The present disclosure relates to flash suppressors. More specifically, the present disclosure relates to sound and flash suppressors such as those disclosed and described in U.S. Pat. No. 8,490,535.
A flash and sound suppressor is intended to conceal the location of a gun when fired. The sound of the firing of a gun and the muzzle flash may pinpoint the location of the gun and provoke a response from an enemy. A suppressor should reduce the sound and limit the flash. It should also not interfere with the trajectory of the bullet.
An improved suppressor is disclosed in commonly-owned U.S. Pat. No. 8,490,535, which is incorporated herein in its entirety by reference.
According to its major aspects and briefly recited, the present disclosure describes a sound suppressor for a firearm. The suppressor includes a housing having an axis, a proximal end and an opposing distal end. Plural baffles are inside the housing, each of them having a central hole. A portion of each baffle is spaced in part from the interior surface of the housing to define a radial gap.
The proximal end of the housing carries an inlet nozzle that covers the proximal end of the housing. The inlet nozzle includes a flared orifice. The space between the inlet nozzle and the plurality of baffles defines a first expansion chamber.
An end cap is carried by and covers the distal end of the housing. The end cap has a proximal surface and a distal surface and an exit hole formed through the end cap for a bullet to pass. The exit hole is shaped so as to include a plurality of grooves that radiate from the proximal surface of the end cap and increase toward the exit hole at the distal surface. The spacing between the proximal surface of the end cap and the plurality of baffles defines a second expansion chamber. This second expansion chamber is smaller than the first expansion chamber.
A feature of the disclosed suppressor is that the radial gaps of any two sequential baffles are not aligned but are rotated with respect to each other by an azimuthal angle.
Another feature of the disclosed suppressor is that the edge of the baffle at the radial gap is beveled.
Other features of the disclosed suppressor are that the baffle has a proximal face and a distal face, and that the proximal face is perpendicular to the axis of the housing but the distal face is not perpendicular to the axis of the housing. Moreover, a portion of the proximal face includes a stepped area resulting in a greater thickness of the baffle at a first portion of the central hole of the baffle and wherein a second portion of the baffle is thinner than the first portion and is thinner at a second portion of the central hole.
The proximal surface of the end cap has a toroidal shape, that is, its inner surface being concave and curved in a toroidal depression around the exit hole of the end cap. The proximal surface of end cap at exit hole is beveled and the distal surface of end cap at each radial groove forms a hemispherical depression.
Those familiar with the art of suppressors and other components for firearms will take note of these and other features and their advantages of the present disclosure in a careful reading the following detailed description accompanied by the drawings.
In the drawings,
Referring now to the figures, there is shown a sound suppressor 10 for a firearm. Sound suppressor 10 reduces the decibel level of sound when the firearm fires a round of ammunition from the level it would be without suppressor 10 and may reduce the visibility of the flash that would otherwise occur at the muzzle end of a firearm 12 compared to that without suppressor 10.
Suppressor 10 includes a housing 14, which has a major axis A parallel to and coaxial with its long dimension, and which housing 14 may be tubular in shape. Housing 14 may be made of a metal or a ceramic material. Suppressor 10 has proximal end 16 and an opposing, distal end 18, with the term proximal end 16 used herein to mean relatively nearer to firearm 12 (
As best seen in
At proximal end 16 of housing 14, there is an inlet nozzle 36 covering the proximal end 16 of housing 14. Inlet nozzle 30 has a flared orifice 44. Inlet nozzle 36 and the plurality of baffles 20 define a first expansion chamber 48 between them.
An end cap 52 covers the distal end 18 of housing 14, as seen in
The plurality of baffles 20 and inner surface 56 of end cap 52 define a second expansion chamber 72 between them. Second expansion chamber 72 is shorter than first expansion chamber 48, which means that the length of second expansion chamber 72 along axis A is less than the length of first expansion chamber 48 along axis A. Therefore, the volume of second expansion chamber 72 is less than that of first expansion chamber 48.
