中国空间科学技术2011，Vol.31Issue(2)：53-57,5.DOI:10.3780/j.issn.1000-758X.2011.02.009
星载可展开天线热振动数值分析
Numerical Analysis of Thermal Induced Vibration for Deployable Antenna
刘劲 1朱敏波 1曹罡1
作者信息
- 1. 西安电子科技大学机电工程学院,西安710071
- 折叠
摘要
Abstract
Thermal induced vibration of a deployable antenna was analyzed by the non-coupling dynamics and finite element method.Thermal dynamic forces was simulated by a half sine wave thermal shock.Typical model node displacement and stress, as well as root mean square of antenna induced by thermal dynamic forces were discussed.The results show that thermal induced vibration of antenna occurs when thermal dynamic forces greatly change.Meanwhile, the dynamic response of thermal induced vibration is significantly greater than that of the static response.关键词
形面精度误差/温度冲击/热振动/可展开天线/卫星Key words
Root mean square/ Thermal shock/ Thermally induced vibration/ Deployable antenna/ Satellite引用本文复制引用
刘劲,朱敏波,曹罡..星载可展开天线热振动数值分析[J].中国空间科学技术,2011,31(2):53-57,5.
