Patent Application
20080148928
1. Field of the Invention
The invention relates to an improved firearm suppressor. The invention also relates to a mounting system and a mounting method.
2. Description of the Related Art
Firearm suppressors are intended to reduce the nerve racking, shooter revealing, and ear damaging effects of muzzle sound, muzzle blast, visible muzzle flash and invisible infrared flash of firearms. The confusion and chaos of close-quarters combat is worsened by multidirectional unexpected muzzle blasts. The futile use of earplugs only restricts communication, reduces group unity and lessens awareness of the surroundings. The problem must be attacked at its source, which is the muzzle.
No suppressor can be effective unless it can first “contain the explosion” of the propellant gases. The prior art baffles form small, partially or non-vented, symmetrical, concave walled compartments which create perfect “reflection contours.” The reflected waves return and even focus the pressure energy back into the lumen for instant escape from the muzzle. The minor turbulences created by those prior art baffles do little to effectively suppress any significant energy. They pressurize quickly and pass the remaining gases and energy straight through “unaltered.”
It is accordingly an object of the invention to provide an improved firearm suppressor, a mounting system and a mounting method, which overcome the hereinafore-mentioned disadvantages of the heretofore-known devices and methods of this general type and which reduce the effects of muzzle sound, muzzle blast, visible muzzle flash and invisible infrared flash of firearms.
With the foregoing and other objects in view there is provided, in accordance with the invention, a firearm suppressor. The suppressor comprises a housing to be mounted to a firearm. The housing defines a lumen therein for receiving gases from the firearm. At least one stripper member is disposed in the lumen for engaging and deflecting the gases. At least one one-way flow element is disposed downstream of the at least one stripper member, in gas flow direction, for permitting a one-way flow of the gases. At least one decompression chamber is disposed downstream of the at least one one-way flow element for reducing energy in the gases. At least one vent is disposed downstream of the at least one decompression chamber for expelling the gases into the atmosphere.
In accordance with another feature of the invention, the at least one stripper member is a plurality of stripper cones being partially spaced apart from each other to define spacings therebetween for the gases.
In accordance with a further feature of the invention, the plurality of stripper cones each include a sharpened upstream edge for catching and deflecting a gas stream into the stripper cones, rounded downstream edges providing aerodynamic surfaces or airfoils for pulling additional gas into the stripper cones acting as a gas trap, and laterally curved spacing ridges maintaining the spacing and steering the gases in laterally curving arcs to decrease an angle of impact with a wall of the housing.
The suppressor according to the invention, has specific structural features for “containment” by deflection and entrapment of the propellant gases to prevent the pressure wave or excited gases from reaching the atmosphere to “create” or become sound. These new features deflect and steer the high-speed, still-expanding gases and pressure waves away from the outlet. A majority of the expanding gases are directed from the suppressor lumen by a system of “stripper cones.” Prior art baffles “allow” some gas deflection while the cone system according to the invention “causes” gas deflection. The system of closely spaced, stacked cones is angled to engage and deflect the fast expanding gases in their forward and angular trajectory. These narrow slots form spreading or increasing volume spaces which help draw in the expanding hot gases. The lumen-facing cone surfaces have “sharpened (upstream) edges” to catch and deflect the gas stream into the cone system and “rounded (downstream) edges” acting as aerodynamic surfaces or airfoils to pull additional gas into the “cone trap.”
The complete system of stripper cones is directly vented into the adjacent portion of the first decompression chamber. The gas flows between the cones, which also have laterally “curved” spacing ridges between each cone serving not only to maintain cone spacing, but also steer the gases in laterally curving arcs to decrease the angle of impact with the wall. The gases are vented laterally and refracted or further curved by the outside suppressor wall due to this low angle of incidence.
These “directed flow” and curved walls create a functionally asymmetrical chamber with no reflective surfaces or symmetrical wall harmonics. The gas flows along the walls toward the rear because of the declining pressure gradient into the larger main portion of the containment and first decompression chamber.
