海军航空大学学报2025，Vol.40Issue(4)：607-615,9.DOI:10.7682/j.issn.2097-1427.2025.04.011
子午线航空轮胎静载接地力学性能仿真分析
Simulation Analysis for Mechanical Properties of Radial Aircraft Tires Under Static Load Conditions
摘要
Abstract
Aiming to study the effects of inflation pressure and vertical load on the stress distribution,grounding imprint,strain,and radial stiffness of the aircraft tire under static load conditions,a finite element model of aircraft tire of a certain type of airliner is established.The results show that,firstly,the equivalent stress is higher around the wire bead,shoulder,and tread under rated conditions.When the tire pressure is too low,the contact area increases,the shoulder bears a larger load,and the tire's wear resistance decreases.As tire pressure increases,radial stiffness rises,contact area decreases,con-tact stress intensifies,and deflection gradually reduces.Higher tire pressure can cause excessive stress on the tread,poten-tially damaging the tire.Secondly,under rated pressure,as the load increases,the tire's deflection increases,the contact imprint shifts from circular to elliptical,and the contact stress concentration moves from the tread center to the shoulders.When the load reaches 150 kN,excessive stress on the shoulders may lead to tire fatigue damage and premature failure.关键词
航空轮胎/有限元分析/力学性能/径向刚度/接地印迹Key words
aircraft tire/finite element analysis/mechanical properties/radial stiffness/tire footprint分类
航空航天引用本文复制引用
胡月,孙文博,王新凯,谭德强,贺强,王晓建..子午线航空轮胎静载接地力学性能仿真分析[J].海军航空大学学报,2025,40(4):607-615,9.基金项目
国家自然科学基金(52205239、52105132、52403031) （52205239、52105132、52403031）
四川省科技计划(2025YFHZ0309) （2025YFHZ0309）
吉林省科技计划(20240602125RC) （20240602125RC）
中央高校基本科研业务费基金(24CAFUC04005、24CAFUC04006) （24CAFUC04005、24CAFUC04006）
四川省通用航空器维修工程技术研究中心资助课题(GAMRC2023ZD04) （GAMRC2023ZD04）
