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1.
考虑滚道表面油层分布的滚动轴承润滑分析 总被引:3,自引:0,他引:3
研究表明供油量对弹流润滑性能产生显著影响.滚动轴承中由于离心力和滚动体的反复滚压,滚道表面上的润滑剂呈现出非均匀分布的特点.大多数润滑剂被推挤到滚道的两侧,致使接触区的入口间隙不能被完全充满,导致乏油润滑,滚动体与滚道间接触压力接近于赫兹压力分布,膜厚较全膜润滑有明显的减小.本文基于润滑剂的流量连续建立滚道表面油层厚度分布模型,考虑润滑接触压力的影响,计算滚道上的侧流量以预测轴承滚道上补给油层厚度及形状随时间的变化规律;进而以此作为滚动体和滚道接触区的入口油层厚度,采用统一Reynolds方程法数值模拟计算每个时刻轴承滚道与滚动体之间的润滑油膜厚度,压力分布等参数,分析轴承在点接触乏油条件下运行的润滑性能. 相似文献
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线接触弹性流体动力润滑的供油条件分析 总被引:7,自引:4,他引:7
以油膜起始位置为参数,求出了等温线接触弹性流体动力润滑问题的完全数值解.通过流量分析,建立了有效供油膜厚与油膜起始位置之间的关系.结果表明,弹性流体动力润滑的供油方式可划分为过量供油、适量供油和乏油3种类型.在过量供油条件下大部分润滑油不能进入接触区,因而并不能改善润滑状态.在适量供油条件下所有润滑油均可通过接触区并能够获得最大的油膜厚度.在乏油条件下所有的润滑油也均可以通过接触区,而油膜厚度则完全由供油量确定.同时,数值结果也指出,只要运动表面存有数量级为1 μm厚的一层油液就足以满足适量供油条件而得到最佳的润滑效果. 相似文献
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椭圆接触弹性流体动力润滑的供油条件分析 总被引:4,自引:1,他引:4
通过数值求解研究了椭圆接触弹流润滑的供油条件,分析了供油油膜厚度对乏油润滑中心膜厚和最小膜厚的影响,以及中心膜厚和最小膜厚与润滑油膜压力区形成位置的关系.结果表明:当供油油膜厚度较小时,中心膜厚和最小膜厚很小,压力区形成位置距Hertz接触区很近,处于严重乏油状态;当供油油膜的厚度达到一定数值时,中心膜厚和最小膜厚基本不变,多余的润滑油几乎不能进入接触间隙,即达到准充分供油状态;当供油油膜厚度继续增加时,乏油区最终消失,达到充分供油或过量供油状态. 相似文献
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采用球-环接触和球-盘接触形式的光干涉润滑油膜测量仪,在定量供油条件下观察两种接触形式下的不同润滑特性,分析了润滑差异性的内在机制.结果显示:在低速条件下球-盘接触膜厚始终高于球-环接触膜厚,由接触几何特性差异导致的不同动压效应、侧泄效应和润滑剂流动是其主要原因;在高速条件下球-盘接触形式易出现入口乏油,而球-环接触在整个测试速度范围内未出现乏油,不同的离心力作用方向是导致这种差异的诱因.试验还观察与分析了黏度对两种接触方式下润滑特性的影响:低速条件下,高黏度润滑剂易导致球-环接触出现乏油;高速条件下,高黏度润滑剂能够推迟球-盘接触时乏油状态的出现. 相似文献
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润滑油在轴承内的分布及其变化规律对轴承的润滑性能有显著影响. 在本文中搭建了滚动轴承模拟试验台,基于激光诱导荧光方法实现了滚动轴承内钢球-外圈接触区附近润滑油分布的观察与测量,获得了润滑油供给油层分布的三维形貌图,研究了不同供油量和转速对轴承内部供给油层分布的影响规律. 试验结果表明充分润滑条件下相邻钢球-外圈接触区供给油池之间会形成相互连接的油带;在高速情况下,钢球-外圈接触区供给油层厚度受前一个接触区尾部空穴影响而减小;供油量的增加会增大表观油池,但并不意味着入口有效供油层的增加. 相似文献
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基于荧光技术,研究了固体表面润湿性对滑块-盘面接触供油的影响. 试验中以静止滑块和旋转玻璃盘构成摩擦副,润滑油围绕该面接触区构成一个供油油池. 结果表明:充分供油条件下,滑块表面的润湿性影响油池润滑剂的分布,但仍能保证接触区润滑剂的充分供给. 限量供油条件下,接触区外滑块表面润湿性影响了油池分布以及入口润滑剂的供给,低润湿性加剧接触区乏油程度,直接导致膜厚的降低. 润滑剂的高表面张力及在盘表面的低粘附都会改善润滑剂在润滑轨道上的回流;润滑剂在盘表面的反润湿现象导致了离散分布的微液滴,对润滑轨道上的回流和润滑油膜的形成起到了正面作用. 相似文献
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Experimental results are presented for a bubbly lubricated externally pressurized circular thrust bearing. The data consists of the measured radial pressure distribution together with the lubricant mass flow rate over a wide range of inlet pressure, air mass flow rate ratio, for an either stationary or rotating bearing.It is shown that the air injection always improves the pressure distribution in the bearing and so can completely avoid the negative pressure generated due to rotational inertia. Also it is shown that the bearing load carrying capacity increases as the injected air mass flow increases, especially at high inlet pressure. The lubricant mass flow rate is reduced by the increase of air mass flow rate and by the decrease of bearing rotational speed.Finally the experimental results described in this paper are in good agreement with the mathematical analysis, based on the homogeneous flow model presented previously. 相似文献
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采用球-盘点接触光干涉油膜测量仪观察了不同钢球和盘表面速度夹角下脂润滑的油膜特性. 试验发现,在表面速度异向条件下呈现出与已有定量脂润滑明显不同的两个特征:接触区入口油池的出现和油膜外形非对称性. 其中入口油池的出现使油膜厚度和润滑持续时间得到显著提升,这一发现也证明将经典的乏油边界条件应用于速度异向工况具有局限性;油膜外形的非对称性主要由滑动分量诱发的接触区温度分布不均匀引起,而且非对称性随着速度和角度的增加而变得明显. 表面速度异向条件下两表面上滚道交叉促进润滑剂回填,是入口油池形成的主要机制. 相似文献
