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涡轴发动机端齿连接结构接触状态分析
引用本文:沈祥,曹鹏.涡轴发动机端齿连接结构接触状态分析[J].航空发动机,2017,43(4):35-40.
作者姓名:沈祥  曹鹏
作者单位:1. 中国商用飞机有限责任公司上海飞机设计研究院,上海,201210;2. 中国航发湖南航空动力机械研究所,湖南株洲,412002
摘    要:为了研究涡轴发动机端齿连接结构接触状态变化的发生机理及规律,根据涡轴发动机端齿连接的结构特征、受力分析和考虑滑移的切向接触受力原理,确定了端齿连接结构齿面接触状态的影响因素;并通过有限元分析方法,研究了齿面接触状态的变化规律。计算结果表明:转速和轴向压紧力对接触状态有重要影响;转速越高,则齿面接触区域变小,接触应力和滑移距离变大;轴向压紧力越大,则齿面接触区域越大,接触应力和滑移距离也越大;而摩擦系数对接触状态的影响不明显。研究结果对端齿连接高速转子的结构设计提供了一定的技术指导。

关 键 词:端齿  接触形式  接触应力  滑移距离  涡轴发动机

Contact State Analysis of Turboshaft Engine Rotor with Curvic-Coupling Joint Structure
Authors:SHEN Xiang  CAO Peng
Institution:1. COMAC Shanghai Aircraft Design and Research Institute, Shanghai 201210, China; 2. AECC China Aviation Powerplant Research Institute, Zhuzhou Hunan 412002, China
Abstract:In order to study the mechanismand law of contact state change of curvic-coupling of turboshaft engine rotor, the influencing factors of contact state for curvic -coupling joint structure were determined according to the structure characteristics, mechanics characteristics, and force principle of tangential contact considering sliding, and the changing rule of contact state for curvic-coupling was studied by finite element analysis method. The calculating results indicate that revolving speed and axial preload have important effects on curvic-coupling contact state; the greater the revolving speed is, the smaller the contact area is, and the greater the contact stress and sliding distance are; the greater the axis preload is, the greater the contact area is, and the greater the contact stress and sliding distance are; and the influence of friction coefficient on contact state is not obvious. The study results provide technical guidance of structure design for rotor with curvic-coupling.
Keywords:curvic-coupling  contact form  contact
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