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飞机牵引滑行技术综述

孙艳坤 张威 杨雄伟 刘积昊 祝恒佳 刘衍希 秦嘉浩

孙艳坤, 张威, 杨雄伟, 刘积昊, 祝恒佳, 刘衍希, 秦嘉浩. 飞机牵引滑行技术综述[J]. 交通运输工程学报, 2023, 23(3): 23-43. doi: 10.19818/j.cnki.1671-1637.2023.03.002
引用本文: 孙艳坤, 张威, 杨雄伟, 刘积昊, 祝恒佳, 刘衍希, 秦嘉浩. 飞机牵引滑行技术综述[J]. 交通运输工程学报, 2023, 23(3): 23-43. doi: 10.19818/j.cnki.1671-1637.2023.03.002
SUN Yan-kun, ZHANG Wei, YANG Xiong-wei, LIU Ji-hao, ZHU Heng-jia, LIU Yan-xi, QIN Jia-hao. Review on aircraft towing taxi technologies[J]. Journal of Traffic and Transportation Engineering, 2023, 23(3): 23-43. doi: 10.19818/j.cnki.1671-1637.2023.03.002
Citation: SUN Yan-kun, ZHANG Wei, YANG Xiong-wei, LIU Ji-hao, ZHU Heng-jia, LIU Yan-xi, QIN Jia-hao. Review on aircraft towing taxi technologies[J]. Journal of Traffic and Transportation Engineering, 2023, 23(3): 23-43. doi: 10.19818/j.cnki.1671-1637.2023.03.002

飞机牵引滑行技术综述

doi: 10.19818/j.cnki.1671-1637.2023.03.002
基金项目: 

国家自然科学基金项目 U2033208

国家自然科学基金项目 12002367

中央高校基本科研业务费专项资金项目 3122020031

详细信息
    作者简介:

    孙艳坤(1980-),女,吉林集安人,中国民航大学副教授,工学博士,从事民航运行支持技术与装备、飞机地面牵引研究

    通讯作者:

    张威(1979-),男,湖南衡阳人,中国民航大学教授,工学博士

  • 中图分类号: V351.3

Review on aircraft towing taxi technologies

Funds: 

National Natural Science Foundation of China U2033208

National Natural Science Foundation of China 12002367

Fundamental Research Funds for the Central Universities 3122020031

More Information
  • 摘要: 从飞机牵引滑行模式的本质出发,分析了牵引滑行的内涵和驱动因素,提出了实现飞机牵引滑行模式需解决的牵引滑行过程运动学及其环境载荷分析、牵引滑行多体系统动力学、飞机前起落架结构力学响应、系统运动感知与控制、牵引滑行装备与物理测试平台以及牵引滑行模式对机场运行规则影响等关键问题,并分析了6项关键问题的研究现状和发展趋势,探讨了实现新模式所面临的技术难点与挑战。分析结果表明:牵引滑行的运动学计算相比于传统牵引的精度和实时性要求更高,要实现牵引滑行的安全估计需建立系统运动的高精度解算算法;高速重载飞机牵引滑行系统的运动状态、机场路面条件、控制输入等多因素作用将可能导致横向失稳、脱抱等极限现象,针对其系统动力学行为开展研究需考虑其结构与系统的非线性特征;为保障前起落架在长距离牵引滑行中承受纵向牵引力和垂向振动力耦合作用下的安全,需研究其结构动态响应和极限工况行为机理;要实现飞行员精确控制牵引滑行运动,需对人机交互模式、飞行员感知控制方法进行研究并开展测试验证;牵引滑行技术可缩短飞机发动机在地面运行阶段的使用时间,降低油耗和碳排放量,但同时会增加机场场面运行的复杂程度,因此,需建立新的机场飞行区场面运行管理规则体系。

     

  • 图  1  飞机离港滑行过程

    Figure  1.  Taxiing process of aircraft leaving port

    图  2  针对不同机场跑道的2种滑行方法

    Figure  2.  Two exiting methods for different airport runways

    图  3  仿真得到的飞机翼尖运动轨迹

    Figure  3.  Wing tip motion trajectories obtained by simulation

    图  4  牵引车-飞机系统模型

    Figure  4.  Tractor-aircraft system model

    图  5  飞机地面动力学相关非线性组件

    Figure  5.  Related nonlinear components in aircraft ground dynamics

    图  6  优化前后车身垂向加速度

    Figure  6.  Vertical accelerations of car body before and after optimization

    图  7  系统模型

    Figure  7.  System model

    图  8  UniTire轮胎印迹坐标系

    Figure  8.  UniTire imprint coordinate system

    图  9  典型民机起落架模型

    Figure  9.  Landing gear models of typical civil aircraft

    图  10  10 000条跑道95%置信度下不平度均值

    Figure  10.  Unevenness mean of 10 000 runways at 95% confidence

    图  11  基于语音和视觉结合的飞机牵引车智能驾驶控制系统

    Figure  11.  Intelligent driving control system of aircraft towing vehicle based on combination of voice and vision

    表  1  2019年全国民航新旧滑行模式费用对比

    Table  1.   Costs comparison of new and old taxiing modes in China's civil aviation in 2019

    费用类型 旧模式 新模式 成本节省
    地面油耗费用/亿元 40.50 4.50 36.00
    发动机工时费/亿元 15.12 0.00 15.12
    费用合计/亿元 55.62 4.50 51.12
    下载: 导出CSV
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  • 收稿日期:  2023-02-03
  • 网络出版日期:  2023-07-07
  • 刊出日期:  2023-06-25

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