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某型直升机行星齿轮机构弹流润滑研究
引用本文:崔利杰,龚小平,仝崇楼.某型直升机行星齿轮机构弹流润滑研究[J].润滑与密封,2007,32(6):118-120.
作者姓名:崔利杰  龚小平  仝崇楼
作者单位:1. 空军工程大学工程学院,陕西西安,710038
2. 空军工程大学理学院,陕西西安,710051
摘    要:分析了某型直升机主减速器行星齿轮机构弹流润滑工况,研究了该齿轮系弹性润滑最薄弱啮合部位,计算得出了行星齿轮传动机构中齿宽、齿轮模数和压力角等齿轮参数对弹性润滑油膜厚度的影响,提出了改进直升机主减速器行星齿轮机械润滑状态的新思路和具体改进方案,结果证明增加行星轮和太阳轮的齿宽、模数和齿轮啮合角及提高润滑油粘度和粘压系数,可有效地改进齿轮润滑,减少齿面失效,提高行星齿轮传动机构的可靠性。

关 键 词:主减速器  行星齿轮机构  齿轮参数  油膜厚度
文章编号:0254-0150(2007)6-118-3
修稿时间:2006-12-29

The Elastohydrodynamic Lubrication Research on the Planetary Gear Mechanism of a Helicopter
Cui Lijie,Gong Xiaoping,Tong Chonglou.The Elastohydrodynamic Lubrication Research on the Planetary Gear Mechanism of a Helicopter[J].Lubrication Engineering,2007,32(6):118-120.
Authors:Cui Lijie  Gong Xiaoping  Tong Chonglou
Abstract:The elastohydrodynamic lubrication(EHL) work condition in the planetary gear transmission of main reducer of a helicopter was analyzed,the weakest mesh in it was investigated,the effect of geared parameters,such as width,module and mesh angle of planetary gear on the lubrication behavior in the planetary gear transmission was calculated,some methods to improve the EHL condition in the transmission were put forward.The result shows that the methods to enlarge width,module and mesh angels of planet and sun gears and enhance the viscosity and pressure-viscosity cofficient of lubricant can improve the lubrication of gears,reduce the invalidation of gear surface, and enhance the reliability of planetary gear transmission efficiently.
Keywords:main reducer  planetary gear mechanism  gear parameters  oil film thickness
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