EP0918975B1 - Mündungsbremse für einen waffenlauf - Google Patents
Mündungsbremse für einen waffenlauf Download PDFInfo
- Publication number
- EP0918975B1 EP0918975B1 EP98928369A EP98928369A EP0918975B1 EP 0918975 B1 EP0918975 B1 EP 0918975B1 EP 98928369 A EP98928369 A EP 98928369A EP 98928369 A EP98928369 A EP 98928369A EP 0918975 B1 EP0918975 B1 EP 0918975B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- brake
- vents
- barrel
- revolution
- projectile
- 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 claims abstract description 9
- 239000004429 Calibre Substances 0.000 claims 3
- 210000002816 gill Anatomy 0.000 description 8
- 210000000003 hoof Anatomy 0.000 description 5
- 230000000694 effects Effects 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000003380 propellant Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000006748 scratching Methods 0.000 description 1
- 230000002393 scratching effect Effects 0.000 description 1
- 230000035939 shock Effects 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
- the technical field of the invention is that of brakes muzzle for weapons tubes, in particular of large caliber.
- a muzzle brake generally has at least two transverse openings which make the interior of the brake communicate with at least two gas receiving vanes, vanes integral with the outside of the brake.
- the propellants When firing a projectile, the propellants are guided by the gills towards the blades and they then exert a thrust on them which compensates for the recoil of the tube tear.
- Patent US1363058 (basis for the preamble of claim 1) shows such a muzzle brake.
- Muzzle brakes are commonly used in the field of field artillery, however their employment is reduced for artillery equipping tanks or vehicles due to the disruption they cause to shooting of arrow projectiles, or sub-calibrated projectiles at detachable shoe.
- the muzzle brake according to the invention allows (any keeping an excellent yield) to avoid any initial disturbance of the projectile trajectory as well damage to the internal surfaces of the brake.
- the subject of the invention is a muzzle brake for a weapon barrel, especially of large caliber, and comprising at minus two gills making the interior of the brake communicate with at least two gas receiving vanes which are integral with the outside of the brake, brake having at least a cylindrical internal bearing to the gauge of the tube and arranged downstream of the gills in the direction of travel of a projectile fired by the tube, brake characterized in that the cylindrical inner surface is separated from the opening (s) which precede it by a concave surface of revolution whose the concavity is oriented towards the rear of the brake.
- the surface of revolution is a conical surface.
- the surface of revolution extends longitudinally over a length which is between 1.5 and 4 times the length of the cylindrical seat.
- the maximum diameter of the surface of revolution is preferably between 108% and 112% of the caliber D of the tube.
- the brake comprises at least two stages, each consisting of at least two vents and at least two gas receiving vanes, two consecutive stages being separated by a cylindrical span preceded by a surface of revolution.
- the muzzle brake 1 is here a brake which comprises a first stage la and a second stage 1b.
- Each stage includes two openings 2a, 2b and two blades of reception of gases 3a, 3b.
- vents 2a, 2b communicate the interior of the brake 1 with the vanes which are integral with the outside of the brake.
- the brake is fixed by thread at the end of a tube 4 of a weapon, here a rifled tube whose caliber (or diameter to stripes background) is D.
- the interior of the brake has two cylindrical seats 5a, 5b to the size of the tube.
- a first litter 5a is arranged downstream of the first openings 2a in the direction of course of a projectile fired by the tube.
- a second range 5b is located downstream of the second vents 2b and emerges outside the brake.
- the internal surface of the brake is also generally the caliber D of the barrel, both at the gills and cylindrical bearings 5a, 5b.
- each litter 5a or 5b is separated from the gills that precede it by a surface of conical revolution 6a or 6b whose concavity is oriented towards a rear part of the brake intended to be fixed to tear.
- Each conical surface extends longitudinally over a length (La or Lb) which is between 60% and 80% of the length La + Pa or Lb + Pb of the dawn considered (Pa and Pb being the lengths of the cylindrical spans 5a and 5b).
