US812140A - Gun-barrel for pistols, rifles, and ordnance. - Google Patents
Gun-barrel for pistols, rifles, and ordnance. Download PDFInfo
- Publication number
- US812140A US812140A US16704401A US1901167044A US812140A US 812140 A US812140 A US 812140A US 16704401 A US16704401 A US 16704401A US 1901167044 A US1901167044 A US 1901167044A US 812140 A US812140 A US 812140A
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- Prior art keywords
- bore
- muzzle
- barrel
- gas
- bullet
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000001105 regulatory effect Effects 0.000 description 8
- 238000010276 construction Methods 0.000 description 7
- 230000003292 diminished effect Effects 0.000 description 4
- 230000035515 penetration Effects 0.000 description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 235000020030 perry Nutrition 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/28—Gas-expansion chambers; Barrels provided with gas-relieving ports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A21/00—Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
- F41A21/32—Muzzle attachments or glands
- F41A21/36—Muzzle attachments or glands for recoil reduction ; Stabilisators; Compensators, e.g. for muzzle climb prevention
- F41A21/38—Muzzle attachments or glands for recoil reduction ; Stabilisators; Compensators, e.g. for muzzle climb prevention adjustable, i.e. the vent holes or the vent area being adjustable
Definitions
- My im rovement consists in perforating the barrel of the-gun at or near the muzzle with several small holes or orifices drilled into the bore at a greater or less an le thereto or otherwise, so as to enter the riflmg at a point inside of the muzzle, or they may be drilled into the barrel from around the outside of the muzzle, so as to enter the bore from the sides of the barrel, or these pressure-relief channels may be so constructed as to run parallel with the bore, or nearly so, and coalesce therewith wholly or in part, as deemed expedient.
- perforations or openings are so calculated as to enter the bore between the lands thereof or Within the grooves of the rifling; but they can be located in any desired position and be of any angle, shape, or size deemed ex edient,'and where the lands are wide enoug to admit. thereof they'can be ar ranged so as to enter the lands as well as the.
- the object of this invention is to improve the barrels of rifled firearms and ordnance of all kinds (as they are now generally manufactured) so as to increase their accuracy and efficiency in ejecting the bullets or. projectiles therefrom, give a more steady and effective flight and a greater range and more penetration thereto, and materially reduce the recoil. This will obviatethe necessity of giving so great a twist to the rifling in order to keep the bullet point-on during its flight,
- openings may take the form of channels constructed at an angle to the line of flight or channels so constructed that the exhaust will be in direction.of or parallel with the line of flight, thus utilizing the escaping force to form a current of moving gas, which by its being capable of moving faster than the p1'o je'otile it pro els precedes the delivery of the same by rus ling through these channels and forms a surrounding or enveloping current in direction of the line of flight, thus materially assisting in accelerating the momentum as well as steadying and aiding the accuracy of the delivery.
- I also provide several lengths, sizes, styles, and variety of construction of regulating or adjustingplugs, which may be inserted into these openings when and where desired.
- the grooves of the bore are uniformly of the same depth throu hout, and the lands are correspondingly a l of the same relative height or protrude uniformly the same into the bore, leaving the bore proper (comprising lands and grooves) all of the same uniform size throughout, save in the best or most accurate ones, where a converging bore or slightlycontracted portion at muzzle is deemed preferable, which serves, if anything, to confine the gas still more securely until the base of the bullet has parted with the muzzle of the piece.
- the chief object of this invention is to provide gas-exits or pressure-relief vents that will permit of the lessening of the tremendous pressure behind as the bullet leaves the bore, so as to deliver it in a steadier manner and at the same time to utilize the escaping 'gas by forming a rapidly-moving current preceding and accompanying its issue and encircling, sustaining, and aiding the flight of the bullet.
- Figure 1- is a perspective view of the device.
- Fig. 2 shows a longitudinal section of Fi .,1.
- Fig. 3 shows a perspective view of a modi cation.
- Fig.- 4 shows a longitudinal view of same.
- Fig. 5 shows various constructions of the adjustable. regulating-plugs. V
- any desired relief can be secured adaptable tovarious charges in the same gun, and the area of escape can be so very accurately and completely controlled and regulated that it can e made to completely transpose itself or to .converge toward or diverge from the center, if deemed expedient, or assume a more or less interrupted character throughout the whole series, either longitudinally orlcircumferentially considered.
