南京航空航天大学学报2024,Vol.56Issue(5) :909-921.DOI:10.16356/j.1005-2615.2024.05.014

考虑间隙的起落架收放机构运动精度可靠性分析

Analysis of Motion Accuracy Reliability for Landing Gear Retracting Mechanism Considering Clearances

徐向前 王宁博 印寅 鄢雨濛 魏小辉 聂宏
南京航空航天大学学报2024,Vol.56Issue(5) :909-921.DOI:10.16356/j.1005-2615.2024.05.014

考虑间隙的起落架收放机构运动精度可靠性分析

Analysis of Motion Accuracy Reliability for Landing Gear Retracting Mechanism Considering Clearances

徐向前 1王宁博 2印寅 1鄢雨濛 1魏小辉 1聂宏1
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作者信息

  • 1. 南京航空航天大学航空航天结构力学及控制全国重点实验室,南京 210016
  • 2. 沈阳飞机设计研究所,沈阳 110035
  • 折叠

摘要

随着飞机起落架收放机构的复杂度不断提升,多关节间隙耦合对机构运动精度的影响更加显著.复杂机构的运动精度可靠性问题呈现出非线性程度高、影响参数多、样本量少的特点,研究难度极大.针对该问题,提出了一种结合理论分析、动力学联合仿真以及间隙磨损的机构运动精度可靠性分析方法.首先,建立考虑7处关节间隙的收放机构动力学模型,研究各关节间隙对机构收放精度的独立影响及耦合影响.然后,建立关节磨损量随收放次数增加的分析模型,获取间隙的变化规律,进而建立收放机构运动精度随收放次数变化的可靠性分析模型.最后,基于自适应Kriging代理模型对起落架收放机构的可靠性进行分析,给出可靠性随机构收放次数的变化规律.研究结果表明,各处结构间隙对机构收放运动精度都有不同程度的影响,机构失效概率呈现先平稳后急剧上升的趋势.所提方法为起落架复杂机构运动可靠性评估提供重要的分析手段.

Abstract

With the increasing complexity of aircraft landing gear retractable mechanism,the effect of multiple structural clearances coupling on the motion accuracy of the mechanism is more significant.The motion accuracy reliability of complex mechanism presents the characteristics of high nonlinear degree,many influencing parameters and small sample size,so it is very difficult to study.For this problem,this paper proposes a method for analyzing the motion accuracy reliability of the mechanism by combining theoretical analysis,dynamics joint simulation,and clearance wear.Firstly,a dynamic model of the retractable mechanism considering seven structural clearances is established to study the independent and coupled effects of structural clearances on the retracting accuracy.Then,the analysis model of the structural wear with the increase of retracting cycles is established to obtain the change rule of clearance,and then the reliability analysis model of retractable mechanism motion accuracy with the change of retracting cycles is established.Finally,based on the adaptive Kriging surrogate model,the reliability of the landing gear retractable mechanism is analyzed,and the variation law of reliability with retracting cycles is provided.The research results show that the structural clearances at different locations have varying degrees of impact on the motion accuracy of the mechanism,and the probability of mechanism failure shows a trend of initially stabilizing and then sharply increasing.The proposed analysis method provides an important analytical means for the motion reliability evaluation of complex landing gear mechanisms.

关键词

起落架收放机构/动力学仿真/间隙磨损/Kriging模型/运动精度可靠性

Key words

landing gear retractable mechanism/dynamic simulation/clearance wear/Kriging model/motion accuracy reliability

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基金项目

国家自然科学基金(52172368)

国家自然科学基金(52275114)

江苏省自然科学基金(BK20220135)

出版年

2024
南京航空航天大学学报
南京航空航天大学

南京航空航天大学学报

CSTPCDCSCD北大核心
影响因子:0.734
ISSN:1005-2615
参考文献量31
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