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多因素影响下的起落架收放系统性能分析

印寅 聂宏 魏小辉 倪华近

印寅, 聂宏, 魏小辉, 等 . 多因素影响下的起落架收放系统性能分析[J]. 北京航空航天大学学报, 2015, 41(5): 953-960. doi: 10.13700/j.bh.1001-5965.2014.0380
引用本文: 印寅, 聂宏, 魏小辉, 等 . 多因素影响下的起落架收放系统性能分析[J]. 北京航空航天大学学报, 2015, 41(5): 953-960. doi: 10.13700/j.bh.1001-5965.2014.0380
YIN Yin, NIE Hong, WEI Xiaohui, et al. Retraction system performance analysis of landing gear with the influence of multiple factors[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 953-960. doi: 10.13700/j.bh.1001-5965.2014.0380(in Chinese)
Citation: YIN Yin, NIE Hong, WEI Xiaohui, et al. Retraction system performance analysis of landing gear with the influence of multiple factors[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(5): 953-960. doi: 10.13700/j.bh.1001-5965.2014.0380(in Chinese)

多因素影响下的起落架收放系统性能分析

doi: 10.13700/j.bh.1001-5965.2014.0380
基金项目: 国家自然科学基金(51105197,51075203);江苏高校优势学科建设工程
详细信息
    作者简介:

    印寅(1986—),男,江苏泰州人,博士研究生,yinyinjordan@163.com

    通讯作者:

    聂宏(1960—),男,安徽宣城人,教授,hnie@nuaa.edu.cn,主要研究方向为飞行器起落装置设计.

  • 中图分类号: V226

Retraction system performance analysis of landing gear with the influence of multiple factors

  • 摘要: 起落架收放系统是集机、电、液的混合复杂系统,影响收放性能的因素也呈多样性.针对目前大多研究并未较好地将收放各部分系统综合考虑的研究现状,提出了一套结合理论分析、多学科仿真技术及试验验证的分析方法,为起落架收放系统提供了较准确的分析手段.首先采用功率键合图法详细地推导了起落架收放系统动力学方程;在理论模型的基础上,建立了结合起落架动力学和液压系统的多学科协同仿真模型,并用试验结果对虚拟样机模型进行验证;最后详细讨论了混合系统中各关键参数对起落架收放性能的影响.研究结果表明,联合仿真模型的压力曲线与试验实测数据吻合良好,同时侧风、摩擦阻力、阻尼孔、液弹、油液泄漏等关键参数对收放性能都有不同程度的影响,分析结果可用于指导起落架收放参数设计、收放故障分析及可靠性研究.

     

  • [1] Currey N S. Aircraft landing gear design:principle and practice[M].Reston:American Institute of Aeronautics and Astronautics Inc,1988:62-64.
    [2] Veaux J. New design procedures applied to landing gear development[J].Journal of Aircraft,1986,25(10):904-910.
    [3] Freund D,McKissack D.Business jet crash landing analysis[C]//42nd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamic,and Materials Conference and Exhibit.Reston:AIAA,2001,2:1472-1482.
    [4] 葛漫江. TB20飞机起落架收放液压系统故障分析[J].航空维修与工程,2003(4):58-59. Ge M J.Analyse trouble of TB20 landing gear hydraulic system[J].Aviation Maintenance & Engineering,2003(4):58-59(in Chinese).
    [5] 王旭东. B737-300型飞机主起落架收放系统故障分析[J].中国民航学院学报,2004,22(6):28-29. Wang X D.Fault analysis of the B737-300 main landing gear retraction system[J].Journal of Civil Aviation University of China,2004,22(6):28-29(in Chinese).
    [6] 任可,苟江,任毅.西门诺尔飞机起落架液压收放系统故障分析[J].航空维修与工程,2010(3):40-42. Ren K,Gou J,Ren Y.Hydraulic retraction defaults of Seminole aircraft landing gear system[J].Aviation Maintenance & Engineering,2010(3):40-42(in Chinese).
    [7] 唐有才,刘振岗,王占勇,等.飞机液压系统故障多的原因探讨及对策[J].液压与气动,2009(10):84-87. Tang Y C,Liu Z G,Wang Z Y,et al.The analysis & countermeasure of the reason for military aircraft hydraulic system fault[J].Chinese Hydraulics & Pneumatics.2009(10):84-87(in Chinese).
    [8] 王慧,喻天翔,雷鸣敏,等.运动机构可靠性仿真试验系统体系结构研究[J].机械工程学报,2011,47(22):191-198. Wang H,Yu T X,Lei M M,et al.Research on the architecture of simulative experiment system for mechanism motion reliability analysis[J]. Journal of Mechanical Engineering,2011,47(22):191-198(in Chinese).
    [9] Noel O. Use of ADAMS in dynamic simulation of landing gear retraction and extension[C]//13th European ADAMS Users's Conference.[S.l.]:Messier-Dowty,1998:1-8.
    [10] Zhang H,Ning J,Schmelzer O.Integrated landing gear system retraction/extension analysis using ADAMS[C]//International ADAMS User Conference.[S.l.]:Messier-Dowty Incorporation,1995:1-10.
    [11] 黄方略,李书,王远达.民机起落架三维收放机构的收放机械效率分析[J].振动、测试与诊断,2013,33(1):187-191. Huang F L,Li S,Wang Y D.Efficiency analysis of a civil airplane three-dimensional retraction mechanism[J].Journal of Vibration,Measure & Diagnosis,2013,33(1):187-191(in Chinese).
    [12] 吴亚峰,郭军. 基于AMESim的飞机液压系统仿真技术的应用研究[J].沈阳工业大学学报,2007,29(4):368-371. Wu Y F,Guo J.Research on simulation technique based on AMESim for aircraft hydraulic system[J].Journal of Shenyang University of Technology,2007,29(4):368-371(in Chinese).
    [13] Ji G M,Zhang L,Dong M.Dynamic simulation on retraction/extension system of an aircraft[C]//2nd International Conference of Artificial Intelligence,Management Science and Electronic Commerce.Piscataway,NJ:IEEE Press,2011:3939-3944.
    [14] 吉国明,董萌,付珍娟.某型飞机起落架收放机构性能仿真[J].火力与指挥控制,2012,37(3):169-173. Ji G M,Dong M,Fu Z J.Performance simulation of retraction/extension mechanism of a certain aircraft[J].Fire Control & Command Control,2012,37(3):169-173(in Chinese).
    [15] 朱武峰,李旭东,丁文勇,等.飞机起落架收放液压系统仿真分析与维修应用[J].液压与气动,2013(6):87-90. Zhu W F,Li X D.Ding W Y,et al.Simulation and maintenance of aircraft landing gear hydraulic system[J].Chinese Hydraulics & Pneumatics,2013(6):87-90(in Chinese).

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出版历程
  • 收稿日期:  2014-06-24
  • 修回日期:  2014-09-05
  • 网络出版日期:  2015-05-20

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