The structural features for deflection take advantage of the energy within the gases such as heat and pressure but mostly its kinetic energy or inertia of movement. Its own great velocity of motion and “tendency to remain in motion” is used as the force to cause its deflection and entrapment.
The deflection of the high-speed gases according to the invention is important for improved suppression.
In accordance with an added feature of the invention, at least one one-way flow element is a plurality of live hinge valves disposed in a collar covering the at least one stripper member.
In accordance with still a further feature of the invention, a support tube is disposed within the housing, and a middle support member is disposed between the support tube and the live hinge collar. The middle support member has an opening formed therein for the gases.
According to this new propellant gas entrapment system for firearm suppressors, after deflection, the gases must be entrapped to complete “containment.” Surrounding the stripper cones is a plurality of live-hinge valves. The live-hinges lift easily as the deflected gases flow into the initial portion of the first decompression chamber and close instantly against the cones to prevent any return flow or escape as the pressures equalize.
The most powerful and clear energy in the propellant gases is the supersonic “pressure wave” of the ejectant, which creates the major part of the muzzle sound, blast, flash and infrared flash. This dominant form of the energies acts by direct impact as one immense pulse of “supersonic” gas pressure wave against the atmosphere which yields a broadband, short interval, very high amplitude sound, characteristically heard as the intense “crack”.
The second or further hidden “noise creating energy” within the gases is the high pressure, heat turbulence and the increased molecular velocities “within and of” the gas molecules themselves. This second form of energy acts by vibrating the air with a series of smaller pulses. This “subsonic” complex has many frequencies and is heard as the longer but less intense “boom.” Both energies are “potential sound” and prevention of their unaltered escape is important to suppression.
The higher-grade supersonic wave energy (pressure plus velocity) is deflected by the stripper cones and entrapped by the valves or “contained” in the chamber. This containment reduces the gases velocity and changes the energy to subsonic. At “containment” (deflection plus entrapment) both forms of energy are confined and combined into lower-grade energy (pressure and turbulence without velocity). This lower energy, (excited pressure) is now controllable by the other features of the suppressor, namely serial decompression, delayed dissipation and sound reduction features of the interior. All of these features work together in a sequence of stages to control the velocity, then pressure and embedded turbulences, then sound progression, to prevent or suppress sound.
The reduction of velocity by entrapment and containment is important for improved suppression.
In accordance with an additional feature of the invention, the at least one decompression chamber includes three decompression chambers having baffles disposed therebetween. The baffles have slits formed therein for conducting a flow of the gases between the decompression chambers.
With the new multichamber, multistage decompression system for firearm suppressors, a suppressor cannot change the “amount” of energy or pressure released by the propellant gases but can alter its ability to make sound with two or more serially connected correctly vented, decompression chambers. These are used to alter this extreme pressure through controlled step-down decompression to near atmospheric levels. Stepped decompression, recompression, decompression between multiple chambers is much more effective against the major pressure drops and high volumes faced by suppressors than any single chamber devices. To obtain an equivalent “rate of change” using only a single chamber would require a suppressor of unusable size.
Controlled decompression of extreme pressure differentials in multiple chambers by controlled venting is important to improved suppression.
In accordance with yet another feature of the invention, steel wool fills at least one of the decompression chambers.
In accordance with yet a further feature of the invention, two end caps are disposed at ends of the housing. At least one of the end caps has an inner surface with non-reflective facets or an anechoic coating, disposed thereon.
According to the new delayed dissipation of energy system for firearm suppressors, the energy dissipated, in either uncontrolled, high amplitude, short interval muzzle “blast” or in controlled, low amplitude, long interval muzzle “flow” is identical. Whether by explosion or by slow leak, or as stopping a car with a wall or by using brakes, all these situations dissipate the same amount of energy; only the “time intervals” differ. Prolonging the time interval of energy dissipation is the important key to efficient suppression.
