期刊文献+

基于比刚度最大的球铰接杆式支撑臂参数设计

Configuration Parameter Design for ADAM-type Articulated Mast Based on Maximizing Specific Stiffness
下载PDF
导出
摘要 球铰接杆式支撑臂的构型参数设计决定了支撑臂的质量、收拢包络尺寸、刚度和强度等特性。文章提出了一种基于球铰接杆式支撑臂展开后比刚度最大的构型参数设计方法,利用MATLAB和ANSYS联合仿真,分析了不同构型参数组合下支撑臂比刚度的变化规律。结果表明,对于20~100m范围内的球铰接杆式支撑臂,纵梁与横杆的长度比及套筒半径的优选范围随支撑臂总长度增加而增加。当支撑臂总长度分别为20m、60m和100m时,对应的套筒半径优选范围分别为0.3~0.4m、0.5~0.7m和0.6~0.9m。提出了基于比刚度最大的支撑臂参数设计流程。利用提出的设计方法对SRTM任务中球铰接杆式支撑臂进行了构型参数设计,设计结果与ADAM杆构型参数相近,表明设计方法正确、可行。 The performances of the ADAM-type mast,such as mass,packaging size,stiffness and strength,are determined by its configuration parameters.A new design of configuration parameters based on maximizing specific stiffness was presented.By MATLAB and ANSYS joint simulation,the varying of specific stiffness with different configuration parameters was analyzed.The simulation results show that the optimum value of the length ratio of longeron to batten and the canister radius increases with the increase of the length of mast,when the length of ADAM-type varies in the range of 20to 100 meters.While the length of mast is 20,60,and 100 meters,the optimum value of the canister radius varies from 0.3to 0.4 meter,0.5to 0.7 meter and 0.6to 0.9 meter respectively.The design flow of configuration parameter based on maximizing specific stiffness is as follow : the canister radius is settled at first,then the length ratio of longeron to batten should be determined,and the number of longitudinal member could be finally settled.By this method,configuration parameters of the mast in the SRTM program are designed,and the results approximate to that of ADAM′s.
出处 《中国空间科学技术》 EI CSCD 北大核心 2013年第4期47-54,共8页 Chinese Space Science and Technology
关键词 球铰接杆式支撑臂 比刚度 构型 模态分析 优化 航天器 Able deployable articulated mast Specific stiffness Configuration Modal analysis Optimization Spacecraft
  • 相关文献

参考文献9

  • 1郭宏伟,刘荣强,邓宗全.空间索杆铰接式伸展臂性能参数分析与设计[J].北京航空航天大学学报,2008,34(10):1186-1190. 被引量:19
  • 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.
  • 4苏斌,关富玲,石卫华,谢铁华.索杆式伸展臂的结构设计与分析[J].工程设计学报,2003,10(5):287-294. 被引量:11
  • 5黎彪,刘志全,程刚,丁锋.球铰接杆式支撑臂构型参数分析[J].中国空间科学技术,2012,32(2):29-34. 被引量:4
  • 6UMLAND 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.
  • 7LEVINE MARIE B.On-orbit microdynamic behavior of a flexible structure:IPEX[C].Kissimmee,Florida:17th International Modal Analysis Conference,1999.
  • 8SRTM hardware-the mast[EB/OL].http://www.shuttlepresskit.com/sts-99/payload57.htm.
  • 9ADAM boom system:superiordeployable stability for precision payload support[EB/OL].http:// www.aec-able.com.

二级参考文献22

  • 1苏斌,关富玲,杨大彬,杨治.索杆式伸展臂的展开驱动设计与动力学分析[J].空间科学学报,2004,24(4):312-320. 被引量:10
  • 2张淑杰,李瑞祥,丁同才.盘绕式杆状展开机构的设计与力学分析[J].力学季刊,2006,27(2):341-347. 被引量:11
  • 3SRTM hardware-the mast: Payload bay[ EB/OL]. Shuttle Press Kit, 2000-01-18. http://www, shuttlepressklt, com/STS -99/ playload57. htm
  • 4Levine M B. Microdynamic behavior of a joint dominated structure on-orbit[R]. AIAA-99-1267, 1999
  • 5Farr T G, Rosen P A. The shuttle radar topography mission[R/ OL]. http ://trs-new. jpl. nasa. gov
  • 6Crawford R F. Strength and efficiency of deployable booms for space applications[ R]. AIAA-1971-396, 1971
  • 7Boom information [ EB/OL 5- AEC-Able Engineering Company Inc, 2004. http://www, aec-able, corn
  • 8Murphey T W. A material structure performance index for strain based deployable trusses[R]. AIAA-2004-1656, 2004
  • 9SHI Wei-hua(石卫华).The Design and Analysis of Rod-Cable Deployable Structures and Research on Framework membrances(索杆式展开结构的设计与分析及骨架式膜结构研究)[D].Hangzhou:Department of Civil Engineering,Zhejiang University,2003.(in Chinese).
  • 10CHEN Wu-jun,GUAN Fu-ling,CHEN Xiang-yang,et al(陈务军,关富玲,陈向阳,等).Study on space mast of octahcdral module[J].Journal of Astronautics(宇航学报),1994,(8):41-47.(in Chinese).

共引文献28

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