- the solid plug a is used for completely shutting off any desired perforation. shows a very small aperture for materially Plug a reducing the volume of the exhaust, while a and a have larger apertures for the purpose of modifying or slightly reducing the volume of exhaust from any desired opening. a is another form of construction of the plug which is susceptible of still further alteration in construction.
- a rifled barrel containing a series of perforations or gas escape openings near the muzzle with means consisting of perforated 1glugs inserted therein, by which the distance om the muzzle to the nearest full 0 enings may be increased or diminished, and t e-area or volume of escape be thereby changed or regulated as desired.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Description
'PATENYTED FEB. 6, 1906.
P. E. KENT.
GUN BARREL FOR PISTOLS, RIFLES, AND ORDNA'NCE. APPLICATION rmm JUNE 14, 1901. 11211211111) JULY 25, 1903.
Witnesses.- 694x61 'fl UNITED sTATEs PATENT. OFFICE.
PERRY E. KENT, OF UTICA, NEW YORK.
GUN- BARREL FOR PISTOLS, RIFLES, AND ORDNANGE Specification of Letters Patent.
Patented Feb. 6, 1906.
Application filed June 14, 1901. Renewed July 25, 1903. Serial No. 167,044.
clear, and exact description of the invention,
which will enable others skilled in the art to which it appertains to make and use the same, reference being had to the accompanying drawings, and to the letters of reference marked thereon, Which'form part of this specification My im rovement consists in perforating the barrel of the-gun at or near the muzzle with several small holes or orifices drilled into the bore at a greater or less an le thereto or otherwise, so as to enter the riflmg at a point inside of the muzzle, or they may be drilled into the barrel from around the outside of the muzzle, so as to enter the bore from the sides of the barrel, or these pressure-relief channels may be so constructed as to run parallel with the bore, or nearly so, and coalesce therewith wholly or in part, as deemed expedient. These perforations or openings are so calculated as to enter the bore between the lands thereof or Within the grooves of the rifling; but they can be located in any desired position and be of any angle, shape, or size deemed ex edient,'and where the lands are wide enoug to admit. thereof they'can be ar ranged so as to enter the lands as well as the.
grooves, or they may enter the lands and grooves alternately, so as to produce a more continuous or less interrupted exhaust; and, further, it consists of providing a means whereby the escape of gas therefrom can be wholl or partially shut off, regulated, or adjuste from any one of, or any series of, or any desired combination of, or the whole of the vents thus provided, at the will of the operator.
The object of this invention is to improve the barrels of rifled firearms and ordnance of all kinds (as they are now generally manufactured) so as to increase their accuracy and efficiency in ejecting the bullets or. projectiles therefrom, give a more steady and effective flight and a greater range and more penetration thereto, and materially reduce the recoil. This will obviatethe necessity of giving so great a twist to the rifling in order to keep the bullet point-on during its flight,
thus decreasing erosion to a great degree and the cause of the excessive heating of the barrel in firing the piece continuously, chiefly due to friction of the bullet on the walls of the bore, in compelling rotation, and to provide improved means for regulating and controlling the escape of gas or pressure from the barrel at the moment of or just prior'to the axit of the projectile. In order to accomplish this result, I provide pressure-relief passages, which operate just prior to the issue of the bullet from the muzzle. These openings may take the form of channels constructed at an angle to the line of flight or channels so constructed that the exhaust will be in direction.of or parallel with the line of flight, thus utilizing the escaping force to form a current of moving gas, which by its being capable of moving faster than the p1'o je'otile it pro els precedes the delivery of the same by rus ling through these channels and forms a surrounding or enveloping current in direction of the line of flight, thus materially assisting in accelerating the momentum as well as steadying and aiding the accuracy of the delivery. I also provide several lengths, sizes, styles, and variety of construction of regulating or adjustingplugs, which may be inserted into these openings when and where desired.
