GB778156A - Improvements in gun systems including at least one gun to be mounted on a support with respect to which it can recoil as a whole against the action of resilient means - Google Patents
Improvements in gun systems including at least one gun to be mounted on a support with respect to which it can recoil as a whole against the action of resilient meansInfo
- Publication number
- GB778156A GB778156A GB27520/55A GB2752055A GB778156A GB 778156 A GB778156 A GB 778156A GB 27520/55 A GB27520/55 A GB 27520/55A GB 2752055 A GB2752055 A GB 2752055A GB 778156 A GB778156 A GB 778156A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gun
- recoil
- spring
- action
- barrel
- 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
Links
- 239000007789 gas Substances 0.000 abstract 3
- 230000035939 shock Effects 0.000 abstract 2
- 239000006096 absorbing agent Substances 0.000 abstract 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 238000010304 firing Methods 0.000 abstract 1
- 239000000843 powder Substances 0.000 abstract 1
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
- F41A25/00—Gun mountings permitting recoil or return to battery, e.g. gun cradles; Barrel buffers or brakes
- F41A25/02—Fluid-operated systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
-
- 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
- F41A5/00—Mechanisms or systems operated by propellant charge energy for automatically opening the lock
- F41A5/18—Mechanisms or systems operated by propellant charge energy for automatically opening the lock gas-operated
- F41A5/20—Mechanisms or systems operated by propellant charge energy for automatically opening the lock gas-operated using a gas piston arranged concentrically around the barrel
-
- 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
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/49—Internally-powered drives, i.e. operated by propellant charge energy, e.g. couplings, clutches, energy accumulators
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Braking Arrangements (AREA)
Abstract
778,156. Automatic guns. BREVETS AERO-MECANIQUES SOC. ANON. Sept. 27, 1955, [Oct. 16, 1954], No. 27520/55. Class 92. Relates to an automatic gun which is movable as a whole for recoil with respect to a support, e.g., an aircraft wing, against the action of a spring and in which this recoil controls a part of the operation of the feed device for the gun. According to the invention powder gases supplied from a tap in the barrel are fed to a device which urges the gun in the recoil direction every time a shot is fired. This arrangement provides the requisite energy for operation of the feed device and permits the provision of a strong spring for urging the gun forwardly after recoil, which spring returns the gun quickly to the firing position and overcomes the shock of the breech block against its return spring at the end of its rearward stroke which shock tends to cause rearward movement of the gun. The gun is supported at the front by an aircraft wing element 6, Fig. 1, through a ball and socket device 7 in which the gun can slide and recoil against the action of a spring 8. At the rear, the gun is supported by an arm 9 hinged at its ends to the gun and to the wing framework. A feed mechanism 10 does not recoil with the gun which slides relatively thereto and is connected by a link 11 to the element 6. At every recoil a finger 12 carried by the gun lifts a roller 13 which serves to wind up a spring operating the feed mechanism. The gun barrel carries a piston 14 movable in a cylinder 15 provided in the ball element 7 and a gas tap 16 in the gun barrel feeds gases into the cylinder 15 to urge the whole of the gun rearwardly with respect to the elements 6, 7 every time a shot is fired, this action being added to the recoil proper. Shock-absorbers 19 may be interposed between a ring 17 on the gun barrel and a ring 18 rigid with the ball 7 and arranged so that the recoil stroke is not braked but at least the end of the forward return movement of the gun is slowed down. Each may consist of an oil filled cylinder 19, Fig. 3 in which moves a piston 20 provided with check valves 21 producing braking action during forward movement of the gun.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LU329415X | 1954-10-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB778156A true GB778156A (en) | 1957-07-03 |
Family
ID=19732586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB27520/55A Expired GB778156A (en) | 1954-10-16 | 1955-09-27 | Improvements in gun systems including at least one gun to be mounted on a support with respect to which it can recoil as a whole against the action of resilient means |
Country Status (8)
Country | Link |
---|---|
US (1) | US2920536A (en) |
BE (1) | BE541451A (en) |
CH (1) | CH329415A (en) |
DE (1) | DE1029710B (en) |
FR (1) | FR1132801A (en) |
GB (1) | GB778156A (en) |
LU (1) | LU33164A1 (en) |
NL (2) | NL100403C (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL112544C (en) * | 1957-02-08 | |||
US2966829A (en) * | 1957-05-02 | 1961-01-03 | Tannenbaum Joseph | Recoil mechanism |
DE1166053B (en) * | 1960-12-17 | 1964-03-19 | Karlsruhe Augsburg Iweka | Recoil amplifier for maneuver cartridges |
FR2718840B1 (en) * | 1994-04-15 | 1996-06-14 | Giat Ind Sa | Device for operating the retracting mass of an artillery piece. |
US9921022B1 (en) * | 2017-06-13 | 2018-03-20 | Michael Noyce Merino | Firearm with gas-assist recoil operation system |
DE102017125056A1 (en) * | 2017-10-26 | 2019-05-02 | L&O Hunting Group GmbH | Moment-free gas drive for a firearm |
US11187486B2 (en) * | 2019-02-19 | 2021-11-30 | Design West Technologies, Inc. | Recoil buffer for machine gun mount |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1227161A (en) * | 1914-04-14 | 1917-05-22 | Hermann Lehmann | Recoil-reducing means for guns. |
US1293021A (en) * | 1916-10-13 | 1919-02-04 | John M Browning | Automatic machine-gun. |
GB418497A (en) * | 1934-04-24 | 1934-10-25 | Charles Edmund Parr | Improvements in means for reducing the recoil in guns |
BE416937A (en) * | 1935-09-05 | |||
DE712087C (en) * | 1936-01-30 | 1941-10-11 | Deutsches Reich Vertreten Durc | Gas pressure charger |
US2140809A (en) * | 1937-02-03 | 1938-12-20 | Colt S Mfg Co | Machine gun |
US2309807A (en) * | 1940-01-18 | 1943-02-02 | Bell Aircraft Corp | Attachment for machine gun cradles |
US2303327A (en) * | 1940-03-06 | 1942-12-01 | Richard C Coupland | Gun mounting |
US2599555A (en) * | 1946-03-11 | 1952-06-10 | Us Navy | Aircraft rocket launcher |
US2746357A (en) * | 1950-04-14 | 1956-05-22 | Paul H Dixon | Feed mechanism |
-
0
- BE BE541451D patent/BE541451A/xx unknown
- NL NL200647D patent/NL200647A/xx unknown
- LU LU33164D patent/LU33164A1/xx unknown
- NL NL100403D patent/NL100403C/xx active
-
1955
- 1955-09-19 DE DEB37229A patent/DE1029710B/en active Pending
- 1955-09-26 CH CH329415D patent/CH329415A/en unknown
- 1955-09-27 GB GB27520/55A patent/GB778156A/en not_active Expired
- 1955-10-03 US US538227A patent/US2920536A/en not_active Expired - Lifetime
- 1955-10-14 FR FR1132801D patent/FR1132801A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR1132801A (en) | 1957-03-18 |
US2920536A (en) | 1960-01-12 |
NL100403C (en) | |
LU33164A1 (en) | |
DE1029710B (en) | 1958-05-08 |
CH329415A (en) | 1958-04-30 |
NL200647A (en) | |
BE541451A (en) |
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