Experimental equipment for study of landing gear mechanisms

被引:0
|
作者
Bogdan, Constantin
Bogdan, Mihaela Liana
Simniceanu, Loreta
Dinca, Livic
机构
关键词
equipment; landing gear; tests; kinematical parameters; mechanisms;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper is described an experimental equipment for study of landing gear mechanisms. For study of landing gear mechanisms, it is necessary that should measure some different kinematical parameters of the mechanisms from landing gear structure during the retraction and deployment. For this scope, P is drawn and made special experimental equipment. For the measurement of the kinematical parameters variations, it is used not only the mentioned equipment, but also the software for processing experimental data Test Point-Keithler.
引用
收藏
页码:99 / 100
页数:2
相关论文
共 50 条
  • [21] The landing gear case study: challenges and experiments
    Boniol, Frederic
    Wiels, Virginie
    Ait-Ameur, Yamine
    Schewe, Klaus-Dieter
    INTERNATIONAL JOURNAL ON SOFTWARE TOOLS FOR TECHNOLOGY TRANSFER, 2017, 19 (02) : 133 - 140
  • [22] The Strength Experimental Design and Data Analysis of The Nose Landing Gear
    Li, Hongjuan
    Cui, Weimin
    Zheng, Fengzhu
    Guo, Junhao
    PROCEEDINGS OF 2013 INTERNATIONAL CONFERENCE ON QUALITY, RELIABILITY, RISK, MAINTENANCE, AND SAFETY ENGINEERING (QR2MSE), VOLS I-IV, 2013, : 832 - 835
  • [23] Experimental Validation for the Performance of MR Damper Aircraft Landing Gear
    Jo, Bang-Hyun
    Jang, Dae-Sung
    Hwang, Jai-Hyuk
    Choi, Yong-Hoon
    AEROSPACE, 2021, 8 (09)
  • [24] Experimental Research on Noise Reduction for Realistic Landing Gear Geometries
    Belyaev, I. V.
    Zaytsev, M. Yu.
    Kopiev, V. F.
    Pankratov, I. V.
    ACOUSTICAL PHYSICS, 2019, 65 (03) : 297 - 306
  • [25] Experimental Research on Noise Reduction for Realistic Landing Gear Geometries
    I. V. Belyaev
    M. Yu. Zaytsev
    V. F. Kopiev
    I. V. Pankratov
    Acoustical Physics, 2019, 65 : 297 - 306
  • [26] Experimental Studies on a Rudimentary Four-Wheel Landing Gear
    Venkatakrishnan, L.
    Karthikeyan, N.
    Mejia, Kevin
    AIAA JOURNAL, 2012, 50 (11) : 2435 - 2447
  • [27] Experimental assessment of low noise landing gear component design
    Dobrzynski, Werner
    Chow, Leung Choi
    Smith, Malcolm
    Boillot, Antoine
    Dereure, Olivier
    Molin, Nicolas
    INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2010, 9 (06) : 763 - 786
  • [28] Kinematic Singularity and Bifurcation Analysis of Sidestay Landing Gear Locking Mechanisms
    Xu K.
    Yin Y.
    Yang Y.
    Nie H.
    Wei X.
    International Journal of Aerospace Engineering, 2021, 2021
  • [29] Experimental study on the aircraft landing gear noise in a large-scale aeroacoustic wind tunnel
    Zhao K.
    Liang J.
    Kopiev V.
    Belyaev I.
    Zhendong yu Chongji/Journal of Vibration and Shock, 2022, 41 (22): : 160 - 172and210
  • [30] Aircraft landing impact parametric study with emphasis on nose gear landing conditions
    Chester, DH
    JOURNAL OF AIRCRAFT, 2002, 39 (03): : 394 - 403