US2567826A - Muzzle recoil check for firearms - Google Patents
Muzzle recoil check for firearms Download PDFInfo
- Publication number
- US2567826A US2567826A US27537A US2753748A US2567826A US 2567826 A US2567826 A US 2567826A US 27537 A US27537 A US 27537A US 2753748 A US2753748 A US 2753748A US 2567826 A US2567826 A US 2567826A
- Authority
- US
- United States
- Prior art keywords
- plates
- muzzle
- firearms
- pile
- recoil check
- 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
- 239000007789 gas Substances 0.000 description 9
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000003628 erosive effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 230000001603 reducing effect Effects 0.000 description 1
- 239000007787 solid Substances 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
- F41A21/32—Muzzle attachments or glands
- F41A21/36—Muzzle attachments or glands for recoil reduction ; Stabilisators; Compensators, e.g. for muzzle climb prevention
Definitions
- This invention relates 'to'a muzzle recoil check for firearms, of the type constituted by a pile of removable cup-shaped deflecting members supported by a cylindrical ibody bored substantially to ithe diameter of the b'arrel'a't the base of the the .said muzzle recoil :check comprising openings permitting the gases to escape-in order to impinge against the deflectors which deflect them laterally and rearwardly.
- the device proposed which combines these various known methods, has been designed with a view to simplifying the construction while ensuring the possibility of readily replacing the defiecting members, which'are exposed to erosion under the effect of the gas jets, and to enable the said device to be adapted with the minimum number of changes to different firin conditions and requirements as to output.
- the new muzzle recoil check is constituted by a hollow cylindrical body fitted on the muzzle of the barrel or made in one piece therewith, and provided with two opposite lateral openings of substantially rectangular form which extend over the entire length of the pile of deflecting members which are constituted by oblong plates bored to the external diameter of the aforesaid body.
- two lateral vanes symmetrically disposed to the right and to the left, and the said elements which are fitted over the said body and maintained in the correct position, being locked one against the other and against a shoulder on the body of the device by means of an end nut.
- Figure 1 is a longitudinal view of the device, one half of which is in section and the other half in elevation,
- Figure 2 is a plan, one half of which is again a sectional view and the other half an external View, I
- Figure 3 is a cross section on the line III-III of Figure 2.
- I designates the hollow cylindrical body of the muzzle recoil check secured by screwing on the beaded muzzle portion 2 of In France May- 31, I947 transverse direction) 'and'natur'ally has a bore "corresponding to the external diameter of the said body.
- the said plates are positioned and prevented from turning by a longitudinal key 5 secured in a groove lb in the body I, while the plates themselves have a similar groove 4a.
- the various plates in the pile which have parallel faces are locked one against the other and against a shoulder lc on the body I by a nut 6 screwed on the free extremity of the said body with the interposition of an adjusted member 1.
- the deflecting plates 4 have laterally hollowed therein concave surfaces 8 and convex surfaces 9 of suitable profile, so as to form guide vanes l0 and the shoulder lc of the body I is similarly shaped at H, so that the assemblage of plates, when mounted on the cylinder, forms on either side thereof three divergent nozzles through which there now the gases which have passed through the openings 3, whereby the desired reducing effect is produced on the recoil of the firearm.
- the pile of plates can be instantly dismounted by simply unscrewing the nut 6.
- the profile of the blades can vary within very wide limits from one vane to the other, and since it is easy to replace one or more of the plates in the same device by plates having vanes of diiferent profile from the vanes of the first plates, this method of construction renders the muzzle recoil check widely adaptable to the firing conditions and to the required output, which is not necessarily the maximum output.
- the angle of deflection from the first nozzle ll-8 is greater than that from the following two nozzles 9-8.
- a muzzle recoil check for firearms comprising a hollow cylindrical body adapted to be fitted on the muzzle of a firearm and having two laterally opposed and longitudinally elongated openings,
- means for controlling and deflecting the escaping gases comprising a pile of aligned deflector plates mounted on said body for longitudinal sliding movement, said plates having flat parallel surfaces for engagement with one another to form a solid pile, means 7 for locking said plates in engagement comprising a shoulder on said body at one end of the pile and anut on said body at the other end of the pile, said plates having projections extending outwardly from both sides of said body, and
- curved recesses cut into the opposite flat surfaces of each projection between its upper and lower margins to form substantially horizontal rearwardly curved vanes extending from said openings to the outer edges of said projections, said projections and vanes forming between them two rows of outwardly extending rearwardly curved nozzles one on each side of said body for de fleeting the gases escaping-through said openings, the vanes of individual plates having different curved profiles and said plates being interchangeable in the pile for adjustment of the curvature of the nozzles and of the recoil checking effect.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Food-Manufacturing Devices (AREA)
Description
Sept. 11, 1951 E, PRACHE 2,567,826
MUZZLE RECOIL CHECK FOR FIREARMS Filed May 17, 1948 Figl.
