Diverging central bore for firearm sound suppressor
An apparatus and methods are provided for a front plate having a diverging central bore for firearm sound suppressors that improves noise and flash characteristics during firing a weapon. The central bore is disposed between a back surface and a front surface of the front plate. An untapered portion of the central bore extends from the back surface to a diverging portion that opens toward the front surface. The diverging portion includes a curvature profile configured to allow for more controlled expansion of high-pressure propellant gases exiting of the suppressor through the central bore. The curvature profile provides an included angle of the central bore that decreases secondary flash events accompanying the expulsion of propellant gases accompanying a fired bullet exiting the suppressor through the central bore. The curvature profile exhibits a cross-sectional area of the central bore that is proportional to a distance along the diverging portion.
1. A front plate for a suppressor for coupling with a muzzle end of a barrel of a firearm for reducing muzzle blast and eliminating muzzle flash, the front plate comprising:
a central bore disposed between a back surface and a front surface of the front plate;
a converging portion of the central bore extending from the back surface wherein the converging portion extends from a backmost surface of the front plate and meets a diverging portion within an interior of the central bore wherein the backmost surface is disposed proximal of the back surface by an offset distance; and
the diverging portion of the central bore opening toward the front surface wherein the front surface encloses the central bore;
a recess disposed away from the central bore and between an outer lip and the central bore.
2. The front plate of claim 1 , wherein the offset distance gives the central bore an overall nozzle length that is greater than the distance between the back surface and the front surface of the front plate.
3. The front plate of claim 1 , wherein the converging portion comprises a throat area of the central bore at the backmost surface.
4. The front plate of claim 1 , wherein the diverging portion comprises an exit area of the central bore at the front surface.
5. The front plate of claim 4 , wherein desirable expansion, speed, and/or turbulence properties of the propellant gases transiting the central bore can be obtained by manipulating any one or more of the throat area, the exit area, a ratio of throat area to exit area, the offset distance, the overall nozzle length, or any combination thereof.
6. The front plate of claim 4 , wherein the throat area and the exit area are configured to produce a desired ratio between a mass flux of the propellant gases transiting the central bore and the mass flux of the propellant gases exiting an annular exit area comprising peripheral vents surrounding the front plate.
7. The front plate of claim 4 , wherein the throat area and the exit area are configured to produce a desired ratio between a mass flux of the propellant gases transiting the central bore and the mass flux of the propellant gases exiting an annular exit area comprising a plurality of peripheral vents surrounding the central bore.