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大跨度双层桁架梁悬索桥颤振性能试验研究

雷永富 李明 孙延国 李明水

雷永富, 李明, 孙延国, 李明水. 大跨度双层桁架梁悬索桥颤振性能试验研究[J]. 西南交通大学学报, 2022, 57(6): 1224-1232. doi: 10.3969/j.issn.0258-2724.20200599
引用本文: 雷永富, 李明, 孙延国, 李明水. 大跨度双层桁架梁悬索桥颤振性能试验研究[J]. 西南交通大学学报, 2022, 57(6): 1224-1232. doi: 10.3969/j.issn.0258-2724.20200599
LEI Yongfu, LI Ming, SUN Yanguo, LI Mingshui. Experimental Study on Flutter Performance of Long-Span Suspension Bridge with Double-Deck Truss Girder[J]. Journal of Southwest Jiaotong University, 2022, 57(6): 1224-1232. doi: 10.3969/j.issn.0258-2724.20200599
Citation: LEI Yongfu, LI Ming, SUN Yanguo, LI Mingshui. Experimental Study on Flutter Performance of Long-Span Suspension Bridge with Double-Deck Truss Girder[J]. Journal of Southwest Jiaotong University, 2022, 57(6): 1224-1232. doi: 10.3969/j.issn.0258-2724.20200599

大跨度双层桁架梁悬索桥颤振性能试验研究

doi: 10.3969/j.issn.0258-2724.20200599
基金项目: 国家自然科学基金(51878580);四川省科技计划(2020YJ0306)
详细信息
    作者简介:

    雷永富(1994—),男,博士研究生,研究方向为结构风工程,E-mail:yflei@my.swjtu.edu.cn

    通讯作者:

    李明(1990—),男,副研究员,博士,研究方向为桥梁及结构风工程、钝体空气动力学,E-mail:liming_bridge@163.com

  • 中图分类号: U441.3

Experimental Study on Flutter Performance of Long-Span Suspension Bridge with Double-Deck Truss Girder

  • 摘要:

    为提高大跨度双层桁架梁悬索桥的颤振性能,以主跨为1 700 m的杨泗港长江大桥为工程背景,通过节段模型风洞试验,分别研究了上中央稳定板、下稳定板、水平翼板以及组合措施对主梁颤振性能的影响,并通过将有效气动措施与主梁原有构件相结合的方法来减小传统气动措施带来的不利影响,针对最优气动方案,研究了阻尼比对主梁颤振性能的影响. 研究结果表明:原主梁断面在0° 和 +3° 攻角下发生了没有明显发散点的单自由度扭转软颤振,颤振临界风速分别为50.5 m/s和31.2 m/s;安装于上层桥面的上中央稳定板、下层桥面的下稳定板以及与人行道底部齐平的水平翼板均能不同程度地提高主梁的颤振稳定性;当把水平翼板与下层桥面的下稳定板组合后,主梁的颤振临界风速增长率可高达34%,在此基础上提出了将上层托架和人行道板加宽、并将下稳定板和检修车轨道相结合的最优气动方案;当扭转阻尼比由0.37%增加至0.52%时,主梁的颤振临界风速可提高11.9%,说明阻尼器可能对发生单自由度扭转软颤振的桥梁起到良好的抑振效果.

     

  • 图 1  杨泗港长江大桥总布置(单位:m)

    Figure 1.  General layout of the Yangsigang Yangtze River Bridge (unit:m)

    图 2  主梁横断面(单位:m)

    Figure 2.  Cross-section of main girder (unit:m)

    图 3  风洞中的桥梁节段模型

    Figure 3.  Section model of main girder in the wind tunnel

    图 4  主梁的扭转位移均方根值随风速变化曲线

    Figure 4.  Variation of the standard deviation of torsional displacements of main girder with the wind speed

    图 5  +3° 攻角下主梁软颤振位移时程与相位图

    Figure 5.  Time history and phase diagram of soft flutter displacements of main girder at an attack angle of +3°

    图 6  上中央稳定板示意

    Figure 6.  Schematic of the upper central stabilizers

    图 7  上中央稳定板对主梁颤振性能的影响

    Figure 7.  Effect of the upper central stabilizer on the flutter performance of the main truss girder

    图 8  下稳定板示意

    Figure 8.  Schematic diagram of the lower stabilizers

    图 9  下稳定板对主梁颤振性能的影响

    Figure 9.  Effect of the lower stabilizers on the flutter performance of the main truss girder

    图 10  水平翼板示意

    Figure 10.  Schematic of the horizontal flap

    图 11  水平翼板对主梁颤振性能的影响

    Figure 11.  Effect of the horizontal flap on the flutter performance of the main truss girder

    图 12  组合措施示意

    Figure 12.  Schematic of combined measures

    图 13  水平翼板与下稳定板组合对主梁颤振稳定性的影响

    Figure 13.  Effect of the combination of the horizontal flap and the lower stabilizer on the flutter performance of main girder

    图 14  优化桁架梁断面

    Figure 14.  Cross-section of the optimized truss girder

    图 15  系统扭转阻尼比对主梁颤振临界风速的影响

    Figure 15.  Effect of system torsional damping ratio on the critical flutter wind speed of the main girder

    图 16  不同阻尼比条件下最优气动方案主梁的扭转位移响应

    Figure 16.  Torsional response of the optimal truss girder in different damping ratio conditions

    表  1  节段模型主要试验参数

    Table  1.   Main test parameters of section model

    参数名称符号缩尺比实桥值理论值实际值
    主桁高/m H 1∶52.67 10.00 0.19 0.19
    主桁宽/m B 1∶52.67 28.000 0.532 0.532
    单位长度质量/(kg•m−1 m 1∶52.672 53 027.00 19.13 19.14
    单位长度质量惯矩/(kg•m) I 1∶52.674 7 465 823.000 0.970 0.979
    一阶竖弯频率/Hz f1 0.117 1.695
    一阶扭转频率/Hz f2 0.284 4.095
    竖弯阻尼比/% ζ1 1 0.50 0.36
    扭转阻尼比/% ζ2 1 0.50 0.37
    扭弯频率比 ε 1 2.418 2.418 2.417
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出版历程
  • 收稿日期:  2020-09-05
  • 修回日期:  2020-11-05
  • 网络出版日期:  2022-08-03
  • 刊出日期:  2020-11-11

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