EP 0653604 B1 19980729 - Stabilising for deployment device for a rocket type projectile
Title (en)
Stabilising for deployment device for a rocket type projectile
Title (de)
Entfaltungseinrichtung für Stabilisatorflügel eines Raketengeschosses
Title (fr)
Dispositif de déploiement pour une ailette de stabilisation de projectile de type roquette
Publication
Application
Priority
FR 9313617 A 19931116
Abstract (en)
[origin: EP0653604A1] The technical field of invention is that of devices for a deployment of fins of projectiles, especially of the rocket type. The deployment device according to the invention is characterised in that it comprises a torsion spring (9), the axis of which is parallel to the axis (XX') of the projectile. It is arranged in a groove (10) made in a collar (17) of a support (5) integral with the projectile (1), on which collar (17) the fin (7) is mounted, the groove having a width larger than the outside diameter of the spring, making it possible to ensure the guidance of the latter and allowing its ejection after the deployment of the fin. The method is used in the field of anti-tank weapons. <IMAGE>
IPC 1-7
IPC 8 full level
F42B 10/14 (2006.01)
CPC (source: EP)
F42B 10/14 (2013.01)
Designated contracting state (EPC)
DE GB SE
DOCDB simple family (publication)
EP 0653604 A1 19950517; EP 0653604 B1 19980729; DE 69412036 D1 19980903; DE 69412036 T2 19981203; FR 2712679 A1 19950524; FR 2712679 B1 19960209
DOCDB simple family (application)
EP 94402075 A 19940919; DE 69412036 T 19940919; FR 9313617 A 19931116