Fault analysis for lock seat slip of space-borne overlapping antenna

QI Xueliang1, WEI Juanfang1, DING Huibing2, LI Yanyong1, ZHANG Chen1

Journal of Vibration and Shock ›› 2019, Vol. 38 ›› Issue (19) : 98-102.

PDF(1571 KB)
PDF(1571 KB)
Journal of Vibration and Shock ›› 2019, Vol. 38 ›› Issue (19) : 98-102.

Fault analysis for lock seat slip of space-borne overlapping antenna

  • QI Xueliang1, WEI Juanfang1, DING Huibing2, LI Yanyong1, ZHANG Chen1
Author information +
History +

Abstract

In operation process, contact surface slip faults of antenna lock seat often happen due to vibration to cause locking state failure of the lock seat.Here, in order to solve this problem, a test analysis method for contact surface mechanical state of antenna lock seat was proposed. Firstly, an overlapped antenna test model was designed and manufactured to do vibration tests.Its frequency response curve and dynamic strain curve were obtained in vibration tests.Then, a spring set equivalent model was introduced on contact surface of the lock seat, and the whole overlapping antenna finite element (FE) model was built. According to the test results, the FE model was modified.Finally,contact force states before and after the lock seat having slip fault were analyzed contrastively to evaluate effects of slip fault on the lock seat performance.

Key words

 Locking device / Deployable antenna / Fault analysis

Cite this article

Download Citations
QI Xueliang1, WEI Juanfang1, DING Huibing2, LI Yanyong1, ZHANG Chen1. Fault analysis for lock seat slip of space-borne overlapping antenna[J]. Journal of Vibration and Shock, 2019, 38(19): 98-102

References

[1] Li L, Cheng L, Mu H, et al. Study on the output performance of an aerospace pyrotechnic device using numerical simulation[C]// Prognostics and System Health Management Conference. IEEE, 2017: 1-6.
[2]Bowman N J, Knippenberg E F. Pyrotechnic devices for use on sterilized spacecraft[J].Journal of Spacecraft & Rockets, 2015, 3(10):1542-1544
[3]高滨.火工驱动分离装置的应用[J].航天返回与遥感, 2004, 25(1):55-59
GAO Bin. Application of Pyrotechnically Actuated Devices[J].SPACECRAFT RECOVERY & REMOTE SENSING, 2004, 25(1):55-59
[4]Guo H, Shi C, Li M, et al. Design and Dynamic Equivalent Modeling of Double-Layer Hoop Deployable Antenna[J].International Journal of Aerospace Engineering, 2018, 2018(4):1-15
[5] 夏晓宇.火工分离装置工作过程性能分析[D]. 国防科学技术大学, 2009.
XIA XiaoYu. Performance analysis of separation pyrotechnics in the operation process [D]. National University of Defense Technology, 2009.
[6]王朋朋,高博,艾永强,牛宝华.基于冲击响应分析的星载可展天线解锁策略优化[J].振动与冲击,2017,36(10):57-62.
WANG Pengpeng,GAO Bo, AI Yongqiang,NIU Baohua.
Release strategy optimization for deployable satellite antennas based on shock response analysis[J]. Journal of Vibration and Shock, 2017,36(10):57-62.
[7]初文华,张阿漫,明付仁,杨文山.SPH-FEM耦合算法在爆炸螺栓解锁分离过程中的应用[J].振动与冲击,2012,31(23):197-202.
CHU Wenhua,ZHANG Aman,MING Furen,YANG Wenshan. Application of three-dimensional SPH-FEM coupling method in unlocking process of an explosion bolt[J]. Journal of Vibration and Shock,,2012,31(23):197-202.
[8] Robert D, Ernst M. Nonlinear finite element evaluation of marman clamp structural capability [C]// Structures, Structural Dynamics, and Materials Conference. 2013.
[9]张永杰, 孙秦.带预紧力受剪螺栓连接刚度分析[J].强度与环境, 2007, 34(4):22-25
ZHANG Yongjie, SUN Qin. Sheared bolt joint stiffness analysis with pre-tightened force[J].Structure &Environment Engineering, 2007, 34(4):22-25
[10]王建民,郑常良.螺栓对接结构的非线性解析建模与分析[J].振动与冲击, 2013, 32(20):5-8
WANG Jianmin, ZHENG Changliang. Nonlinear analytical modeling and analysis for bolted joint structures[J].Journal of Vibration and Shock, 2013, 32(20):5-8
[11]陈学前,杜强,冯加权.螺栓连接非线性振动特性研究[J].振动与冲击, 2009, 28(7):196-198
CHEN Xueqian, DU Qiang, FENG Jiaquan. Nonlinear vibrational characteristic of bolt-joints[J].Journal of Vibration and Shock, 2009, 28(7):196-198
[12]卫洪涛,孔宪仁,王本利,张相盟.基于振型转换的螺栓连接梁非线性振动研究[J].振动与冲击,2014,33(12):42-47+92.
WEI Hongtao,KONG Xianren,WANG Benli,ZHANG Xiangmeng. Non-linear dynamic response of a beam with bolted joint based on modal shape transfer[J]. Journal of Vibration and Shock, 2014,33(12):42-47+92.
[13] Song Y, Mcfarland D M, Bergman L A, et al. Modeling of the Dynamics of Jointed Beam Structures[C]// ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. 2003:1091-1100.
[14]薛闯, 贾建军, 舒嵘,等.装配体结构有限元分析中的螺钉连接模型[J].科学技术与工程, 2006, 6(7 ):825-828
XUE Chuang, IA Jian-jun, HU Rong, et al. Bolted joint models of finite element assemblies[J].Science Technology and Engineering, 2006, 6(7):825-828
[15] 华参庆.机载设备连接螺栓有限元分析[C]// Msc, Software虚拟产品开发. 美国MSC软件公司北京代表处, 2008.
HUA Shen-Qing. Finite element analysis of airborne equipment connection bolts [C]// Msc, Software virtual product development. American MSC software company Beijing representative office, 2008.
[16] 楼梦麟.连接子结构与子结构模态综合法[J].振动工程学报, 1995, 8(1):52-56
Lou MengLin. Link substructure and modal synthesis for substructuring[J].Journal of Vibration Engineering, 1995, 8(1):52-56
PDF(1571 KB)

335

Accesses

0

Citation

Detail

Sections
Recommended

/