Abstract:
A firearm compensator, to be affixed to the muzzle of a gun for reducing at least one of flash and recoil, utilizes a vectored flow nozzle, an expansion chamber containing a prominent thrust surface and flow-directing structures below the barrels center line, and flash-hiding ports. A compression ramp containing dimple-like structures connects the bottom of the gun muzzle to the bottom of the prominent thrust surface. Upon firing the gun, gasses depart from their linear trajectory as they flow past the vectored flow nozzle, flow diagonally downward past a dimpled compression ramp in the expansion chamber, and strike the thrust surface. A plurality of substantially horizontal elongated ports in the expansion chamber aids in flash suppression.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
       [0001]    This application claims the benefit of the filing date of U.S. Provisional Patent Application No. 62/203,552 filed Aug. 11, 2015, the disclosure of which is hereby incorporated herein by reference. 
     
    
     FIELD OF INVENTION 
       [0002]    This invention relates to the field of recoil-reducing muzzle devices for firearms. More specifically, the invention comprises a vectored flow nozzle and expansion chamber with a means of substantially diverting the main, forward trajectory of gas flow of a gunshot to strike a surface more directly, thereby producing a counterforce to reduce recoil. 
       BACKGROUND OF THE INVENTION 
       [0003]    Muzzle brakes, categorically, are seen as being incompatible with combat, as they are often criticized as causing more problems than they solve. To define terms, muzzle brakes are muzzle devices that are affixed to the end of a firearm&#39;s muzzle for the primary purpose of reducing recoil. The term “compensator” is often used synonymously. Regardless, muzzle brakes and compensators feature very conventional designs that branch off very little from two main archetypes. One of the quintessential designs is an open, multi-baffle design featuring one or more surfaces that allow expanding gases to strike, thereby imparting an indirect, somewhat angled counter-recoil force. Most gases exit this type of design laterally outward to the sides of the compensator and strike the cooler air of the outside atmosphere all at once, causing a bright flash and concussion felt by the shooter and those nearby. These designs often vary in the number of baffle chambers or in the tolerance allowed for each bullet to pass through during its flight, but they work under the same design principles. Designs featuring upward-facing ports demonstrate another design architype. These devices utilize jets of expanding gases firing upward to produce a force to counteract the upward movement of the muzzle. The result is lessened muzzle rise but also a blinding flash appearing directly in the shooter&#39;s immediate field of view. Both types of designs allow gases to expand into ports or open baffle chambers and do nothing to bend or substantially alter the primary, forward trajectory of the gases from a gunshot. In short, they leverage the property of expansion alone. 
       BRIEF SUMMARY OF THE INVENTION 
       [0004]    Briefly described, aspects of the present invention may provide an improved recoil-reducing apparatus in front of the muzzle of a firearm. It is an aspect of this invention to provide a highly efficient anti-recoil apparatus that addresses both horizontal and vertical recoil simultaneously. It is another aspect of this invention to minimize back-blast and flash experienced by the shooter. These aspects of the invention are accomplished utilizing a vectored flow nozzle, an expansion chamber, substantial anti-recoil surfaces, compression, strategically-placed ports, dimpled surfaces, ports, and exit recess prongs. 
         [0005]    It is an aspect of this invention to more efficiently use the force contained in the primary, forward trajectory of a gun&#39;s gases in a way that alters that trajectory and generates a counter-recoil force as a result. An embodiment of the present invention utilizes a vectored flow nozzle positioned in front of the muzzle (and there are many means of attachment including muzzle engagement via threads or even over another muzzle device as a “quick-detach” mount) and a prominent, primary anti-recoil surface inside an expansion chamber to provide an enhanced means of using hot, expanding gases from a gunshot to impart more forces onto a baffle-like counter-recoil surface by changing the trajectory of the gases. The shape of the vectored flow nozzle may be aptly described as a short section of bent conduit or angled throat which actively guides the gases escaping from a firearm&#39;s muzzle away from their straight, longitudinally forward trajectory. The vectored flow nozzle is positioned very closely against the muzzle of the gun, yet is part of the compensator; this close proximity allows the vectored flow nozzle to interact with the gases before they get much chance to expand. Dimensionally, the space between the walls of the vectored flow nozzle is large enough to allow the projectile to pass through untouched. Upon firing, the gunshot&#39;s hot, expanding gases leave the firearm&#39;s muzzle, enter the compensator, are deflected by the vectored flow nozzle from their initial trajectory (i.e. expanding and traveling straight forward, coaxial to the gun&#39;s barrel) to their new trajectory (i.e. expanding and traveling forward but now at a lowered angle, downward from the centerline of the gun&#39;s barrel). This new trajectory aims the gases more directly at one or more prominent counter-recoil surfaces within the expansion chamber immediately following the vectored flow nozzle. Conversely, the projectile, due to its stabilization (for example, from the spin imparted from the firearm&#39;s rifling), continues along its straight pathway along the barrel&#39;s centerline axis unchanged by the vectored flow nozzle and exits the compensator safely. The present compensator&#39;s expansion chamber is positioned in front of the vectored flow nozzle; this expansion chamber extends beneath the centerline of the barrel and is defined by generally planar side-walls, a ceiling, a primary counter-recoil surface, a compression ramp connecting the vectored flow nozzle and the bottom of the primary anti-recoil surface, and a front wall in an exemplary embodiment. Once the gases pass through the vectored flow nozzle, they flow forward and downward along the compression ramp (the floor directly connecting the vectored flow nozzle and the bottom of the primary anti-recoil surface), which compresses the gases—the compression ramp acts as an anti-recoil surface in itself. Gases strike the counter-recoil surface, and impart a greater force into the primary anti-recoil surface than were they merely allowed to stay on their initial, original trajectory and expand into the counter-recoil surface. Furthermore, the front wall of the invention which contains the departure recess where the bullet exits may also be substantially curved or angled to increase forces that lower muzzle rise in an exemplary embodiment. 
