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多叶式径向动压气体箔片轴承预紧力仿真

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为获取多叶式径向动压气体箔片轴承大预紧装配过程中各部件状态,基于显式动力学方法建立了该类轴承的非线性接触模型,并讨论了预紧量、静态偏心率对转轴表面应力分布的影响,研究结果表明:多叶式箔片结构在平箔片搭接区域及与转轴接触区域应力较大;当无静态偏心时,转轴表面应力分布呈周期对称状态,有静态偏心时,则呈余弦形式,且应力波峰波谷数量与箔片数量一致;同时,预紧量越大,转轴表面应力越大,而静态偏心率越大,转轴表面主要受压区峰谷间应力差越大.
Preload Simulation of Aerodynamic Multi-leaf Foil Journal Bearing
In order to obtain the states of various components in the assembly process of the aerodynamic multi-leaf foil journal bearing with a large preload,a nonlinear contact model was established based on the explicit dynamic method,and the effects of the preload amount and static eccentricity on the surface stress distribution of the rotating shaft were discussed.The research results show that the stress of the multi-leaf foil structure is greater in the foil overlap area and the contact area with the rotating shaft.When there is no static eccentricity,the stress distribution on the surface of the rotating shaft is periodic symmetry,and when there is static eccentricity,it is in cosine form,and the number of stress peaks and troughs is consistent with the leaf's number.At the same time,the greater the preload,the greater the surface stress,and the greater the static eccentricity,the greater the peak-valley stress difference in the main bearing zone on the surface of the rotating shaft.

aerodynamic foil bearingpreloadnonlinear contactnumerical simulationsurface stress

黄钟文、郭雨、罗欣洋、梁波、杨昌宝、于焕春、张广辉、徐科繁、樊红星

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中国航空工业集团公司 南京机电液压工程研究中心航空机电系统综合航空科技重点实验室,江苏 南京 211106

哈尔滨工业大学 能源科学与工程学院,黑龙江 哈尔滨 150001

空军装备部驻南京地区第三军事代表室,江苏 南京 211106

动压气体箔片轴承 预紧力 非线性接触 数值仿真 表面应力

2024

节能技术
国防科技工业节能技术服务中心

节能技术

CSTPCD
影响因子:0.601
ISSN:1002-6339
年,卷(期):2024.42(1)
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