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侧风非均匀积水道面耦合作用下飞机偏出跑道的行为特征

张耀华 种小雷 任怡楠 周则圆

张耀华, 种小雷, 任怡楠, 周则圆. 侧风非均匀积水道面耦合作用下飞机偏出跑道的行为特征[J]. 交通运输工程学报, 2026, 26(8): 231-242. doi: 10.19818/j.cnki.1671-1637.2026.324
引用本文: 张耀华, 种小雷, 任怡楠, 周则圆. 侧风非均匀积水道面耦合作用下飞机偏出跑道的行为特征[J]. 交通运输工程学报, 2026, 26(8): 231-242. doi: 10.19818/j.cnki.1671-1637.2026.324
ZHANG Yao-hua, CHONG Xiao-lei, REN Yi-nan, ZHOU Ze-yuan. Characteristics of aircraft runway veer-off behavior due to coupled action of crosswind and uneven water accumulation on pavement[J]. Journal of Traffic and Transportation Engineering, 2026, 26(8): 231-242. doi: 10.19818/j.cnki.1671-1637.2026.324
Citation: ZHANG Yao-hua, CHONG Xiao-lei, REN Yi-nan, ZHOU Ze-yuan. Characteristics of aircraft runway veer-off behavior due to coupled action of crosswind and uneven water accumulation on pavement[J]. Journal of Traffic and Transportation Engineering, 2026, 26(8): 231-242. doi: 10.19818/j.cnki.1671-1637.2026.324

侧风非均匀积水道面耦合作用下飞机偏出跑道的行为特征

doi: 10.19818/j.cnki.1671-1637.2026.324
详细信息
    作者简介:

    张耀华(1999-),男,陕西神木人,工学博士研究生,E-mail:18098046259@163.com

    通讯作者:

    种小雷(1973-),男,陕西西安人,教授,博士生导师,工学博士,E-mail:kgy_cxl@163.com

  • 中图分类号: V351.11

Characteristics of aircraft runway veer-off behavior due to coupled action of crosswind and uneven water accumulation on pavement

More Information
    Corresponding author: CHONG Xiao-lei, professor, PhD, E-mail: kgy_cxl@163.com
Article Text (Baidu Translation)
  • 摘要: 建立了侧风与道面非均匀积水耦合动力学模型,分析了侧风气动力矩、积水不平衡阻力矩与前轮纠偏力矩之间的作用关系;构建了基于欧拉-拉格朗日耦合算法与机械系统动力学自动分析的联合仿真体系,实现了从局部轮组滑水作用力识别到整机滑跑偏出响应模拟的跨尺度传递;研究了积水厚度差异、侧风速度及侧风方向对飞机质心轨迹、侧向偏移量和机身偏转角的影响规律,提出了以18.7 m质心侧向偏移量作为A320飞机在45 m宽跑道上发生偏出跑道的安全判据。研究结果表明:在240 km·h-1速度接地时,10 mm的积水厚度差可造成16 kN的摩阻力差异;6 mm积水厚度差可造成11.6 m最终侧向偏移;道面湿滑放大了侧风的偏出效应,相同侧风条件下湿滑跑道飞机最大偏转角约为干跑道的2.8倍;在侧风与非均匀积水共同作用下,飞机侧向偏移显著增加,并可能在滑跑过程中突破跑道安全限值;非均匀积水通过左右主起落架纵向阻力差诱发偏转力矩,是飞机偏出跑道的重要内在驱动力;侧风主要通过气动侧向力和偏航力矩改变飞机横向运动状态,并在湿滑道面条件下进一步放大偏出效应;当积水力矩与侧风力矩方向相同时,飞机偏转姿态显著增大,当二者作用力方向同向叠加时,飞机轨迹偏离速率明显提高。研究结果可为跑道积水监测、侧风运行限制及着陆滑跑偏出风险评估提供理论依据和数据支撑。

     

  • 图  1  耦合动力学理论模型

    Figure  1.  Coupled dynamics theoretical model

    图  2  A320轮组滑水仿真模型

    Figure  2.  A320 wheel set hydroplaning simulation model

    图  3  A320飞机着陆滑跑多体动力学模型

    Figure  3.  Multi-body dynamics model for landing roll of A320 aircraft

    图  4  仿真模型验证结果

    Figure  4.  Simulation model validation results

    图  5  A组工况仿真结果

    Figure  5.  Simulation results for operating condition A

    图  6  Fv变化曲线

    Figure  6.  Variation curves of F with v

    图  7  B组工况仿真结果

    Figure  7.  Simulation results for operating condition B

    图  8  C组工况仿真结果

    Figure  8.  Simulation results for operating condition C

    表  1  轮组滑水仿真模型参数

    Table  1.   Wheel set hydroplaning simulation model parameters

    类别 指标参数 数值 类别 指标参数 数值
    轮胎规格 轮胎外径/mm 1 168 轮毂参数 轮毂密度/(kg‧m-3 7 800
    轮胎内径/mm 508 弹性模量/MPa 2×104
    轮胎宽度/mm 432 流体参数 流体初始密度/(kg‧m-3 1 000
    轮胎胎压/kPa 1 140 动力黏度/(mPa‧s) 1.0×103
    轮胎轴载/kN 153.2 积水范围/m3 1.5×1.5×(0.3+h),h为积水深度
    沟槽深度/mm 17 道面材料 密度/(kg‧m-3 7 850
    沟槽数量 4 弹性模量/MPa 3.5×104
    沟槽宽度/mm 20 泊松比 0.15
    下载: 导出CSV

    表  2  ADAMS仿真参数

    Table  2.   ADAMS simulation parameters

    参数 数值 参数 数值
    机长/m 37.57 垂直刚度/(kN·m-1 2 400
    翼展/m 35.80 垂直阻尼/(N·s·m-1 28
    主起落架横向间距/m 7.59 纵向滑移刚度/(N·m-1 2 000
    机身底部距地面/m 1.72 机翼面积/m2 122.4
    主起落架分配系数 0.95 侧风风速/(m·s-1 0~17
    单侧轮组积水厚度/mm 3~13 受风面面积/m2 31
    积水厚度差/mm 0~10 侧风合力/kN 0~17.67
    等效扭转刚度/(N·m·rad-1 3.5×105 旋转阻尼系数/(N·m·s·rad-1 800
    下载: 导出CSV

    表  3  仿真工况

    Table  3.   Simulated operating conditions

    工况组别 编号 左侧积水深度/mm 右侧积水深度/mm 积水厚度差异Δh/mm 侧风速度vw/(m·s-1
    A组:积水影响 A1 5 3 2 0
    A2 9 3 6 0
    A3 13 3 10 0
    B组:侧风影响 B1 0 0 0 -5
    B2 3 3 0 -5
    B3 0 0 0 -10
    C组:耦合影响 C1 9 3 6 -5
    C2 9 3 6 5
    C3 13 3 10 10
    下载: 导出CSV
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  • 收稿日期:  2025-12-23
  • 录用日期:  2026-05-27
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