Released control release mechanism in particular for use in the space industry

摘要

The invention concerns a device forming a mechanism, in particular for use in the space industry, characterised in that it comprises in combination: two structural elements ( 100, 200 ) capable of relative displacement, locking means ( 300 ) adapted to prevent initially the relative displacement between the two structural elements ( 100, 200 ), and means ( 400 ) for controlled locking of the locking means ( 300 ) designed to prevent initially the release thereof, then when activated, successively, in a first phase, a sliding action in controlled amplitude of the locking means ( 300 ), for limited release between the two structural elements ( 100, 200 ), then in a second phase, complete release of the locking means ( 300 ) and hence of the structural elements ( 100, 200 ).