Global Patent Index - EP 1092941 A1

EP 1092941 A1 20010418 - Device for correcting the trajectory of a spin-stabilized guided projectile

Title (en)

Device for correcting the trajectory of a spin-stabilized guided projectile

Title (de)

Einrichtung zur Veränderung der Flugrichtung eines rotationsstabilisierten Lenkgeschosses

Title (fr)

Dispositif de correction de trajectoire pour projectiles guides gyroscopes

Publication

EP 1092941 A1 20010418 (FR)

Application

EP 00402839 A 20001013

Priority

FR 9912915 A 19991015

Abstract (en)

The trajectory correction mechanism has a rotating mortar shell. The rear of the shell has rear stabilizer protrusions (7). There is a mechanism driving a canard wing (37) out from the shell forward section in the proximity fuze position. An Independent claim is also included for a projectile using this trajectory correction mechanism.

Abstract (fr)

Le dispositif de correction de trajectoire de l'invention s'applique à un projectile de mortier ou à un obus d'artillerie entraîné en rotation en roulis lorsqu'il est lancé. Ce dispositif comporte un empennage (7) et une fusée de proximité (3) munie d'un pilotage par canard (37). <IMAGE>

IPC 1-7

F42B 10/64; F42B 10/14; F42B 10/24

IPC 8 full level

F42B 10/14 (2006.01); F42B 10/24 (2006.01); F42B 10/64 (2006.01)

CPC (source: EP)

F42B 10/14 (2013.01); F42B 10/24 (2013.01); F42B 10/64 (2013.01)

Citation (applicant)

US 5439188 A 19950808 - DEPEW JR HERBERT D [US], et al

Citation (search report)

Designated contracting state (EPC)

AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

DOCDB simple family (publication)

EP 1092941 A1 20010418; EP 1092941 B1 20050810; AT E301816 T1 20050815; DE 60021822 D1 20050915; DE 60021822 T2 20060608; FR 2799833 A1 20010420; FR 2799833 B1 20021025

DOCDB simple family (application)

EP 00402839 A 20001013; AT 00402839 T 20001013; DE 60021822 T 20001013; FR 9912915 A 19991015