I lcvelufor Jacgues E il apraclze,
Attorneys Patented Sept. 11 1951 STATES OFFICE --.MUZZLE RECOIL CHECKJ QR-EIREARMS Jacques Emilien Praehe,fFontenay sous Bois, France, assignor to Schneider (lie, Paris,
France, 'a, special partnership of France a plication-Marv, 194's, "se i l'nafzassv 1 Claim.
1 "This invention relates 'to'a muzzle recoil check for firearms, of the type constituted by a pile of removable cup-shaped deflecting members supported by a cylindrical ibody bored substantially to ithe diameter of the b'arrel'a't the base of the the .said muzzle recoil :check comprising openings permitting the gases to escape-in order to impinge against the deflectors which deflect them laterally and rearwardly.
In devices comprising piles of deflectors of this nature, it is known to'c'losethe lowerpartofthe gaps separating the deflecting elements in'o'rd'er to prevent the gases escaping therefrom from scoring the ground below the gun. Muzzle recoil checks are also known which comprise solely lateral discharge orifices.
The device proposed, which combines these various known methods, has been designed with a view to simplifying the construction while ensuring the possibility of readily replacing the defiecting members, which'are exposed to erosion under the effect of the gas jets, and to enable the said device to be adapted with the minimum number of changes to different firin conditions and requirements as to output.
According to the invention, the new muzzle recoil check is constituted by a hollow cylindrical body fitted on the muzzle of the barrel or made in one piece therewith, and provided with two opposite lateral openings of substantially rectangular form which extend over the entire length of the pile of deflecting members which are constituted by oblong plates bored to the external diameter of the aforesaid body. there being formed in each of the said plates two lateral vanes symmetrically disposed to the right and to the left, and the said elements which are fitted over the said body and maintained in the correct position, being locked one against the other and against a shoulder on the body of the device by means of an end nut.
One embodiment of the invention is illustrated, by way of example, in the accompanying drawings, in which:
Figure 1 is a longitudinal view of the device, one half of which is in section and the other half in elevation,
Figure 2 is a plan, one half of which is again a sectional view and the other half an external View, I
Figure 3 is a cross section on the line III-III of Figure 2.
In these figures, I designates the hollow cylindrical body of the muzzle recoil check secured by screwing on the beaded muzzle portion 2 of In France May- 31, I947 transverse direction) 'and'natur'ally has a bore "corresponding to the external diameter of the said body. The said plates are positioned and prevented from turning by a longitudinal key 5 secured in a groove lb in the body I, while the plates themselves have a similar groove 4a. The various plates in the pile which have parallel faces are locked one against the other and against a shoulder lc on the body I by a nut 6 screwed on the free extremity of the said body with the interposition of an adjusted member 1.
The deflecting plates 4 have laterally hollowed therein concave surfaces 8 and convex surfaces 9 of suitable profile, so as to form guide vanes l0 and the shoulder lc of the body I is similarly shaped at H, so that the assemblage of plates, when mounted on the cylinder, forms on either side thereof three divergent nozzles through which there now the gases which have passed through the openings 3, whereby the desired reducing effect is produced on the recoil of the firearm.
As will be seen, the pile of plates can be instantly dismounted by simply unscrewing the nut 6.
Of course, the profile of the blades can vary within very wide limits from one vane to the other, and since it is easy to replace one or more of the plates in the same device by plates having vanes of diiferent profile from the vanes of the first plates, this method of construction renders the muzzle recoil check widely adaptable to the firing conditions and to the required output, which is not necessarily the maximum output.
It will be seen that in the embodiment illustrated the angle of deflection from the first nozzle ll-8 is greater than that from the following two nozzles 9-8. However, it may be advantageous toadopt the opposite arrangement in order to prevent deflection of the sheet of gases on to the gun crew, the gas sheets issuing from the downstream nozzles being broken against the what manner the same is to be performed, I
declare that what I claim is:
A muzzle recoil check for firearms comprising a hollow cylindrical body adapted to be fitted on the muzzle of a firearm and having two laterally opposed and longitudinally elongated openings,
for the escape of gases;"and means for controlling and deflecting the escaping gases comprising a pile of aligned deflector plates mounted on said body for longitudinal sliding movement, said plates having flat parallel surfaces for engagement with one another to form a solid pile, means 7 for locking said plates in engagement comprising a shoulder on said body at one end of the pile and anut on said body at the other end of the pile, said plates having projections extending outwardly from both sides of said body, and
curved recesses cut into the opposite flat surfaces of each projection between its upper and lower margins to form substantially horizontal rearwardly curved vanes extending from said openings to the outer edges of said projections, said projections and vanes forming between them two rows of outwardly extending rearwardly curved nozzles one on each side of said body for de fleeting the gases escaping-through said openings, the vanes of individual plates having different curved profiles and said plates being interchangeable in the pile for adjustment of the curvature of the nozzles and of the recoil checking effect.
