图 13  不同速度下动子加速度响应

    Figure 13.  Acceleration response of mover at different speeds

    图 14  不同速度下垂向滑块受力响应

    Figure 14.  Force response of vertical slider at different speeds

    图 15  不同横向间隙下杜瓦动力学响应

    Figure 15.  Dynamic response of Dewar under different lateral clearances

    图 16  不同横向间隙下动子横向位移

    Figure 16.  Lateral displacement of mover under different lateral clearances

    图 17  不同垂向间隙下杜瓦动力学响应

    Figure 17.  Dynamic response of Dewar under different vertical clearances

    图 18  不同垂向间隙下动子垂向位移

    Figure 18.  Vertical displacement of mover under different vertical clearances

    表  1  动力学评价指标

    Table  1.   Dynamic evaluation indicators

    参数 数值
    杜瓦横向位移/mm ±5
    杜瓦垂向位移/mm ±5
    杜瓦横向加速度/g ±5
    杜瓦垂向加速度/g ±5
    下载: 导出CSV

    表  2  大气环境动力学响应

    Table  2.   Dynamic response in atmospheric environment

    最高
    速度/
    (km·h−1
    杜瓦横
    向位移
    幅值/mm
    杜瓦垂
    向位移
    幅值/mm
    杜瓦横
    向加速度
    幅值/(×g)
    杜瓦垂
    向加速度
    幅值/(×g)
    400 0.79 2.15 0.13 0.23
    700 1.54 7.45 0.49 0.82
    下载: 导出CSV
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  • 收稿日期:  2025-06-15
  • 修回日期:  2025-12-28
  • 网络出版日期:  2026-03-30

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