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基本信息:
- 专利标题: 卫星用折叠型指向天线装置
- 申请号:CN201810308764.5 申请日:2018-04-08
- 公开(公告)号:CN108539360B 公开(公告)日:2020-02-18
- 发明人: 李春晖 , 王涵 , 董毅 , 苏晟 , 田毅辉 , 王见 , 马志祥 , 张顺波
- 申请人: 上海航天测控通信研究所
- 申请人地址: 上海市闵行区中春路1777号
- 专利权人: 上海航天测控通信研究所
- 当前专利权人: 上海航天测控通信研究所
- 当前专利权人地址: 上海市闵行区中春路1777号
- 代理机构: 上海汉声知识产权代理有限公司
- 代理人: 王叶娟; 胡晶
- 主分类号: H01Q1/08
- IPC分类号: H01Q1/08 ; H01Q3/08
The invention provides a folding type directional antenna device for a satellite. A supporting base can be mounted to the mounting portion of a satellite body; a pitch rotating mechanism is connectedwith the supporting base and is connected with an azimuth rotating mechanism; the azimuth rotating mechanism is connected with an antenna assembly; a restraining device is connected with the antenna assembly; the antenna assembly cannot rotate on the azimuth rotating mechanism when being restrained by the restraining device; and the antenna assembly can be folded relative to the supporting base bymeans of the pitch rotating mechanism; when the restraining device is released, the pitch rotating mechanism can rotate relatively, the azimuth rotating mechanism can rotate relatively, and the rotation axis of the pitch rotating mechanism is perpendicular to the rotation axis of the azimuth rotating mechanism; and the antenna assembly can rotate to realize orientation in different directions through the azimuth rotating mechanism and the pitch rotating mechanism. In a limited satellite installation and use space, the installation of the antenna can be realized, the antenna is far away from the satellite body after the antenna is unfolded, so that the influence of the satellite body can be decreased, and a two-dimensional rotation orientation function can be realized.
公开/授权文献:
- CN108539360A 卫星用折叠型指向天线装置 公开/授权日:2018-09-14
IPC结构图谱:
H | 电学 |
--H01 | 基本电气元件 |
----H01Q | 天线 |
------H01Q1/00 | 天线零部件或与天线结合的装置 |
--------H01Q1/08 | .折叠天线或其附件的装置 |