古乐,崔海旭,马芳,张静静,张传伟,崔淑慧.低黏度燃料介质中部分膜点接触弹流润滑分析[J].表面技术,2017,46(6):49-54.
GU Le,CUI Hai-xu,MA Fang,ZHANG Jing-jing,ZHANG Chuan-wei,CUI Shu-hui.Partial EHL Analysis of Point Contact in Low Viscosity Fuel[J].Surface Technology,2017,46(6):49-54
低黏度燃料介质中部分膜点接触弹流润滑分析
Partial EHL Analysis of Point Contact in Low Viscosity Fuel
投稿时间:2017-04-10  修订日期:2017-06-20
DOI:10.16490/j.cnki.issn.1001-3660.2017.06.008
中文关键词:  燃料润滑  点接触部分膜弹流  有限差分法  油膜厚度
英文关键词:fuel lubrication  partial EHL of point contact  finite difference method  film thickness
基金项目:
作者单位
古乐 哈尔滨工业大学 机电工程学院,哈尔滨 150001 
崔海旭 哈尔滨工业大学 机电工程学院,哈尔滨 150001 
马芳 中国航发哈尔滨轴承有限公司,哈尔滨 150001 
张静静 中国航发哈尔滨轴承有限公司,哈尔滨 150001 
张传伟 哈尔滨工业大学 机电工程学院,哈尔滨 150001 
崔淑慧 哈尔滨工业大学 机电工程学院,哈尔滨 150001 
AuthorInstitution
GU Le School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China 
CUI Hai-xu School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China 
MA Fang Haring Bearing Corporation of AECC, Harbin 150001, China 
ZHANG Jing-jing Haring Bearing Corporation of AECC, Harbin 150001, China 
ZHANG Chuan-wei School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China 
CUI Shu-hui School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, China 
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中文摘要:
      目的 某型发动机转子系统直接采用JP-10燃料对传动部件进行润滑,但燃料润滑的可靠性是限制其应用的瓶颈技术之一,因此拟研究传动部件在JP-10介质中的润滑状态。方法 建立点接触部分膜弹流模型,模型以弹流润滑理论与弹性固体接触理论为基础,应用有限差分法进行完全数值求解。通过比较在JP-10、航空润滑油4050和4109介质中,油膜厚度、油膜压力及粗糙接触压力的分布,分析了JP-10的润滑性能。结果 JP-10形成的油膜厚度与压力均小于另外两种润滑油,JP-10介质中的粗糙接触压力远大于另外两种润滑油中的粗糙接触压力。结论 JP-10的润滑性能比常用的航空润滑油弱,其润滑可靠性较低,需要采取先进表面加工技术对传动部件间的接触表面进行防护,同时在合理范围内提高流体卷吸速度,提高表面加工质量,有利于流体润滑膜的形成。
英文摘要:
      JP-10 fuel has directly used to lubricate transmission parts in certain type of aero-engine. However, reliability of fuel lubrication is one of the obstacles restricting its application. A partial EHL model of point contact was established to study lubricating conditions of the transmission parts in low viscosity fuel JP-10. Finite difference method was used to obtain numerical solution of this model, which was based on elastohydrodynamic lubrication theory and elastic contact theory. The lubricating property of JP-10 was studied by comparing distributions of film thickness, film pressure and contact pressure among JP-10, aero lubricant 4050 and 4109. The film thickness and pressure of JP-10 were lower than that of the other lubricants, while asperity contact pressure in JP-10 was higher. Either lubricating property or lubricating reliability of JP-10 was lower than that of common aero oils. Advanced surface processing techniques, higher rotating speed within reasonable limits and higher surface precision are conducive to formation of fluid lubricating film.
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