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基于ease-off的弧齿锥齿轮齿面高阶接触分析方法

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为应对弧齿锥齿轮二阶接触分析方法的不足与其高阶接触理论实现的复杂问题,基于ease-off拓扑曲面方程与弧齿锥齿轮齿面方程的结合以及传动误差与接触迹线和ease-off之间的解析关系,提出以传动比高阶导数和接触迹线短程曲率为高阶接触参数的离散齿面的高阶接触分析方法,并建立基于有限差分的简便计算方法。结果表明,高阶齿面的传动比高阶导数波动值分别为0。003 1、0。001 9与0。001,数值反映齿面形貌的全局特性;接触线短程曲率波动值分别为0。0000769、0。000 586和0。000 127,说明沿接触迹线的齿面接触过程的复杂性。结果不仅验证了离散齿面高阶接触分析方法的正确性与有效性,而且说明该方法降低了高阶接触参数的计算难度,为齿面全局设计提供了可能。
High-order contact analysis method of spiral bevel gear tooth surface based on ease-off
In order to deal with the shortcomings of the second-order contact analysis method of spiral bevel gears and the complex problems of its high-order contact theory realization,based on the combination of ease-off topological surface equation and tooth surface equation of spiral bevel gears and the analytical relationship between transmission error and contact trace and ease-off,a high-order contact analysis method for discrete tooth surfaces with high-order contact parameters of high-order derivative of transmission ratio and short-range curvature of contact trace was proposed,and a simple calculation method based on finite difference was established.The results showed that the fluctuation values of the high-order derivative of the transmission ratio of the high-order tooth surface were 0.003 1,0.001 9 and 0.001,respectively,which reflected the global characteristics of the tooth surface morphology.The short-range curvature fluctuation values of the contact line were 0.000 076 9,0.000 586 and 0.000 127,respectively,indicating the complexity of the tooth surface contact process along the contact trace.The results not only verified the correctness and effectiveness of the discrete tooth surface high-order contact analysis method,but also showed that the method reduced the calculation difficulty of high-order contact parameters,providing the possibility for the global design of tooth surface.

spiral bevel gearease-offhigh-order contact analysisfinite difference methodglobal contact problems

陈鹏、王三民、李飞

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西北工业大学机电学院,西安 710072

弧齿锥齿轮 ease-off 高阶接触分析 有限差分法 全局接触问题

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(6)
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