US1555026A - Muzzle brake - Google Patents

Muzzle brake Download PDF

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Publication number
US1555026A
US1555026A US709264A US70926424A US1555026A US 1555026 A US1555026 A US 1555026A US 709264 A US709264 A US 709264A US 70926424 A US70926424 A US 70926424A US 1555026 A US1555026 A US 1555026A
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Prior art keywords
gases
muzzle brake
rings
gun
muzzle
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Expired - Lifetime
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US709264A
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John B Rose
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/32Muzzle attachments or glands
    • F41A21/36Muzzle attachments or glands for recoil reduction ; Stabilisators; Compensators, e.g. for muzzle climb prevention

Description

sept. 29, 1925. l 1,555,026,
- J. B. ROSE MUZZLE BRAKE Filed April 26,. 1924 gf-L- paanfea sept. 29, i925. unir-ED- STAT-ES JOHN B. Resia, or WARRENTON, vrneINIA.
. ,Muzznn BRAKE.
Application 'mea April 2s, 1924. serial' No. 109,264.
(GBA-MED UNDER THE ACT 40F MARCH 3, 1883; v22 STAT. I.. 625:)
. To all 'whom it. may'comem:
Be it known that I, JOHN B.- Rosn, a cit-izen of the United States, and a resident of Warrenton, countyof Fauquier, and State 5 lof Virginia have invented an Improvement in Muzzle rakes, of which the following is a specification.
The invention .described herein lmay be used by the Government, or any of its oflicers or employees in prosecution of work for the Government, or by any other person in the United States, without paymentto me of any ro alty thereon, in accordance with the act of arch 3,1883. .Y My invention relates, in general terms, to muzzlebrakes for guns, which are designed to check 'the energy of recoil by utilizing the gases generated 'upon dischargeof the piece. More particularly my invention resides in the provision of means for dissipating the gases in any desired direction.
To attain the maximum edect, devices of this character have been so constructed that the full force of the gases' are diverted against the brake in such a manner that the yforce of resistance will be exerted as nearly parallel as possible to the\direction of recoil. Consequently, the released gases will be -projected along the line of recoil and will 30 seriously embarrass the crew which is serving the gun. Since the successful application and practical operation 'of a device of this character is dependent upon the effect of the gases on the gun crew it is necessary in order to secure a maximum operating efiiciency to so control the final disposition of the escaping gases that the recoil brake will not only be effective but that the gun crew will not be seriouslyhampered.
By proper adjustment of the size, shape,
and disposition of the gas exits, I create a resultant movement 'of the gases after eX- pulsion which will deflect them in any desired direction. To these and other ends, my invention consists in the construction, arrangement and combination of parts, described hereinafter and pointed out inthe claims forming a part of this specification.
One embodiment of my invention is illustrated by way of example in the accompanying drawings, in which, k
` Fig. 1 is a side elevatlon of a gunemploying mymuzzle brake;
Fig. 2 is aside elevation of the muzzle brake, partly 1n longitudinal section toshow the1 arrangement'of the deflecting elements; an
Fig. '3 is a sectional v-iew taken on the line 3 3 of'Fig. 2. l
In the drawings in which like characters fof reference designate like or similar'parts, 1 indicates the barrel of agun, having an enlarged portion 2,which is screw threaded to receive a muzzle brake 3. The muzzle brake 3 is cylindrical' in shape and comprises an attaching collar 4, a rnt collar 5, and a plurality of spaced connecting ribs 6 to permit lateral expansion of the gases generated by explosion. 'The attaching collar 4 is formed with an annular fiange 7 against which is seated a baffle plate 8 secured by means of screw bolts '9. A'ring 10 thread-- edly mounted on the attaching collar 4 abuts against the baiilerplate 8 and receives the terminal portion of the screw bolts'9. The
elements of the muzzle brake 3 are internally threaded to receive a. series of spaced baflie plates 11 mounted on tie rods 12 and anchored in a base ring 13, which rests flush against the face of the muzzle.
The baflie rings 11 are formed with a bore slightly larger than the bore of the gun so. as to permit free passage of the projectile and they are furtl er provided with concave vrear faces of' variable degree to receive the impact ofthe gases and togovern the d irection of'expansion. The forward face of each ring is of irregular convexity so as to more readily direct the escaping gases into the concave :tace of the next preceding ring. The convex and concave faces of these rings are so formed and designed that the gases directed by a few of the rearmost rings will diverge forwardly, while the gases directedb the remaining rings w-ill diverge rearwar ly, it being preferable that the gases escaping from between the rear-l most rings have the least divergence of anyv of the forwardly diverted streams of gas, while the gas escaping from 'between the foremost rings will leave the least'divergence of any of the rearwardly directed streams of gas; the object being to leave the resultant rearward movement of the gases sufficiently divergent to avoid injury los' to the gun crew and gun mount, while at the same time securing a sufiicie'nt rearward direction. of the gases t0 provide a useful breaking force.
In operation, the force of the explosion generates gases which follow the projectile through the 4bore of the gun. These gases upon flowing from the muzzle of the gun` iinpinge upon the haiile rings A to N and escape through the spaces between the ribs (l: The direction of exit of the gases is shown by arrows a to n and is controlled by the degree of concavity of each particular ring. t will thus be seen that the gases following the direction a to e will move forwardly of the gun crew while the gases following the direction f to fn, will be diverted rearwardly towards 'the crew. By this arrangement the resultant movement of the gases after emission from the muzzle brake may be so Controlled that their final dissipation will not seriously affect the crew operating the gun. i
By proper adjustment of the size, shape and disposition of the bafie rings, it is possible to' create a resultant movement of the gases in any desired direction.
Having thus described my inventiomwhat I claim is:
1. A muzzle brake for guns comprising a casing and a plurality of spaced baffle rings, the rings nearest thegun muzzle having forwardly directed exits and the more remote casing formed with a plurality ofspacedV ribs and a set ofbaffle rings mounted on rods and adapted for threaded engagement within the casing.
4. A muzzle brake for guns provided with spaced discharge ports, the forwardly situated ports adapted to discharge gases in a rearwardly divergent direction; and the rearwardly situated ports adapted to discharge gases in a forwardly divergent direction.
5. A muzzle brake for guns provided with spaced discharge ports'arranged to direct the escaping gases along converging lines, whereby a resultant movement ofthe gases will be had in a direction to clear the gun crew.
JOHN B; ROSE.
US709264A 1924-04-26 1924-04-26 Muzzle brake Expired - Lifetime US1555026A (en)

