The invention relates to a repeated locking and releasing mechanism, in particular to a linkage type space repeated locking and releasing mechanism. The linkage type space repeated locking and releasing mechanism aims at solving the problem that reliability and controllability of an existing locking and releasing mechanism in the locking process are poor. The linkage type space repeated locking and releasing mechanism comprises a repeatable locking and releasing mechanism and a linkage driving mechanism. The repeatable locking and releasing mechanism comprises a locking mechanism and a locked assembly. The locking mechanism comprises a connection rod, a rocker connection rod shaft, a rocker, a lock hook rocker shaft, a lock hook, a locking shell, a bearing base, a worm, a worm gear, a first transition gear, a first transition gear shaft, a second transition gear shaft, a second transition gear, a crank gear, a crank connection rod shaft, a rocker shaft and a crank gear shaft. The linkage type space repeated locking and releasing mechanism is used in the aerospace field.
Linkage type space repeated locking and releasing mechanism
2016-02-03
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
Repeated locking and releasing mechanism of on-orbit load module
European Patent Office | 2020
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