F42B5/16

Subsonic polymeric ammunition cartridge
11248885 · 2022-02-15 · ·

The present invention provides a subsonic ammunition cartridge including a polymeric casing body comprising a generally cylindrical hollow polymer body having a body base at a first end thereof and a mouth at a second end to define a propellant chamber; a propellant insert positioned in the propellant chamber to reduce the internal volume of the propellant chamber, wherein the propellant chamber has an internal volume that is between 25 and 80% less than the open internal volume of a standard casing of equivalent caliber; and a primer insert positioned at the body base and in communication with the propellant chamber.

Subsonic polymeric ammunition cartridge
11248885 · 2022-02-15 · ·

The present invention provides a subsonic ammunition cartridge including a polymeric casing body comprising a generally cylindrical hollow polymer body having a body base at a first end thereof and a mouth at a second end to define a propellant chamber; a propellant insert positioned in the propellant chamber to reduce the internal volume of the propellant chamber, wherein the propellant chamber has an internal volume that is between 25 and 80% less than the open internal volume of a standard casing of equivalent caliber; and a primer insert positioned at the body base and in communication with the propellant chamber.

Cartridge System
20210396502 · 2021-12-23 ·

A cartridge for improving explosive dynamics of ammunition. The cartridge comprises a casing comprising a powder chamber. The powder chamber comprising a powder chamber length among a plurality of inner chambers. The plurality of inner chambers comprise at least a first chamber, and a second chamber. The casing comprises a powder chamber casing portion comprising a portion of the casing wrapped around side portions of the powder chamber. A cartridge chamber inner wall comprises an inner portion of the powder chamber casing portion. The powder chamber casing portion comprises a plurality of thicknesses which comprise at least a first thickness and a second thickness.

Cartridge System
20210396502 · 2021-12-23 ·

A cartridge for improving explosive dynamics of ammunition. The cartridge comprises a casing comprising a powder chamber. The powder chamber comprising a powder chamber length among a plurality of inner chambers. The plurality of inner chambers comprise at least a first chamber, and a second chamber. The casing comprises a powder chamber casing portion comprising a portion of the casing wrapped around side portions of the powder chamber. A cartridge chamber inner wall comprises an inner portion of the powder chamber casing portion. The powder chamber casing portion comprises a plurality of thicknesses which comprise at least a first thickness and a second thickness.

Lightweight cartridge case

The present invention discloses a lightweight hybrid cartridge case (100) for a cartridged ammunition and a method of manufacture (200). The lightweight hybrid cartridge case (100) includes a cap (110) with a cylindrical sidewall (112) connected a base (120); a polymer shell (150) is insert-molded onto the sidewall of the cap; and an overmolded sleeve (180) is formed to cover the metal-polymer joint between the cap (110) and the polymer sleeve (150). The cylindrical sidewall (112) covered by the overmolded sleeve (180) has a plurality of stepped ridges (132, 132a), preferably with one stepped ridge (133) having a C-stepped edge (134).

Lightweight cartridge case

The present invention discloses a lightweight hybrid cartridge case (100) for a cartridged ammunition and a method of manufacture (200). The lightweight hybrid cartridge case (100) includes a cap (110) with a cylindrical sidewall (112) connected a base (120); a polymer shell (150) is insert-molded onto the sidewall of the cap; and an overmolded sleeve (180) is formed to cover the metal-polymer joint between the cap (110) and the polymer sleeve (150). The cylindrical sidewall (112) covered by the overmolded sleeve (180) has a plurality of stepped ridges (132, 132a), preferably with one stepped ridge (133) having a C-stepped edge (134).

Device for controlling a rate of gas pressure increase in a gun barrel
11199383 · 2021-12-14 ·

A device is disclosed for controlling a rate of gas pressure increase generated by a propellant for propelling a projectile from an upstream towards a downstream end of a gun barrel. The device includes a first surface area defined by the propellant and a deterrent applied to a second surface area defined by the first surface area, the second surface area being less than the first surface area. The arrangement is such that the second surface area defines a deterrent free third surface area of the propellant. A primer is operatively disposed relative to the third surface area such that when the primer is activated, the third surface area of the propellant is ignited. The arrangement is such that firstly, while the third surface area is burning and generating gas between the upstream end of the gun barrel and the projectile, the rate of gas pressure increase begins to propel the projectile towards the downstream end of the gun barrel. Secondly, the third surface area of the propellant while burning exposes a progressively increasing surface area of the propellant for burning together with an associated increased generation of gas, the increasing surface area of the propellant defining a concave crater, the crater having a wall which progressively increases in surface area during the burning such that the rate of increase in gas pressure continues to increase for accelerating the projectile towards the downstream end of the gun barrel.

Device for controlling a rate of gas pressure increase in a gun barrel
11199383 · 2021-12-14 ·

A device is disclosed for controlling a rate of gas pressure increase generated by a propellant for propelling a projectile from an upstream towards a downstream end of a gun barrel. The device includes a first surface area defined by the propellant and a deterrent applied to a second surface area defined by the first surface area, the second surface area being less than the first surface area. The arrangement is such that the second surface area defines a deterrent free third surface area of the propellant. A primer is operatively disposed relative to the third surface area such that when the primer is activated, the third surface area of the propellant is ignited. The arrangement is such that firstly, while the third surface area is burning and generating gas between the upstream end of the gun barrel and the projectile, the rate of gas pressure increase begins to propel the projectile towards the downstream end of the gun barrel. Secondly, the third surface area of the propellant while burning exposes a progressively increasing surface area of the propellant for burning together with an associated increased generation of gas, the increasing surface area of the propellant defining a concave crater, the crater having a wall which progressively increases in surface area during the burning such that the rate of increase in gas pressure continues to increase for accelerating the projectile towards the downstream end of the gun barrel.

METHOD OF MAKING POLYMER AMMUNITION HAVING A WICKING TEXTURING
20210381813 · 2021-12-09 · ·

One embodiment of the present invention provides a making a polymeric ammunition having wicking texturing about the projectile end.

METHOD OF MAKING A POLYMERIC SUBSONIC AMMUNITION CARTRIDGE
20210372754 · 2021-12-02 · ·

The present invention provides a method of making a subsonic ammunition cartridge having a polymeric casing body having a generally cylindrical hollow polymer body having a body base at a first end thereof and a mouth at a second end to define a propellant chamber; a propellant insert positioned in the propellant chamber to reduce the internal volume of the propellant chamber, wherein the propellant chamber has an internal volume that is at least 10% less than the open internal volume of a standard casing of equivalent caliber; and a primer insert positioned in the body base and in communication with the propellant chamber.