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齿轮风阻损失仿真及其实际应用
引用本文:梁作斌,杜佳佳,郭梅.齿轮风阻损失仿真及其实际应用[J].航空动力学报,2017,32(6):1419-1424.
作者姓名:梁作斌  杜佳佳  郭梅
作者单位:中国航空发动机集团有限公司 沈阳发动机研究所 航空发动机动力传输航空科技重点试验室,沈阳 110015
摘    要:对多种齿形大小相似但种类不同的齿轮进行了仿真研究,对轮齿周围的空气流场以及齿面压力场进行了分析,并对某型航空发动机中央传动锥齿轮的风阻损失进行了评估.结果表明,齿轮的风阻损失由压力损失和黏性力损失构成,其中黏性力损失占比为4%~17%.由于壁面作用,斜齿轮轮齿旋向不同也引入了约60%的风阻损失差异.航空发动机中央传动锥齿轮的风阻损失则在总损失中占比约为49%. 

关 键 词:风阻损失    圆柱齿轮    锥齿轮    计算流体动力学(CFD)    航空发动机
收稿时间:2015/8/28 0:00:00

Simulation of gear windage losses and its application
LIANG Zuobin,DU Jiajia,GUO Mei.Simulation of gear windage losses and its application[J].Journal of Aerospace Power,2017,32(6):1419-1424.
Authors:LIANG Zuobin  DU Jiajia  GUO Mei
Abstract:Several different types of gears,yet with similar size,were simulated.The air flow around gear teeth and the pressure distribution on gear teeth surfaces were studied.The windage losses of a specificinternal bevel gear adopted in an aero engine was calculated.Result showed that,gear windage losses were consist of pressure loss and viscous force loss,and viscous force loss occupied ratio of 4%-17%.60% difference in windage losses of helical gears with opposite hand of helix suggests the effect of wall.Windage losses for internal bevel gear in aero engine occupied about 49% of total transmission losses.
Keywords:windage losses  cylindrical gear  bevel gear  computation fluid dynamics (CFD)  aero engine
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