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US709264A US1555026A (en) 1924-04-26 1924-04-26 Muzzle brake

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US709264A US1555026A (en) 1924-04-26 1924-04-26 Muzzle brake

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2538045A (en) * 1943-04-02 1951-01-16 Sperry Corp Gun mounting
US2870679A (en) * 1952-11-25 1959-01-27 Richard V Collins Flash suppressor
US2900875A (en) * 1950-05-11 1959-08-25 John H Fergus Flash and noise suppressor for high pressure gas exhausts
US4619182A (en) * 1983-01-31 1986-10-28 Saab-Scania Aktiebolag Arrangement for deflecting powder gases from an aircraft weapon
US5325759A (en) * 1993-04-19 1994-07-05 Warner Joseph G Flash suppressor
US20040123729A1 (en) * 2002-06-24 2004-07-01 Meyers Brad E. Flash suppressor apparatus and methods
US7581482B1 (en) * 2005-07-28 2009-09-01 The United States Of America As Represented By The Secretary Of The Army Supersonic turning vane
US20170160036A1 (en) * 2015-08-11 2017-06-08 Drew Nolle Walker Optimized flow compensator
USD808490S1 (en) 2016-04-15 2018-01-23 Vista Outdoor Operations Llc Suppressor
US10088261B1 (en) 2015-11-30 2018-10-02 Paul A. Oglesby Blast mitigation device
US10209022B1 (en) 2015-11-24 2019-02-19 Paul A. Oglesby Muzzle device and venturi blast shield
US10234230B1 (en) * 2015-11-09 2019-03-19 Paul A. Oglesby Flash suppressor and flash suppressor assembly
US10508878B1 (en) 2017-02-22 2019-12-17 Paul A. Oglesby Blast shield attachment system

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2538045A (en) * 1943-04-02 1951-01-16 Sperry Corp Gun mounting
US2900875A (en) * 1950-05-11 1959-08-25 John H Fergus Flash and noise suppressor for high pressure gas exhausts
US2870679A (en) * 1952-11-25 1959-01-27 Richard V Collins Flash suppressor
US4619182A (en) * 1983-01-31 1986-10-28 Saab-Scania Aktiebolag Arrangement for deflecting powder gases from an aircraft weapon
US5325759A (en) * 1993-04-19 1994-07-05 Warner Joseph G Flash suppressor
US8104394B2 (en) 2002-06-24 2012-01-31 B. E. Meyers Flash suppressor apparatus and methods
US20040123729A1 (en) * 2002-06-24 2004-07-01 Meyers Brad E. Flash suppressor apparatus and methods
US6837139B2 (en) * 2002-06-24 2005-01-04 Meyers Brad E Flash suppressor apparatus and methods
US20050066802A1 (en) * 2002-06-24 2005-03-31 Meyers Brad E. Flash suppressor apparatus and methods
US7302774B2 (en) * 2002-06-24 2007-12-04 Meyers Brad E Flash suppressor apparatus and methods
US20090178549A1 (en) * 2002-06-24 2009-07-16 Meyers Brad E Flash Suppressor Apparatus and Methods
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
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
US10234230B1 (en) * 2015-11-09 2019-03-19 Paul A. Oglesby Flash suppressor and flash suppressor assembly
US10209022B1 (en) 2015-11-24 2019-02-19 Paul A. Oglesby Muzzle device and venturi blast shield
US10088261B1 (en) 2015-11-30 2018-10-02 Paul A. Oglesby Blast mitigation device
USD808490S1 (en) 2016-04-15 2018-01-23 Vista Outdoor Operations Llc Suppressor
US10508878B1 (en) 2017-02-22 2019-12-17 Paul A. Oglesby Blast shield attachment system

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