Narrowing high strength polymer-based cartridge for blank and subsonic ammunition
First Claim
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1. A high strength polymer-based cartridge for subsonic ammunition comprising:
- a first end having a mouth;
a projectile disposed in the mouth;
a shoulder disposed below the mouth forming a bottleneck cartridge; and
at least a wall, molded from a polymer, between the first end and a second end of the upper component opposite the first end forming a propellant chamber; and
an insert joined to the second end;
wherein the wall comprises a thickness at least 1.25 times greater than a standard thickness of a wall of a standard cartridge,wherein the propellant chamber between the mouth and the insert is unobstructed, andwherein the propellant chamber comprises a powder load having a load density greater than 40%.
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Abstract
A high strength polymer-based cartridge casing includes a cartridge body, molded from a polymer, having a first end and an opposing second end, and enclosing a volume. A bullet is removably engaged with the first end and an insert is engaged to the second end. A shoulder portion is located proximate the first end and a propellant chamber formed in the volume. The propellant chamber has a first diameter proximate to the shoulder, a second diameter proximate to the insert and greater than the first diameter, and a linear slope disposed between the first diameter and the second diameter.
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Citations
4 Claims
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1. A high strength polymer-based cartridge for subsonic ammunition comprising:
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a first end having a mouth; a projectile disposed in the mouth; a shoulder disposed below the mouth forming a bottleneck cartridge; and at least a wall, molded from a polymer, between the first end and a second end of the upper component opposite the first end forming a propellant chamber; and an insert joined to the second end; wherein the wall comprises a thickness at least 1.25 times greater than a standard thickness of a wall of a standard cartridge, wherein the propellant chamber between the mouth and the insert is unobstructed, and wherein the propellant chamber comprises a powder load having a load density greater than 40%. - View Dependent Claims (2, 3, 4)
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Specification