JACQUES EMILIEN PRACHE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITE'Q STATES PATENTS Number Name Date 1,948,496 Barnes Feb. 2'7, 1934 2,088,380 Methlin July 27, 1937 FOREIGN PATENTS Number Country Date 125,141 Great Britain Apr. 17, 1919 715,769 France Sept. 29, 1931 454,533 Great Britain Oct. 2, 1936 828,320 France May 16, 1938 OTHER REFERENCES Pages 32-36, May-June 1945 issue of The Coast Artillery Journal.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR646871X | 1947-05-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2567826A true US2567826A (en) | 1951-09-11 |
Family
ID=9001714
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US27537A Expired - Lifetime US2567826A (en) | 1947-05-31 | 1948-05-17 | Muzzle recoil check for firearms |
Country Status (3)
Country | Link |
---|---|
US (1) | US2567826A (en) |
FR (1) | FR958162A (en) |
GB (1) | GB646871A (en) |
Cited By (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2663961A (en) * | 1950-07-07 | 1953-12-29 | White Madge Burnam | Choke for gun barrels |
US2953972A (en) * | 1958-09-02 | 1960-09-27 | Hans C Sorensen | Muzzle equalizer and blast minimizer for gun |
US3672255A (en) * | 1965-02-23 | 1972-06-27 | Us Army | Equal impulse firearm |
US4619182A (en) * | 1983-01-31 | 1986-10-28 | Saab-Scania Aktiebolag | Arrangement for deflecting powder gases from an aircraft weapon |
US5317825A (en) * | 1993-03-11 | 1994-06-07 | C.G.I. Corporation | Choke assembly for a shotgun |
US5320022A (en) * | 1993-02-18 | 1994-06-14 | Gunstar, Inc. | Apparatus for reducing recoil and muzzle climb from discharge of firearms |
US5415073A (en) * | 1994-03-14 | 1995-05-16 | Ciluffo; Gary | Recoil reducer for rifle, handgun, or shotgun |
US5631438A (en) * | 1995-04-17 | 1997-05-20 | Martel; Phillip C. | Adjustable gas pressure deflector |
WO1998054533A1 (en) * | 1997-05-30 | 1998-12-03 | Giat Industries | Muzzle brake for weapon barrel |
WO2002065045A2 (en) | 2001-02-09 | 2002-08-22 | Champion Edwin J | Muzzle brake |
US20050252365A1 (en) * | 2004-05-17 | 2005-11-17 | Giat Industries | Muzzle brakes for weapons |
US20080173166A1 (en) * | 2007-01-23 | 2008-07-24 | Andry Mark L | Shotgun choke |
US7581482B1 (en) * | 2005-07-28 | 2009-09-01 | The United States Of America As Represented By The Secretary Of The Army | Supersonic turning vane |
US20100269387A1 (en) * | 2006-02-28 | 2010-10-28 | Cornell Drajan | Muzzle Break |
US7895787B1 (en) | 2008-01-11 | 2011-03-01 | Andry Mark L | Porting feature for firearm |
US8424440B1 (en) * | 2011-07-13 | 2013-04-23 | The United States Of America As Represented By The Secretary Of The Army | Low blast overpressure muzzle brake |
WO2013160330A1 (en) * | 2012-04-24 | 2013-10-31 | Tda Armements S.A.S | Noise attenuator for a mortar |
WO2016115478A1 (en) * | 2015-01-16 | 2016-07-21 | Surefire, Llc | Firearm attachment |
US20160223281A1 (en) * | 2015-02-03 | 2016-08-04 | Edward Rigor Randall | Recoil reducing muzzle brake |
RU2616086C1 (en) * | 2016-01-11 | 2017-04-12 | Александр Алексеевич Семенов | Combined muzzle brake of artillery weapon |
US20170160036A1 (en) * | 2015-08-11 | 2017-06-08 | Drew Nolle Walker | Optimized flow compensator |
USD828899S1 (en) * | 2017-02-23 | 2018-09-18 | Crosman Corporation | Silencer |
US10088262B2 (en) * | 2016-09-26 | 2018-10-02 | U.S. Arms Llc | Muzzle brake device |
US10473415B2 (en) * | 2016-09-26 | 2019-11-12 | U.S. Arms Company Llc | Muzzle brake device |
US10520272B1 (en) * | 2018-03-23 | 2019-12-31 | The United States Of America As Represented By The Secretary Of The Army | Cannon recoil inhibitor and impulse noise attenuator |
WO2020055468A1 (en) * | 2018-09-13 | 2020-03-19 | James Eric Mcmillan | Muzzle brake device |
WO2020086201A3 (en) * | 2018-09-21 | 2020-06-18 | Christopher Armstrong | Muzzle brake device |
US10731940B2 (en) * | 2016-09-26 | 2020-08-04 | U.S. Arms Company Llc | Muzzle brake device |
US10788284B1 (en) * | 2019-05-09 | 2020-09-29 | The United States Of America As Represented By The Secretary Of The Army | Grounded and vehicular mounted weapons with improved recoil stability |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE510724A (en) * | 1951-04-18 | |||
DE1123951B (en) * | 1959-02-11 | 1962-02-15 | Rheinmetall Gmbh | Muzzle brake for firearms |
DE3205530A1 (en) * | 1982-02-17 | 1983-08-25 | Aktiebolaget Bofors, 69180 Bofors | MUFF BRAKE FOR ARTILLERY PROTECTORS |
DE4025546C2 (en) * | 1990-08-11 | 2002-03-14 | Rheinmetall W & M Gmbh | Muzzle brake for a large-caliber barrel weapon |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB125141A (en) * | ||||
FR715769A (en) * | 1930-04-26 | 1931-12-09 | Anciens Ets Skoda | Brake for muzzle hole |
US1948496A (en) * | 1932-02-17 | 1934-02-27 | Gladeon M Barnes | Muzzle brake for guns |
GB454533A (en) * | 1936-02-03 | 1936-10-02 | Vickers Armstrongs Ltd | Improvements in or relating to means for modifying the recoil of a gun |
US2088380A (en) * | 1934-12-07 | 1937-07-27 | Schneider & Cie | Muzzle recoil check for guns |
FR828320A (en) * | 1936-11-21 | 1938-05-16 | Brev & Procedes Coanda Sa D Et | Anti-kickback brake for firearms and the like |
-
0
- FR FR958162D patent/FR958162A/fr not_active Expired
-
1948
- 1948-05-06 GB GB12502/48A patent/GB646871A/en not_active Expired
- 1948-05-17 US US27537A patent/US2567826A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB125141A (en) * | ||||
FR715769A (en) * | 1930-04-26 | 1931-12-09 | Anciens Ets Skoda | Brake for muzzle hole |
US1948496A (en) * | 1932-02-17 | 1934-02-27 | Gladeon M Barnes | Muzzle brake for guns |
US2088380A (en) * | 1934-12-07 | 1937-07-27 | Schneider & Cie | Muzzle recoil check for guns |
GB454533A (en) * | 1936-02-03 | 1936-10-02 | Vickers Armstrongs Ltd | Improvements in or relating to means for modifying the recoil of a gun |
FR828320A (en) * | 1936-11-21 | 1938-05-16 | Brev & Procedes Coanda Sa D Et | Anti-kickback brake for firearms and the like |
Cited By (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2663961A (en) * | 1950-07-07 | 1953-12-29 | White Madge Burnam | Choke for gun barrels |
US2953972A (en) * | 1958-09-02 | 1960-09-27 | Hans C Sorensen | Muzzle equalizer and blast minimizer for gun |
US3672255A (en) * | 1965-02-23 | 1972-06-27 | Us Army | Equal impulse firearm |
US4619182A (en) * | 1983-01-31 | 1986-10-28 | Saab-Scania Aktiebolag | Arrangement for deflecting powder gases from an aircraft weapon |
US5320022A (en) * | 1993-02-18 | 1994-06-14 | Gunstar, Inc. | Apparatus for reducing recoil and muzzle climb from discharge of firearms |
US5317825A (en) * | 1993-03-11 | 1994-06-07 | C.G.I. Corporation | Choke assembly for a shotgun |
US5415073A (en) * | 1994-03-14 | 1995-05-16 | Ciluffo; Gary | Recoil reducer for rifle, handgun, or shotgun |
US5631438A (en) * | 1995-04-17 | 1997-05-20 | Martel; Phillip C. | Adjustable gas pressure deflector |
US6216578B1 (en) | 1997-05-30 | 2001-04-17 | Giat Industries | Muzzle brake for weapon barrel |
