Method of making a polymeric subsonic ammunition cartridge

• US 10,048,052 B2
• Filed: 09/24/2015
• Issued: 08/14/2018
• Est. Priority Date: 11/10/2010
• Status: Active Grant

• Current Assignee: Velocity Holdings LLC (Energy Transfer LP)
• Original Assignee: True Velocity, Inc.
• Inventors: Burrow, Lonnie
• Primary Examiner(s): Bergin, James S
• Application Number:
  US14/863,567
• Publication Number:
  US 20170089679A1
• Time in Patent Office: 1,055 Days
• Field of Search: 102466, 102465, 102467, 102470
• CPC Class Codes: F42B 33/001 Devices or processes for assembling ammunition, cartridges or cartridge elements from parts
• CPC Class Codes: F42B 5/16 characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder chemical composition C06B; F42B5/24 takes precedence
• CPC Class Codes: F42B 5/307 formed by assembling several elements
• CPC Class Codes: F42C 19/0807 characterised by the particular configuration of the transmission channels from the priming energy source to the charge to be ignited, e.g. multiple channels, nozzles, diaphragms or filters
• CPC Class Codes: F42C 19/083 characterised by the shape and configuration of the base element embedded in the cartridge bottom, e.g. the housing for the squib or percussion cap

Abstract

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 between 25 and 80% 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.

Claims

1. A method of preparing a polymeric subsonic ammunition comprising the steps of:

providing a substantially cylindrical primer insert comprising a base having a top surface opposite a bottom surface, a substantially cylindrical coupling flange that extends from the top surface, a primer recess in the bottom surface, a flash hole aperture positioned in the primer recess extending through the bottom surface, a flash aperture groove positioned in the primer recess around the flash hole aperture, and an extraction flange positioned about the circumference of the bottom surface;

forming a polymeric middle body by molding at a first end a first polymer composition over the substantially cylindrical coupling flange into the flash hole aperture and into the flash aperture groove and molding a second end comprising a neck coupling region, wherein the first polymer composition extends from the neck coupling region to the flash aperture groove to form the polymeric middle body to form a propellant chamber having a propellant chamber volume;

forming a polymeric bullet-end component from a second polymer composition, wherein the polymeric bullet-end component comprises a polymeric coupling region opposite a bullet aperture separated by a neck region;

positioning a propellant chamber insert in the propellant chamber to reduce the propellant chamber volume by between 25 and 80% to a subsonic propellant chamber volume; and

coupling the neck coupling region to the polymeric coupling region to form a subsonic propellant chamber from the bullet aperture to the primer flash hole aperture.

2. The method of claim 1, wherein the polymeric bullet-end component comprises a shoulder positioned between the substantially cylindrical polymeric coupling end and the bullet aperture.

3. The method of claim 1, wherein the subsonic propellant chamber volume is about 25.1, 25.2, 25.3, 25.4, 25.5, 25.6, 25.7, 25.8, 25.9, 26.0, 26.25, 26.5, 26.75, 27, 27.5, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46, 47, 48, 49, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65, 66, 67, 68, 69, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 80% or incremental variations thereof less than the propellant chamber volume.

4. The method of claim 1, wherein the subsonic propellant chamber volume contains a propellant volume such that a projectile does not exceed a velocity of 1200 feet per second at sea level under standard atmospheric conditions when fired.

5. The method of claim 1, wherein the subsonic propellant volume limits the velocity of a projectile to less than 1086 feet per second at standard atmospheric conditions when fired.

6. The method of claim 1, further comprising the step of securing a projectile to the bullet aperture by a mechanical interference, adhesive, ultrasonic welding, the combination of molding in place and adhesive, or hot crimping after molding.

7. The method of claim 1, wherein the first polymer composition comprises a polymers, copolymers of individual monomers selected from the group consisting of polybutylene terephthalates, 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-butadiene-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 and copolymer mixtures thereof.

8. The method of claim 1, wherein the second polymer composition comprises a polymer, copolymer of individual monomers 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-butadiene-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 method of claim 1, wherein the propellant chamber insert comprises a polymer, copolymer of individual monomers 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-butadiene-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.

10. The method of claim 1, wherein the first polymer composition, the second polymer composition and the propellant insert independently comprise a material selected from the group consisting of polyphenylsulfone, polycarbonate, and polyamide.

11. The method of claim 1, wherein the first polymer composition, the second polymer composition and the propellant insert independently comprise 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.

12. The method of claim 1, wherein the propellant chamber insert has a substantially cylindrical shape.

13. The method of claim 1, wherein the propellant chamber insert has a free formed shape.

14. The method of claim 1, wherein the propellant chamber insert has a one or more ribs extending into the propellant chamber.

15. The method of claim 1, wherein the propellant chamber insert has a radial cross-section selected from the group consisting of circular, ovoid, octagonal, hexagonal, triangular, star, ribbed, square and a combination thereof.

16. The method of claim 1, wherein the radial cross-section of the propellant chamber insert is irregular in shape or tapers along its longitudinal length.

17. The method of claim 1, wherein the polymeric middle body, the polymeric bullet-end component and the propellant chamber insert independently comprise the same polymeric material or different polymeric materials.