A military firearm may have a flash hider threaded to the end of its barrel. The flash hider is intended to reduce both the primary flash caused by the initial explosion of the powder charge when a round of ammunition is fired, and the secondary flash caused when the partially combusted gases and hot air from the barrel reignite following the shock of meeting the colder air surrounding the end of the barrel. The visible flash is an indication of the marksman's location. Hiding the flash makes it difficult to locate that marksman.
A sound suppressor reduces the sound of a firearm being fired for the same objective for which a flash hider reduces flash, namely, to make it more difficult to detect the location of the marksman. A sound suppressor is inherently a flash hider because it is typically a closed cylinder and thus prevents the flash from being seen while it performs its primary function of suppressing sound.
Both a flash hider and a sound suppressor are typically fitted to the threaded end of the barrel of a firearm.
The present invention is a combination of a flash hider, a sound suppressor and a coupler that holds the sound suppressor to a flash hider. The flash hider does not need to be removed to use the sound suppressor or replaced after the sound suppressor is removed. Furthermore, the coupler enables the suppressor to be attached to the flash hider rather than to the barrel proximate to the flash hider so that the flash hider forms a nozzle at the entrance to the sound suppressor and thereby facilitates the operation of the suppressor. The present coupler also enables the sound suppressor to be removed and installed quickly and securely.
A feature of the present flash hider is that it is characterized by three tines that are slightly tapered, that are long, and that contain stepped features on their sides that face the gaps between the tines. These stepped features expand the distance between the tines for hot gases traveling radially from the central bore of the flash hider and allow those gases to cool quickly. The steps also create turbulent mixing with the cooler air outside the flash hider to reduce the shock of the hot gases hiting the cooler air and to reduce the temperature differential between the two to avoid reignition and the attendant secondary flash.
A feature of the present sound suppressor is that its internal baffle structure moves a portion of the axial flow of high energy gases radially and into a path where those gases cross and re-cross the centerline of the suppressor to turbulently mix with the axial flow and more quickly give up heat to the baffles and to the suppressor housing itself for more effective sound suppression.
A feature of the coupler is that it can be quickly unlocked and rotated clockwise to secure a flash suppressor to a flash hider, or unlocked and rotated counter-clockwise to allow the suppressor to be removed. A spring lock automatically locks the coupler and is unlocked simply by pressing the spring lock handle.
These and other features and their advantages will be apparent to those of ordinary skill in the art from a careful reading the Detail Description of Embodiments accompanied by the following Drawings.
In the figures,
The present device is a quickly-disconnectable sound suppressor for a firearm. The device is also a quick-disconnect flash and sound suppressor for a firearm with a flash hider on the end of its barrel. Finally, the present device is a coupler for attaching a sound suppressor to a flash hider.
Referring now to
Flash hider 12 has a first or proximal end 30 and an opposing second or distal end 32. Flash hider 12 is essentially a tube with a central bore 34 that defines a wall 36. First end 30 has interior threads 38 that allow flash hider 12 to be threaded to the barrel of a firearm (not shown). Flash hider 12 has an exterior surface 40 that carries an annular recess 42 and, distal to recess 42, several flat surfaces 44. Toward its second end 32, wall 36 of flash hider 12 has gaps 46 which define three tines 48.
Tines 48 are long and tapered toward second end 32 and carry at least one step 50 on each side that faces gap 46. A step 50 is a pair of angled changes in the surface of tines 48 that widen the distance from one tine 48 to the next as measured azimuthally, so that, when hot combustion gases from central bore 34 flow radially between tines 48 and through gaps 46, they expand to cool. The side of a tine 48 is initially more or less radially directed. At a step 50, that generally radial direction abruptly angles azimuthally away from the adjacent tine 48 and then returns abruptly to a generally radial direction much like a step in a stairway.
Suppressor 14 is a closed tube with a first or proximal end 60 and an opposing, second or distal end 62. Suppressor 14 may be further defined by a first portion 64 and a second portion 66. First portion is configured to receive flash hider 12 and to be coupled to flash hider 12 by collar 16, as will be explained below.
First portion 64 has an opening 68 dimensioned to receive second end 32 of flash hider 12. First portion 64 of flash hider 64 has an exterior surface 70 with a gear surface 72 at first end 60 followed by a series of annular holes 74 which are followed in turn by exterior threads 76. These three features: gear surface 72, holes 74 and exterior threads enable suppressor to be coupled to flash hider.
To couple, which means in this case to keep flash hider 12 and suppressor 14 locked together, the three camming latches 18 are first placed in annular holes 74 of suppressor. Then collar 16, which has interior threads 90, is slipped over first portion 64 of suppressor, as best seen in
To prevent unintentional movement of collar 16, spring lock 20 prevents its rotation. Spring lock 20, as best seen in
The attachment of a suppressor 14 to a firearm will inevitably affect the ballistic performance of the firearm. There are potentially six orientations of suppressor with respect to flash hider 12 if flat surfaces 44 are six in number such as would be the case if flash hider 12 had a hexagonal cross-section at the point between its first end 30 and its second end 32. One of those six orientations will likely have the least impact on the ballistics and perhaps an impact that is so negligible that the firearm does not have to be re-zeroed. If so, that orientation can be marked by the user so that whenever the suppressor 14 is coupled to the flash hider 12 on the end of that particular firearm, the same rotational orientation of sound suppressor 14 can be obtained.
Inside second portion 66 of sound suppressor 14, best seen in
Blast baffle 120 has a rear surface 130 that acts as a second nozzle in directing a portion of those hot gases passing though central hole 128 radially while a remaining portion continues forward to a first disc baffle of plural disc baffles 132. Each disc baffle 132 is a partial circular disc, with a central hole 134 and a radial opening 136 which may be formed simply by eliminating a section of what would otherwise be a perfectly circular shape. Housing 126 is formed with slots 138 along its length, as best seen in
Those familiar with firearms and their attachments will appreciate that many modifications and substitutions can be made to the foregoing preferred embodiments of the present invention without departing from the spirit and scope of the present invention, defined by the appended claim.
Priority is claimed to U.S. provisional patent application Ser. No. 61/375,530, filed Aug. 20, 2010; to U.S. non-provisional patent application Ser. No. 13/032,804 filed Feb. 23, 2011, which in turn claims priority to U.S. provisional patent application Ser. No. 61/309,047 filed Mar. 1, 2010; to U.S. provisional patent application Ser. No. 61/375,339, filed Aug. 20, 2010; and to U.S. provisional patent application 61/375,620, filed Aug. 20, 2010, all of which are incorporated by reference herein in their entirety.
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