The invention uses specific structural features to intentionally expand this time line to lower acoustic results. Expanding the time interval must begin by having containment or the “zero point” on the time line. Only then can the repetitious decompression from one chamber and recompression in the next chamber begin by controlled venting. Without containment, the escape begins before the peak of the pressure has even arrived. There is no “time line” of delay because there is no delay. Only after gases are “contained” can the second part or controlled delay by venting begin. Each venting is interspersed with time consuming reverse flow passageways, which are lined with either non-reflective faceted surfaces or anechoic coatings and filled with acoustic steel wool. These serially connected, asymmetric, decompression and passage chambers have sound restricting “slit vents” located at their opposite ends.
Sound (a circular pulsating pressure wave) passes through round holes leaving the pressure pulse relatively intact. Narrow slits easily pass pressure but delay and break up the symmetrical wave forms causing disorganization, scatter and phase shifting. The gases must travel back and forth through another obstacle the “pressure passing” but “sound suppressing” steel wool, which further breaks up the symmetry of sound and further prolongs the delay time.
The features according to the invention, which control and prolong or delay the dissipation time interval, are important for improved suppression.
Accordingly, in the new internal sound reduction system for firearm suppressors, in order to prevent or reduce internally produced or continued sounds, all of the internal surfaces are treated with one or more of the following sound reduction techniques: non-harmonically opposed surfaces, anti-reflective surface angles, non-focusing concave surfaces, non-symmetrical chambers, non-parallel surfaces, positively refractive surfaces and absorptive techniques such as faceted non-reflective surfaces and anechoic coatings.
The reduction of internally generated, internally transmitted or continued sound by refraction, phase shifting and absorption, is important to improved suppression.
With regard to the improved “subsonic bullet fire” suppression system for firearm suppressors, it is noted that some heavy subsonic bullets have a supersonic propellant wave front which exits with the bullet and mimics the classic supersonic muzzle “crack.” Short-barrel, large-bore firearms with abundant fast-burn modern propellants are notorious for their unexpected and disproportional muzzle blast. Not only is the gas flow supersonic, but a clear surplus of burning gas continues well after the bullet has left the barrel.
This containment of this powerful supersonic wave and surplus gas according to the invention, is important to improved suppression.
Regarding the improved “supersonic bullet fire” suppression system for firearm suppressors, it is also noted that supersonic bullets emit two independent sonic “booms.” The first is heard from the supersonic propellant wave front, which exits with the bullet and the second is heard all along the bullet's path caused by the shockwave of its speed. Supersonic bullet fire appears louder at the muzzle because at the instant of bullet exit “both of the sonic waves are superimposed” plus the hidden secondary noise of the gas turbulence is also present and added. Downrange, the bullet speed noise remains and cannot be suppressed at the muzzle, but moving away from the shooter the sound has less amplitude and even becomes Doppler shifted lower in frequency. Since the sonic wave travels downrange as an “enlarging donut,” it is distorted and reflected upward by the terrain interference. The downrange observer has only indistinct awareness of direction or the shooter's position. The loudest sound and flash most revealing of the shooter's position comes from the muzzle. Downrange the muzzle flash is seen first, followed by the slight whiz of bullet passage, then the vague sonic boom of the bullet and lastly the distant muzzle blast. Only the muzzle flash and muzzle blast localize the shooters' position. Supersonic rounds have been considered non-suppressible, but the most significant negatives of propellant shockwave blast, secondary gas turbulence blast, visible muzzle flash and infrared flash, are all well suppressed by the “containment” suppressor according to the invention.
The containment, conversion and control of the supersonic components of the muzzle blast, muzzle sound, muzzle flash and infrared flash at the muzzle, are important for improved supersonic bullet fire suppression.
In accordance with yet an added feature of the invention, there is provided at least one vent valve for venting gases at excess pressure from the lumen. The at least one vent valve has a tube for the gases and a spring cooperating with the tube for absorbing pressure of the gases.
In accordance with still another feature of the invention, there is provided a support tube disposed within the housing, two end caps disposed at ends of the housing outside the support tube, tie rods interconnecting the end caps, and at least one vent valve disposed at one of the end caps for relieving excess pressure.
