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多因素作用下航天轴承预紧力分析
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  • 英文篇名:Analysis on Preload of Aerospace Bearings Under Multiple Factors
  • 作者:于清焕 ; 宁峰平 ; 孙锟 ; 赵永生
  • 英文作者:YU Qinghuan;NING Fengping;SUN Kun;ZHAO Yongsheng;CFHI Dalian Engineering & Technology Co.,Ltd.;Parallel Robot and Mechatronic System Laboratory of Hebei Province Yanshan University;School of Mechanical and Power Engineering, North University of China;
  • 关键词:角接触球轴承 ; 航天轴承 ; 静力学分析 ; 预紧力
  • 英文关键词:angular contact ball bearing;;aerospace bearing;;statics analysis;;preload
  • 中文刊名:CUCW
  • 英文刊名:Bearing
  • 机构:一重集团大连工程技术有限公司;燕山大学河北省并联机器人与机电系统实验室;中北大学机械与动力工程学院;
  • 出版日期:2019-05-05
  • 出版单位:轴承
  • 年:2019
  • 期:No.474
  • 语种:中文;
  • 页:CUCW201905001
  • 页数:6
  • CN:05
  • ISSN:41-1148/TH
  • 分类号:6-10+14
摘要
针对复杂的空间环境,以航天机构驱动单元轴系的71807C角接触球轴承为研究对象,基于滚动轴承静力学建立了滚动轴承预紧模型。在预紧模型的基础上,建立了环境温度、工作载荷、安装过盈量和磨损量多因素作用下轴承预紧力计算模型,并以71807C型角接触球轴承为例,分析多因素作用下轴承预紧力变化规律。结果表明:在低温、小过盈工况下,预紧力随磨损深度增大而极易出现预紧失效;磨损初期,轴承工作在高温、大过盈量工况下,较易出现机构卡死;环境温度、安装过盈量、磨损量对预紧影响显著,径向载荷影响较小。
        Aimed at complex space environment, taking angular contact ball bearings 71807 C for aerospace mechanism drive unit shafting as research objects, the model for preload is established based on statics of rolling bearings. Based on the model, the calculation model is established for preload of the bearings under multiple factors such as ambient temperature, operating load, installation interference and wear, the variation rule is analyzed for preload of the bearings under multiple factors. The results show that the preload is decreased with increase of wear depth under low temperature and small interference. The seizure of the bearings is more likely to appear at initial stage of wear under high temperature and large interference. The ambient temperature, installation interference and wear have remarkable effects on preload, and the radial load has less effect.
引文
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