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作 者:吴垚[1,3] 郗文君 张彩丽[1] 曹巨江[1] 杨利花[3] WU Yao;XI Wenjun;ZHANG Caili;CAO Jujiang;YANG Lihua(College of Mechanical and Electrical Engineering,Shaanxi University of Science and Technology,Xi'an 710021,China;Energy Management Low Voltage Division,Schneider(Xi'an)Innovation Technology Company,Limited,Xi'an 710075,China;School of Aerospace Engineering,Xi'an Jiaotong University,Xi'an 710049,China)
机构地区:[1]陕西科技大学机电工程学院,西安710021 [2]施耐德(西安)创新技术有限公司低压事业部,西安710075 [3]西安交通大学航天航空学院,西安710049
出 处:《航空动力学报》2022年第9期1979-1991,共13页Journal of Aerospace Power
基 金:国家科技重大专项资助项目(J2019-Ⅳ-0021-0089);国家自然科学基金面上项目(11872288);陕西省自然科学基础研究计划资助项目(2022JQ-002);陕西科技大学引进人才博士启动基金项目(2021BJ-11)。
摘 要:基于能量守恒原理推导计入气体稀薄效应的修正能量方程及其有限差分表达式,并通过偏导数法和有限差分法联立求解修正Reynolds方程、修正能量方程、气体黏温关系和气膜厚度方程,详细研究了微型气体轴承静动态性能随结构参数、轴颈倾斜方位角和黏温热效应的变化规律。结果表明:气膜热效应提高了微型气体轴承的承载能力、摩擦因数和动态刚度系数,而降低了直接阻尼系数,轴颈倾斜误差对微型气体轴承的静、动态性能均产生不利影响,计算结果可为提高微型气体动压轴承-转子系统的稳定性提供重要理论依据。Due to the ultra-thin gas film of microbearing and various loads caused by the high-speed rotation of micro rotor,the effects of gas rarefaction,viscosity-temperature relation and journal misalignment on the lubrication characteristics of micro gas bearing cannot be neglected.The modified energy equation and its finite difference expression considering rarefaction effect were derived based on the energy conversation,and the modified Reynolds equation,modified energy equation,gas viscosity-temperature relationship and film thickness equation were solved simultaneously by partial derivative method and finite difference method.The influences of structural parameters,misalignment angle and thermal effect on static and dynamic performance of microbearings were investigated in detail.Results showed that the load capacity,friction coefficient and dynamic stiffness coefficient of gas microbearing were improved by the gas film temperature,while the direct damping coefficient was reduced.The journal misalignment had an adverse influence on the static and dynamic performance of microbearing.Therefore,the results can provide an important theoretical basis for improving the stability of gas microbearing-rotor system in microfluidic devices.
关 键 词:微型气体轴承 轴颈倾斜 稀薄效应 修正能量方程 热流体动力润滑
分 类 号:V229.2[航空宇航科学与技术—飞行器设计] TH133.312[机械工程—机械制造及自动化]
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