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Reduced energy MSR system

  • US 10,466,022 B2
  • Filed: 09/25/2018
  • Issued: 11/05/2019
  • Est. Priority Date: 03/25/2016
  • Status: Active Grant
First Claim
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1. A reduced energy cartridge, comprising:

  • a polymer case having a polymer case wall, the polymer case including;

    a generally cylindrical body portion defining a first outer diameter about a longitudinal axis, the body portion including a base portion defining a base lumen;

    a neck portion defining a second outer diameter about the longitudinal axis that is less than the first outer diameter, the neck portion defining a neck lumen; and

    a tapered portion extending between the body portion and the neck portion;

    a projectile including a first portion disposed within the neck lumen and a second portion extending forwardly beyond the polymer case;

    a reinforcement liner including a sleeve portion, a shoulder portion, and a flange portion, wherein;

    the sleeve portion defines one of a right-cylindrical geometry and a tapered-cylindrical geometry from a proximal end of the sleeve portion to a distal end of the sleeve portion, the sleeve portion being disposed at least partially within the base lumen and defining a sleeve lumen that is substantially concentric about the longitudinal axis,the shoulder portion extends radially outward from the proximal end of the sleeve portion and defines a radiused inner surface, andthe flange portion extends from a proximal end of the shoulder portion and extends radially outward and beyond the shoulder portion and extends rearwardly beyond the base portion of the polymer case, the flange portion defining a minimum inner diameter that is the same as an inner diameter of the proximal end of the shoulder portion; and

    a propellant unit disposed within the sleeve lumen, the propellant unit including;

    a housing including a body portion and a hollow rim portion that cooperate to define a cavity, the hollow rim portion being registered against the radiused inner surface of the shoulder portion of the reinforcement liner;

    a propellant charge disposed inside the cavity for producing a quantity of propellant gas; and

    a priming material disposed inside the hollow rim portion for igniting the propellant charge,wherein the propellant unit and reinforcement liner cooperate to define a recess at a proximal end of the reduced energy cartridge,wherein the reduced energy cartridge is a rim fire cartridge.

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