It is noted regarding the new automatic overpressure release system for firearm suppressors, that in a containment-type suppressor, the containment volume and decompression rate are limited. Effective decompression between each round fired requires approximately two and three seconds for a “select” rate of fire limit of 20 to 30 rounds per minute, while still retaining good suppression. Sustained or automatic fire overcomes the containment and decompression limits, so that automatic pressure relief vents are placed in the rear of the primary containment chamber to vent excess pressures. Sustained fire is well tolerated using the relief vents, but muzzle noise does increase because containment, decompression, delay and internal sound reduction features have been bypassed. At times when sustained fire is required, the need for suppression becomes less important.
These structural features according to the invention, which automatically adjust for and release excess pressures, are important to improved suppression of sustained or automatic fire.
A new easy serviceability structure for firearm suppressors is provided by avoiding welded or fused assemblies and using dividable parts and sub-assembles held by simple fasteners and unique part-into-part supporting members. This entire suppressor according to the invention, including mounts, is quickly removable and can be completely disassembled for easy service.
In accordance with yet an additional feature of the invention, a support tube is disposed within the housing, at least one torsion spring retainer unit is disposed on the support tube, and at least one barrel mount is disposed on the at least one retainer unit for mounting the suppressor on a barrel of the firearm.
In accordance with again another feature of the invention, the at least one torsion spring retainer unit includes two torsion spring retainer units, and the at least one barrel mount includes a front barrel mount to be screwed to a threaded button on the barrel and a rear barrel mount to be fused to the barrel.
In accordance with again a further feature of the invention, the retainer units have inwardly-projecting locking lugs for holding the retainer units to the support tube.
In accordance with again an added feature of the invention, the rear barrel mount has a mount body with pressurizing ports formed therein, split rings to be disposed within the mount body and a compression driver for expanding and contracting respective ones of the split rings between the mount body and the barrel.
In accordance with again an additional feature of the invention, end caps are disposed at ends of the housing, and the front barrel mount has a nut disposed at one of the end caps.
In accordance with still another feature of the invention, the front and rear suppressor mounts have in-ramps, out-ramps and receivers for the locking lugs of the retainer units, permitting the suppressor to be directly pushed on and pulled off by turning.
The new alignment integrity system for firearm suppressors maintains the barrel-to-suppressor alignment during combat or field use, which is important for shooter safety. If a bullet strikes a displaced suppressor structure, the “following round” is fired into an occluded passage with possible catastrophic results. Alignment integrity is also important to reducing the bullet-to-suppressor wall clearance, which is important to prevent “blow-by” and to improve efficiency. The integrity of the connection must tolerate normal active use and even abuse while still retaining perfect alignment.
Prior art “can” type suppressors with single point, one-ended mountings and a right angle joining between the “can” wall and the end plate, have such poor alignment integrity as to make their use in combat or even knock-about situations unsafe.
The invention maintains alignment integrity by an interlocking, part-into-part, triple through-bolted, “truss stiffened” structure including the end caps, which locks to the mounts with four axis security and extends over and integrates with the barrel. The suppressor and barrel become as one piece. The major portion of the suppressor structure encases over the barrel and is retained by a widely separated bolted-on front barrel mount and a pressured fused rear barrel mount. The attachment mounts integrate with the barrel and lock to the suppressor with engaging matched parts having four or more locking lugs.
A new quick attachment system for firearm suppressors is provided because a versatile weapon system requires a secure and quickly attachable and removable suppressor.
The prior art uses ineffective screw-on “can type” or non-easily removable integrated suppressors.
The invention not only provides more stability and efficacy than any prior suppressor, but also with a quick attachment and removal system. Two length-wise separated mounting collars strongly affixed to the firearm barrel mate with matching separated collars in the suppressor with four or more spring-driven locking lugs allowing quick self-locking, easy-releasing use. Both the forward and rear locking lug receivers have tapered linear “in ramps” which allow easy finding of the ramps and direct push-on attachment of the suppressor. These “in ramps” narrow at the rear and drop into deeper engagements or locking lug receivers. These deeper locking engagements have bottom matching laterally running “out ramps” for quarter-turn unlocking and pull-off detachment of the suppressor. This more effectively secured integrated suppressor can be mounted or dismounted from the firearm in less than two seconds.
