Method of making polymeric subsonic ammunition

Patent metadata

Field	Value
Publication number	US-2016377399-A1
Application number	US-201514751973-A
Country	US
Kind code	A1
Filing date	Jun 26, 2015
Priority date	Nov 10, 2010
Publication date	Dec 29, 2016
Grant date	—

Abstract

The present invention provides a method of making a subsonic ammunition 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

What is claimed is:

1 . A method of making a polymeric subsonic ammunition having a substantially cylindrical metal primer insert comprising the steps of:
providing a substantially cylindrical insert comprising a top surface opposite a bottom surface and a substantially cylindrical coupling element that extends from the bottom surface to form a circumferential surface, a primer recess in the top surface that extends toward the bottom surface, a primer flash hole aperture positioned in the primer recess to extend through the bottom surface, and a flange that extends circumferentially about an outer edge of the top surface; forming a substantially cylindrical polymeric middle body comprising the steps of overmolding a polymer composition over the substantially cylindrical insert by molding the polymer composition over the substantially cylindrical coupling element, over the circumferential surface, forming a substantially cylindrical polymeric middle body extending from the substantially cylindrical insert, and forming a substantially cylindrical polymeric coupling end at the end of the substantially cylindrical polymeric middle body; forming a propellant insert 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; forming a substantially cylindrical open-ended polymeric bullet-end component comprising the steps of forming a polymeric bullet-end coupling component opposite a bullet-end aperture from a second polymer composition, wherein the polymeric bullet-end coupling component mates to the substantially cylindrical polymeric coupling end; adhering the polymeric bullet-end coupling component mates to the substantially cylindrical polymeric coupling end to form a propellant chamber having a bullet-end aperture opposite a primer flash hole; inserting a primer insert into the primer flash hole aperture; at least partially filling the propellant chamber with a propellant; and frictionally fitting a projectile in the bullet-end aperture, wherein the primer, the propellant and the bullet form a sealed propellant chamber.

2 . The method of claim 1 , wherein the polymer composition extends at least partially into the primer flash hole aperture to form a primer flash hole.

3 . The method of claim 1 , wherein the polymer composition does not extend into the primer flash hole aperture which forms a primer flash hole.

4 . The method of claim 1 , wherein the propellant insert is formed as part of the substantially cylindrical polymeric middle body.

5 . The method of claim 1 , wherein the propellant insert is formed as a separate portion and inserted into the substantially cylindrical polymeric middle body.

6 . The method of claim 1 , wherein the substantially cylindrical open-ended polymeric bullet-end component comprises a shoulder positioned between the substantially cylindrical polymeric bullet-end and the bullet-end aperture and a neck positioned between the shoulder and the bullet-end aperture.

7 . The method of claim 1 , 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.

8 . The method of claim 1 , wherein the substantially cylindrical primer insert further comprises a flash hole groove formed about the primer aperture on the bottom surface and the polymer extends over the substantially cylindrical inner surface to the flash hole groove to form a primer flash hole.

9 . The method of claim 1 , 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.

10 . The method of claim 1 , 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.

11 . The method of claim 1 , wherein the projectile is secured to the bullet aperture by a mechanical interference, adhesive, ultrasonic welding, the combination of molding in place, bonding, welding, gluing, adhesive, or hot crimping after molding.

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

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

14 . The method of claim 1 , wherein the 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.

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

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

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

18 . The method of claim 1 , 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.

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

20 . The method of claim 1 , 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.

21 . The method of claim 1 , wherein the propellant chamber is formed of a separate propellant insert disp

Assignees

• True Velocity Inc

Inventors

• Burrow Lonnie

Classifications

• F42B33/0207

  Processes for loading or filling propulsive or explosive charges in containers · CPC title

• F42B33/001 Primary

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

• F42C19/0807

  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 title

• F42B33/02

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

• F42C19/083

  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 · CPC title