         [0006]    To enhance the change in primary gas trajectory, dimples or ridges may be included on the exemplary embodiment on the compression ramp laterally forward of the vectored flow nozzle. The dimples, similar to those on a golf ball, interact with gas flow and alter the boundary layer between laminar flow and turbulent flow. The gases rush by the compression ramp on their way to collide with the primary anti-recoil surface on the far end of the expansion chamber positioned beneath the centerline axis of the barrel. With dimples (it should be noted that these may take the form of ridges or similar artifacts—the term dimples may denote either dimples or other similar features and should be considered synonymous) on the compression ramp, the gases rush by more closely to the compression ramp&#39;s surface. The result is a greater change in the primary trajectory of the gases allowing a more direct collision with the primary anti-recoil surface. In an exemplary embodiment, the primary anti-recoil surface may be a curved surface to maximize surface area. In an alternative embodiment, the primary anti-recoil surface may be a substantially straight, angled surface to maximize the degree to which the gases strike the anti-recoil surface head-on. 
         [0007]    To further enhance the change in primary gas trajectory, one or more interior thrust beams may be provided within the expansion chamber. An interior thrust beam spans the internal width of the expansion chamber and provides numerous benefits. These benefits include, for example, providing the gases an additional surface to thrust against, providing structural support for the compensator itself, and providing the gases a structure that may directly influence their trajectory as they rush into the expansion chamber. The interior thrust beam may take the shape of an inverted airfoil, for instance, in an alternative embodiment of the invention, wherein that shape is employed to leverage fluid dynamics and create a net downward force, thereby mitigating muzzle rise. Furthermore, internal thrust beams may complement or be used in place of the vectored flow nozzle, depending upon the embodiment. In an exemplary embodiment of the invention, multiple interior thrust beams are used to direct gases toward the primary anti-recoil surface to maximize the net counter-recoil forced generated. 
         [0008]    It is another aspect of the invention to reduce flash. Very closely related to flash reduction, it is another aspect of the invention to reduce back-blast as felt by the shooter. The vectored flow nozzle forces the gas to take a longer route through the expansion chamber due to its new trajectory (diagonally forward and downward is longer than its traditional straight forward trajectory), giving these gases more opportunity to mix with the ambient air within the expansion chamber—more exposure to air within the expansion chamber has the effect of slowing the gases down more prior to exiting the compensator (reducing gas plumes from gas striking outside air). Furthermore, the vectored flow nozzle prevents most gas from exiting the compensator via the departure recess—thereby further mitigating any flash in the shooter&#39;s field of view. The expansion chamber further comprises a plurality of elongated, approximately horizontal ports on the lateral side walls of the expansion chamber proximal to the anti-recoil surface. Theses ports allow for oxygen exposure to the under-oxygenated gases flowing through the expansion chamber, thereby allowing an opportunity for combustion to begin internally, rather than allowing gases to be exposed to fresh oxygen only after departing from the compensator. 
         [0009]    Furthermore, these ports allow some expanding gases to bleed off and exit the compensator in such a way that does not cause a plume once gas strikes the air of the outer atmosphere, thereby further minimizing flash. Gases exiting the compensator through these ports are allowed to exit in a manner that minimizes their presence in the shooter&#39;s field of view. In the compensator&#39;s preferred embodiment, these ports are positioned proximal to the primary anti-recoil surface and angled surfaces connected to the ports on their leading edges called bleed ramps. These bleed ramps provide guidance for gases as they exit the compensator via the ports. The bleed ramps send gases laterally outward and longitudinally forward from the compensator, in a diagonal direction. This imparts a direction to the exiting gases that moves them away from the shooter, while also forcing gases to exit in a controlled fashion, thereby minimizing concussion. Because gases strike different parts of the expansion chamber at different times, the bleed ramps force gases to take a pre-determined course—a course which, due to the nature of fluid dynamics, becomes one that gases approaching the ports also take as a result (in essence gases follow the trajectory of the preceding gas ahead of it). In terms of gas flow, some gas will exit via the ports, while other gas is simultaneously striking the primary anti-recoil surface. Once the gas has struck this surface, the gas flows along the path of the gases that have already just exited the compensator, thereby influencing the path of the gases that would otherwise reflect back at the shooter. Instead, these gases exiting via the ports exit laterally outward and longitudinally forward from the ports (as opposed to laterally directly to the side, or worse, back at the shooter). 
         [0010]    In another embodiment of the invention, ports may be placed on the ceiling on the invention to maximize the production of downward forces that combat muzzle rise. Interestingly enough, due to the volume of the expansion chamber, ports placed on the ceiling of the compensator not only allow fresh oxygen to enter the expansion chamber causing an increased likelihood of having any flash or combustion contained within the compensator internally, but also allow the hot gases of the gun shot to bleed off into the atmosphere in such a way that minimizes the opportunity for under-oxygenated gases to strike the outer atmosphere all at once and flash. The shape of the compensator allows for ceiling ports to further increase forces that lower muzzle rise while also minimizing flash. Ports may be placed close to or distant from the front wall containing the departure recess depending on the desired effect that is to be achieved. Ports further away from the front wall serve more, for example, to introduce oxygen to the expansion chamber, to reduce flash, and to provide moderate muzzle climb reduction whereas ports proximal to the front wall provide, for example, more muzzle climb reduction. Furthermore, ports arranged away from the front wall may extend to the side walls to further introduce oxygen to the expansion chamber. 
         [0011]    Additionally, in yet another embodiment of the invention, ports in the form of substantially forward-facing vents may be positioned on the primary anti-recoil surface as well as on the front wall, whether curved or angled, in an effort to diffuse gases forward, in front of the compensator, thereby lowering the internal pressure of the expansion chamber when hot gases are rushing through it and diffusing the blast forward. Such ports may be angled slightly upward to impart a downward force. To further decrease internal pressure within the expansion chamber, ports, comprising various port shapes, may be placed proximal to the approximately planar side walls of the compensator. 
         [0012]    In another embodiment of the invention, flash reduction and back-blast reduction can be further mitigated by an internal structure within the expansion chamber, called the internal flow mound. The internal flow mound is positioned above the centerline axis of the barrel on the ceiling of the expansion chamber, proximal to the front wall of the compensator. Essentially, the internal flow mound is a structure that decreases the total internal height of the expansion chamber. When gases strike the primary anti-recoil surface, some gases that do not exit the compensator via ports or the exit recess begin to travel upward, forming a circular pattern, or eddy, within the expansion chamber. If another shot is fired within close enough succession while the gases forming an eddy pattern remain within the expansion chamber, the subsequent shot&#39;s gases may expel from the compensator far more gases than would come from a single shot—the result is an increased flash and back-blast. The internal flow mount decreases the total diameter of the maximum eddy possible within the expansion chamber, thereby decreasing any likelihood of increased flash or back-blast due to internal flow dynamics. 
         [0013]    In addition to the above mentioned means for reducing flash and back-blast, an exemplary embodiment of the compensator utilizes and arrangement of prong-like structures surrounding the expansion chamber&#39;s bullet departure recess. These prongs interact with the gases exiting the expansion chamber where the bullet exits. Upon striking the outside air these gases begin to form a toroidal shape, or plume. The prongs force the gases beginning to form a plume to flow past and around the prongs, thereby spreading out the gases increasing their exposed surface area and preventing the gases from having the opportunity to ignite all at once causing flash. In its preferred embodiment, the compensator&#39;s prong arrangement leaves the very top and bottom areas closed to stop any remaining flash from entering the shooter&#39;s field of view or prevent any gases from being channeled downward (during prone shooting gases directed downward will kick up dust and debris). Prongs can further provide a number of additional less obvious benefits that lend themselves readily to combat, such as being sized appropriately to facilitate the attachment of a bayonet or simply provide a means of stabbing or poking (i.e. breaking a window, or prodding enemy personnel). 
         [0014]    According to an embodiment, a recoil-reducing apparatus configured to be affixed to a muzzle of a gun having a gun barrel having a longitudinal axis comprises a muzzle engagement recess configured to be positioned coaxial to and longitudinally forward of the gun barrel, a vectored flow nozzle positioned coaxial to and longitudinally forward of the muzzle engagement recess, and an expansion chamber positioned longitudinally forward of the vectored flow nozzle. The vectored flow nozzle is configured to deflect expanding gases off the longitudinal axis and to divert the expanded gases along a new trajectory vertically downward relative to the longitudinal axis. 
         [0015]    According to an embodiment, a recoil-reducing apparatus configured to be affixed to a muzzle of a gun having a gun barrel comprises a muzzle engagement recess configured to be positioned coaxial to and longitudinally forward of said gun barrel and an expansion chamber positioned longitudinally forward of the muzzle engagement recess. The expansion chamber comprises a front wall, a ceiling extending from the muzzle engagement recess to the front wall and comprising an internal flow mound proximal to said front wall, an anti-recoil surface extending from the front wall and facing the muzzle, a compression ramp extending longitudinally from the muzzle engagement recess to the anti-recoil surface, first and second lateral walls extending from the muzzle engagement recess to the front wall and from the ceiling to the compression ramp, and a departure recess defined in the front wall and positioned longitudinally forward of and coaxial to said gun barrel. 
         [0016]    According to an embodiment, a recoil-reducing apparatus configured to be affixed to a muzzle of a gun having a gun barrel comprises a muzzle engagement recess configured to be positioned coaxial to and longitudinally forward of said gun barrel, an expansion chamber positioned longitudinally forward of said muzzle engagement recess, and a thrust beam spanning a width of the expansion chamber. 
         [0017]    According to an embodiment, a recoil-reducing apparatus configured to be affixed to a muzzle of a gun having a gun barrel comprises a muzzle engagement recess configured to be positioned coaxial to and longitudinally forward of said gun barrel and an expansion chamber positioned longitudinally forward of said muzzle engagement recess. The expansion chamber comprises a front wall, a ceiling extending from the muzzle engagement recess to the front wall, an angled anti-recoil surface extending from the front wall and facing the muzzle, a compression ramp extending longitudinally from the muzzle engagement recess to the angled anti-recoil surface, first and second lateral walls extending from the muzzle engagement recess to the front wall and from the ceiling to the compression ramp, a departure recess defined in the front wall and positioned longitudinally forward of and coaxial to said gun barrel, and at least one port for exhaust gases to exit the expansion chamber. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0018]      FIG. 1  shows a perspective view of the compensator affixed to the end of a gun barrel. 
           [0019]      FIG. 2  shows a perspective view of the embodiment of the compensator displayed in  FIG. 1  with additional features. 
           [0020]      FIG. 3  shows an exploded view of the compensator&#39;s embodiment displayed in  FIG. 2 . 
           [0021]      FIG. 4  shows a sectional view of an embodiment of the compensator in  FIG. 3 . 
           [0022]      FIG. 5  shows the sectional view of the embodiment of the compensator from  FIG. 4  illustrating gas flow. 
           [0023]      FIG. 6  shows a sectional view of an alternate embodiment of the compensator from  FIG. 4  with a modified means of attachment to the gun barrel. 
           [0024]      FIG. 7  shows a sectional view of an alternate embodiment of the compensator in  FIG. 4  with an angled anti-recoil surface. 
           [0025]      FIG. 8  shows a sectional view of an alternate embodiment of the compensator in  FIG. 7  with an angled front wall. 
           [0026]      FIG. 9  shows a sectional view of an alternate embodiment of the compensator in  FIG. 5  with a curved front wall, interior thrust beams, and a forward facing vent. 
           [0027]      FIG. 10  shows a perspective view of an alternate embodiment of the compensator displayed in  FIG. 1  with alternative port arrangements. 
           [0028]      FIG. 11  shows an exploded view of an alternate embodiment of the compensator displayed in  FIG. 3  featuring an interior thrust beam. 
       
    
    
     DETAILED DESCRIPTION 
       [0029]    Unconventional compensator designs, such as those featuring an asymmetric expansion chamber with a prominent anti-recoil surface, may allow gases to expand and, in doing so, strike a baffle surface and impart some force, which combats the gun&#39;s recoil indirectly. In this design, gases do not strike the baffle surface head-on, or rather, normal to the baffle&#39;s surface. Instead, gases strike the baffle surface at a glancing angle—this is highly inefficient, as more energy is transferred when gases strike normal to a counter-recoil surface. Leveraging the principles and insight gathered from studying fluid dynamics as it relates to firearms, specifically compressible supersonic and even hypersonic flow, it becomes readily apparent that massive levels of force, friction, velocity, heat, etc. are present. Where the gas flows, force and energy follow as well. Even what may seem like a somewhat small change in flow can yield vastly different results given the forces at work. That said, these traditional muzzle brake and compensator designs do not attempt to alter the primary vector of the escaping gases (i.e. straight forward) as they leave the muzzle. A need remains to be able to actively alter and influence the primary gas trajectory and redirect the gases onto a more direct collision course with a counter-recoil surface, thereby achieving a highly efficient degree of recoil reduction, and allowing for the compensator to take on both rearward recoil and muzzle climb (upward recoil) simultaneously. 
         [0030]    Traditional muzzle brakes or compensators can obscure the shooter&#39;s field of view (i.e. the area directly vertically above the muzzle of a gun), blind them, redirect uncomfortable pressure waves back at them or to those in the immediate vicinity, or—even worse—give away the shooter&#39;s position to the enemy due to flash. These common downsides are major detractors when considering their use in combat. Muzzle flash is caused when under-oxygenated gases exit a gun barrel and are exposed to the cool air of the outer-atmosphere in such a way that the gases achieve a high ratio of volume to surface area. When a critical mass is reached and the cooler outside air interacts with the hot expanding gases of a gunshot, the gas becomes exposed to enough oxygen to allow for full combustion. Due to a high ratio of internal volume to surface area (for example, in the case of a shape such as a toroid or gas plume), the ignition happens all at once, resulting in a bright, conspicuous blast—similar to a thermobaric explosion. A need remains to be able to effectively accomplish both recoil reduction as well as flash reduction and back-blast reduction in such a way that all are accomplished effectively. 
         [0031]    In  FIG. 1 , a gun barrel  11  having an axis  13  down the barrel&#39;s centerline is shown at a perspective view. To more clearly describe the compensator, an axes system is defined whereby the arrow at  15  indicates the vertical axis, the arrow at  17  indicates the lateral axis, and the arrow at  19  indicates the longitudinal axis. This embodiment of the compensator is affixed to the gun barrel  11  along its axis  13  via its muzzle engagement recess  33 . The compensator is a coaxial extension of the gun barrel along the barrel&#39;s centerline axis. In this embodiment, the compensator&#39;s muzzle engagement recess  33  attaches to the gun barrel via threads (not shown) on the end of the gun. The engagement recess  33  is thus positioned coaxial to and longitudinally forward of the gun barrel  11 . To better assist in installing the compensator, wrench flats  29  on the lateral sides of the muzzle engagement recess  33  are shown per an exemplary embodiment. Anatomically, this view also shows one of the side walls  39  on the lateral side of the compensator, along with horizontally elongated ports  27 , the expansion chamber ceiling  31 , curved primary anti-recoil surface  43 , front wall  41 , and the departure recess  35 . The elongated ports  27  are substantially parallel to the ceiling  31  and their openings in terms of vertical height are ideally smaller than the diameter of the departure recess. The elongated ports  27  may be level (i.e. at  0 ° relative to the longitudinal axis  19 ) at their optimal angle so as not to, upon firing, impart any force on the gun barrel  11  that may add to muzzle climb due to gases escaping at a longitudinal angle, while also keeping gases out of the shooter&#39;s immediate field of view. Alternatively, the elongated ports  27  may be angled upward as even a small upward angle of +5° to +15° can assist in generating additional force to counter muzzle rise. Conversely, the elongated ports  27  may be angled slightly downward. For example, a downward angle of −5° to −15°, while suboptimal for counteracting muzzle rise, can nevertheless be employed to angle gases further away from the shooter&#39;s immediate field of view. While the elongated ports  27  are illustrated as being generally uniform, alternative embodiments may take the form of port arrangements with as few as one elongated port on each side of the planar side walls  39 . Additionally, the elongated ports  27  may take the form of different lengths. 
         [0032]    When the gun is fired, a projectile travels along the barrel&#39;s axis  13 , passes through the compensator at the muzzle engagement recess  33  and exits the compensator at the departure recess  35 . Expanding gases (not shown) take a very different path. The projectile&#39;s stability allows for virtually a straight trajectory along the barrel&#39;s centerline axis  13 . The gases, on the other hand, leave the barrel  11 , are deflected off of their forward trajectory along the barrel&#39;s centerline axis  13  by the vectored flow nozzle (not shown) and are diverted to their new trajectory that is longitudinally forward and vertically downward. This new trajectory diverts gases onto a more direct course with the curved primary anti-recoil surface  43 , and exiting the compensator via the elongated ports  27  and, to a minor extent, also via the departure recess  35 . 
         [0033]    In terms of manufacturing materials, the compensator may be manufactured through additive means (such as 3D-printing) or via investment casting and welding. Furthermore, it is recommended that the disclosed anatomical parts of the compensator be integral with each other for strength, resulting in one solid item, and homogeneous in terms of the material used. Suitable materials may include steel, nickel-chromium alloys, titanium, cobalt chrome, or other sturdy metals. 
         [0034]    In  FIG. 2 , an exemplary embodiment to the compensator shown in  FIG. 1  is illustrated. This embodiment additionally includes prongs  53  surrounding the departure recess  35 . As some gases (not shown) exit via the departure recess  35 , they expand into the prongs  53  and break apart, preventing a gas plume and minimizing flash. Furthermore, this embodiment of the compensator includes orientation bars  63  defined on the ceiling  31  of the expansion chamber. These orientation bars  63  serve to assist in installing the compensator on a barrel  11  in a straight, level manner. For instance, the orientation bars  63 , when at the 12 o&#39;clock position, confirm the compensator is orientated in the correct vertical position, thereby allowing the compensator to work as designed. The orientation bars  63 , thus, act as a visual cue, allowing a user looking at the compensator to quickly determine the compensator&#39;s position (i.e. whether it is off-center or not). 
         [0035]      FIG. 3  shows an exploded view of the embodiment of the compensator seen in  FIG. 2  in the form of two longitudinally-cut halves. This view provides insight in to the inner workings of the compensator. The threads  37  defined in the muzzle engagement recess  33  are now visible. The vectored flow nozzle  21  lies longitudinally forward of the threads  37  and the muzzle engagement recess  33 . The vectored flow nozzle  21  is integral to the compensator and connects the muzzle engagement recess  33  to the rest of the compensator, acting as a gateway to the expansion chamber  25 . In terms of its dimensions, the vectored flow nozzle&#39;s walls surround the barrel&#39;s axis  13  and come in very close proximity to the projectile (not shown) when it passes through the compensator along the barrel&#39;s axis  13 . The vectored flow nozzle  21  is placed very closely to the end of the gun barrel (not shown) due to the threads  37  in the muzzle engagement recess  33  attaching to the end of the gun barrel (not shown), thereby placing the vectored flow nozzle  21  very close to, but not attached to, the gun barrel. The gun barrel (not shown) engages via the threads  37  and upon firing, expels hot, expanding gases (not shown) longitudinally forward and vertically level along the barrel&#39;s axis  13  until it reaches the vectored flow nozzle  21 , at which point, the gases change course to flow vertically downward and longitudinally downward as they enter the expansion chamber  25 . After gases change their primary trajectory to one with a downward angle, the downward angle of the gases increases as they rush past the compression ramp  47 . In this embodiment, a plurality of dimples  49  is defined on the surface of the compression ramp  47 . The compression ramp  47  acts as an anti-recoil surface, pushing the gun barrel down when gases strike it. The compression ramp dimples  49  increase the surface area of the compression ramp, induce drag on the gases rushing past them (thereby acting as their own counter-recoil surfaces), and draw gases closer to the surface of the compression ramp  47 . The net effect is more gases on a direct collision course with the curved primary anti-recoil surface  43  and therefore more counter-recoil force generated by the compensator. Furthermore, the vectored flow nozzle  21 , assisted by the dimples  49  on the compression ramp  47 , allows for a decrease in flash produced by the compensator because gases no longer simply follow the barrel&#39;s axis  13  and exit via the departure recess  35 . 
         [0036]      FIG. 4  shows a sectional view of the embodiment of the compensator from  FIG. 3  affixed to a threaded gun muzzle  23 , allowing a more clear view of the vectored flow nozzle  21 . As depicted, the vectored flow nozzle very clearly is angled to guide gas flow  65  forward and downward, yet allow a clear, straight path for a projectile  61  to pass through the compensator without deviating from its trajectory along the barrel&#39;s axis  13 . As stated previously, the vectored flow nozzle  21  is integral to the rest of the compensator and dictates the downward angle of gas flow  65  into the expansion chamber  25 . As the projectile  61  passes through the compensator, it passes through the vectored flow nozzle  21  within very close proximity to each other; this tight tolerance allows the vectored flow nozzle to engage with the gas flow  65  before it has a change to really expand. Optimally, the inner diameter of the vectored flow nozzle will be very comparable if not equal to the diameter of the exit recess  35 , which is only slightly larger than the diameter of the projectile  61 . Furthermore, optimally, the downward angle of the walls of the vectored flow nozzle  21  ranges from −15° to −30° from the barrel&#39;s axis  13 . The larger the projectile  61  caliber is, the steeper the recommended downward angle of the vectored flow nozzle becomes so as to prevent gases from exiting a therefore physically larger departure recess  35 . Furthermore, steeper downward angles in the walls of the vectored flow nozzle  21  impart more counter-recoil forces due to more gas flow  65  striking the curved primary anti-recoil surface  43 . Gases  65  flow along their new trajectory, are deflected downward more as they rush past the dimples  49  on the compression ramp  47 , at which point gases proceed to strike the curved primary anti-recoil surface  43  and exit via the elongated ports  27 . The port bleed ramps  55 , defined in the elongated ports  27 , are angled surfaces that further vector gases diagonally (i.e. laterally outward and longitudinally forward) away from the shooter so as to minimize any concussion or flash experienced. 
         [0037]      FIG. 5  shows the sectional view of the embodiment of the compensator from  FIG. 4  once gas strikes the curved primary anti-recoil surface  43 . The elongated ports (not shown) and port bleed ramps (not shown) are only omitted from this figure to illustrate the interaction of the eddy  67  within the compensator. Some gas flow  65  forms an eddy  67  and circles within the compensator. To minimize this, an internal flow mound  51 , defined in the expansion chamber&#39;s ceiling  31  and being in close proximity to the front wall  41 , reduces the maximum diameter the eddy  67  can become while also leaving clearance for the projectile  61 , thereby minimizing the potential for increased flash during rapid firing. The internal flow mound  51  extends vertically downward from the ceiling  31  in close proximity to the projectile  61  as it passes through the expansion chamber  25 . In an exemplary embodiment, the flow mound  51  may be as close as a few one hundredths of an inch—it may be as close as possible without risking possible contact with the projectile, taking into account the manufacturing tolerances for both, the compensator as well as the projectile. In its preferred embodiment, the integral flow mound  61  extends vertically downward to be level to the upper portion of the departure recess  35 . 
         [0038]      FIG. 6  shows a sectional view of an alternate embodiment of the compensator from  FIG. 4  with a modified means of attachment to the gun barrel  11 . This embodiment attaches over an existing muzzle device  59  where the muzzle engagement recess  33  connects via a quick-detach mount  57  and functions in otherwise the same manner as the embodiment of the compensator shown in  FIG. 4 . For the purpose of clarity, an example of an existing muzzle device  59  is a traditional muzzle brake featuring a quick-detach mount  57  allowing itself to be affixed to the gun barrel  11 . 
         [0039]      FIG. 7  shows a sectional view of an alternate embodiment of the compensator from  FIG. 4  featuring aflat primary anti-recoil surface  45 . The flat primary recoil surface provides gas flow  65  the opportunity to strike a substantially planar surface angled to be perpendicular to its trajectory, resulting in the generation of a sharp impulse of anti-recoil force and is angled relative to the longitudinal axis of the gun barrel  11 . 
         [0040]      FIG. 8  shows a sectional view of yet another embodiment of the compensator from  FIG. 4  featuring an angled front wall  41  that joins the angled flat primary anti-recoil surface  45 . This configuration angles the front wall  41  with the angled flat primary anti-recoil surface  45  to maximize the total surface area perpendicular to the gas flow  65  due to the aiming of these gases by the vectored flow nozzle  21 . 
         [0041]      FIG. 9  shows a sectional view of an alternate embodiment of the compensator in  FIG. 5  a curved front wall  68  that joins the curved primary anti-recoil surface  43 , thereby catching and cradling gas flow  65  in a way that provides a downward force and therefore further decreases muzzle climb.  FIG. 9  also features a plurality of interior thrust beams  72 , which serve to redirect the trajectory of the gas flow  65  to maximize the effectiveness of the curved primary anti-recoil surface  43 . The interior thrust beams  72  within the expansion chamber  25  span the lateral width of the chamber, provide structural integrity and act as an additional surface for the gas flow  65  to strike against. In an exemplary embodiment, the interior thrust beams  72  are substantially wing-like in appearance and structure, being relatively flat, having a relatively thin cross-section, and able to influence the path of gas flow  65 . The curved front wall  68  naturally allows for maximum surface area when catching expanding gases from the gas flow  65  that may be traveling along the barrel axis  13  and departing from the intended downward trajectory due to the aiming of these gases by the vectored flow nozzle  21 . Furthermore, this alternate embodiment also features a forward-facing vent  71  defined in the curved primary anti-recoil surface  43  allowing the gas flow  65  to exit the compensator substantially forward. In this illustration, the forward-facing vent  71  is angled slightly upward to allow gas flow  65  exiting the compensator to impart a downward force further mitigating muzzle rise. 
         [0042]      FIG. 10  displays a perspective view of an alternate embodiment of the compensator in  FIG. 1  featuring various porting configurations. Elongated ports  27  can be seen on the side walls  39  of the compensator alongside  73  non-elongated wall ports. These different port types can work together forming a synergy between the two types, wherein non-elongated wall ports  73  allow for gas flow (not shown) to be aimed, generating more force to counter recoil and lower the compensator&#39;s internal pressure, elongated ports  27  allow for flash reduction and concussion mitigation. In addition to these, vertical ports  69  can be seen proximal to the front wall  41 . Furthermore, ports that are distant from the front wall  41 , hereafter referred to as distal ports  70 , can be seen someone proximal to the muzzle engagement recess  33 . Distal ports  70  allow gas flow to exit in a way allowing for a lower internal pressure within the compensator while also introducing oxygen into the compensator, limiting flash, lowering recoil, and mitigating muzzle rise. Furthermore, several forward-facing vents  71  can be seen defined in the curved primary anti-recoil surface  43 . These forward-facing vents  71  provide another means of reducing pressure within the compensator but also may provide muzzle climb reduction as well. 
         [0043]      FIG. 11  displays an exploded view of an alternate embodiment of the compensator in  FIG. 3  featuring a plurality of interior thrust beams  72 . This three dimensional, exploded view provides additional insight in terms of the preferred positioning of the interior thrust beams  72  positioned within the expansion chamber  25 . 
         [0044]    Various embodiments of invention are described below. 