- the length La (or Lb) is understood between 1.5 and 4 times the length Pa (or Pb).
- the maximum diameter ⁇ a or ⁇ b of the conical surface 6a, 6b is between 108% and 112% of the caliber D of the tube.
- a maximum diameter ⁇ a or ⁇ b such that the belt of an arrow projectile cannot come completely out of its housing on the shoe of the projectile.
- the aerodynamic forces exerted on the projectile as well as centrifugal force (due to scratches) have the effect of initiating an opening movement of the hoof of the projectile.
- the gases are also exerted on the belt and have the effect of removing it from the hoof.
- the projectile belt is therefore subjected to a extension effort and it initiates an outward movement from its hoof housing.
- the internal diameter of the brake is of the caliber of the weapon at the level of the gills, the belt is deformed opposite of these.
- the conical surfaces 6a and 6b therefore go in turn receive the projectile belt contact and they will guide it so as to reposition it in its hoof housing.
- the cylindrical ranges 5a and 5b to the caliber of the weapon then ensure the guidance of the projectile which leaves the weapon without disturbance or obliquity.
- each conical surface with a surface of concave revolution whose concavity will be oriented towards the rear of the brake.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Braking Arrangements (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Valves And Accessory Devices For Braking Systems (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
Claims (5)
- Mündungsbremse (1) für einen Waffenlauf, in erster Linie für großkalibrige Waffen, mit mindestens zwei Schlitzen (2a, 2b), die das Innere der Bremse mit mindestens zwei Gasaufnahmeschaufeln (3a, 3b) verbinden, die fest mit der Aussenseite der Bremse verbunden sind, wobei die Bremse mindestens eine zylindrische innere Auflage (5a, 5b) mit dem Kaliber des Laufs aufweist, die nach den Schlitzen in Richtung des Wegs eines von der Waffe abgeschossenen Geschosses angeordnet ist, gekennzeichnet dadurch, dass die innere zylindrische Auflage (5a, 5b) von dem oder den davorliegenden Schlitz(en) (2a, 2b) durch eine konkave Umlauffläche (6a, 6b) getrennt ist, deren Konkavität zur Rückseite der Bremse gerichtet ist.
- Mündungsbremse gemäß dem Anspruch 1, gekennzeichnet dadurch, dass die Umlauffläche (6a, 6b) eine Kegelfläche bildet.
- Mündungsbremse gemäß dem Anspruch 1 oder 2, gekennzeichnet dadurch, dass sich die Umlauffläche (6a, 6b) längs über eine Länge (La, Lb) erstreckt, die zwischen 1,5 und 4 Mal die Länge (Pa, Pb) der zylindrischen Auflage (5a, 5b) beträgt.
- Mündungsbremse gemäß einem der Ansprüche 1 bis 3, gekennzeichnet dadurch, dass der maximale Durchmesser (Δa, Δb) der Umlauffläche (6a, 6b) zwischen 108 und 112 % des Laufkalibers D beträgt.
