The invention relates to a pressing force adjusting device for stacking satellite solar wings, and mainly relates to the technical field of stacking satellites, the pressing force adjusting device comprises a base, a driving mechanism arranged on the base, a plurality of adjusting mechanisms arranged on the base and a guide mechanism arranged on the base; the adjusting mechanism comprises a limiting cylinder fixedly arranged on the base in a penetrating mode, a transmission rod arranged on the limiting cylinder in a penetrating mode, a connecting block rotationally connected in the axis direction of the transmission rod and a limiting ring arranged on the connecting block. The connecting block is in sliding connection with the limiting cylinder in the axis direction of the limiting cylinder, one end of the transmission rod is in threaded fit with the limiting cylinder, and the other end of the transmission rod is in meshing transmission connection with the base. The device has the advantages of being good in structural stability and high in space utilization rate.
本申请涉及一种用于堆叠卫星太阳翼的压紧力调节装置,主要涉及堆叠卫星的技术领域,其包括底座、设在所述底座上的驱动机构、多个设在所述底座上的调节机构和设在所述底座上的导向机构;所述调节机构包括固定穿设在所述底座上的限位筒、穿设在所述限位筒上的传动杆、绕所述传动杆轴线方向转动连接的连接块和设在所述连接块上的限位环;所述连接块与所述限位筒沿所述限位筒的轴线方向滑动连接,所述传动杆的一端与所述限位筒螺纹配合,另一端与所述底座啮合传动连接。本申请具有结构稳定性好、空间利用率高的优点。
Pressing force adjusting device for stacking satellite solar wings
一种用于堆叠卫星太阳翼的压紧力调节装置
19.01.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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