EP 0308344 A1 19890322 - Rearward closure for a missile container.
Title (en)
Rearward closure for a missile container.
Title (de)
Rückseitenverschluss für einen Raketenbehälter.
Title (fr)
Opercule arrière pour conteneur de missile.
Publication
Application
Priority
FR 8712862 A 19870917
Abstract (en)
The closure comprises a plurality of elements (10) which are mounted between two upper (7) and lower (8) supporting members and which are capable of being deformed from an initial closing position by the gases generated during the ignition of the missile (2), characterised in that each element (10) of the closure is elastic and is deformed about at least one rounded part (19) formed on said lower member (8). The invention is used particularly for missile containers on board warships. <IMAGE>
Abstract (fr)
L'Opercule comporte plusieurs éléments (10) qui sont montés entre deux organes supports supérieurs (7) et inférieurs (8), et qui sont susceptibles de se déformer d'une position intiale de fermeture par les gaz produits lors de la mise à feu du missile (2), caractérisé en ce que chaque élément (10) de l'opercule est élastique et se déforme autour d'au moins une partie arrondie (19) ménagée sur ledit organe inférieur (8). Application notamment aux conteneurs de missiles embarqués sur des bâtiments de guerre.
IPC 1-7
IPC 8 full level
F41F 3/04 (2006.01)
CPC (source: EP)
F41F 3/0413 (2013.01)
Citation (search report)
- GB 1540503 A 19790214 - MCEVOY OILFIELD EQUIPMENT CO
- US 2445423 A 19480720 - EASTMAN FRED C
- US 4134327 A 19790116 - PIESIK EDWARD T
Designated contracting state (EPC)
ES GB IT
DOCDB simple family (publication)
EP 0308344 A1 19890322; EP 0308344 B1 19920415; ES 2031261 T3 19921201; FR 2620808 A1 19890324; FR 2620808 B1 19900112
DOCDB simple family (application)
EP 88402343 A 19880916; ES 88402343 T 19880916; FR 8712862 A 19870917