Numerical investigation of toggle assembly of landing gears in aircraft: Technical note

被引：0
|
作者：
Gopalakrishnan T. [1 ]
Saravanan R. [2 ]
Karunakaran K. [1 ]
机构：
[1] Dept. Of Mech. Engg, Vels Institute of Sci, Tech. And Adv. Studies, Chennai, Tamil Nadu
[2] Dept. Of Mech. Engg, Ellenki College of Engg. And Tech, Hyderabad, TS
来源：
International Journal of Vehicle Structures and Systems | 2019年 / 11卷 / 02期
关键词：
Aircraft; Landing gear; Numerical analysis; Toggle assembly;
D O I：
10.4273/ijvss.11.2.17
中图分类号：
学科分类号：
摘要：
In aircraft design functional components are of top priority. This numerical investigation is used for evaluating the fulfilment of strength requirement of the landing gear toggle assembly. The landing gear is the structure which supports the aircraft and helps in taxiing, take-off and landing of the aircraft. Hence it is suffered by more fatigue load than the other applications. The replacement of steel to aluminium was investigated. Every part is individually analysed and its part with sub-assemblies is also investigated. © 2019. MechAero Foundation for Technical Research & Education Excellence.
引用
收藏
页码：199 / 202
页数：3
相关论文
共 50 条
  • [1] Solid modeling for landing gears of aircraft
    Shu Ju Cai Ji Yu Chu Li, 2 (188-190):
  • [2] A CRITICAL STUDY OF AIRCRAFT LANDING GEARS
    MCBREARTY, JF
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (05): : 263 - 280
  • [3] Investigation of random runway effect on landing of an aircraft with active landing gears using nonlinear mathematical model
    Sivakumar, S.
    Selvakumaran, T.
    Sanjay, B.
    JOURNAL OF VIBROENGINEERING, 2021, 23 (08) : 1785 - 1799
  • [4] Friction analysis of aircraft landing gears due to landing impact
    Baskaran, Sanjay
    Sivaprakasam, Sivakumar
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART J-JOURNAL OF ENGINEERING TRIBOLOGY, 2022, 236 (02) : 274 - 283
  • [5] Large aircraft landing gears - a brief overview
    Besch, H. -Martin
    6TH INTERNATIONAL MUNICH CHASSIS SYMPOSIUM 2015, 2015, : 685 - 715
  • [6] Shimmy vibration analysis of aircraft landing gears
    Esmailzadeh, E
    JOURNAL OF VIBRATION AND CONTROL, 1999, 5 (01) : 45 - 56
  • [7] AIRCRAFT LANDING GEARS - THE PAST, PRESENT AND FUTURE.
    Young, D.W.
    Proceedings of the Institution of Mechanical Engineers. Part D, Transport engineering, 1986, 200 (D2): : 75 - 92
  • [8] Variable stroke fatigue test for aircraft landing gears
    Chen, Chao
    Hu, Botao
    Chen, Xiangming
    Chai, Yanan
    Zhang, Chun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2025, 239 (06) : 2117 - 2128
  • [9] Dynamics and Energy Conversion of Aircraft Landing Gears at Touchdown
    Wang, W. J.
    2016 3RD INTERNATIONAL CONFERENCE ON MECHANICS AND MECHATRONICS RESEARCH (ICMMR 2016), 2016, 77
  • [10] Study on landing impact force of carrier-based aircraft landing gears
    Wei, Xiaohui
    Nie, Hong
    Zhongguo Jixie Gongcheng/China Mechanical Engineering, 2007, 18 (05): : 520 - 523
12345