FR2764056A1 (en) * | 1997-05-30 | 1998-12-04 | Giat Ind Sa | MOUTH BRAKE FOR WEAPON TUBE |
WO1998054533A1 (en) * | 1997-05-30 | 1998-12-03 | Giat Industries | Muzzle brake for weapon barrel |
WO2002065045A2 (en) | 2001-02-09 | 2002-08-22 | Champion Edwin J | Muzzle brake |
US20050252365A1 (en) * | 2004-05-17 | 2005-11-17 | Giat Industries | Muzzle brakes for weapons |
FR2870331A1 (en) * | 2004-05-17 | 2005-11-18 | Giat Ind Sa | MOUTH BRAKE FOR ARMY |
EP1600723A1 (en) * | 2004-05-17 | 2005-11-30 | Giat Industries | Muzzle brake for firearm |
US7296505B2 (en) | 2004-05-17 | 2007-11-20 | Giat Industries | Muzzle brakes for weapons |
US7581482B1 (en) * | 2005-07-28 | 2009-09-01 | The United States Of America As Represented By The Secretary Of The Army | Supersonic turning vane |
US7600461B1 (en) * | 2005-07-28 | 2009-10-13 | The United States Of America As Represented By The Secretary Of The Army | Muzzle brake for cannon |
US20100269387A1 (en) * | 2006-02-28 | 2010-10-28 | Cornell Drajan | Muzzle Break |
US20080173166A1 (en) * | 2007-01-23 | 2008-07-24 | Andry Mark L | Shotgun choke |
US7895787B1 (en) | 2008-01-11 | 2011-03-01 | Andry Mark L | Porting feature for firearm |
US8424440B1 (en) * | 2011-07-13 | 2013-04-23 | The United States Of America As Represented By The Secretary Of The Army | Low blast overpressure muzzle brake |
WO2013160330A1 (en) * | 2012-04-24 | 2013-10-31 | Tda Armements S.A.S | Noise attenuator for a mortar |
AU2016206547B2 (en) * | 2015-01-16 | 2019-09-12 | Surefire, Llc | Firearm attachment |
WO2016115478A1 (en) * | 2015-01-16 | 2016-07-21 | Surefire, Llc | Firearm attachment |
US10274278B2 (en) | 2015-01-16 | 2019-04-30 | Surefire, Llc | Firearm attachment |
US20160223281A1 (en) * | 2015-02-03 | 2016-08-04 | Edward Rigor Randall | Recoil reducing muzzle brake |
US9689636B2 (en) * | 2015-02-03 | 2017-06-27 | Edward Rigor Randall | Recoil reducing muzzle brake |
US20170160036A1 (en) * | 2015-08-11 | 2017-06-08 | Drew Nolle Walker | Optimized flow compensator |
US10466004B2 (en) * | 2015-08-11 | 2019-11-05 | Drew Nolle Walker | Optimized flow compensator |
RU2616086C1 (en) * | 2016-01-11 | 2017-04-12 | Александр Алексеевич Семенов | Combined muzzle brake of artillery weapon |
US10088262B2 (en) * | 2016-09-26 | 2018-10-02 | U.S. Arms Llc | Muzzle brake device |
US10473415B2 (en) * | 2016-09-26 | 2019-11-12 | U.S. Arms Company Llc | Muzzle brake device |
US10731940B2 (en) * | 2016-09-26 | 2020-08-04 | U.S. Arms Company Llc | Muzzle brake device |
EP3665430A4 (en) * | 2016-09-26 | 2021-05-19 | McMillan, James Eric | Muzzle brake device |
USD828899S1 (en) * | 2017-02-23 | 2018-09-18 | Crosman Corporation | Silencer |
US10520272B1 (en) * | 2018-03-23 | 2019-12-31 | The United States Of America As Represented By The Secretary Of The Army | Cannon recoil inhibitor and impulse noise attenuator |
WO2020055468A1 (en) * | 2018-09-13 | 2020-03-19 | James Eric Mcmillan | Muzzle brake device |
WO2020086201A3 (en) * | 2018-09-21 | 2020-06-18 | Christopher Armstrong | Muzzle brake device |
US10788284B1 (en) * | 2019-05-09 | 2020-09-29 | The United States Of America As Represented By The Secretary Of The Army | Grounded and vehicular mounted weapons with improved recoil stability |
Also Published As
Publication number | Publication date |
---|---|
FR958162A (en) | 1950-03-04 |
GB646871A (en) | 1950-11-29 |
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