Lugs, pins or balls are frequently used to secure or position one object or tube in or over another object or tube. By penetrating the one object and engaging the other object, the engaging lugs, pin or balls can mark, detent, limit or lock the two objects in relative position. This inter-engagement of objects can be loosely held as in ball bearings marking a detent with just spring pressure or by a stronger, more permanent fitment by constricting or expanding collars or locking mechanisms which hold the engaging devices firmly embedded into both objects.
In prior art systems which use spring retention of the locking or position holding lugs, pins or balls rely on large, complex, multipart systems to hold the springs. Those more permanent attachments of the spring mechanism use screws, bolts, rivets, welding or separate additional ring clip devices. With the prior art round torsion, round coil or long flat tension-compression springs, the securing methods are not only complex and failure prone, but even worse they are large, which prevents small compact constructions or uses.
The spring attaching devices must hold or secure the spring in proper position longitudinally, vertically, laterally and rotationally.
The securing lugs, pins or balls also require separate containment devices to prevent their loss or outward escape from the working shaft or over-penetration and loss inwardly if the inner object is removed or the inverse, depending on their orientation.
In a new self-retaining torsion spring locking lug system according to the invention, the securing or locking mechanism is held by the retaining spring's own structure. The springs are not machine fastened to either object but are held in basic or initial plane position or placement by its matching fitment over, around or inside of one of the two objects. The new self-retaining, flat spiral or flat zigzagging torsion spring or springs are secured in all four planes or axes as in lengthwise; vertically, laterally and rotationally, by small end projections extending from the engaging lug, pin or ball, which penetrate matching holes or indentations in the retainer springs. The pins or lugs retain the spring and the spring retains the pins or lugs.
The new spiral, circular or zigzag construction according to the invention creates a torsion spring that can be used in a much more compact area than conventional long, spiral, coil or wound springs because of its own retention by part-into-part fitment rather than additional machining, attachments or devices. They have small foot prints or space requirements and have very limited vertical space requirements. They allow the point of spring effort to be placed much closer to the point of the spring's attachment, adding to its compactness.
The new flat, self-retaining torsion spring system according to the invention has a longer spring travel range and more consistent spring pressure throughout its range of motion. The improved system is easily and cost-effectively manufactured, installed, removed and maintained.
In the new self-retaining torsion spring locking lug system, the new locking lug retainer springs are not fastened to the main support tube, but are held in position by its matching diameter fitment over the support tube and secured lengthwise, laterally, and rotationally by small end projections extending from the locking lugs, which penetrate matching holes in the end of the retainer springs. This circular flat structure of a compact torsion spring according to the invention allows their use in much more compact areas than conventional prior art tension/compression, long coil or wound springs. They allow the point of spring effort to be placed closer to the point of the spring's support. They are simple nonattached, self-retaining retainer springs with lugs having shoulders to prevent over penetration and have a more compact vertical height than conventional coiled springs for use in confined spaces. The spring rate and length of a more constant spring effort zone are also enhanced by these new circular flat torsion springs as compared to prior art flat tension/compression or coiled wound springs. The springs retain the lugs and the lugs retain the springs.
According to the new bolt-on front barrel mount for firearm suppressors, the front suppressor mount is secured to the barrel's threaded shaft by a socket driven nut. The front suppressor mount has a forward taper for easy passage of the suppressor. The front mount contains two or more tapered entrance ramps for the locking lugs in the matching suppressor mount. Not only should the suppressor be easy to attach and detach from the weapon, but the mounts must also be field removable. An easily removed barrel end mount improves weapon versatility.
