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航空高速齿轮泵齿轮端面摩擦副的润滑特性

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针对航空外啮合齿轮泵齿轮端面摩擦副磨损严重的问题,在齿轮端面开设仿特斯拉阀型槽和椭圆孔组合的新型复合织构以改善润滑特性.基于流体动力润滑理论和有限元仿真计算方法建立齿轮织构端面摩擦副的润滑理论分析模型,分别在有无织构条件下仿真分析了端面液膜内流体的压力分布和速度分布,研究了工况和结构参数对齿轮端面开启性和密封性的影响规律.结果表明:织构产生的流体动压力可使齿轮端面摩擦副非接触运行,对减摩增效具有积极作用;综合考虑齿轮端面摩擦副的开启性和控漏性,织构结构参数即槽深取7~9 μm、高度差取5~6μm、倾斜角取0°~10°、形状因子取0.4~0.5为宜.
Lubrication Characteristics of Gear End Face Friction Pairs of Aviation High-speed Gear Pumps
Aiming at the serious wear problems of gear end face friction pairs of aviation external gear pumps,a new compound texture combining Tesla valve groove type and elliptical shape was opened on the gear end faces to improve lubrication performance.Based on hydrodynamic lubrication theory and finite element simulation calculation method,a theoretical analysis model of gear textured end face friction pair lubrication was established.Pressure distribution and velocity distribution of flu-id within the end face liquid films were simulated and analyzed under conditions with and without tex-ture,and the effects of operating and structural parameters on the openness and sealing performance of gear end faces were studied.The results show that the hydrodynamic pressure generated by the tex-ture may make the gear end face friction pairs run non-contact,which has a positive effect on reducing friction and increasing efficiency.With the comprehensive consideration of the openness and leakage control performance of gear end face friction pairs,groove depth is as 7~9 μm,height difference is as 5~6 μm,inclination angle is as 0°~10°,and shape factor is as 0.4~0.5 are the optimal structural pa-rameters for the texture structure.

high speed gear pumpend face friction paircompound texturehydrodynamic lubri-cationstructural optimization

陈源、熊典峰、李运堂、高永操、李传仓、王冰清、金杰

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中国计量大学机电工程学院,杭州,310018

浙江环誉泵业科技有限公司,海宁,314400

高速齿轮泵 端面摩擦副 复合织构 液动润滑 结构优化

国家自然科学基金国家自然科学基金浙江省自然科学基金浙江省高校基本科研业务费项目

5190551352005470LZ23E0500022021YW07

2024

中国机械工程
中国机械工程学会

中国机械工程

CSTPCD北大核心
影响因子:0.678
ISSN:1004-132X
年,卷(期):2024.35(7)