航空科学技术2024，Vol.35Issue(11)：1-12,12.DOI:10.19452/j.issn1007-5453.2024.11.001
基于不平整跑道的飞机滑跑动力学模型研究综述
Review of Dynamic Model of Aircraft Taxing on Uneven Runways
摘要
Abstract
The random vibration caused by the unevenness of the runway will not only affect the comfort of passengers during the landing,but also cause the damage of the landing gear structure and bring safety risks.Therefore,it is of great theoretical value and practical significance to study the dynamic behavior of the aircraft running system on the uneven runway.Based on the structural characteristics of the dynamic model of the aircraft skid system,this paper focuses on the development of the nonlinear aircraft skid system from the two-mass model,the multi-degree of freedom model to the multi-body model.Considering the influence of the uneven runway on the system,the description method of the uneven runway is sorted out in detail.Then,in order to obtain reasonable external load,the influence of the uneven runway on the aircraft skid system is analyzed from the power spectrum method in the frequency domain and the harmonic superposition method in the time domain.Finally,based on the development of aircraft skid system and the problems faced in the process of skid,the future research direction of complex structure and environment on aircraft skid dynamics modeling and analysis is summarized.关键词
飞机滑跑/起落架/随机动力学/随机振动/功率谱密度Key words
aircraft taxiing/landing gear/stochastic dynamics/random vibration/power spectral density分类
航空航天引用本文复制引用
张莹,秦若冰,金峥嵘,刘冲冲,石学成,贾万涛..基于不平整跑道的飞机滑跑动力学模型研究综述[J].航空科学技术,2024,35(11):1-12,12.基金项目
国家自然科学基金(12172286,11872306) （12172286,11872306）
航空科学基金(201941053004) National Natural Science Foundation of China(12172286,11872306) （201941053004）
Aeronautical Science Foundation of China(201941053004) （201941053004）
