EP 1936317 A1 20080625 - Nozzle
Title (en)
Nozzle
Title (de)
Düse
Title (fr)
Buse
Publication
Application
Priority
EP 06126990 A 20061222
Abstract (en)
The invention relates to a nozzle (1) for a weapon (2) comprising a launcher (4) which constitutes a guide for a projectile or missile (6). The nozzle (1) comprises a wall (8), a first opening (10) connected to the launcher (4) and a second opening (12). The area of the first opening (10) is smaller than the area of the second opening (12). The nozzle (1) is provided with means (18; 18') for reducing the pressure of gases (16) from the projectile (6) inside and behind the nozzle (1) when firing the weapon (2). A circumferential element (26) is arranged at the first opening (10) of the nozzle (1). An opening area (28) of the circumferential element (26) is less than the area of the first opening (10) of the nozzle (1).
IPC 8 full level
F41A 1/08 (2006.01); F41F 3/045 (2006.01)
CPC (source: EP US)
F41A 1/08 (2013.01 - EP US)
Citation (applicant)
- SE 0301626 L 20041206 - SAAB AB [SE]
- SE 0301627 L 20041019 - SAAB AB [SE]
Citation (search report)
- [XY] NL 6509893 A 19660131
- [Y] US 2598256 A 19520527 - HICKMAN CLARENCE N
- [Y] DE 1678189 A1 19720113 - BUCKLISCH LUDWIG
- [Y] GB 1213711 A 19701125 - KARLSRUHE AUGSBURG IWEKA [DE]
- [X] US 2557151 A 19510619 - SKINNER LESLIE A, et al
- [DA] EP 1484572 A1 20041208 - SAAB AB [SE]
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
Designated extension state (EPC)
AL BA HR MK RS
DOCDB simple family (publication)
EP 1936317 A1 20080625; EP 1936317 B1 20091111; AT E448459 T1 20091115; DE 602006010422 D1 20091224; ES 2333666 T3 20100225; US 2010275763 A1 20101104
DOCDB simple family (application)
EP 06126990 A 20061222; AT 06126990 T 20061222; DE 602006010422 T 20061222; ES 06126990 T 20061222; US 331907 A 20071221