         [0045]    A recoil-reducing apparatus configured to be affixed to a muzzle of a gun having a gun barrel, wherein the apparatus comprises: a muzzle engagement recess configured to be positioned coaxial to and longitudinally forward of said gun barrel; a vectored flow nozzle positioned coaxial to and longitudinally forward of said muzzle engagement recess; an expansion chamber positioned longitudinally forward of said vectored flow nozzle comprising: a front wall; a ceiling extending from the muzzle engagement recess to the front wall; an angled anti-recoil surface extending from the front wall and facing the muzzle; a compression ramp extending longitudinally from the vectored flow nozzle to the flat anti-recoil surface; first and second lateral walls extending from the vectored flow nozzle to the front wall and from the ceiling to the compression ramp; a departure recess defined in the front wall and positioned longitudinally forward of and coaxial to said gun barrel and said vectored flow nozzle; and a plurality of approximately horizontal elongated ports defined in the first and second lateral walls proximal to the flat anti-recoil surface, wherein the expansion chamber defines an asymmetric internal volume expanding downward relative to the longitudinal axis of the gun barrel; and/or 
         [0046]    Said compression ramp includes a plurality of surface dimples; and/or 
         [0047]    A plurality of prongs are positioned longitudinally forward of and in close proximity to said departure recess; and/or 
         [0048]    Said muzzle engagement recess engages said muzzle via threads on said gun barrel; and/or 
         [0049]    Said muzzle engagement recess engages an existing muzzle device on said gun barrel via a quick-detach mount; and/or 
         [0050]    Said ceiling in said expansion chamber further comprises an internal flow mound proximal to said front wall; and/or 
         [0051]    Said approximately horizontal elongated ports further comprise bleed ramps; and/or 
         [0052]    Said front wall is angled. 
         [0053]    A recoil-reducing apparatus configured to be affixed to a muzzle of a gun having a gun barrel, wherein the apparatus comprises: a muzzle engagement recess configured to be positioned coaxial to and longitudinally forward of said gun barrel; a vectored flow nozzle positioned coaxial to and longitudinally forward of said muzzle engagement recess; an expansion chamber positioned longitudinally forward of said vectored flow nozzle comprising: a front wall; a ceiling extending from the muzzle engagement recess to the front wall; a curved anti-recoil surface extending from the front wall and facing the muzzle; a compression ramp extending longitudinally from the vectored flow nozzle to the curved anti-recoil surface; first and second lateral walls extending from the vectored flow nozzle to the front wall and from the ceiling to the compression ramp; a departure recess defined in the front wall and positioned longitudinally forward of and coaxial to said gun barrel and said vectored flow nozzle; and a plurality of approximately horizontal elongated ports defined in the first and second lateral walls proximal to the curved anti-recoil surface, wherein the expansion chamber defines an asymmetric internal volume expanding downward relative to the longitudinal axis of the gun barrel; and/or 
         [0054]    Said compression ramp includes a plurality of surface dimples; and/or 
         [0055]    A plurality of prongs are positioned longitudinally forward of and in close proximity to said departure recess; and/or 
         [0056]    Said muzzle engagement recess engages said muzzle via threads on said gun barrel; and/or 
         [0057]    Said muzzle engagement recess engages an existing muzzle device on said gun barrel via a quick-detach mount; and/or 
         [0058]    Said ceiling in said expansion chamber further comprises an internal flow mound proximal to said front wall; and/or 
         [0059]    Said approximately horizontal elongated ports further comprise bleed ramps; and/or 
         [0060]    Said front wall is angled. 
         [0061]    Although the description above contains many specificities, these should not be construed as limiting the scope of embodiments but as merely providing illustrations of some of several embodiments. Different embodiments may include different combinations of one or more disclosed features. 
         [0062]    While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. For instance, while the illustrations and the associated descriptions may include different aspects of the invention, one or more features may be omitted in a given embodiment without departing from the scope of the invention. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority. 
       DRAWINGS—REFERENCE NUMERALS 
       [0063]      11  gun barrel 
         [0064]      13  barrel axis 
         [0065]      15  vertical axis 
         [0066]      17  lateral axis 
         [0067]      19  longitudinal axis 
         [0068]      21  vectored flow nozzle 
         [0069]      23  gun muzzle 
         [0070]      25  expansion chamber 
         [0071]      27  elongated ports 
         [0072]      29  wrench flats 
         [0073]      31  ceiling 
         [0074]      33  muzzle engagement recess 
         [0075]      35  departure recess 
         [0076]      37  threads 
         [0077]      39  side wall 
         [0078]      41  front wall 
         [0079]      43  curved primary anti-recoil surface 
         [0080]      45  angled primary anti-recoil surface 
         [0081]      47  compression ramp 
         [0082]      49  compression ramp dimples 
         [0083]      51  internal flow mound 
         [0084]      53  prongs 
         [0085]      55  port bleed ramps 
         [0086]      57  quick-detach mount 
         [0087]      59  Existing muzzle device 
         [0088]      61  projectile 
         [0089]      63  orientation bars 
         [0090]      65  gas flow 
         [0091]      67  eddy 
         [0092]      68  curved front wall 
         [0093]      69  vertical ports 
         [0094]      70  distal ports 
         [0095]      71  forward-facing vent 
         [0096]      72  interior thrust beam 
         [0097]      73  non-elongated wall ports