A subsonic ammunition cartridge casing having an engineered internal volume designed to allow for the introduction of precisely the amount of propellant necessary at precisely the desired location to reproducibly produce the desired projectile velocity and internal pressure is provided. The subsonic
A subsonic ammunition cartridge casing having an engineered internal volume designed to allow for the introduction of precisely the amount of propellant necessary at precisely the desired location to reproducibly produce the desired projectile velocity and internal pressure is provided. The subsonic shell casing has an engineered internal propellant cavity built into the internal body of the casing itself that does not necessarily depend on the introduction of a separate volume reducing device such as tubing, filler, foam filler and the like. This ensures the integrity of the case, does not result in anything being expelled through the muzzle of the weapon other than the projectile, does not have any burning or combusting components, allows for very precise control of the internal volume and thus chamber pressure, and is economical to produce.
대표청구항▼
1. A subsonic ammunition article comprising; a casing defining a generally cylindrical hollow body having a cap at a first end thereof and a caselet at a second end thereof, the caselet having a proximal end defining a body region and a distal end defining a neck region, wherein the cap is interconn
1. A subsonic ammunition article comprising; a casing defining a generally cylindrical hollow body having a cap at a first end thereof and a caselet at a second end thereof, the caselet having a proximal end defining a body region and a distal end defining a neck region, wherein the cap is interconnected with the proximal end of said caselet such that the casing at least partially encloses an internal cavity, and wherein the outer diameter of the caselet narrows from a first diameter at the body region to a second diameter at the neck region;at least one propellant chamber disposed within the internal cavity of the casing, the propellant chamber having an open internal volume that is at least 20% reduced in comparison to the open internal volume of a standard casing of identical caliber;a propellant disposed and confined within said propellant chamber;a primer disposed at the first end of said casing in combustible communication with said propellant;wherein the caselet and the propellant chamber at least partially comprise a polymeric material; andwherein the ratio of the minimum thickness of the wall of the body region of the caselet to the average wall thickness of the neck region of the ammunition casing is greater than 3. 2. The ammunition article according to claim 1 wherein said polymeric material additionally comprises at least one additive selected from the group consisting of plasticizers, lubricants, molding agents, fillers, thermo-oxidative stabilizers, flame-retardants, coloring agents, compatibilizers, impact modifiers, release agents, reinforcing fibers. 3. The ammunition article according to claim 1, additionally comprising one or more projectiles fitted in the second end. 4. The ammunition article according to claim 3, wherein the projectile upon firing does not exceed the velocity of 1086 feet per second at standard atmospheric conditions. 5. The ammunition article according to claim 3, wherein the projectile is secured to the casing by an interconnection selected from the group consisting of mechanical interference, adhesive, ultrasonic welding, the combination of molding in place and adhesive, and hot crimping after the act of molding. 6. The ammunition article according to claim 1, wherein the polymeric material comprises a material selected from the group consisting of polyphenylsulfone, polycarbonate, and polyamide. 7. The ammunition article according to claim 1, wherein the polymeric material comprises a translucent or transparent polymer. 8. The ammunition article according to claim 1, wherein the polymeric material comprises a polymeric material possessing a glass transition temperature of less than 250° C. 9. The ammunition article according to claim 1, wherein the cap and the caselet are joined using one of either a snap fit or threads. 10. The ammunition article according to claim 9, wherein the ammunition article headspace is adjusted by rotating the threads clockwise and/or counterclockwise until a desired headspace distance is reached. 11. The ammunition article according to claim 1, wherein the space defined between the outer wall of the caselet and the wall of the propellant chamber is formed of a solid material. 12. The ammunition article according to claim 1, wherein the propellant chamber has a radial cross-section selected from the group consisting of circular, ovoid, octagonal, hexagonal, triangular, and square. 13. The ammunition article according to claim 1, wherein the radial size of the propellant chamber tapers along its longitudinal direction. 14. The ammunition article according to claim 1, wherein the propellant chamber is formed of a separate restrictor body disposed within the internal cavity of the casing. 15. The ammunition article according to claim 14, wherein the caselet and restrictor body are formed of different polymeric materials. 16. The ammunition article according to claim 14, wherein the caselet and restrictor body are formed from the same polymeric material. 17. The ammunition article according to claim 1, wherein the propellant chamber and caselet are formed of a single integral caselet body. 18. The ammunition article according to claim 17, wherein the single integral caselet body is manufactured from two or more polymeric materials in a blend mixture. 19. The ammunition article according to claim 17, wherein the single integral caselet body is manufactured from two or more polymeric materials in distinct layers. 20. The ammunition article according to claim 17, wherein the cap and the single integral caselet body are joined using one of either a snap fit or threads.
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