一种连杆式锁紧释放装置及航天器
By using a linkage-type locking and releasing device, the rotational movement of the sliding sleeve and the linkage solves the problem of unstable steel ball locking in existing technologies, achieving stable locking and convenient unlocking of spacecraft equipment, and is suitable for unlocking and separating spacecraft equipment.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING WEINA STAR TECH CO LTD
- Filing Date
- 2025-11-11
- Publication Date
- 2026-07-17
AI Technical Summary
Existing clamping and release mechanisms on spacecraft have the problem of potential crushing of the contact surface during steel ball locking, resulting in unstable locking and inconvenient unlocking.
The locking and releasing device adopts a linkage type, including a base, a sliding sleeve, a puller, a split nut assembly, a linkage, and a tension spring. The rotation of the sliding sleeve drives the linkage to deflect, thereby achieving locking and unlocking, avoiding the problem of crushing of the contact surface due to the steel ball locking.
It achieves stable and reliable locking, can withstand large locking forces, and is easy to unlock. It has a compact structure and is suitable for unlocking and separating equipment in spacecraft.
Smart Images
Figure CN121516276B_ABST
Abstract
Citation Information
Patent Citations
Split nut type unlocking and releasing device and reusable unlocking and releasing device
CN113955155A
Locking and releasing device for spacecraft and spacecraft
CN121376222A
Actuator
US20190112838A1