中国航空学报(英文版)2024,Vol.37Issue(2) :343-359.DOI:10.1016/j.cja.2023.12.011

Gear walk instability caused by brake-disc friction characteristics

Xiaoqiong DU Bin LI Wen CAI Linyin LUO
中国航空学报(英文版)2024,Vol.37Issue(2) :343-359.DOI:10.1016/j.cja.2023.12.011

Gear walk instability caused by brake-disc friction characteristics

Xiaoqiong DU 1Bin LI 1Wen CAI 2Linyin LUO3
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作者信息

  • 1. School of Aeronautics,Northwestern Polvtechnical University,Xi'an 710072,China
  • 2. Department of Mechanical Engineering,University of Michigan,Ann Arbor 48109,USA
  • 3. AVIC General Huanan Aircraft Industry Co.Ltd.,Zhuhai 519040,China
  • 折叠

Abstract

A multi-body dynamic rigid-flexible coupling model of landing gear is established to study the gear walk instability caused by the friction characteristics of the brake disc.After validat-ing the model with the experimental results,the influence of the landing gear structure and braking system parameters on gear walk is further investigated.Among the above factors,the slope of the graph for the friction coefficient of the brake disc and the relative velocity of brake stators and rotors is the most influential factor on gear walk instability.Phase trajectory analysis verifies that gear walk occurs when the coupling of multiple factors causes the system to exhibit an equivalent negative damping trend.To consider a more realistic braking case,a back propagation neural net-work method is employed to describe the nonlinear behavior of the friction coefficient of the brake disc.With the realistic nonlinear model of the friction coefficient,the maximum error in predicting the braking torque is less than 10%and the effect of the brake disc temperature on gear walk is performed.The results reveal that a more negative friction slope may contribute to a more severe unstable gear walk,and reducing the braking pressure is an effective approach to avoid gear walk,which provides help for future braking system design.

Key words

Gear walk/Friction characteristics of brake disc/Brake-induced vibration/Negative damping/Rigid-flexible coupling/Negative slope of braking torque

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基金项目

National Natural Science Foundation of China(11872312)

Program of Introducing Talents of Discipline to Universities,China(BP0719007)

Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University,China(CX2022002)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
被引量1
参考文献量2
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