The invention relates to a flexible solar wing which comprises a lifting mechanism, a pressing and releasing mechanism, a shear fork type unfolding mechanism, a flexible substrate, a top rigid plate, a bottom rigid plate, a bottom support and a top support. The bottom support and the top support are connected to the two ends of the shear fork type unfolding mechanism respectively, and the lifting mechanism is installed on the bottom support. The top rigid plate and the bottom rigid plate are connected to the two ends of the front face of the shear fork type unfolding mechanism respectively, the multiple flexible substrates are connected to the portion, between the top rigid plate and the bottom rigid plate, of the shear fork type unfolding mechanism, and the adjacent flexible substrates are connected through hinges. The bottom rigid plate and the flexible substrate are connected through a hinge; the pressing and releasing mechanisms are installed on the top rigid plate and the bottom rigid plate respectively. The flexible solar wing has the advantages that the flexible solar wing is large in surface area when unfolded and small in size when folded and compressed.
本发明涉及一种柔性太阳翼,包括举升机构、压紧释放机构、剪叉式展开机构、柔性基板、顶部刚性板、底部刚性板、底部支架及顶部支架;在所述剪叉式展开机构的两端分别连接有所述底部支架和所述顶部支架,在所述底部支架上安装有所述举升机构;在所述剪叉式展开机构前面的两端部分别连接有所述顶部刚性板和所述底部刚性板,在所述剪叉式展开机构上位于所述顶部刚性板和所述底部刚性板之间连接有多个所述柔性基板,相邻所述柔性基板之间通过铰链连接,所述底部刚性板和所述柔性基板之间通过铰链连接;所述压紧释放机构分别安装在所述顶部刚性板和所述底部刚性板上。优点在于:充分体现了柔性太阳翼在展开时表面积大,收拢压紧时体积小的优势。
Flexible solar wing
一种柔性太阳翼
2025-03-04
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |