Method of making a polymeric subsonic ammunition cartridge

US11118882B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11118882-B2
Application numberUS-201916519619-A
CountryUS
Kind codeB2
Filing dateJul 23, 2019
Priority dateNov 10, 2010
Publication dateSep 14, 2021
Grant dateSep 14, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

Opening claim text (preview).

What is claimed is: 1. A method of preparing a polymeric subsonic ammunition cartridge 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 substantially cylindrical primer wall that extends from the bottom surface; a substantially cylindrical primer recess is formed by the inner surface of the substantially cylindrical primer wall; a primer flash aperture formed in the substantially cylindrical primer recess extending through the top surface opposite a bottom surface and a groove formed on the circumference of the primer flash aperture; forming a substantially cylindrical polymeric middle body comprising the steps of forming from a polymer composition a substantially cylindrical polymeric coupling region that extends over the substantially cylindrical primer insert and into the primer flash aperture and into the groove to form a flash hole; forming a propellant chamber extending from the substantially cylindrical polymeric coupling region to the primer flash hole; and coupling a substantially cylindrical polymeric bullet-end component to the substantially cylindrical polymeric middle body, wherein the substantially cylindrical polymeric bullet-end component comprises a substantially cylindrical polymeric coupling end opposite a bullet aperture, wherein the substantially cylindrical polymeric coupling end mates to the substantially cylindrical polymeric coupling region and extends the propellant chamber from the bullet aperture to the primer flash hole. 2. The method of claim 1 , further comprising inserting a propellant insert 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. 3. The method of claim 2 , wherein the substantially cylindrical polymeric bullet-end component further comprises a shoulder positioned between the substantially cylindrical polymeric coupling end and the bullet aperture. 4. 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. 5. 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. 6. 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. 7. The method of claim 2 , further comprising the step of inserting a primer into the substantially cylindrical primer recess; inserting propellant into the propellant chamber; and 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. 8. 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. 9. 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. 10. The method of claim 2 , wherein the propellant insertcomprises 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. 11. The method of claim 2 , wherein the substantially cylindrical polymeric middle body, the substantially cylindrical polymeric bullet-end component and the propellant insert independ

Assignees

Inventors

Classifications

  • F42B33/001Primary

    Devices or processes for assembling ammunition, cartridges or cartridge elements from parts · CPC title

  • Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges {(F42B33/004 takes precedence)} · CPC title

  • 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 title

  • F42B12/745Primary

    the core being made of plastics; Compounds or blends of plastics and other materials, e.g. fillers · CPC title

  • formed by assembling several elements · CPC title

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What does patent US11118882B2 cover?
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 prope…
Who is the assignee on this patent?
True Velocity Ip Holdings Llc
What technology area does this patent fall under?
Primary CPC classification F42B33/001. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 14 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).