The subject technology relates generally to firearms accessories and specifically to firearm sound suppressors (aka suppressors).
Sound suppressors for firearms are widely known in the gun and shooting sports communities and are used to mitigate the noise associated with the firing of weapons. The theory of sound suppression is founded upon the redirection of a large portion of the gas associated with ignition of a round of ammunition from the muzzle of the firearm. Adding a suppressor at the muzzle of a firearm directs the gases from a fired round into blast chambers formed within the suppressor by a succession of stacked spacer components called baffles. The greater the amount of gas that can be directed to blast chambers within the suppressor and prevented from rapidly exiting the muzzle of the firearm, the greater the degree of achieved suppression of sound.
Unfortunately, the more hot gases that are redirected within the suppressor, the hotter the suppressor gets during operation. This heat presents a problem, especially when using lighter weight metals or composite plastics as components within the device or in connection with the outer tube (aka sleeve) of the suppressor. In one aspect of the subject technology, the structure of the suppressor is configured such that those interior core components that are more susceptible to heat buildup are substantially thermally isolated from the outer tube. A cooling plenum, or air gap, is provided between the core components and outer tube. Additionally, ports in the front and rear end caps are in operative engagement to the air gap, so as to encourage a cooling air flow.
In one aspect of the subject technology, the suppressor is constructed in such a manner so as to create a metallic core assembly that is thermally isolated from an outer sleeve which may be fabricated from carbon fiber or other composite material. The carbon fiber outer sleeve (aka outer tube) has desirable strength and weight characteristics, and is made from carbon fiber cloth or tow weave utilizing a high temperature resistant carbon fiber resin and/or a composite laminate construction that utilizes a layer of ceramic cloth bonded to the carbon fiber cloth to create a thermal barrier.
In one aspect, the subject technology comprises a series of stacked and/or coupled baffles which form a series of blast chambers, one of which may include a flash suppressor, all enclosed within a carbon fiber outer sleeve.
In one aspect of the subject technology, the problem of mitigating the overheating of suppressors is solved by incorporating an outer cooling plenum with induced airflow therein, surrounding a series of stacked and/or coupled baffles, one or more of which acting as blast chambers.
Further features of the inventive aspects will become apparent to those skilled in the art to which the aspects relate from reading the specification and claims with reference to the accompanying drawings, in which:
The general arrangement of a suppressor 1 for a firearm is shown in
In one aspect, core assembly 3 includes six operatively coupled (aka stacked, or placed in a stacked arrangement) baffles 2, primary baffle 12, muzzle adapter 10, blast chamber 8, and front and rear caps 6, 4. Muzzle adapter 10 is operatively connected to blast chamber 8 such that muzzle adapter 10 is radially inside of blast chamber 8. Blast chamber 8 is operatively connected to a first end of primary baffle 12. A second end of primary baffle 12 is operatively connected to the stacked baffles 2 on a first end. A second end of stacked baffles 2 is operatively connected to front cap 6. The foregoing connectivity of blast chamber 8, muzzle adapter 10, primary baffle 12, stacked baffles 2, each individual baffle 2 as connected together to form stacked baffles 2, and front cap 6 can be achieved by threaded connection (e.g.
In some aspects, muzzle adapter 10 is operatively connected to blast chamber 8. In some aspects (
One or more baffles 2 are utilized. Each baffle 2 has a body portion 47, middle portion 50, and front portion 40. The front portion 40 is tapered as shown (e.g.
Each of body portion 47, middle portion 50, and front portion 40 of baffle 2 have exterior and interior surfaces. An interior chamber 48 is formed in baffle 2 and defined by the interior surfaces of body portion 47, middle portion 50, and front portion 40. Each baffle 2 is adapted such that a projectile can enter central hole 46 and travel through interior chamber 48. Through-holes 45 are operatively connected to interior chamber 48. In one aspect, heat sink fins 44 are disposed on an exterior surface 49 of body portion 47 of baffle 2, and on an exterior surface of blast chamber 8, and on an exterior surface of primary baffle 12. Heat sink fins 44 facilitate heat transfer into air gap (aka internal air volume) 23 that is formed when outer sleeve 13 is attached. In one aspect, (e.g.
Primary baffle 12 has a body portion 51. An interior chamber 52 is defined within primary baffle 12 having a tapered front portion 58 through which is disposed a central hole 59 and a plurality of through-holes 60. The plurality of through-holes 60 are disposed similarly to through-holes 45 in baffle 2 as depicted in
A projectile enters into muzzle adapter 10 and travels through muzzle adapter 10 and blast chamber 8, and then through primary baffle 12, and then through the stacked baffles 2, and then through front cap 6, as does the ignited gas that accompanies the projectile. Sound and heat incidental to the ignited gas and projectile are dissipated in core assembly 3. Consequently, core assembly 3 can be dangerously hot to the touch. Outer sleeve 13 is operatively connected to core assembly 3 such that an air gap 23 exists between exterior surfaces of blast chamber 8, primary baffle 12, and stacked baffles 2. Outer sleeve 13 is preferably made from a thermally insulating material and thus is relatively less hot to the touch than core assembly 3. In one aspect, outer sleeve 13 is secured to front cap 6 and rear cap 4 (rear cap 4 may be integral to blast chamber 8) such that air gap 23 exists between core assembly 3 and outer sleeve 13.
Holes 5 are disposed through rear cap 4. Holes 7 are disposed through front cap 6. Holes (aka apertures) 5 & 7 are in fluid communication with, and facilitate heat dissipation from, air gap 23. In one aspect, the size and quantity of holes 5 relative to holes 7 is adjusted so that expanding hot air is directionally induced to create an air flow. Hot expanding air will naturally expand and flow towards a larger opening. This relative size can be achieved by the relative number of holes and/or the relative size of the holes. It should be understood that such inducement can be caused in either direction. In one aspect, the holes in the front cap are larger than the holes in the rear cap thereby inducing airflow in a forward direction.
In one aspect, the distance from the interior surface of outer sleeve 13 and exterior surfaces of blast chamber 8, primary baffle 12, and stacked baffles 2 is approximately 10 mm. As shown in the various figures, holes 5, 7 are disposed through, and circumferentially spaced around an outer portion of each of rear cap 4 and front cap 6. The circumferential placement, hole size, and quantity of holes can be adjusted to affect air flow and heat dissipation.
In one aspect, outer sleeve 13 is made from a carbon fiber cloth or tow weave utilizing a high temperature resistant carbon fiber resin and/or a composite laminate construction that utilizes a layer of ceramic cloth bonded to the carbon fiber cloth to create a thermal barrier. In one aspect, the components comprising core assembly 3 are fabricated from titanium, aluminum or other corrosion resistant material.
In one aspect, the stacked baffles 2 are screwed together in series, the rear-most of which being threadedly connected to a first end of primary baffle 12. A second end of primary baffle 12 is in turn threadedly connected to blast chamber 8.
Referring to
While this invention has been shown and described with respect to a detailed embodiment thereof, it will be understood by those skilled in the art that changes in form and detail thereof may be made without departing from the scope of the claims of the invention.
This application claims priority to U.S. provisional application 62/464,478, filed Feb. 28, 2017, the contents of which are hereby incorporated by reference.
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Number | Date | Country | |
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62464478 | Feb 2017 | US |