A removable barrel end mount, which exposes the bare end or threaded barrel button, is important for quick change use in multi-mission requirements. The barrel end mount is secured by a special end driven socket nut, which is simple to remove, leaving the threaded barrel end clear and ready for quickly mounting other devices.
Through the use of the new semi-permanent rear barrel mount for firearm suppressors, the rear barrel mount remains on the barrel and is securely locked in place. This rear suppressor mount is part of the widely spaced two mount system which locks the suppressor in all four axes with improved security. This rear mount is field installable and semi-permanently locked to the barrel with the security of a machined attachment. The three-piece rear mount is formed of the mount body, which slides over the barrel having a formed under-cut space for thin split rings of a softer more malleable metal or other suitable material. The third piece or threaded end cap slides over the barrel first and screws into the rear mount, retaining and expanding the overlapping split rings strongly engaging the mount to the barrel. In order to ensure increased security of attachment to the mount surface, multiple holes are formed in the wall of the rear mount giving enhanced grasp by softer material split rings under high pressure. This new mounting feature provides machined security against dislodgement without machining expense or permanently scarring the weapon and can be done in the field without skilled assistance.
In accordance with still a further feature of the invention, a fusing fixture is to be placed over the rear barrel mount. The fusing fixture has pressure bolts threaded therethrough for applying pressure to the rear barrel mount and fusing the rear barrel mount to the barrel. The fusing fixture is removed after fusing.
With the new high-pressure, flow-fusing or flow-bonding device, the rear mount is well secured by the previously described expansion of the softer pure aluminum or other suitable material split rings by the threaded internal collar compression.
In situations where ultimate strength is required in mounting the rear suppressor mount to the barrel or in other object-into-object permanent mountings, a process of high pressure flow-fusing or bonding is presented.
Ultimate strength and permanent mounting of these metal to metal objects is accomplished by use of the access holes in the walls of the object, in this case the rear mount (over the split rings) and a special high-pressure, flow-fusing fixture.
The softer metal or other suitable material rings are used to lock the mount or outer object to the barrel or inner object by using extremely high pressure to flow the compressed material into the microscopic irregularities of both the inner and outer objects. Known similar metals are commonly used to fuse, bond or solder metal objects together. The heat flowing is replaced in this case with pressure flowing by the use of extreme pressure through a pressure generating fixture.
Under heat or extreme pressure, metals become more liquid in nature and behave under the laws of hydraulics. By using an array of small bolts through the special fixture surrounding the rear mount or other object to be affixed and using the precut access holes over the split rings, the small bolts can be turned into the soft inner split rings generating a force sufficient to flow the ring material like heavy syrup. The forces, created by the small pistons are measured in the order of many tons per square inch, causing the now flowing material to fill the irregularities of the inner and outer surfaces, identical to soldering. This process works well with machine cut aluminum alloy barrels and other similar objects which cannot tolerate the damaging heat.
The resultant evenly distributed retaining pressure is not only less scarring and destructive to the barrel surface, but does not cause concentrated stress distortions in the barrel wall which alter the accuracy or aim point of the barrel, as do single or focused pressure point retaining devices.
The high-pressure, metal flow-fusing fixture is constructed to form fit over the “mount or other device” to be fixed in place. The high-pressure inducing fixture is constructed of hardened steel or other suitable material and is constructed to slide over or to be clamped over or around the suppressor mount or target item with great strength. The created space on the underside of the mount or device to be affixed conforms to the barrel or the target item but leaves a spacing for the soft metal fusing layer. A flowable but sufficiently strong metal, like pure aluminum, or other suitable material, is used to fill this cavity completely in the form of split rings or coils. Steel vertical end seals are used to contain the flowable material from escape.
Small diameter, fine thread, hardened bolts fitted through the fixture are turned in sequenced rotation to create an even and extreme pressure of many tons per square inch against the relatively soft flowable metal or other suitable material. The physical laws of hydraulics allow for extreme pressure to be placed on the larger surface by the small bolts in inverse proportion to their diameters. The smaller the bolt or “piston” diameter, the greater the pressure that can be forced against the larger surface area. The mechanical advantage created by the smaller, fine threaded bolts turned into the soft material is almost beyond measure.
