GB1204214A - Improvements in recoilless guns - Google Patents
Improvements in recoilless gunsInfo
- Publication number
- GB1204214A GB1204214A GB108768A GB108768A GB1204214A GB 1204214 A GB1204214 A GB 1204214A GB 108768 A GB108768 A GB 108768A GB 108768 A GB108768 A GB 108768A GB 1204214 A GB1204214 A GB 1204214A
- Authority
- GB
- United Kingdom
- Prior art keywords
- socket
- cartridge case
- cartridge
- missile
- teeth
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- 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
- F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
- F41A1/08—Recoilless guns, i.e. guns having propulsion means producing no recoil
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/05—Cartridges, i.e. cases with charge and missile for recoilless guns
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
1,204,214. Recoilless guns; cartridges. BRITISH AIRCRAFT CORP. Ltd. 8 April, 1969 [8 Jan., 1968], No. 1087/68. Headings F3A and F3C. A recoilless gun comprises a barrel 4 having a rearwardly opening socket 2 formed at the rear end thereof and in which a cartridge case having a nozzle 14 at its rearward end and a missile can be mounted. The missile may be loaded into the barrel through the socket 2 before the cartridge case is placed in position. Means are provided for connecting the cartridge case to the socket 2 and one or more bleed passages 46 extend from a forward portion of the barrel to the socket such that, after the firing of the cartridge the connecting means retains the cartridge case in the socket until the missile clears the entrance port(s) of the bleed passage(s) 46. Then propellant gas passes to the socket 2 to urge the cartridge ease away from the walls thereof and cause the breaking or disengagement of the connecting means to allow the cartridge case and nozzle to be ejected rearwardly from the gun. In the construction shown the propellant charge 20 and igniter 42 are annular members arranged between the outer wall of the cartridge case and a perforated member 22. The missile 26 is provided with a driving band 28 and fins 30. The connecting means consists of a nip 32 attached to the cartridge case and provided with teeth 36 mounted on the ends of frangible arms 34, the teeth sitting in notches in the outer surface of the socket 2. A longitudinal groove extends between each notch and the end face of the socket along which grooves the teeth travel in the cartridge loading operation. The grooves may narrow towards their forward ends (Fig. 2, not shown). The teeth may be each provided with a sloping face such that they slide out of the notch when gas forces the cartridge case rearwardly or further gas bleed passages may communicate directly with the notches (Fig. 4, not shown). The socket may be frusto-conical with a complementary frustoconical cartridge case. The nozzle of the cartridge case may be formed by a part spherical member mounted in a cylinder by radial arms (Fig. 3, not shown). The socket may be of a frusto-conical configuration (Fig. 5, not shown).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB108768A GB1204214A (en) | 1968-01-08 | 1968-01-08 | Improvements in recoilless guns |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB108768A GB1204214A (en) | 1968-01-08 | 1968-01-08 | Improvements in recoilless guns |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1204214A true GB1204214A (en) | 1970-09-03 |
Family
ID=9715943
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB108768A Expired GB1204214A (en) | 1968-01-08 | 1968-01-08 | Improvements in recoilless guns |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1204214A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2352270A1 (en) * | 1976-05-17 | 1977-12-16 | Bofors Ab | MISSILE NON-RECOIL FIRE DEVICE |
FR2530331A1 (en) * | 1982-07-16 | 1984-01-20 | Europ Propulsion | AMMUNITION FOR SHOOTING WEAPONS WITHOUT BACK |
-
1968
- 1968-01-08 GB GB108768A patent/GB1204214A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2352270A1 (en) * | 1976-05-17 | 1977-12-16 | Bofors Ab | MISSILE NON-RECOIL FIRE DEVICE |
FR2530331A1 (en) * | 1982-07-16 | 1984-01-20 | Europ Propulsion | AMMUNITION FOR SHOOTING WEAPONS WITHOUT BACK |
US4484524A (en) * | 1982-07-16 | 1984-11-27 | Societe Europeenne De Propulsion | Projectile for recoilless weapon |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3482516A (en) | Caseless cartridges having the projectile housed in the propellant charge | |
US3485170A (en) | Expendable case ammunition | |
US3011404A (en) | Liquid propellant squeeze-bore gun with deformable projectile sabot | |
US3336871A (en) | Traveling ignition charge | |
US4063486A (en) | Liquid propellant weapon system | |
US4028994A (en) | Micro-precision timed firing handgun | |
US3680485A (en) | Salvo squeezebore projectile | |
GB853789A (en) | Improvements in and relating to a self-propelled projectile | |
US3769912A (en) | Spin-stabilized projectiles | |
US4782758A (en) | Ammunition round | |
GB945409A (en) | Deployable fin assemblies for self-propelled projectiles | |
US4132149A (en) | Liquid propellant weapon system | |
US3688697A (en) | Solid grain caseless ammunition propellant | |
US3139795A (en) | Tandem loaded firing tubes | |
US3547030A (en) | Rocket and cartridge case therefor | |
US3396658A (en) | Small arms cartridge | |
US4681038A (en) | Ammunition cartridge case | |
US4126078A (en) | Liquid propellant weapon system | |
US3326128A (en) | Rockets and combinations of rockets and cases | |
GB1465550A (en) | Projectile launching device | |
US2359814A (en) | Illuminating shell | |
US2924149A (en) | Recoilless gun with reverse gas flow | |
US3575112A (en) | Segmented propellant charge for telescoped caseless ammunition | |
US2771607A (en) | Device for shooting pins and bolts | |
US3044363A (en) | Propulsion means for projectiles |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |