卫星载荷无接触支承外转子旋转关节结构
By designing the stator and rotor structures, and combining a rotating motor, magnetic levitation bearings, and sensor arrays, five-degree-of-freedom active control of the satellite payload was achieved. This solved the problems of high precision and reliability of the satellite payload's non-contact support and provided protection against magnetic levitation instability.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING INST OF CONTROL ENG
- Filing Date
- 2025-01-07
- Publication Date
- 2026-07-17
AI Technical Summary
Existing technologies are insufficient to achieve five-degree-of-freedom active control of satellite payloads, and cannot meet the high requirements of satellite engineering for non-contact support capabilities and control precision.
It adopts a stator and rotor structure, combined with a rotary motor, magnetic levitation bearing assembly, sensor assembly and self-unlocking locking device to achieve five degrees of freedom active control. The magnetic levitation bearing assembly provides contactless support, the mechanical protection bearing serves as a backup, and the backlash elimination device enables active switching.
It achieves high-precision rotation control and stable support for satellite payloads, provides protection against magnetic levitation instability, and improves the reliability and mechanical resistance of the rotating joint.
Smart Images
Figure CN119637119B_ABST