Polymeric Subsonic Cartridge with Nested Propellant Insert

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Solution Overview

Problem

Traditional methods for producing subsonic ammunition result in issues such as inconsistent propellant burn, reduced accuracy, and failure to efficiently cycle semi-automatic or fully automatic weapons due to the empty volume in the propellant chamber, leading to variations in velocity and potential weapon jamming.

Innovation Solution

A method involving a polymeric subsonic ammunition casing with a reduced propellant chamber volume, achieved by incorporating a propellant insert that reduces the internal volume of the propellant chamber by 25-80% compared to standard casings, utilizing a polymeric middle body and bullet-end component with a primer insert and propellant chamber design that includes ribs and a diffuser to manage pressure and ignition.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If the propellant chamber volume is reduced to achieve subsonic velocities, then the projectile velocity is reduced to subsonic range, but the empty volume causes inconsistent propellant burn and reduced accuracy

Engineering Contradiction:
Improveprojectile velocityVSAvoidpropellant burn consistency
Core Design Contradiction:
SpeedVSReliability

Solution Approach 1:

A propellant insert is nested within the propellant chamber, occupying the empty space between the propellant charge and the chamber walls. This nested structure eliminates the harmful empty volume while maintaining the reduced propellant quantity needed for subsonic velocities, ensuring consistent propellant burn and improved accuracy.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The propellant insert acts as an intermediary element that mediates between the reduced propellant charge and the propellant chamber walls. It provides a physical barrier that prevents propellant migration and ensures uniform burning, resolving the inconsistency caused by the empty volume.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Speed

If the propellant charge is reduced to achieve subsonic velocities, then the projectile velocity is reduced, but the empty volume causes propellant detonation due to high burn rates

Engineering Contradiction:
Improveprojectile velocityVSAvoidpropellant detonation
Core Design Contradiction:
SpeedVSObject-affected harmful factors

Solution Approach 1:

The propellant insert is nested within the propellant chamber to eliminate empty space, preventing propellant migration and ensuring uniform burn rates. This prevents the high burn rates that lead to detonation while maintaining subsonic velocities.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The propellant insert is positioned beforehand to cushion and contain the propellant charge, preventing it from migrating or burning too rapidly. This pre-positioned structure prevents detonation by ensuring controlled, uniform burn rates.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

3Speed

If the propellant charge is reduced to achieve subsonic velocities, then the projectile velocity is reduced, but the chamber pressure is insufficient to cycle semi-automatic or fully automatic weapons

Engineering Contradiction:
Improveprojectile velocityVSAvoidchamber pressure
Core Design Contradiction:
SpeedVSStress or pressure

Solution Approach 1:

The propellant insert changes the physical parameters of the propellant chamber by reducing the effective volume and altering the burn surface area. This increases the chamber pressure and gas volume generated during combustion, enabling reliable cycling of semi-automatic and fully automatic weapons while maintaining subsonic projectile velocities.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The nested propellant insert structure optimizes the combustion chamber geometry, increasing pressure efficiency. This allows the reduced propellant charge to generate sufficient chamber pressure for weapon cycling despite the lower velocity requirement.

Inventive Principle:
Principle #7Nested doll (Nesting)

4Speed

If traditional methods are used to reduce propellant charge for subsonic ammunition, then the velocity is reduced, but the empty volume requires complex solutions such as inert fillers, expandable inner sleeves, or foamed inserts

Engineering Contradiction:
Improveprojectile velocityVSAvoidcartridge structure
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The propellant insert is a simple nested structure that occupies the empty space in the propellant chamber. This straightforward nested design eliminates the need for complex inert fillers, expandable sleeves, or foamed inserts, reducing cartridge structure complexity while effectively eliminating empty volume.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The invention extracts the problematic empty volume from the propellant chamber by introducing a simple propellant insert. This extracted approach eliminates the need for complex multi-component solutions, simplifying the overall cartridge structure.

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS10048052B2Method of making a polymeric subsonic ammunition cartridge
Publication Date: 2018.08.14 TRUE VELOCITY IP HOLDINGS LLC
  • US10048052B2 patent drawing
  • US10048052B2 patent drawing
  • US10048052B2 patent drawing

AI summary

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.