Anti-rebound locking device for the deployable fin of a...

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Reexamination Certificate

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Reexamination Certificate

active

07919739

ABSTRACT:
The invention relates to a locking device for a deployable surface or fin of a projectile characterized in that it incorporates at least one flexible tongue, one end of which protrudes in the groove, a recess to the side of the groove enabling the tongue to bend in a first direction to enable the fin to enter the groove.

REFERENCES:
patent: 3031967 (1962-05-01), Jasse
patent: 3598345 (1971-08-01), Suter
patent: 4709878 (1987-12-01), Titley
patent: 4728058 (1988-03-01), Brieseck et al.
patent: 5762294 (1998-06-01), Jimmerson
patent: 6739548 (2004-05-01), Bittle et al.
patent: 40 17 504 (1993-07-01), None
patent: 1 536 271 (1969-04-01), None
patent: 2 860 577 (2005-04-01), None

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