A feature of the disclosed suppressor 10 is that any two adjacent baffles 20 are rotated by an azimuthal angle with respect to each other so that radial gaps 28 of those adjacent baffles 20 are not aligned. If 14 housing defines a cylindrical coordinate system with the z-direction coincident with the major axis A and the radial direction is radial with respect to axis A, and with the housing at a fixed radius from the axis A, then a third orthogonal dimension is given by the azimuthal angle with respect an arbitration initial radius extending perpendicular to axis A. The rotation of baffle 20 about axis A with respect to an adjacent baffle 20 may be 180 degrees, as shown in
Baffle 20 has a proximal face 76 closer to proximal end 16 and a distal face 80 facing away from proximal end 16 and closer to distal end 18 of housing 14 of suppressor 10. Proximal face 76 and distal face 80 are generally perpendicular to axis A of housing 14, however, distal face 80 is at an angle slightly smaller than perpendicular, so that said distal face 80 leans toward said proximal end 16. Accordingly as combustion gases pass through radial gap 28 in between the immediate baffle 20 and the next baffle 20, the volume between the immediate and next baffles 20 increases drawing the gases across axis A in a serpentine path and toward the next radial gap 28. In addition, proximal face 76 has a first portion 84 and a second portion 88 that lie in different planes, namely, first portion 84 may be perpendicular to axis A; second portion 88 is not perpendicular to axis A but is nearly perpendicular to first portion 84, as best seen in
Radial gap 28 is an opening between a portion of baffle 20 and a portion of housing 14 wherein the portion of baffle 20 is radially displaced from the portion of housing 14 to define a radial gap 24. At that portion, baffle 20 has an edge 100 and there, the interior surface housing 14, thereby leaving a gap between edge 102 of baffle 20 and housing 14 where baffle 20 and housing 14 separate. Edge 100 may also be beveled.
Beveled edge 100 is formed to channel combustion gases from baffles 20. Also, second portion 88 of proximal face 76 of baffle 20 is not perpendicular to axis A but leans slightly toward inlet nozzle 36 away from radial gap 28 beginning at edge 102 in order to urge relatively more combustion gas toward radial gap 28. The relative sizes of first portion 84 and second portion 88 determines the amount of gas that flow through central hole 22 compared to radial gap 28.
Inner surface 46 of end cap 46 has a toroidal shape, that is, inner surface 46 has a concave depression formed therein that is circular about exit hole 64 and is deeper between exit hole 64 and housing 14 and shallower toward exit hole 64 and housing 14. Inner surface 46 is formed in this toroidal shape to turn combustion gases moving from inlet nozzle 30 to end cap 42 back for mixing in second expansion chamber 72 before venting at exit hole 54.
Outer surface 56 of end cap 52 has plural radial grooves 68 formed in it, with three grooves 68 shown in in
First expansion chamber 48, defined by the space between inlet nozzle 36 and baffles 20 and is larger than second expansion chamber 72, which is defined by the space between baffles 20 and end cap 52. First expansion chamber 38 is larger than second expansion chamber 72 because of the need to accommodate the greater speed and volume of the combustion gases flowing into first expansion chamber 38. Those gases expand into first expansion chamber 48 as they pass from nozzle 36, thereby commencing to cool. Baffles 20 then divide the combustion gases between so that some flow through central holes 24 following the fired bullet and others are directed by baffles 20 through radial gap 28, which is larger than central hole 24. Because each successive baffle 20 is rotated by an azimuthal angle with respect to the previous one, combustion gases repeatedly cross and re-cross the axis of housing 14 mixing with and calving off additional combustion gases that have flowed through central hole 24, gradually transferring the heat they hold to housing 14 directly and through baffles 20 so that suppressor 10 acts as a heat exchanger to cool the combustion gases prior to exit.
End cap 52 uses its inner surface 56 to increase residency time and mixing of combustion gases prior to their exit through exit hole 64. From exit hole 64 hole, combustion gases expand radially through grooves 58 for additional, radial dispersion and separation. Sound is reduced and flash is reduced
Those skilled in the art of firearm suppressors will appreciate that many modifications and substitutions may be made in the foregoing embodiments without departing from the spirit and scope of the present disclosure, which is defined by the appended claims.
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