摘要
Aiming at the pitch circle position of a spur gear in an aeroengine,considering the thermal effect of elastohydrodynamic lubrication,the effects of velocity parameters(-u),load parameters(-w)and material parameters(-g)on isothermal solution and thermal solution were studied. Three empirical formulas widely used to calculate the minimum oil film thickness under isothermal conditions are compared and analyzed. It is found that the error between the isothermal solution and thermal of elastohydrodynamic lubrication calculated by the formula of Грубин and Dowson is large within the working conditions studied in this paper. Yang’s formula has a small error in isothermal solution and thermal solution under low velocity or moderate load parameters,which can be directly used to predict the minimum oil film thickness of line contact in some working conditions. All three isotherm empirical formulas overestimate the effect of load parameters. The relative error of 10% is taken as the boundary between the quantized isothermal solution and thermal solution,and the reference range of each dimensionless parameter is given.
投稿的翻译标题 | General Analysis of Minimum Film Thickness in Line Contact Elastohydrodynamic Lubrication |
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源语言 | 繁体中文 |
文章编号 | 210824 |
期刊 | Tuijin Jishu/Journal of Propulsion Technology |
卷 | 44 |
期 | 3 |
DOI | |
出版状态 | 已出版 - 3月 2023 |
关键词
- Aeroengine
- Elastohydrodynamic lubrication
- Film thickness
- Line contact
- Thermal effect