• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2017, Vol. 53 ›› Issue (11): 68-74.doi: 10.3901/JME.2017.11.068

• 航天工程中机构可靠性及其动力学和系统控制基础研究 • 上一篇    下一篇

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装配位置偏差对航天精密轴承磨损的影响

宁峰平1,2, 姚建涛2,3, 安静涛2, 赵永生2,3   

  1. 1. 中北大学机械与动力工程学院 太原 030051;
    2. 燕山大学河北省并联机器人与机电系统实验室 秦皇岛 066004;
    3. 燕山大学先进锻压成形技术与科学教育部重点实验室 秦皇岛 066004
  • 出版日期:2017-06-05 发布日期:2017-06-05
  • 作者简介:

    宁峰平,1984年出生,博士,讲师。主要研究方向为航天机构可靠性影响因素作用机理分析及其演化规律分析。

    E-mail:ning_fengping@163.com

    姚建涛(通信作者),男,1980年出生,博士,副教授。主要研究方向为机器人技术、多维力传感器技术、并联机构理论及应用。

    E-mail:jtyao@ysu.edu.cn

    赵永生(通信作者),男,1962年出生,博士,教授,博士研究生导师。主要研究方向为机器人技术,传感器技术,先进制造技术。

    E-mail:yszhao@ysu.edu.cn

  • 基金资助:
    * 国家重点基础研究发展计划(973计划,2013CB733000)和中北大学校基金(XJJ2016003)资助项目; 20160628收到初稿,20170328收到修改稿;

Effect of Assembly Situation Variation on Wear of Space Precision Bearings

NING Fengping1,2, YAO Jiantao2,3, AN Jingtao2, ZHAO Yongsheng2,3   

  1. 1. School of Mechanical and Power Engineering, North University of China, Taiyuan 030051;
    2. Parallel Robot and Mechatronic System Laboratory of Hebei Province, Yanshan University, Qinhuangdao 066004;
    3. Key Laboratory of Advanced Forging & Stamping Technology and Science of Ministry of Education Yanshan University, Qinhuangdao 066004
  • Online:2017-06-05 Published:2017-06-05

摘要:

以航天机构中的精密球轴承为研究对象,考虑轴向预紧力和装配位置偏差,研究了航天精密轴承磨损演化规律。基于轴承静力学和Archard磨损模型,分析轴承内圈各个角位置的磨损状况,预测润滑膜磨损导致润滑失效位置。建立轴承静力学平衡方程,获得轴向预紧力与轴向位移、径向装配位置偏差与其引起径向力的关系。利用Archard磨损模型,结合各个滚珠受力和在接触区的运动状况,分析轴承不同角位置磨损的状况。分别分析轴承各角位置磨损随轴向力、径向力和磨损时间的演化规律。研究结果表明:在单考虑轴向预紧力时,内圈各角位置磨损相同,且磨损深度与轴向预紧力呈线性关系;综合考虑轴向预紧力和装配位置偏差时,装配位置偏差导致轴承内部径向力呈指数趋势变化;径向位置偏差导致内圈各角位置磨损深度差距很大;径向位置偏差增大,靠近偏差方向的位置磨损加剧,背离偏差方向的位置磨损减弱;随着磨损时间延长,各角位置的磨损深度差距越来越大;径向位置偏差导致各角位置的接触角差别很小,而是各角位置的径向力差异却较大。

关键词: 磨损, 预紧力, 装配位置偏差, 航天轴承

Abstract:

Taking the precision ball bearings in spacecraft mechanism as a research object, the wear law of space precision bearings is investigated by considering axis preload and assembly situation deviation. Based on the statics of the rolling bearing and the Archard wear model, wear condition is analyzed at each angular position of inner ring, and position of lubrication failure caused by wear of lubrication film is predicted. Firstly, the static equilibrium equation of bearing is established, the relationship between the bearing axial load and axial displacement is obtained, and the relationship of radial assembly variation and the introduced radial load is obtained as well. Then, by using the Archard wear model at the same time combining the force and the movement of ball in contact regional, the wear of the bearing is analyzed in different angle position. In addition, the evolution law of wear with the axial force, radial force and wear time is analyzed at each angle position, respectively. The results showed that: when axial force alone is considered, the wear of each angle position of the inner ring is the same. What’s more, there exists linear relationship between wear depth and axial force. However, internal radial force changes exponentially with the radial position deviation when axial preload and assembly situation deviation are comprehensively considered. Radial position deviation leads to great difference in wear depth at each angular position of the inner ring. When radial force increases, the wear near the deviation direction increases while that away from the deviation direction weakens. With the wear time coursing, the difference of wear depth at each position keeps widening. The difference in contact angle caused by radial deviation is very small while that in radial force is large at different angular positions.

Key words: assembly situation deviation, preload, wear, space bearing