飞行器舵机摆线减速器输出装置传热分析
CSTR:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:

重庆教委科学技术研究项目资助(KJ122202)


Heat transfer analysis of the output unit of cycloidal reducers for aircraft actuator
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    为探究飞行器舵机在高温下的工作情况针对飞行器舵机摆线减速器利用Unigraphics NXHypermesh和ANSYS等软件基于有限元方法对减速器输出机构进行传热分析。采用高阶四面体单元对减速器销轴输出机构进行有限元离散并在与舵翼直接相连的输出机构凸台采用等温加载经数值计算得到飞行器输出机构温度分布及变化状况。结果表明:有限元方法可以有效地分析飞行器输出机构传热情况舵翼温度和摆线轮定位位置是影响减速器正常工作时间的重要因素降低舵翼温度以及将摆线轮靠销轴远热端定位可提高飞行器舵机寿命。

    Abstract:

    To investigate the work condition of the aircraft actuators in high temperatureheat transfer process of the output unit of a cycloidal reducer of the actuator is taken into account by Unigraphics NXHypermesh and ANSYS softwares based on finite element analysis(FEA).The temperature distribution of the output unit is obtained by meshing modelapplying loads and solving discrete problems.Thenthe temperature variation of the output unit is gotten by sampling and processing the data of FEA results.In the endthree main conclusions are drawn.Firstthe heat transfer process of the output units of cycloidal reducers of actuators can be analyzed by FEA efficiently.Secondthe temperature of the rudder and the design position of cycloid gears are two major factors in the operating life of reducers.Thirdthe operating life can be improved by lowering the rudder temperature and installing the cycloidal gear as far as possible away from the heat source.

    参考文献
    相似文献
    引证文献
引用本文

钟晖,谭儒龙,陈兵奎,易文翠.飞行器舵机摆线减速器输出装置传热分析[J].重庆大学学报,2014,37(5):8-12.

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2013-11-30
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2014-06-03
  • 出版日期:
文章二维码