Subsonic polymeric ammunition cartridge

• US 10,429,156 B2
• Filed: 05/29/2015
• Issued: 10/01/2019
• Est. Priority Date: 11/10/2010
• Status: Active Grant

• Current Assignee: Velocity Holdings LLC (Centerpoint Energy Incorporated)
• Original Assignee: Velocity Holdings LLC (Centerpoint Energy Incorporated)
• Inventors: Burrow, Lonnie
• Primary Examiner(s): Freeman, Joshua E
• Assistant Examiner(s): Cochran, Bridget A
• Application Number:
  US14/725,699
• Publication Number:
  US 20160349023A1
• Time in Patent Office: 1,586 Days
• Field of Search: 102466
• CPC Class Codes: F42B 5/307 formed by assembling several elements

Abstract

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 at least 10% 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.

Claims

1. A subsonic ammunition cartridge comprising:

a primer insert comprising

a top surface opposite a bottom surface,

a substantially cylindrical coupling element that extends from the bottom surface,

a primer recess in the top surface that extends toward the bottom surface,

a primer flash aperture positioned in the primer recess to extend through the bottom surface, and

a flash aperture groove positioned in the primer recess around the primer flash aperture;

a polymer mid-body that extends from a projectile end over the substantially cylindrical coupling element and into the primer flash aperture and into the flash aperture groove to form a flash hole;

a substantially cylindrical open-ended polymeric bullet-end connected to the projectile end and extending to a shoulder and terminating at a forward end opening; and

a propellant chamber formed between the forward end opening and the bottom surface.

2. The subsonic ammunition cartridge of claim 1, further comprising a propellant chamber insert into the propellant chamber to reduce the internal volume of the propellant chamber.

3. The subsonic ammunition cartridge of claim 2, wherein the internal volume is reduced by about 10, 10.5, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, or 25%.

4. The subsonic ammunition cartridge of claim 2, wherein the internal volume does not contain enough of a propellant for a projectile to exceed the velocity of 1200 feet per second at sea level under standard atmospheric conditions when fired.

5. The subsonic ammunition cartridge of claim 2, wherein the internal volume does not contain enough of a propellant for a projectile to exceed the velocity of 1086 feet per second at standard atmospheric conditions when fired.

6. The subsonic ammunition cartridge of claim 2, wherein the polymer body comprises a material selected from the group consisting of polyphenylsulfone, polycarbonate, and polyamide.

7. The subsonic ammunition cartridge of claim 2, wherein the polymeric casing body and the substantially cylindrical open-ended polymeric bullet-end independently comprise a polymers selected from the group consisting of polyurethane prepolymer, cellulose, fluoro-polymer, ethylene inter-polymer alloy elastomer, ethylene vinyl acetate, nylon, polyether imide, polyester elastomer, polyester sulfone, polyphenyl amide, polypropylene, polyvinylidene fluoride or thermoset polyurea elastomer, acrylics, homopolymers, acetates, copolymers, acrylonitrile-butadinen-styrene, thermoplastic fluoro polymers, inomers, polyamides, polyamide-imides, polyacrylates, polyatherketones, polyaryl-sulfones, polybenzimidazoles, polycarbonates, polybutylene, terephthalates, polyether imides, polyether sulfones, thermoplastic polyimides, thermoplastic polyurethanes, polyphenylene sulfides, polyethylene, polypropylene, polysulfones, polyvinylchlorides, styrene acrylonitriles, polystyrenes, polyphenylene, ether blends, styrene maleic anhydrides, polycarbonates, allyls, aminos, cyanates, epoxies, phenolics, unsaturated polyesters, bismaleimides, polyurethanes, silicones, vinylesters, urethane hybrids, polyphenylsulfones, copolymers of polyphenylsulfones with polyethersulfones or polysulfones, copolymers of poly-phenylsulfones with siloxanes, blends of polyphenylsulfones with polysiloxanes, poly(etherimide-siloxane) copolymers, blends of polyetherimides and polysiloxanes, and blends of polyetherimides and poly(etherimide-siloxane) copolymers.

