[1]陈舒文,刘晖,李福海,等.含接触碰撞的飞机地面牵引载荷分析[J].哈尔滨工程大学学报,2017,38(11):1794-1799.[doi:10.11990/jheu.201606075]
 CHEN Shuwen,LIU Hui,LI Fuhai,et al.Research on aircraft towing load with contact-impact effects[J].hebgcdxxb,2017,38(11):1794-1799.[doi:10.11990/jheu.201606075]
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含接触碰撞的飞机地面牵引载荷分析(/HTML)
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《哈尔滨工程大学学报》[ISSN:1006-6977/CN:61-1281/TN]

卷:
38
期数:
2017年11期
页码:
1794-1799
栏目:
出版日期:
2017-11-25

文章信息/Info

Title:
Research on aircraft towing load with contact-impact effects
作者:
陈舒文1 刘晖12 李福海1 张海12
1. 南京航空航天大学 民航学院, 江苏 南京 211106;
2. 南京航空航天大学 飞行模拟与先进培训工程技术研究中心, 江苏 南京 211106
Author(s):
CHEN Shuwen1 LIU Hui12 LI Fuhai1 ZHANG Hai12
1. School of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China;
2. Institute Center of Flight Simulation and Advanced Engineering Technology Training, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
关键词:
飞机牵引系统牵引接头载荷连接间隙接触碰撞前起落架牵引杆牵引车
分类号:
V214
DOI:
10.11990/jheu.201606075
文献标志码:
A
摘要:
由于受到操作失误或作业环境的影响,飞机地面牵引过程可能会产生较大载荷,甚至危及飞机结构安全。本文采用修正的非线性等效弹簧阻尼模型来描述飞机牵引系统连接间隙,以波音某机型为参考,建立了含接触碰撞的飞机地面牵引系统的刚柔耦合动力学模型。对经过加油管地沟的飞机牵引事故作为典型案例进行分析,结果表明:牵引车与牵引杆的连接间隙对飞机的下阻力臂载荷影响较大,当连接间隙过大或下阻力臂存在疲劳裂纹时,受到较大的冲击载荷,飞机牵引杆及前起落架可能发生损伤。

参考文献/References:

[1] 中国民航不安全事件统计分析报告(2011)[R].北京:中国民航科学技术研究院, 2011.
[2] Civil Aviation Authority of Macao, China. Accident investigation report, Aircraft accident no.Accid01/06[R]. 2008.
[3] 张宏. 民用飞机地面支援设备研制规范体系的研究[J].民用飞机设计与研究, 2010(1):61-62.ZHANG Hong. Research on the specification system of civil aircraft ground support equipment development[J]. Civil aircraft design and research, 2010(1):61-62.
[4] 曹大树,姚红宇,薛彩军,等.某型飞机前起落架断裂损伤分析[J].材料工程, 2008(6):36-39.CAO Dashu, YAO Hongyu, XUE Caijun, et al. Fracture damage analysis of a nose landing gear[J]. Journal of materials engineering, 2008(6):36-39.
[5] 闫岷,赵立军,姜继海.飞机牵引车结构及动力传动系统的发展[J].液压与气动, 2009(12):1-4.YAN Min, ZHAO Lijun, JIANG Jihai. Development of structure and power transmission system in aircraft towing tract[J]. Chinese hydraulics & pneumatics,2009,12:1-4.
[6] 田普跃,于英.飞机牵引车制动特性的分析与计算[J].车辆与动力技术, 2002(2):34-38.TIAN Jinyue, YU Ying. Analysis and calculation of braking performance on airplane towing tractor[J]. Vehicle & power technology,2002(2):34-38.
[7] 包继华,孙承顺,张建武,等. 某牵引车多体系统动力学建模与仿真[J].上海交通大学学报, 2003, 37(11):1767-1771.BAO Jihua, SUN Chengshun, ZHANG Jianwu, et al. Dynamic modeling and simulation for a towing tractor based on the multi-body theory[J]. Journal of Shanghai Jiao Tong University, 2003, 37(11):1767-1771.
[8] 苑绍志,李幼德,李静. 基于多领域协同车辆建模仿真平台的牵引力控制系统研究[J].中国机械工程, 2007,18(12):1487-1490.YUAN Shaozhi, LI Youde, LI Jing. Study on TCS based on vehicle collaborative modeling & simulation platform[J]. China mechanical engineering, 2007, 18(12):1487-1490.
[9] INFANTE V, REIS L, FREITAS M D. Failure analysis of landing gears trunnions due to service[J]. Engineering failure analysis, 2014, 41(3):118-123.
[10] ASI O, ÖNDER Y. Failure analysis of an aircraft nose landing gear piston rod end[J]. Engineering failure analysis, 2013, 32(3):283-291.
[11] FLORES P, AMBROSIO J. Revolute joints with clearance in multibody systems[J]. Computers & structures, 2004, 3:1359-1369.
[12] KHULIEF Y A. Modeling of impact in multibody systems:an overview[J]. Journal of computational and nonlinear dynamics, 2013(8):021012-1-15.
[13] FLORES P, SIO J, CLARO J, et al. Influence of the contact-impact force model on the dynamic response of multi-body systems[J]. Proceedings of the institution of mechanical engineers Part K:journal of multi-body dynamics, 2006, 220(1):21-34.
[14] 秦志英,陆启韶. 基于恢复系数的碰撞过程分析[J].动力学和控制学报,2006,12(4):294-298.QIN Zhiying, LU Qishao. Analysis of impact process model based on restitution coefficient[J]. Journal of dynamics and control, 2006, 12(4):294-298.
[15] HUNT K H, CROSSLEY F R E. Coefficient of Restitution Interpreted as Damping in Vibroimpact[J]. Journal of Applied Mechanics, 1975, 42(2):440-445.
[16] LANKARANI H M, NIKRAVESH P E. A contact force model with hysteresis damping for impact analysis of multi-body systems[J]. J Mech Des, 1990, 112:369-376.
[17] QIN Zhiying, LU Qishao, Analysis of impact process model based on restitution coefficient[J]. Journal of dynamics and control, 2006, 12(4):294-298.
[18] YOSHIYWKI T. 提高超高强度4340钢低温断裂韧性的热处理技术[J]. 兵器材料科学与工程, 1988(11):70-74.YOSHIYWKI T. Improve the heat treatment technology of high strength steel 4340 fracture toughness at low temperature[J]. Ordnance material science and engineering, 1988(11):70-74.
[19] 刘文礼. 反坦克火箭弹用4140超高强度钢的研究[J]. 兵器材料科学与工程, 1986(4):11-17.LIU Wenli. Research of anti-tank rockets with high strength steel 4140[J]. Ordnance material science and engineering, 1986(4):11-17.

备注/Memo

备注/Memo:
收稿日期:2016-06-24。
基金项目:国家自然科学基金项目(U1233104).
作者简介:陈舒文(1990-),女,博士研究生;刘晖(1970-),男,副教授.
通讯作者:陈舒文,E-mail:csw_nuaa@126.com.
更新日期/Last Update: 2017-11-30