is discharged, there is left on the muzzle of the piece a deposit of burned powder or aresiduum which radiates from the bore outwardly and seenis to be more or less in evidence, ac-
rounding, countersunk, or flat, and diminishes in density as the radius increases. This is caused by the gas or propelling forces w1thin the barrel seeking exit and indicates a spiteful blast at the muzzle at right angles to the line of flight and leads to the conclusion that when the base of the comparatively slow moving bullet arrives at the edge of the muzzle the more elastic gas rushes out and past it 111 all directions and more sharply and detrimentally so just at this very instant of parting with the edge of the muzzle. This powerfu esca ing gas at the instant of separation catc es onto the burs at the base of the bullet (left there by the lands of the rifling) or other imperfections and forces the rear of the now independently-moving and unsupported pros Whenever a rifle, cannon, or other firearm cordingly as the construction of the muzzle [S v jec'tile out of a correct line, giving it a -tendency to wabble and vary from the direction imparted to it coincident withthe bore of the arm, causing it to keyhole or turn over in its flight or tip more or less in spite of its rotary motion, causing the base of the bullet to rotate around a periphery greater than its own circumference, thereby developing an unnecessary area of air-resistance. Consequently less penetration is obtained, and an unsteady, erratic, and unreliable flight is the result, and in my estimation it is chiefly due to this eccentric centrifugal force caused by the deleterious action of the gas upon the base of the bullet as it leaves the guiding confines of the bore which is the sole cause of the wellknown corkscrew motion so common to all elongated projectiles during the first portion of their fli ht. It is to overcome this tendency v that a s arp twist is necessary, and more particularly so in modern high-power rifles. In all properly constructed rifledarms the grooves of the bore are uniformly of the same depth throu hout, and the lands are correspondingly a l of the same relative height or protrude uniformly the same into the bore, leaving the bore proper (comprising lands and grooves) all of the same uniform size throughout, save in the best or most accurate ones, where a converging bore or slightlycontracted portion at muzzle is deemed preferable, which serves, if anything, to confine the gas still more securely until the base of the bullet has parted with the muzzle of the piece. The chief object of this invention is to provide gas-exits or pressure-relief vents that will permit of the lessening of the tremendous pressure behind as the bullet leaves the bore, so as to deliver it in a steadier manner and at the same time to utilize the escaping 'gas by forming a rapidly-moving current preceding and accompanying its issue and encircling, sustaining, and aiding the flight of the bullet. I
Referring to the accompanying drawings, Figure 1- is a perspective view of the device. Fig. 2 shows a longitudinal section of Fi .,1. Fig. 3 shows a perspective view of a modi cation. Fig.- 4 shows a longitudinal view of same. Fig. 5 shows various constructions of the adjustable. regulating-plugs. V
It is apparent that by combining lateral entrances to the bore and longitudinal exits at the muzzle and then pluggingthe outer end of the lateral hole an exhaust is thereby created at the muzzle around and encircling the one from the bore and parallel with the line of flight prior to the exit of the bullet, thus creating a current of rapidly-moving atmosphere in the path which the bullet is to travel, which not only greatly lessens the 7 air resistance which the bullet would otherwise. meet upon emerging from the bore,
but by being delivered in a correct manner from the muzzle of a gun with this improvement the peculiargyrations which the projectile has heretofore been subject to does not now exist. Therefore more penetration and greater accuracy is the result, and not on account of attaining an increased muzzle velocity, but by materially reducing the area of the air-resisting surface of the bullet durin its flight in consequence of its being delivere with its longitudinal axis coincident with the axis of the bore instead of in the usual manner, whereby the rear axis of the bullet is forced to diverge from its path or compelled to assume a greater or less angle with the tangent of the trajectory. It is also ap arent in this construction that with the ex aust at cling escaping gas, which completely surore behind rounds the one issuing from the the bullet, the one from the bore is more completely confined to its own circumferential column, and therefore does not get the chance to so detrimentally effect the bullet at the instant of its delivery by so vicious a diverging, influence which is effectively neutralized, and
the whole column is kept moving in a more com act and less detrimental manner, with the efore-mentioned results.
Referring more particularly to the openings for the escape of gas both longitudinally and circumferentially, I refer to make them all of a uniform size, so t at one plug may be interchangeable throughout; but as very few rifled barrels exactly correspond throughout with those of other makers it is obvious that the style, size, and formation of the perforations will be governed by the arm it is to be used upon and the conditions to be met. It is very evident, however, that by the use of these adjustable regulating-plu s any desired relief can be secured adaptable tovarious charges in the same gun, and the area of escape can be so very accurately and completely controlled and regulated that it can e made to completely transpose itself or to .converge toward or diverge from the center, if deemed expedient, or assume a more or less interrupted character throughout the whole series, either longitudinally orlcircumferentially considered.
The solid plug a is used for completely shutting off any desired perforation. shows a very small aperture for materially Plug a reducing the volume of the exhaust, while a and a have larger apertures for the purpose of modifying or slightly reducing the volume of exhaust from any desired opening. a is another form of construction of the plug which is susceptible of still further alteration in construction.
