The invention relates to the technical field of aerospace equipment, in particular to a satellite solar wing. The satellite solar wing comprises an antenna substrate, a heat dissipation plate and a charging module. The charging module is arranged on one side of the heat dissipation plate, and the antenna substrate is attached to the other side of the heat dissipation plate. The satellite solar wing has the advantages that the charging module and the antenna substrate are arranged in a stacked mode, the size of the satellite solar wing is reduced, the heat dissipation plate is arranged on the side, close to the antenna substrate, of the charging module, and the heat dissipation efficiency after the size of the satellite solar wing is reduced is guaranteed.
本发明涉及航天设备技术领域,具体而言,涉及一种卫星太阳翼。卫星太阳翼包括天线基板、散热板和充电模组;所述充电模组设置在所述散热板的一侧,所述天线基板贴设在所述散热板的另一侧。本发明实施例的有益效果是:通过将充电模组和天线基板进行层叠设置,减小了卫星太阳翼的体积,通过在充电模组靠近天线基板的一侧设置散热板,保证了在减小卫星太阳翼的体积后的散热效率。
Satellite solar wing
一种卫星太阳翼
2021-12-03
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Solar wing driving device, solar wing unfolding equipment and satellite
Europäisches Patentamt | 2024
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