Flexible solar wing unfolding mechanism with high unfolding-folding ratio
A deployment mechanism and flexible technology, applied in the aerospace field, can solve the problems of poor reliability of the solar wing deployment mechanism, large size of the deployment mechanism, complex mechanical structure, etc., and achieve a simple and uncomplicated mechanical structure, saving launch costs, and high expansion-to-receive ratio. Effect
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[0101] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0102] see Figure 3 to Figure 10 shown;
[0103] A flexible solar wing deployment mechanism with a high expansion-to-contraction ratio of the present invention, the deployment mechanism includes:
[0104] bottom plate 1;
[0105] a scissor bar assembly 4 integrated into the base plate 1; and
[0106] The solar blanket assembly 11 connected with the scissor bar assembly 4;
[0107] Expanding bodies also include:
[0108] The drive assembly 5 integrated in the base plate 1;
[0109] The driving assembly 5 has a driving motor 501 and a transmission gear 503 that is transmitted with the driving motor 501, and the transmission gear 503 extends to the upper part of the bottom plate 1;
[0110] The drive assembly 5 is in transmission connection w...
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