The invention discloses a solar cell array structure which is arranged on the upper surface of a satellite and comprises a foldable structure formed by at least one semi-rigid substrate and a buffer substrate which are alternately arranged, a pressing point located on the foldable structure and a shear type unfolding and locking mechanism, wherein a solar cell circuit is arranged on the first surface of the semi-rigid substrate.
本发明公开一种太阳电池阵结构,布置于卫星的上表面,包括交替布置的至少1块半刚性基板以及缓冲基板所形成的可折叠结构,位于可折叠结构上的压紧点,以及剪式展开锁定机构。其中,半刚性基板的第一表面上布置有太阳电池电路。
Solar cell array structure and unfolding method
一种太阳电池阵结构及展开方法
2020-12-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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