- Mündungsbremse gemäß einem der Ansprüche 1 bis 4, gekennzeichnet dadurch, dass sie mindestens zwei Stufen besitzt, die jeweils aus mindestens zwei Schlitzen (2a, 2b) und mindestens zwei Gasaufnahmeschaufeln (3a, 3b) bestehen, wobei die zwei aufeinanderfolgenden Stufen durch eine zylindrische Auflage (5a) getrennt sind, vor der eine Umlauffläche (6a) liegt.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR9706704A FR2764056B1 (fr) | 1997-05-30 | 1997-05-30 | Frein de bouche pour tube d'arme |
| FR9706704 | 1997-05-30 | ||
| PCT/FR1998/001061 WO1998054533A1 (fr) | 1997-05-30 | 1998-05-28 | Frein de bouche pour tube d'arme |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0918975A1 EP0918975A1 (de) | 1999-06-02 |
| EP0918975B1 true EP0918975B1 (de) | 2000-07-12 |
Family
ID=9507456
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP98928369A Expired - Lifetime EP0918975B1 (de) | 1997-05-30 | 1998-05-28 | Mündungsbremse für einen waffenlauf |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6216578B1 (de) |
| EP (1) | EP0918975B1 (de) |
| AT (1) | ATE194703T1 (de) |
| DE (1) | DE69800211T2 (de) |
| FR (1) | FR2764056B1 (de) |
| WO (1) | WO1998054533A1 (de) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2826151C1 (ru) * | 2023-03-27 | 2024-09-04 | Федеральное государственное военное казённое образовательное учреждение высшего профессионального образования "Военная академия Материально-технического обеспечения имени генерала армии А.В. Хрулева" Министерства обороны Российской Федерации | Способ перераспределения расхода пороховых газов в каналах дульного тормоза и конструкция дульного тормоза |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7886650B1 (en) | 2001-11-08 | 2011-02-15 | Herbert Rosenthal | Reverse thrust system with integral conduits and nozzles for the reduction of muzzle jump and/or recoil in firearms and weapons |
| US20030084780A1 (en) * | 2001-11-08 | 2003-05-08 | Herbert Rosenthal | Reverse thrust system with integral conduits and nozzles for the reduction of muzzle jump and/or recoil in firearms and weapons |
| US7047862B1 (en) * | 2003-05-09 | 2006-05-23 | The United States Of America As Represented By The Secretary Of The Navy | MK38 small caliber dearmer aiming device |
| US8973481B2 (en) | 2003-11-06 | 2015-03-10 | Surefire, Llc | Firearm sound suppressor |
| US6948415B2 (en) * | 2003-11-06 | 2005-09-27 | Surefire, Llc | System for attaching a noise suppressor to a firearm |
| US7676976B2 (en) | 2003-11-06 | 2010-03-16 | Surefire, Llc | Systems for attaching a noise suppressor to a firearm |
| FR2870331B1 (fr) * | 2004-05-17 | 2006-06-30 | Giat Ind Sa | Frein de bouche pour arme |
| US7032339B1 (en) | 2004-09-27 | 2006-04-25 | Roger Bounds | Lateral projection muzzle brake |
| US7062874B1 (en) | 2004-12-16 | 2006-06-20 | Surefire, Llc | Method and apparatus for installing a fixture to the muzzle end of a firearm |
| US7530299B1 (en) * | 2005-07-14 | 2009-05-12 | Charles Poff | Firearm muzzle brake |
| 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 |
| US7954414B2 (en) * | 2006-10-04 | 2011-06-07 | Surefire, Llc | Muzzle brake |
| 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 |
| USD677357S1 (en) | 2011-10-25 | 2013-03-05 | Surefire, Llc | Suppressor |
| FR2989773A1 (fr) * | 2012-04-24 | 2013-10-25 | Tda Armements Sas | Attenuateur de bruit pour mortier |
| DE102015104311A1 (de) * | 2015-03-23 | 2016-09-29 | Rolf-Dieter Reich | Kompensator für eine Schusswaffe |
| US10473415B2 (en) * | 2016-09-26 | 2019-11-12 | U.S. Arms Company Llc | Muzzle brake device |