If it is found more desirable or beneficial (in using several kinds or varieties of explosives or more or less quantities thereof or for any other cause) to increase the distance from the muzzle to the first series of openings or diminish the capacities thereof, it is obvious that it can be very quickly, easily, and effectively accomplished, so that virtually by this construction and the use of the plugs here provided not only the capacities of the several vent-holes may be nicely regulated, but the approximate distance from the muzzle to the first or other circumferential series of openings may be virtually increased or diminlshed at will, thereby practically allowing the exhausting or venting of the pressure within the barrel to be accomplished nearer to or farther away from the muzzle or the volume thereof diminished or increased at either end of the longitudinal series or any intermediate portion thereof. It is apparent that by compelling this relief-exhaust to be delivered through these gas-ports independent from and encircling the main one issuing from the bore a separate enveloping preceding current is formed that not only relieves the excessive ressure at the muzzle at the moment of deivery, but also creates a suction in front of the bore proper, into the vortex of whichthe projectile is launched with a pulling force" from in front, as well as a pushing efiect from bghind from the gas yet contained in the barre Having full described this invention, what I claim, and esire to secure by Letters Pat: cut, is
1. A rifled barrel containing a series of perforations at the muzzle, adjacent to and encircling the borc, having the egress of the several openings located between the circumference of the barrel and the bore of the iece, and the ingress to the rear of the muzz e.
2. A rifled barrel containing a series of longitudinal gas-escape channels located between the-circumference of the barrel and the periphery of'the bore, having their openings at the muzzle, and intersecting the bore rearwardly thereof, permitting a portion of the gas-pressure to thereby escape past the bullet, in direction of'and substantially parallel to the line'of flight, prior to the exuding of the bullet, thus forming a preceding, encompassing, and separate current from the one im mcdiately thereafter issuing from the bore.
3. A rifled barrel containing a series of perforations encircling the muzzle, entering the bore at an angle to the line of flight, with means which enter into said perforations by means of which one or more of said perforations can be diminished, adjusted or varied in capacity.
4. A rifle-barrel containing a series of perforations encircling the muzzle and entering the bore of the piece, in combination with one or more plugs inserted therein for reguwith means for partially closing said holes by the use of plugs or their equivalent entering said holes, essentially as shown and described.
7. A rifled barrel containing a series of erforations or gas escape openings encirc ing the muzzle and entering the bore thereof, with means entering into any one or more of said perforations by which the circumferential area of gas-escape may be diminished, regulated or changed wholly or in part, essentially as described.
8. A rifle-barrel containing a series of erforations orgas-escape 'openings encirc ing the muzzle, and means by which the longitudinal area of gas-esca e may be varied, regulated, or changed in ependently of the circumferential area, essentially as set forth.
9. A rifled barrel containing a series of perforations or gas escape openings near the muzzle, with means consisting of perforated 1glugs inserted therein, by which the distance om the muzzle to the nearest full 0 enings may be increased or diminished, and t e-area or volume of escape be thereby changed or regulated as desired.
10. "A gun-barrel containing a series of gasescape openings encircling the bore, fitted with plugs containing openings through which the propelling force may find exit prior to the bullet leaving the muzzle thereof.
11. A gun-barrelcontaining a multiple of longitudinal gas-escape channels, adjacent to and encircling the bore of the iece, having their exits between the circum erence of the barrel and the periphery of the bore, intersecting the bore rearwardly of the muzzle, through which a portion of the gas-pressure may escape prior to the parting of the rear end of the bullet with the muzzle of the piece in direction of the line of flight; in combination with spirally-cut grooves or rifling within the bore of the piece.
12. A rifle -barrel containing a series of lateral gas escape channels, one or more of which are estopped at the outer opening of same. with lugs, coalescing with a series of In Witness whereof I have afiixe'cl my siglongitudinaFgas-escape channels located benature,inpresence of two Witnesses, this 12th tween the circumference of the bore and the day of June, 1901.
