首页|波箔型空气箔片轴承疲劳寿命的计算方法

波箔型空气箔片轴承疲劳寿命的计算方法

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以波箔型空气箔片轴承为例,构建了波箔变形的力学模型,并结合可压缩气体雷诺方程,建立求解气膜压力的流固耦合算法.在此基础上对顶箔和波箔进行应力分析,运用线性疲劳损伤累计理论构建了顶箔和波箔的疲劳寿命计算方法,结合具体算例进行数值研究.结果表明:轴承正常运转时,波箔的疲劳损伤率远大于顶箔的疲劳损伤率;在忽略启停阶段对顶箔摩擦磨损的前提下,轴承的疲劳寿命主要由波箔决定;波箔的疲劳寿命随波拱圆弧角度、波拱圆弧半径和波距的增大而减小,随半径间隙和波箔厚度的增大而增大.
Calculation Method for Fatigue Life of Wave Foil Type Air Foil Bearings
Taking wave foil type air foil bearings as examples,a mechanical model of wave foil deformation is built,and a fluid-solid coupling algorithm for solving gas film pressure is established by combining Reynolds equation of compressible gas.On this basis,the stress analysis of top foil and wave foil is carried out,and the calculation method for fatigue life of top foil and wave foil is established by using linear fatigue damage accumulation theory.The numerical study is carried out with specific examples.The results show that the fatigue damage rate of wave foil is much higher than that of top foil when the bearings are operated normally;the fatigue life of the bearings is mainly determined by wave foil under the premise of ignoring friction and wear of top foil during start and stop stage;the fatigue life of wave foil decreases with the increase of arc angle of wave arch,arc radius of wave arch and wave distance,and increases with the increase of radius gap and thickness of wave foil.

plain bearingfoil bearingmechanical modelnumerical calculationfatigue lifemaximum stress

宁培栋、李双敏、安琦

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华东理工大学 机械与动力工程学院,上海 200237

滑动轴承 箔片轴承 力学模型 数值计算 疲劳寿命 最大应力

2025

轴承
洛阳轴承研究所

轴承

北大核心
影响因子:0.336
ISSN:1000-3762
年,卷(期):2025.(1)