期刊文献+

球铰接杆式支撑臂构型参数分析 被引量:4

Configuration Parameter Analysis for ADAM-type Articulated Mast
下载PDF
导出
摘要 论述了球铰接杆式支撑臂的组成和主要构型参数。利用有限元分析软件建立了球铰接杆式支撑臂有限元模型,进行了模态分析并与试验结果进行了对比,验证了模型的正确性;分析了单元段跨距、套筒半径、横向框架边数和斜拉索预紧力对支撑臂性能的影响。结果表明单元段跨距的增加有利于支撑臂总体性能的提升,而套筒半径和横向框架边数的增加能提高支撑臂刚度但同时增加了系统总质量。斜拉索预紧力应从最小允许预紧力和球铰取得最大刚度值时对应的预紧力中选取较大值。分析结果为支撑臂的工程设计提供了依据。 The configuration of ADAM-type articulated mast was described, and main configuration parameters were chosen. Finite element models of the ADAM-type mast were built up by ANSYS. Using these models, mode analysis was carried out. By comparing the analysis results with experiment results, the correctness of the finite element models was validated. The effects of bay length, canister radius, cross-section side and preload of the diagonal cables on the performance of the mast were analyzed. The analysis results show that the performance can be improved by increasing the bay length. The bending stiffness and mass of the mast will be promoted as the canister radius increases. The preloads of the diagonal cables should be selected between the allowable minimum value and the value corresponding to the situation when the ball sockets obtain maximum stiffness. These conclusions could be applied in mast engineering design.
出处 《中国空间科学技术》 EI CSCD 北大核心 2012年第2期29-34,54,共7页 Chinese Space Science and Technology
基金 国防科技工业民用航天专项科研技术研究项目
关键词 球铰接杆式支撑臂 展开机构 构型 有限元法 参数分析 航天器 Able deployable articulated mast Deployable mechanism Configuration Finite element method Parameter analysis Spacecraft
  • 相关文献

参考文献7

二级参考文献44

共引文献47

同被引文献32

  • 1管国阳,矫桂琼,张增光.2D-C/SiC复合材料的宏观拉压特性和失效模式[J].复合材料学报,2005,22(4):81-85. 被引量:52
  • 2BURGARDT B,CARTRAUD P.Continuum modeling of beamlike lattice trusses using averaging methods[J].Computers and Stuctures,1999,73:267-279.
  • 3NOOR AHMED K,MIKULAS MARTIN M.Continuum modeling of larger lattice structures status and projections[R].NASA-TP-2767,1988.
  • 4UMLAND JEFFREY W,EISEN HOWARD.SRTM on-orbit structural dynamics[C].Seattle,WA:42nd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference and Exhibit,2001.
  • 5LEVINE MARIE B.On-orbit microdynamic behavior of a flexible structure:IPEX[C].Kissimmee,Florida:17th International Modal Analysis Conference,1999.
  • 6SRTM hardware-the mast[EB/OL].http://www.shuttlepresskit.com/sts-99/payload57.htm.
  • 7ADAM boom system:superiordeployable stability for precision payload support[EB/OL].http:// www.aec-able.com.
  • 8Hasselnmn T K, Anderson M C. Development of a large amplitude 3D microgravity suspension system [ C ]. 38thAIAA/ASME/ASCE/ AHS /ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, CA, 1997.
  • 9Wang L H, Hu Z D, Zhong Z, et al. Dynamic analysis of an axially translating visco-elastic beam with an arbitrarity varying length[J]. Acta Mech, 2010, 214:225 -244.
  • 10Amos A K, Qu B. The dynamic equations of motion for a deploying telescopic beam [ C 1. 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and AI&A/ASME Adaptive Structures Forum, La Jolla, CA, 1993.

引证文献4

二级引证文献9

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