| US20180087861A1 (en) * | 2016-09-26 | 2018-03-29 | James Eric McMillan | Muzzle brake device |
| US10731940B2 (en) * | 2016-09-26 | 2020-08-04 | 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 |
| KR102076365B1 (ko) * | 2018-09-20 | 2020-02-11 | (주)두레텍 | 탄환의 비행안정과 반동을 저감하는 장치. |
| US11432837B2 (en) * | 2018-09-21 | 2022-09-06 | Christopher Armstrong | Multifunctional surgical instrument |
| USD906463S1 (en) * | 2019-02-21 | 2020-12-29 | Macson McGuirk | Muzzle brake |
| USD928903S1 (en) * | 2019-02-28 | 2021-08-24 | The United States Of America As Represented By The Secretary Of The Army | Muzzle brake |
| EP3869143A1 (de) * | 2020-02-20 | 2021-08-25 | BAE SYSTEMS plc | Mündungsbremse |
| US11768050B2 (en) * | 2020-02-20 | 2023-09-26 | Bae Systems Plc | Muzzle brake |
| RU2744219C1 (ru) * | 2020-06-16 | 2021-03-03 | Денис Эрнестович Львов | Дульный тормоз-компенсатор (ДТК) |
| RU2745462C1 (ru) * | 2020-07-28 | 2021-03-25 | Денис Эрнестович Львов | Дульный тормоз-компенсатор (ДТК) с системой прерывания сверхзвукового газового потока |
| USD1008399S1 (en) | 2020-10-29 | 2023-12-19 | William Ronald VanFossan | Muzzle brake |
| US11262150B1 (en) | 2020-10-29 | 2022-03-01 | William Ronald VanFossan | Muzzle brake |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US817134A (en) * | 1903-02-21 | 1906-04-03 | William Davidson Condit | Gun. |
| US1363058A (en) | 1921-02-10 | 1920-12-21 | T F Shanahn | Car construction |
| US1854974A (en) * | 1930-02-08 | 1932-04-19 | Bernat Samuel | Silencer |
| FR825614A (fr) * | 1936-11-24 | 1938-03-09 | Dispositif anti-recul pour canons, fusils, armes automatiques, etc. | |
| CH244079A (de) * | 1944-12-30 | 1946-08-31 | Oerlikon Buehrle Ag | Mündungsbremse für Feuerwaffen. |
| FR911049A (fr) * | 1945-05-24 | 1946-06-26 | Frein de bouche pour armes à feu portatives de tous genres | |
| GB606478A (en) * | 1946-01-18 | 1948-08-13 | Jules Andre Norbert Galliot | Improvements in or relating to muzzle brakes and like reaction devices |
| FR958162A (de) * | 1947-05-31 | 1950-03-04 | ||
| US3368453A (en) * | 1966-03-24 | 1968-02-13 | John J. Shaw | Muzzle brake |
| US3492912A (en) * | 1966-09-01 | 1970-02-03 | Ashbrook Clifford L | Recoil controlling device |
| US5036747A (en) * | 1987-08-11 | 1991-08-06 | Mcclain Iii Harry T | Muzzle brake |
-
1997
- 1997-05-30 FR FR9706704A patent/FR2764056B1/fr not_active Expired - Fee Related
-
1998
- 1998-05-28 DE DE69800211T patent/DE69800211T2/de not_active Expired - Fee Related
- 1998-05-28 WO PCT/FR1998/001061 patent/WO1998054533A1/fr not_active Ceased
- 1998-05-28 EP EP98928369A patent/EP0918975B1/de not_active Expired - Lifetime
- 1998-05-28 AT AT98928369T patent/ATE194703T1/de not_active IP Right Cessation
- 1998-05-28 US US09/180,236 patent/US6216578B1/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2826151C1 (ru) * | 2023-03-27 | 2024-09-04 | Федеральное государственное военное казённое образовательное учреждение высшего профессионального образования "Военная академия Материально-технического обеспечения имени генерала армии А.В. Хрулева" Министерства обороны Российской Федерации | Способ перераспределения расхода пороховых газов в каналах дульного тормоза и конструкция дульного тормоза |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2764056B1 (fr) | 1999-07-16 |
| DE69800211D1 (de) | 2000-08-17 |
| DE69800211T2 (de) | 2000-12-21 |
| FR2764056A1 (fr) | 1998-12-04 |
| ATE194703T1 (de) | 2000-07-15 |
| WO1998054533A1 (fr) | 1998-12-03 |
| US6216578B1 (en) | 2001-04-17 |
| EP0918975A1 (de) | 1999-06-02 |
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