期刊文献+

间隙对平面机构运动特性的影响分析 被引量:15

Effects analysis of clearance on kinetic characteristic of plane mechanism
下载PDF
导出
摘要 由于装配、制造误差和磨损,运动副中的间隙是不可避免的,在机构运行期间,间隙使实际机构与理想机构的运动发生偏离,降低了机构运动精度。以含间隙曲柄摇杆机构为研究对象,建立了系统的动力学方程,并基于ADAMS进行了动力学仿真,仿真计算结果能够准确的预测含间隙机构的运动特性;利用ADAMS软件进行动力学仿真分析,可以提高效率,降低成本。 The clearances in mechanism are unavoidable for the assemblage;manufacturing errors and wear. The movements of the real mechanism are deflection from the ideal mechanism for the clear- ances and the motion accuracy is decreased. The dynamics equation of the crank and rocker with clear- ances is established and the dynamics simulation is made using ADAMS. The results of the simulation will predict the dynamic performances accurately. And it can also increase the efficiency and decrease the cost.
机构地区 哈尔滨工业大学
出处 《机械设计与制造》 北大核心 2010年第2期17-18,共2页 Machinery Design & Manufacture
关键词 间隙 ADAMS 机构 动力学仿真 Clearance ADAMS Mechanism Dynamics simulation
  • 相关文献

参考文献4

二级参考文献24

  • 1吴德隆 阎绍泽 黄铁球 张永.空间大型伸展机构动力学研究[A].陈滨主编.动力学振动与控制的研究[C].长沙:湖南大学出版社,1998.239—245.
  • 2Miura K,Furuya H.Variable geometry truss and its application to deployable truss and space crane.Acta Astronautica,985,2(7~8)99~607
  • 3Gantes Charis.An improved analytical model for the prediction of the nonlinear behavior of flat and curved deployable space frames.Journal of Constructional Steel Research 1997,44(1~2)29~158
  • 4Mitsugi Jin,Ando Kazuhide.Deployment analysis of large space antenna using flexible multibody dynamics simulation.Acta Astronautica,2000,47(1)19~26
  • 5Wada B K,Kedikian R.Experimental studies:Benefits of load control on deployment and structural linearity.AIAA-95-1140-CP:3529-3535
  • 6Hachkowski M R,Peterson L D,Lake M S.Friction model of a revolute joint for a precision deployable spacecraft structure.J.Spacecraft and Rockets,1999,6(4)591~598
  • 7Bullock S J,Peterson L D.Nanometer regularity in the mechanics of a precision deployable spacecraft structure joint.J.Spacecraft and Rockets,999,36(5)758~764
  • 8阎绍泽,黄铁球,张永,吴德隆.航天多铰接机械系统动力学分析与设计.中国机械工程学会第三届青年学术会议论文集,北京:机械工业出版社,1998,10:207-210
  • 9吴德隆,阎绍泽,黄铁球,张永.航天柔性多体系统动力学与自适应结构研究.见:全国多体系统动力学与控制学术研讨会论文集,邓可顺,洪嘉振,齐朝晖主编.2000, 7:1-7
  • 10陈洪彬,阎绍泽,申永胜.含间隙铰可展结构动力学仿真研究.美国MDI公司2001年ADAMS中国用户年会会议论文,2001-06.

共引文献36

同被引文献96

引证文献15

二级引证文献53

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部