The embodiment of the invention discloses a solar wing lifting mechanism. The solar wing lifting mechanism comprises a base fixed to a satellite; the at least two first support arms are rotatably connected with the base; the bearing platform is used for bearing the solar wing driving mechanism; the second supporting arm is rotatably connected with the bearing table and corresponds to the first supporting arm; the first support arm and the second support arm are rotatably connected through a rotating assembly; the rotating assembly comprises a driving part; the lifting mechanism has a folded state and an unfolded state; under the driving of the driving piece, the lifting mechanism is converted into an unfolded state from a folded state; when the lifting mechanism is in a folded state, the first support arm and the second support arm are close to each other; when the lifting mechanism is in an unfolded state, the first supporting arm and the second supporting arm are separated and located on the same straight line. According to the mechanism, the solar wing driving mechanism and the solar wing on the bearing table can be lifted to the position away from the satellite from the position close to the satellite, and the solar wing is driven by the solar wing driving mechanism to rotate so as to be aligned with the sun.
本申请实施例公开一种太阳翼举升机构,包括:固定于卫星上的底座;与底座可转动连接的至少两个第一支臂;还包括:用以承载太阳翼驱动机构的承载台;与承载台可转动连接的与第一支臂对应设置的第二支臂;第一支臂和第二支臂之间通过转动组件可转动连接;转动组件包括有驱动件;举升机构包括有收拢状态和展开状态;在驱动件的驱动下,举升机构由收拢状态转化为展开状态;当举升机构处于收拢状态时,第一支臂与第二支臂靠拢;当举升机构处于展开状态时,第一支臂与第二支臂分离,且位于同一直线上。该机构,能将位于承载台上太阳翼驱动机构及太阳翼由靠近卫星的位置举升至远离卫星的位置,在太阳翼驱动机构的带动下太阳翼转动,从而对准太阳。
Solar wing lifting mechanism
一种太阳翼举升机构
2023-04-04
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
European Patent Office | 2024
|Engineering Index Backfile | 1961
|Engineering Index Backfile | 1943
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