首页 | 本学科首页   官方微博 | 高级检索  
     检索      

航空发动机弧齿锥齿轮的润滑状态研究
引用本文:魏文山,林基恕,丁津原,夏延秋,杨文通.航空发动机弧齿锥齿轮的润滑状态研究[J].航空动力学报,1998,13(3):298-301,348.
作者姓名:魏文山  林基恕  丁津原  夏延秋  杨文通
作者单位:中国航空工业总公司606所,东北大学
摘    要:利用空间点接触齿面啮合理论的矢量法,推导啮合点位置、接触点曲率半径和齿面上接触点的运动速度及其方向。以轮齿加载接触分析(LTCA)方法确定各瞬时单齿承载百分比。计算两齿面间的油膜厚度和膜厚比,作为润滑状态的理论判据。同时以扫描电镜观测分析300小时台架试验后的齿面形貌,结合理论判据,确定典型工况下的弧齿锥齿轮齿面润滑状态。

关 键 词:航空发动机  弧齿锥齿轮  润滑  摩擦
收稿时间:8/1/1997 12:00:00 AM
修稿时间:1997/10/1 0:00:00

A STUDY ON LUBRICATION OF SPIRAL BEVEL GEARS IN AEROENGINE
Wei Wenshan,Lin Jishu,Ding Jinyuan,Xia Yanqiou and Yang Wentong.A STUDY ON LUBRICATION OF SPIRAL BEVEL GEARS IN AEROENGINE[J].Journal of Aerospace Power,1998,13(3):298-301,348.
Authors:Wei Wenshan  Lin Jishu  Ding Jinyuan  Xia Yanqiou and Yang Wentong
Institution:5th Dept.Shenyang Aeroengine Research Institute,Shenyang 110015;5th Dept.Shenyang Aeroengine Research Institute,Shenyang 110015;Mechanical Engineering Institute,Shenyang 110006;Mechanical Engineering Institute,Shenyang 110006;Mechanical Engineering Institute,Shenyang 110006
Abstract:The vector method of the gear engagement theory is used to describe the manufacturing and meshing process of the spiral bevel gears in the aeroengine.The geometry and kinematic parameters of each contact point are considered,including the position,the curvature and the speed of each contact point on the tooth surface.The load on tooth in each contact position is determined with the help of Loaded Tooth Contact Analysis (LT CA) and the thickness of oil film on each contact position is obtained as theoretical foundation for judging the lubrication state.Meanwhile,300 hours test of the gears has been made and the topographical feature of the tooth surface by means of scanning electron microscope is investigated.The results of calculation and experiment show that the gears are under boundary lubrication and partial elasto-hydrodynamic lubrication.
Keywords:Aircraft engine  Spiral bevel gears  Lubrication  Friction
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号