circumference of the barrel, permitting the PERRY E. KENT. 5 gas to escape approximately parallel to the Witnesses:
line of flight separately from the blast issuing G. M. JONES,
from the bore. CLAUDE E. HAKES.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16704401A US812140A (en) | 1901-06-14 | 1901-06-14 | Gun-barrel for pistols, rifles, and ordnance. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16704401A US812140A (en) | 1901-06-14 | 1901-06-14 | Gun-barrel for pistols, rifles, and ordnance. |
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US812140A true US812140A (en) | 1906-02-06 |
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US16704401A Expired - Lifetime US812140A (en) | 1901-06-14 | 1901-06-14 | Gun-barrel for pistols, rifles, and ordnance. |
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Cited By (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442899A (en) * | 1946-04-08 | 1948-06-08 | William H Mcallister | Choke attachment for gun barrels |
US2466400A (en) * | 1947-11-06 | 1949-04-05 | Ennis Darwin Tucker | Recoil-reducing and shot-patterncontrolling device for shotguns |
US2558200A (en) * | 1946-01-29 | 1951-06-26 | William F Schmeling | Shotgun choke |
US2916970A (en) * | 1956-02-10 | 1959-12-15 | John F Mutter | Anti-recoil gun barrels |
US4058050A (en) * | 1976-07-19 | 1977-11-15 | Dan Wesson Arms, Inc. | Gun leveling device |
US4534264A (en) * | 1983-04-06 | 1985-08-13 | Tarnoff Sherwin S | Recoil reducer |
US5033356A (en) * | 1990-01-16 | 1991-07-23 | Richardson H Gary | Firearm with noise suppressor |
US5092223A (en) * | 1991-01-22 | 1992-03-03 | Hudson Lee C | Muzzle brake and flash hider |
US5320022A (en) * | 1993-02-18 | 1994-06-14 | Gunstar, Inc. | Apparatus for reducing recoil and muzzle climb from discharge of firearms |
US5509345A (en) * | 1994-01-26 | 1996-04-23 | Cyktich; James M. | Muzzle attachment for improving firearm accuracy |
US5753846A (en) * | 1996-11-19 | 1998-05-19 | Sigma Research Inc. | Barrel extender with recoil reduction |
US20030024377A1 (en) * | 2001-08-03 | 2003-02-06 | Diller E. Wendell | Elongated vented gun barrel |
EP1432310A4 (en) * | 2001-01-31 | 2006-06-21 | Univ Arizona | METHOD FOR THE TREATMENT OF CHRONIC HEART FAILURE AND / OR INCREASED CHOLESTERIN MIRROR BY MEANS OF 3,5-DIIODYTHROPROPIONIC ACID, AND METHOD FOR THE PRODUCTION THEREOF |
WO2008090385A1 (en) * | 2007-01-23 | 2008-07-31 | Kukhaleishvili Rati | Method for increasing the muzzle velocity of a bullet in a rifle-bore weapon and a barrel of the abramian's rifle-bore weapon |
US20100294118A1 (en) * | 2009-05-21 | 2010-11-25 | Colt Canada Corporation | Firearm flash suppressor |
US8091263B1 (en) | 2010-07-30 | 2012-01-10 | John Palmer | Reduced recoil choked shotgun barrel |
EP2479526A1 (en) * | 2011-01-22 | 2012-07-25 | Rudolf Lehnert | Return compensator |
US8695474B2 (en) | 2010-05-06 | 2014-04-15 | Battle Comp Enterprises, Llc | Muzzle device and method of tuning thereof |
US9303939B1 (en) * | 2015-05-21 | 2016-04-05 | Ar1510 Llc | Tunable muzzle brake |
US10012464B2 (en) * | 2015-09-16 | 2018-07-03 | NG2 Defense, LLC | Muzzle signature management device |
US20200025495A1 (en) * | 2018-01-23 | 2020-01-23 | Delta P Design, Inc. | Suppressor with blowout panel |
US10809033B2 (en) | 2017-11-29 | 2020-10-20 | Michael P. Tindal | Firearm compensator |
US20210356226A1 (en) * | 2020-01-31 | 2021-11-18 | Dustin Nicklaus Fromholtz | Muzzle brake compensator |
US20220049918A1 (en) * | 2015-08-12 | 2022-02-17 | John L. Baker | Structured Firearm Barrel |
US20240280340A1 (en) * | 2023-02-17 | 2024-08-22 | James Matthew Underwood | Muzzle device assemblies |
-
1901
- 1901-06-14 US US16704401A patent/US812140A/en not_active Expired - Lifetime