8. The subsonic ammunition cartridge of claim 2, wherein the propellant insert comprises a polymers selected from the group consisting of polyurethane prepolymer, cellulose, fluoro-polymer, ethylene inter-polymer alloy elastomer, ethylene vinyl acetate, nylon, polyether imide, polyester elastomer, polyester sulfone, polyphenyl amide, polypropylene, polyvinylidene fluoride or thermoset polyurea elastomer, acrylics, homopolymers, acetates, copolymers, acrylonitrile-butadinen-styrene, thermoplastic fluoro polymers, inomers, polyamides, polyamide-imides, polyacrylates, polyatherketones, polyaryl-sulfones, polybenzimidazoles, polycarbonates, polybutylene, terephthalates, polyether imides, polyether sulfones, thermoplastic polyimides, thermoplastic polyurethanes, polyphenylene sulfides, polyethylene, polypropylene, polysulfones, polyvinylchlorides, styrene acrylonitriles, polystyrenes, polyphenylene, ether blends, styrene maleic anhydrides, polycarbonates, allyls, aminos, cyanates, epoxies, phenolics, unsaturated polyesters, bismaleimides, polyurethanes, silicones, vinylesters, urethane hybrids, polyphenylsulfones, copolymers of polyphenylsulfones with polyethersulfones or polysulfones, copolymers of poly-phenylsulfones with siloxanes, blends of polyphenylsulfones with polysiloxanes, poly(etherimide-siloxane) copolymers, blends of polyetherimides and polysiloxanes, and blends of polyetherimides and poly(etherimide-siloxane) copolymers.

9. The subsonic ammunition cartridge of claim 2, further comprising 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 and reinforcing agents.

10. The subsonic ammunition cartridge of claim 2, wherein the propellant insert has a substantially cylindrical shape or a free formed shape.

11. The subsonic ammunition cartridge of claim 2, wherein the propellant insert has a one or more ribs extending into the propellant chamber.

12. The subsonic ammunition cartridge of claim 2, wherein the propellant insert has a radial cross-section selected from the group consisting of circular, ovoid, octagonal, hexagonal, triangular, star, ribbed, square and a combination thereof.

13. The subsonic ammunition cartridge of claim 2, wherein the radial cross-section of the propellant chamber is irregular along its longitudinal length.

14. The subsonic ammunition cartridge of claim 2, wherein the radial size of the propellant chamber tapers along its longitudinal direction.

15. The subsonic ammunition cartridge of claim 2, wherein the polymeric casing body and propellant insert are formed of different polymeric materials.

16. The subsonic ammunition cartridge of claim 2, wherein the polymeric casing body and propellant insert are formed of the same polymeric materials.

17. The subsonic ammunition cartridge of claim 2, wherein the propellant chamber is formed of a separate propellant insert disposed within the internal cavity of the generally cylindrical hollow polymer body.

18. An ammunition case subsonic propellant insert comprising:

a polymeric propellant insert adapted to fit in a propellant chamber of an ammunition case to reduce an internal volume by at least 10% that of a standard casing of equivalent caliber.

19. The ammunition case subsonic propellant insert of claim 18, wherein the polymeric propellant insert comprise a polymers selected from the group consisting of polyurethane prepolymer, cellulose, fluoro-polymer, ethylene inter-polymer alloy elastomer, ethylene vinyl acetate, nylon, polyether imide, polyester elastomer, polyester sulfone, polyphenyl amide, polypropylene, polyvinylidene fluoride or thermoset polyurea elastomer, acrylics, homopolymers, acetates, copolymers, acrylonitrile-butadinen-styrene, thermoplastic fluoro polymers, inomers, polyamides, polyamide-imides, polyacrylates, polyatherketones, polyaryl-sulfones, polybenzimidazoles, polycarbonates, polybutylene, terephthalates, polyether imides, polyether sulfones, thermoplastic polyimides, thermoplastic polyurethanes, polyphenylene sulfides, polyethylene, polypropylene, polysulfones, polyvinylchlorides, styrene acrylonitriles, polystyrenes, polyphenylene, ether blends, styrene maleic anhydrides, polycarbonates, allyls, aminos, cyanates, epoxies, phenolics, unsaturated polyesters, bismaleimides, polyurethanes, silicones, vinylesters, urethane hybrids, polyphenylsulfones, copolymers of polyphenylsulfones with polyethersulfones or polysulfones, copolymers of poly-phenylsulfones with siloxanes, blends of polyphenylsulfones with polysiloxanes, poly(etherimide-siloxane) copolymers, blends of polyetherimides and polysiloxanes, and blends of polyetherimides and poly(etherimide-siloxane) copolymers.