# US 10,480,915 B2 · Method of making a polymeric subsonic ammunition cartridge > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,480,915 B2 - Document ID: US10480915B2 - Status: Granted - Kind: B2 - Application number: 14/725,946 - Filed: 2015-05-29 - Published: 2016-12-01 - Granted: 2019-11-19 - Earliest claimed: 2010-11-10 - Assignees: True Velocity IP Holdings, LLC - Applicants: True Velocity IP Holdings, LLC - Inventors: Lonnie Burrow - Web page: https://patentgrep.com/patent/US10480915B2 ## CPC - F42B 12/745: {the core being made of plastics; Compounds or blends of plastics and other materials, e.g. fillers} - 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}) - F42B 5/307: formed by assembling several elements - F42B 33/001: {Devices or processes for assembling ammunition, cartridges or cartridge elements from parts} - F42B 33/02: Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges {(F42B33/004 takes precedence)} - 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} - F42B: EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION (explosive compositions C06B; fuzes F42C; blasting F42D) - F42C: AMMUNITION FUZES (blasting cartridge initiators F42B3/10; chemical aspects C06C); ARMING OR SAFETY MEANS THEREFOR (filling fuzes F42B33/02; fitting or extracting primers in or from fuzes F42B33/04; containers for fuzes F42B39/30) ## 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 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. ## Claims ### Claim 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 element that extends from the top surface; a primer recess formed in the bottom surface; a primer flash hole aperture positioned in the primer recess to extend through the bottom surface; and a flash hole groove positioned in the primer recess around the primer flash hole aperture; forming a substantially cylindrical polymeric middle body by overmolding the substantially cylindrical primer insert through the primer flash hole aperture into the flash hole groove and extending the overmolding to a substantially cylindrical polymeric coupling region; providing a substantially cylindrical polymeric bullet-end component comprising a substantially cylindrical polymeric coupling end opposite a bullet aperture; inserting a propellant insert into the propellant chamber to reduce the internal volume of the propellant chamber by at least 10% less; coupling the substantially cylindrical polymeric coupling end to the substantially cylindrical polymeric coupling region to form a propellant chamber that extends from the bullet aperture to the primer flash hole; inserting a diffuser into the primer recess; inserting a primer into the primer recess to contact the diffuser; adding a propellant to the propellant chamber; and inserting a projectile in the bullet aperture. ### Claim 2 (depends on 1) The method of claim 1, further comprising the step of inserting a propellant chamber insert into the propellant chamber to reduce the internal volume of the propellant chamber. ### Claim 3 (depends on 2) The method of claim 2, wherein the substantially cylindrical polymeric bullet-end component comprises a shoulder positioned between the substantially cylindrical polymeric coupling end and the bullet aperture. ### Claim 4 (depends on 2) The method of claim 2, wherein the internal volume that is about 10.1, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, or 25% less than the open internal volume of a standard casing of equivalent caliber. ### Claim 5 (depends on 2) The method of claim 2, wherein the propellant chamber 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. ### Claim 6 (depends on 2) The method of claim 2, wherein the propellant chamber contains a propellant volume such that a projectile does not exceed the velocity of 1086 feet per second at standard atmospheric conditions when fired. ### Claim 7 (depends on 2) The method of claim 2, wherein the projectile is secured to the bullet aperture by a mechanical interference, adhesive, ultrasonic welding, the combination of molding in place and adhesive, or hot crimping after molding. ### Claim 8 (depends on 2) The method of claim 2, wherein the substantially cylindrical polymeric middle body 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. ### Claim 9 (depends on 2) The method of claim 2, wherein the substantially cylindrical polymeric bullet-end component 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. ### Claim 10 (depends on 2) The method 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. ### Claim 11 (depends on 2) The method of claim 2, wherein the substantially cylindrical polymeric middle body, the substantially cylindrical polymeric bullet-end component and the propellant insert independently comprise a material selected from the group consisting of polyphenylsulfone, polycarbonate, and polyamide. ### Claim 12 (depends on 2) The method of claim 2, wherein the substantially cylindrical polymeric middle body, the substantially cylindrical polymeric bullet-end component 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. ### Claim 13 (depends on 2) The method of claim 2, wherein the propellant insert has a substantially cylindrical shape or a free formed shape. ### Claim 14 (depends on 2) The method of claim 2, wherein the propellant insert has a one or more ribs extending into the propellant chamber. ### Claim 15 (depends on 2) The method 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. ### Claim 16 (depends on 2) The method of claim 2, wherein the radial cross-section of the propellant chamber is irregular in shape or tapers along its longitudinal length. ### Claim 17 (depends on 2) The method of claim 2, wherein the substantially cylindrical polymeric middle body, the substantially cylindrical polymeric bullet-end component and the propellant insert independently comprise the same polymeric material or different polymeric materials. ### Claim 18 (depends on 2) The method 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. ### Claim 19 (depends on 2) The method of claim 2, further comprising a diffuser ring positioned in the primer recess between the primer and the flash hole groove.