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Yongbin Zhang 《Flow, Turbulence and Combustion》2011,87(4):707-723
The present paper proposes a simplified model for calculating hydrodynamic lubrication film thickness in elastoplastic line
contacts. According to the Saint-Venant’s principle, the pressure in the contact is taken as uniformly distributed, this gives
the contact surface elastic deformations in the inlet zone far away from the contact center close to real ones while gives
those close to the contact center greater than real ones. This treatment is validated for hydrodynamic lubricated elastic
contacts for relatively light loads and high rolling speeds. It gives the film thickness at the contact center a little higher
than that calculated based on the real elastic model. The treatment is extended to a hydrodynamic lubricated elastoplastic
line contact. The contact surfaces in the inlet zone are assumed as elastic and their deformations are calculated based on
the uniform pressure distribution in the elastoplastic contact area. An inlet zone analysis is taken for obtaining the calculating
equation of the hydrodynamic film thickness at the contact center. The equation overestimates the central film thickness but
gives a satisfactory film thickness prediction for the heavy load which gives significant plastic deformations in the elastoplastic
contact. It is found that when the load is lighter than 0.6 w
pc
, the contact can be taken as elastic when calculating the central film thickness, while when the load is heavier than 0.6 w
pc
, the contact can be taken as fully plastic; Here w
pc
is the critical load for the contact fully plastic deformation. The plastic deformation in an elastoplastic line contact
is found to reduce the hydrodynamic lubrication film thickness in the contact. This reduction is greater for higher rolling
speeds and heavier loads. However, it is significantly dropped with increasing surface hardness. 相似文献
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The paper is focused on the influence of surface micro-cavities in non-conformal contact on tribological quantities, such
as lubricant film thickness, contact pressure and especially rolling contact fatigue (RCF). Both the possible negative and
positive effects of surface texturing under mixed lubrication conditions are considered. The lubricant film thickness was
measured using optical test rig based on thin film colorimetric interferometry, where the contact is realized between steel
ball and glass disc. The experimental apparatus consisting of two discs loaded and running against roller specimen was used
for measurement of RCF. Obtained results confirmed the key effect of micro-features depth on film thickness and RCF behavior
under rolling/sliding conditions. 相似文献
16.
HKD-1型航空润滑油特征剪切应力及有效粘压系数确定的研究 总被引:2,自引:0,他引:2
在球盘式拖动力试验机上,对HKD-1型航空润滑油进行拖动力测量,给出了根据拖动力试验曲线的非线性上升段确定润滑油有效粘压系数和特征应力的方法,对HKD-1型航空润滑油在试验条件下的粘压系数和特征应力进行分析,并建立了其计算公式.结果表明:特征应力和有效粘压系数的求解方法简单合理,其计算公式的拟合精度较高,可为轴承动态特性设计提供计算依据;随着接触压力、入口油温和滚动速度增加,HKD-1型航空润滑油的特征应力增大,其粘压系数减小;滚动速度对特征应力和粘压系数的影响小于接触压力和入口油温. 相似文献