The invention provides a two-stage floating butt joint type on-orbit replaceable mechanism and a pallet device thereof. The on-orbit replaceable mechanism comprises an outer shell, a cargo carrying assembly, a mechanical active butt joint locking assembly and a two-stage floating electric appliance interface assembly. The two-stage floating electric appliance interface assembly comprises an active butt joint part and a passive butt joint part; the active butt joint part is arranged on the outer shell and a shell of the cargo carrying assembly, the passive butt joint part is arranged on a passive butt joint spacecraft, and the active butt joint part and the passive butt joint part are matched to achieve butt joint of electric appliance interfaces; a butt-joint locking mechanism of the mechanical active butt-joint locking assembly is installed on the outer shell and the cargo carrying assembly, and the mechanical active butt-joint locking assembly drives a lead screw nut structure through a motor to drive a connecting rod structure of the butt-joint locking mechanism to stretch out and draw back, so that butt-joint and locking of the butt-joint locking mechanism and an external device with a locking hole are achieved. The device has the characteristics of high docking precision, high docking rigidity, good carrying stability, convenience in on-orbit operation and the like.

    本发明提供一种双级浮动对接式在轨可替换机构及其货盘装置,在轨可替换机构包括:外壳体及货物搭载组件、机械主动对接锁紧组件及双级浮动电器接口组件;所述双级浮动电器接口组件包括主动对接部分和被动对接部分;主动对接部分设置在外壳体及货物搭载组件的外壳上,被动对接部分设置在被动对接航天器上,主动对接部分和被动对接部分相配合实现电器接口对接;机械主动对接锁紧组件的对接锁紧机构安装在外壳体及货物搭载组件上,机械主动对接锁紧组件通过电机驱动丝杠螺母结构,带动对接锁紧机构的连杆结构伸缩,使对接锁紧机构与外部带有锁紧孔的装置实现对接和锁定。本发明具有对接精度高、对接刚度强、搭载稳定性好及便于在轨操作等特性。


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    Titel :

    Two-stage floating butt joint type on-orbit replaceable mechanism and pallet device thereof


    Weitere Titelangaben:

    一种双级浮动对接式在轨可替换机构及其货盘装置


    Beteiligte:
    LI TIEYING (Autor:in) / YOU BINDI (Autor:in) / YU DATENG (Autor:in) / XU XINBO (Autor:in) / YOON KYUNG (Autor:in) / KONG PENG (Autor:in) / WANG AIMING (Autor:in) / ZHANG QIANG (Autor:in) / XING YANJUN (Autor:in) / ZHAO XI (Autor:in)

    Erscheinungsdatum :

    2024-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS



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