Effect of the impact load on the main welding outer cylinder of large aircraft landing gear

被引:0
|
作者
Wang, H.F. [1 ,2 ]
Song, W.W. [1 ]
Wang, J.L. [1 ]
Zuo, D.W. [2 ]
Duan, X.L. [1 ]
机构
[1] School of Mechanical Electronic and Information Engineering, Huangshan University, Huangshan 245041, China
[2] College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
关键词
Loads (forces) - Finite element method - Cylinders (shapes) - Cracks - Welding;
D O I
10.4028/www.scientific.net/KEM.567.169
中图分类号
学科分类号
摘要
引用
收藏
页码:169 / 173
相关论文
共 50 条
  • [31] Analysis of the Dynamic and Static Load of Light Sport Aircraft Composites Landing Gear
    Chen, Pu-Woei
    Chang, Shu-Han
    Yu, Tsung-Hsign
    NEW MATERIALS AND PROCESSES, PTS 1-3, 2012, 476-478 : 406 - +
  • [32] Aircraft landing gear load prediction based on LSTM-KAN network
    Feng, Kaiyuan
    Wang, Du
    Dong, Mingli
    Lou, Xiaoping
    Zhang, Yiqun
    Deng, Chaofan
    Zhu, Lianqing
    OPTICAL FIBER TECHNOLOGY, 2025, 90
  • [33] Experimental study on the effect of landing gear fairing on amphibious aircraft
    Jiang, Rong
    Wu, Bin
    Zhang, Ke
    Li, ChengHua
    2018 IEEE 8TH INTERNATIONAL CONFERENCE ON UNDERWATER SYSTEM TECHNOLOGY: THEORY AND APPLICATIONS (USYS), 2018,
  • [34] New method of attenuating landing impact force on carrier-based aircraft landing gear
    Faculty 102, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    Hangkong Xuebao, 2007, 2 (324-327):
  • [35] Numerical continuation analysis of a three-dimensional aircraft main landing gear mechanism
    Knowles, J. A. C.
    Krauskopf, B.
    Lowenberg, M.
    NONLINEAR DYNAMICS, 2013, 71 (1-2) : 331 - 352
  • [36] Fatigue analysis of a P180 aircraft main landing gear wheel flange
    Bagnoli, F.
    Bernabei, M.
    ENGINEERING FAILURE ANALYSIS, 2008, 15 (06) : 654 - 665
  • [37] Numerical continuation analysis of a three-dimensional aircraft main landing gear mechanism
    J. A. C. Knowles
    B. Krauskopf
    M. Lowenberg
    Nonlinear Dynamics, 2013, 71 : 331 - 352
  • [38] Selection Methodology of Composite Material for Retractable Main Landing Gear Strut of a Lightweight Aircraft
    Ahmad, Muhammad Ayaz
    Rafiq, Hamza
    Shah, Syed Irtiza Ali
    Khan, Sabih Ahmad
    Rizvi, Syed Tauqeer ul Islam
    Shams, Taimur Ali
    APPLIED SCIENCES-BASEL, 2022, 12 (11):
  • [39] Leakage fault diagnosis method of aircraft landing gear hydraulic cylinder based on wavelet packet
    Tang, Jie
    Liu, Qiang
    Hu, Jianwei
    Huo, Jinjian
    Wang, Liwen
    JOURNAL OF ENGINEERING-JOE, 2019, (13): : 427 - 431
  • [40] A method for determining the horizontal impact load based on the rotational speed of the aircraft's wheel in a landing gear drop test
    Wang, Huaitao
    Wu, Dafang
    Wang, Feng
    Ren, Haoyuan
    INTERNATIONAL JOURNAL OF CRASHWORTHINESS, 2018, 23 (06) : 627 - 634