The compressed metal or material becomes hot and flows like heavy syrup into the microscopic irregularities of the target items, in this case the barrel on one side and the underside of the mount on the other. Whether by using heat to flow metal or by using pressure to flow metal, the accomplished fusing, bonding or soldering of dissimilar metals is the same.
The pressure flowing fixture is removed after cooling and the fitted immoveable collar and mount are now pressure-bonded to the barrel with great security or as any other object piece can be attached to its target item. Parts can be attached with machined-on strength without the machining expense or exposing sensitive barrels or other objects to damaging heat.
The process and fixture allow metal-fused security inexpensively and portably in the field without special assistance, saving time and money.
Shoulders on the small diameter bolts limit their depth to prevent damage to the barrel or other objects. Variations of this process and fixture can be used to fuse by high pressure flow-fusing of many similar or dissimilar metals with great strength.
With the objects of the invention in view, there is also provided a mounting system. The system comprises a first object formed of a relatively hard material and a second object formed of a relatively soft material. The second object is disposed outside the first object at a distance, defining a cavity between the first and second objects. A fusing fixture is to be placed outside the second object for fusing the second object to the first object, and to be removed after fusing. Pressure bolts are threaded through the fusing fixture for applying pressure to the second object, causing the relatively soft material to flow and fill the cavity.
With the objects of the invention in view, there is additionally provided a mounting method. The method comprises providing a first object formed of a relatively hard material, placing a second object formed of a relatively soft material outside the first object at a distance defining a cavity between the first and second objects, and placing a fusing fixture outside the second object. Pressure is applied to the second object with pressure bolts threaded through the fusing fixture, causing the relatively soft material to flow and fill the cavity for fusing the second object to the first object. The fusing fixture is removed after fusing.
Of course, the position of the first and second objects could be reversed, with the fusing fixture operating from the inside.
In accordance with a concomitant feature or mode of the invention, the first object is a barrel of a firearm, and the second object is a suppressor mount.
Other features which are considered as characteristic for the invention are set forth in the appended claims.
Although the invention is illustrated and described herein as embodied in an improved firearm suppressor, a mounting system and a mounting method, it is nevertheless not intended to be limited to the details shown, since various modifications and structural changes may be made therein without departing from the spirit of the invention and within the scope and range of equivalents of the claims.
The construction and method of operation of the invention, however, together with additional objects and advantages thereof will be best understood from the following description of specific embodiments when read in connection with the accompanying drawings.
Referring now to the figures of the drawings in detail and first, particularly, to
Several of the previously-described figures as well as
A live hinge collar 17 can be seen in
The exploded view of
It may be seen from
The gases continue to pass through the slits 29 between the three chambers, through the steel wool 30 and over the facets 31 and/or the anechoic coating, while the speed of the gases and therefore the sound produced thereby continue to dissipate. The gases finally leave the lumen 2′ or interior of the cover or housing 2 through the vents 65 shown in
Partially-exploded and fully-exploded views of the suppressor 1 can be respectively seen in
As is seen in
The rear suppressor mount 61 is formed of three pieces, namely a mount body 66, which slides over the barrel 15 and has a non-illustrated under-cut space for thin split rings 67 of a softer more malleable metal or other suitable material, and a threaded compression driver 68 which slides over the barrel 15 first and screws into the mount body 66, retaining and expanding the overlapping split rings 67 to strongly engage the mount 61 to the barrel 15. In order to ensure increased security of attachment, multiple holes 69 are formed in the mount body 66, providing additional gripping by the softer material split rings 67 under high pressure. A process of high-pressure flow-fusing or bonding is presented where ultimate strength is required.
It can be seen from
Small, finely threaded, hardened bolts 71 are screwed through the fixture 70 and turned in sequence to create an even and extreme pressure against the relatively soft material of the rear suppressor mount 61, from the condition shown in
