FIELD: weapons and ammunition.
SUBSTANCE: proposed device comprises cylindrical tube with open front end and rear wall composed by detachable cover. Concentric stiffness ribs are arranged at cover outer surface. Detachable cover is fastened with the tube by quick-release locks in amount of at least two secured to cylindrical tube outer surface via diametrically opposite hooks made at detachable cover front stiffness ribs. Cylindrical surface is made on cylindrical tube inner surface to thrust against appropriate conical surface of stabiliser unit obturator. Shaped ledges made at detachable cover wall inner surface are arranged in appropriate cavities of stabiliser unit support.
EFFECT: higher reliability, simplified design, ease of fitting in and out of place.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
PROTECTION DEVICE OF SHELL STABILISER UNIT | 2010 |
|
RU2426065C1 |
ROCKET | 2002 |
|
RU2202761C1 |
DEVICE FOR SECURING DETACHABLE SIGHT FOR HUNTING GUN | 1987 |
|
RU1501662C |
CONSTRUCTION OF HYPERSONIC PROJECTILE WITH SELF-PRESSURIZING COMPRESSIVE DETONATION JET ENGINE HAVING HIGH WORKING PRESSURE AND USING HIGH EXPLOSIVE CHARGE FOR PROPULSION | 2005 |
|
RU2325614C2 |
CASE FOR ARTILLERY SHELL | 2000 |
|
RU2169342C1 |
GLIDING AMMUNITION | 2012 |
|
RU2509287C1 |
GUIDED MISSILE LAUNCHING DEVICE | 1997 |
|
RU2114371C1 |
FAST-RELEASE SILENCER | 2012 |
|
RU2494333C1 |
SHAPED-CHARGE AMMUNITION | 1996 |
|
RU2110753C1 |
TRANSPORT-LAUNCHING PACK FOR ROCKETS AND METHOD OF ITS MANUFACTURE | 2000 |
|
RU2166166C1 |
Authors
Dates
2014-08-27—Published
2013-04-09—Filed