Evaluation of the Aircraft Landing Gear Crashworthiness by Crash Drop Test

2020 ◽  
Vol 44 (5) ◽  
pp. 377-382
Author(s):  
Tae-Uk Kim ◽  
Seunggyu Lee ◽  
Donggeon Lee ◽  
JeongJun Jo ◽  
SeokNam Shin
Keyword(s):  
Landing Gear ◽  
Drop Test ◽  
Aircraft Landing ◽  
Aircraft Landing Gear

scholarly journals Experimental Research on Aircraft Landing Gear Drop Test Based on MRF Damper

2011 ◽  
Vol 15 ◽  
pp. 4712-4717 ◽  
Author(s):  
Zhu Shixing ◽  
Wang Peng ◽  
Tian Jing
Keyword(s):  
Experimental Research ◽  
Landing Gear ◽  
Drop Test ◽  
Aircraft Landing ◽  
Aircraft Landing Gear

Optimization of the cushion properties of amphibious aircraft landing gear by simulation and drop test

2012 ◽  
Vol 19 (11) ◽  
pp. 1753-1760 ◽  
Author(s):  
Caijun Xue ◽  
Yue Wang ◽  
Bin Sun ◽  
Fenjin Xu
Keyword(s):  
Landing Gear ◽  
Drop Test ◽  
Aircraft Landing ◽  
Aircraft Landing Gear

scholarly journals 1002 Aerodynamic noise reduction for aircraft landing gear

2009 ◽  
Vol 2009 (0) ◽  
pp. 321-322
Author(s):  
Kazuhide Isotani ◽  
Kenji Hayama ◽  
Akio Ochi ◽  
Toshiyuki Kumada
Keyword(s):  
Noise Reduction ◽  
Landing Gear ◽  
Aerodynamic Noise ◽  
Aircraft Landing ◽  
Aircraft Landing Gear

Nonlinear Transient Analysis of Aircraft Landing Gear Brake Whirl and Squeal

1995 ◽  
Author(s):  
Matt H. Travis
Keyword(s):  
Finite Element ◽  
Transient Analysis ◽  
Landing Gear ◽  
Friction Modeling ◽  
Explicit Integration ◽  
Aircraft Landing ◽  
Aircraft Landing Gear ◽  
Nonlinear Transient ◽  
Element Approach ◽  
Stiffness And Damping

Abstract The feasibility of computing non-linear transient finite element simulations of aircraft landing gear brake whirl and squeal is demonstrated and discussed. Methodology to conduct the high frequency brake transient analysis is developed using an explicit integration finite element approach. Results indicate the approach has the capability to simulate brake dynamic behavior in dynamometer and aircraft landing gear installations — thus enabling evaluation of modifications to braking systems that lead to more stable and robust designs. A simple multi-disk brake model is developed and described. Modeling techniques for including the dynamometer road wheel and runway in the simulations are given. Issues such as piston housing hydraulic fluid stiffness and damping effects, and parametric friction modeling are discussed.

Study on Magneto-rheological Damper Control of Aircraft Landing Gear Based on LADRC

2021 ◽  
pp. 830-840
Author(s):  
Lei Dong ◽  
Zengqiang Chen ◽  
Mingwei Sun ◽  
Qinglin Sun ◽  
ZhenPing Yu
Keyword(s):  
Landing Gear ◽  
Aircraft Landing ◽  
Aircraft Landing Gear ◽  
Damper Control ◽  
Magneto Rheological
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