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弹流润滑螺旋锥齿轮热摩擦行为分析
引用本文:王延忠,周元子,陈聪慧,郭梅,赵兴福.弹流润滑螺旋锥齿轮热摩擦行为分析[J].航空动力学报,2011,26(10):2382-2387.
作者姓名:王延忠  周元子  陈聪慧  郭梅  赵兴福
作者单位:1. 北京航空航天大学机械工程及自动化学院,北京,100191
2. 中国航空工业集团公司沈阳发动机设计研究所,沈阳,110015
3. 中国航空工业集团公司哈尔滨东安发动机(集团)有限公司,哈尔滨,150060
基金项目:国家自然科学基金(50875009); 航空科学基金(20090451009); 基础科研项目(B0620060424)
摘    要:针对直升机主减速器中的高速重载螺旋锥齿轮,建立了点接触热弹流润滑分析数学模型,包括Reynolds方程、能量方程和膜厚方程等,采用数值方法求解弹流润滑状态下的齿面摩擦因数.模型中考虑了润滑油黏度和密度随压力、温度的变化,并通过轮齿承载接触分析(LTCA)获得齿面真实载荷和卷吸速度、相对滑动速度等运动学变量.基于真实齿面...

关 键 词:螺旋锥齿轮  弹流润滑  摩擦因数  有限元热分析  本体温度  闪温
收稿时间:2010/11/9 0:00:00
修稿时间:2011/2/28 0:00:00

Thermal tribology analysis of spiral bevel gears in EHD lubrication
WANG Yan-zhong,ZHOU Yuan-zi,CHEN Cong-hui,GUO Mei and ZHAO Xing-fu.Thermal tribology analysis of spiral bevel gears in EHD lubrication[J].Journal of Aerospace Power,2011,26(10):2382-2387.
Authors:WANG Yan-zhong  ZHOU Yuan-zi  CHEN Cong-hui  GUO Mei and ZHAO Xing-fu
Institution:School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;Harbin Dongan Engine (Group) Corporation Limited, Aviation Industry Corporation of China, Harbin 150060, China
Abstract:The thermal elastohydrodynamic (EHD) analysis of lubrication was applied to investigate the friction factor of spiral bevel gears in helicopter's main transmission system.The calculation was based on the simultaneous solution of the Reynolds,energy and elasticity equations,including variations of lubricant viscosity and density in relation to pressure and temperature.The real contact load and velocities of sliding and entrainment between meshing tooth surfaces were treated based on loaded tooth contact analysis (LTCA) of spiral bevel gears.A thermal finite element analysis based on one-tooth sector model developed by real tooth profile was actualized,with calculated heat flow rate generated by sliding friction as thermal load and heat convection coefficients of all exposed surfaces as thermal boundary conditions.The tooth temperature field in steady state and flash temperature of contact location in transient state over several revolutions were investigated.The obtained results were reported and discussed.The comparison with analytical and experimental results from references and gear bench test was given in the end.
Keywords:spiral bevel gears  elastohydrodynamic lubrication  friction factor  thermal finite element analysis  bulk temperature  flash temperature
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