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两种航空润滑油润滑性能对比研究
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江苏省自然科学基金项目(BK20161187).


Comparative Analysis on Lubricating Properties of Two Aviation Lubricating Oils
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    摘要:

    利用ASTM D4636标准氧化安定性模拟氧化装置,对国产某型航空润滑油和进口航空润滑油50-1-4Φ在不同温度下进行模拟氧化试验,对比分析氧化后2种润滑油的运动黏度、抗磨性能和承载能力的变化规律。结果表明:在175 ℃氧化温度以下,2种润滑油的运动黏度均比较稳定,仅随温度小幅增加,可以长期使用;在200 ℃氧化温度以上,2种润滑油的运动黏度随温度变化幅度较大,均不能长期使用;在超高温度环境中,航空润滑油可能出现黏度下降的情况,将不利于流体润滑油膜的产生,其中国产某型航空润滑油更能适应短时间的超高温环境;氧化作用对2种润滑油的抗磨性能影响不大,氧化后的国产某型航空润滑油抗磨性能略高于50-1-4Ф;氧化作用有利于2种润滑油承载能力的提高,氧化后的国产某型航空润滑油的承载能力比50-1-4Ф更强。

    Abstract:

    Simulated oxidation tests of a domestic aviation lubricant and an imported aviation lubricant 50-1-4Φ at different temperatures were carried out by using ASTM D4636 standard oxidation stability simulator.The kinematic viscosity,antiwear performance and bearing capacity of the two lubricants after oxidization were analyzed and compared.The results show that,below the oxidation temperature of 175 ℃,the kinematic viscosity of the two lubricants is relatively stable,it can be used for a long time and the kinematic viscosity only has a slight increase with temperature.More than the oxidation temperature of 200 ℃,the kinematic viscosity of the two lubricants varies greatly with temperature and can’t be used for a long time.In the ultrahigh temperature environment,the viscosity of the two lubricants may decrease, which will be unfavorable to the formation of lubrication film.However,the domestic aviation lubricant can better adapt to the ultrahigh temperature environment in a short time.Oxidation has little effect on the antiwear performance of the two lubricants.After oxidation,the antiwear performance of the domestic aviation lubricant is slightly higher than that of 50-1-4Φ.Oxidation is beneficial to the improvement of the bearing capacity of the two lubricants.The bearing capacity of the domestic aviation lubricant is better than that of 50-1-4Φ after oxidation.

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宗营,姜旭峰,孙元宝.两种航空润滑油润滑性能对比研究[J].润滑与密封,2019,44(11):94-99.
. Comparative Analysis on Lubricating Properties of Two Aviation Lubricating Oils[J]. Lubrication Engineering,2019,44(11):94-99.

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  • 在线发布日期: 2020-03-19
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