A spacecraft on-orbit servicing mechanism

CN117566127BActive Publication Date: 2026-08-28CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
View PDF 2 Cites 0 Cited by

Patent Information

Application Number
CN202410020626.2
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-01-05
Publication Date
2026-08-28
Estimated Expiration
2044-01-05

AI Technical Summary

Technical Problem

航天器所处的空间环境复杂恶劣,若其在任务中出现功能失效的情况,损失巨大

Benefits of technology

[0015]与现有技术相比,本发明能够取得如下有益效果:一种航天器在轨维护机构,包括支撑组件、直线运动导轨组件和连接组件,支撑组件包括支撑垫片和基座,支撑垫片上设置有第一连接件,第一连接件用于将支撑垫片连接至航天器主体,基座通过第二连接件连接于支撑垫片,基座上开设有第一安装槽;直线运动导轨组件可滑动地安装于第一安装槽,以使直线运动导轨组件能够沿Z轴方向释放自由度;连接组件通过锁紧组件可拆卸地连接于直线运动导轨组件,连接组件用于连接被维护件。由此,能够实现Z轴方向双向自由度释放、其他方向高承载,为航天器局部被维护件在地面装调阶段提供稳定性和刚度功能,在发射阶段提供承载功能,在在轨运行阶段提供热变形释放功能,便于局部被维护件的在轨维护。

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN117566127B_ABST
    Figure CN117566127B_ABST
Patent Text Reader

Abstract

The present application relates to linear motion mechanism technical field, specifically to a kind of spacecraft on-orbit maintenance mechanism, including support assembly, linear motion guide rail assembly, connecting assembly and locking assembly, support assembly includes support gasket and pedestal, first installation slot is opened in pedestal;Linear motion guide rail assembly is slidably installed in first installation slot, and can release freedom along Z axis;Connecting assembly is used to connect the maintenance piece;Locking assembly is used to detachably connect the connecting assembly on the linear motion guide rail assembly. Thus, Z axis bidirectional freedom release, other direction high bearing can be realized, and one-way freedom release of Z axis is realized by cooperating with stop block, and Z axis direction bearing is realized by cooperating with flexible joint, to provide support, bearing, thermal deformation release and other functions for the maintenance piece, facilitate the on-orbit maintenance of the maintenance piece, so as to achieve integrated breakthrough design: a set of mechanism realizes launch bearing, kinematic installation, on-orbit maintenance upgrade three functions.
Need to check novelty before this filing date? Find Prior Art

Citation Information

Patent Citations

  • Flexible supporting structure applied to back inspection type oblong reflector

    CN107703603A

  • Space camera on-orbit maintenance mechanism

    CN117028765A