Cited By (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2558200A (en) * | 1946-01-29 | 1951-06-26 | William F Schmeling | Shotgun choke |
US2442899A (en) * | 1946-04-08 | 1948-06-08 | William H Mcallister | Choke attachment for gun barrels |
US2466400A (en) * | 1947-11-06 | 1949-04-05 | Ennis Darwin Tucker | Recoil-reducing and shot-patterncontrolling device for shotguns |
US2916970A (en) * | 1956-02-10 | 1959-12-15 | John F Mutter | Anti-recoil gun barrels |
US4058050A (en) * | 1976-07-19 | 1977-11-15 | Dan Wesson Arms, Inc. | Gun leveling device |
US4534264A (en) * | 1983-04-06 | 1985-08-13 | Tarnoff Sherwin S | Recoil reducer |
US5033356A (en) * | 1990-01-16 | 1991-07-23 | Richardson H Gary | Firearm with noise suppressor |
US5092223A (en) * | 1991-01-22 | 1992-03-03 | Hudson Lee C | Muzzle brake and flash hider |
US5320022A (en) * | 1993-02-18 | 1994-06-14 | Gunstar, Inc. | Apparatus for reducing recoil and muzzle climb from discharge of firearms |
US5509345A (en) * | 1994-01-26 | 1996-04-23 | Cyktich; James M. | Muzzle attachment for improving firearm accuracy |
US5753846A (en) * | 1996-11-19 | 1998-05-19 | Sigma Research Inc. | Barrel extender with recoil reduction |
EP1432310A4 (en) * | 2001-01-31 | 2006-06-21 | Univ Arizona | METHOD FOR THE TREATMENT OF CHRONIC HEART FAILURE AND / OR INCREASED CHOLESTERIN MIRROR BY MEANS OF 3,5-DIIODYTHROPROPIONIC ACID, AND METHOD FOR THE PRODUCTION THEREOF |
US20030024377A1 (en) * | 2001-08-03 | 2003-02-06 | Diller E. Wendell | Elongated vented gun barrel |
WO2008090385A1 (en) * | 2007-01-23 | 2008-07-31 | Kukhaleishvili Rati | Method for increasing the muzzle velocity of a bullet in a rifle-bore weapon and a barrel of the abramian's rifle-bore weapon |
US20100294118A1 (en) * | 2009-05-21 | 2010-11-25 | Colt Canada Corporation | Firearm flash suppressor |
US8342071B2 (en) * | 2009-05-21 | 2013-01-01 | Colt Canada Corporation | Firearm flash suppressor |
US8695474B2 (en) | 2010-05-06 | 2014-04-15 | Battle Comp Enterprises, Llc | Muzzle device and method of tuning thereof |
US8091263B1 (en) | 2010-07-30 | 2012-01-10 | John Palmer | Reduced recoil choked shotgun barrel |
EP2479526A1 (en) * | 2011-01-22 | 2012-07-25 | Rudolf Lehnert | Return compensator |
US9303939B1 (en) * | 2015-05-21 | 2016-04-05 | Ar1510 Llc | Tunable muzzle brake |
US20220049918A1 (en) * | 2015-08-12 | 2022-02-17 | John L. Baker | Structured Firearm Barrel |
US11709030B2 (en) * | 2015-08-12 | 2023-07-25 | John L. Baker | Structured firearm barrel |
US10012464B2 (en) * | 2015-09-16 | 2018-07-03 | NG2 Defense, LLC | Muzzle signature management device |
US10809033B2 (en) | 2017-11-29 | 2020-10-20 | Michael P. Tindal | Firearm compensator |
US10890403B2 (en) * | 2018-01-23 | 2021-01-12 | Delta P Design, Inc. | Suppressor with blowout panel |
US11326850B2 (en) * | 2018-01-23 | 2022-05-10 | Delta P Design, Inc. | Suppressor with blowout panel |
US20220221243A1 (en) * | 2018-01-23 | 2022-07-14 | Delta P Design, Inc. | Suppressor with blowout panel |
US20200025495A1 (en) * | 2018-01-23 | 2020-01-23 | Delta P Design, Inc. | Suppressor with blowout panel |
US12152852B2 (en) * | 2018-01-23 | 2024-11-26 | True Velocity IP Holdings, Inc. | Suppressor with blowout panel |
US20250146780A1 (en) * | 2018-01-23 | 2025-05-08 | True Velocity IP Holdings, Inc. | Suppressor with blowout panel |
US20210356226A1 (en) * | 2020-01-31 | 2021-11-18 | Dustin Nicklaus Fromholtz | Muzzle brake compensator |
US11703296B2 (en) * | 2020-01-31 | 2023-07-18 | Dustin Nicklaus Fromholtz | Muzzle brake compensator |
US20240280340A1 (en) * | 2023-02-17 | 2024-08-22 | James Matthew Underwood | Muzzle device assemblies |
US12359886B2 (en) * | 2023-02-17 | 2025-07-15 | James Matthew Underwood | Muzzle device assemblies |
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