GB1340386A - Combination of and infantry weapon and its ammunition - Google Patents
Combination of and infantry weapon and its ammunitionInfo
- Publication number
- GB1340386A GB1340386A GB1476271*[A GB1476271A GB1340386A GB 1340386 A GB1340386 A GB 1340386A GB 1476271 A GB1476271 A GB 1476271A GB 1340386 A GB1340386 A GB 1340386A
- Authority
- GB
- United Kingdom
- Prior art keywords
- case
- projectile
- extension
- guide body
- tubular guide
- 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
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/052—Means for securing the rocket in the launching apparatus
-
- 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
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/58—Electric firing mechanisms
- F41A19/68—Electric firing mechanisms for multibarrel guns or multibarrel rocket launchers or multicanisters
-
- 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
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/58—Electric firing mechanisms
- F41A19/69—Electric contacts or switches peculiar thereto
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/045—Rocket or torpedo launchers for rockets adapted to be carried and used by a person, e.g. bazookas
- F41F3/0455—Bazookas
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
1340386 Ammunition containers; infantry weapon SARMAC SA 13 May 1971 [21 May 1970] 14762/71 Headings F3C and F3A An infantry weapon comprises a tubular guide body for guiding a self-propelled projectile which is housed in a case, a control device for firing the projectile, and a device at the rear of the tubular guide body for locking the front end of the case in the weapon so that the case is located in an extension of the tubular guide body. Means are provided for releasing the case at or after the time of firing of the projectile and before the emergence of the projectile from the front end of the tubular guide body and allowing ejection of the case by the propulsion gases of the projectile. In an embodiment a weapon, Fig. 1, has three tubular guide bodies 1, 2 and 3, Figs. 3 and 5. Each of the latter has an extension 6 which receives a case 5 therein. The inside bore of each case contains a projectile 4, Fig. 6, and is the same size as the bore of each tubular guide body. The front end 7 of each case is held to a respective extension 6 by a member 8, Fig. 2, which is mounted on the respective guide body. The member 8 has a portion 9 which can pass through an orifice 10 formed in the extension 6 and into a groove 13 of the case 5. Release is effected by propulsion gases of the projectile which are decelerated by an inner peripheral shoulder 15, then pass through orifices 14 in the bottom of the groove 13 and through the orifice 10, or manually using a lever 17. When the member 8 is in the fastening position a switch closes an electrical circuit leading to an electrically-operated detonator 27, Fig. 7. Shoulders 16 on the case permit its ejection by the propulsion gases. In other embodiments the member 8 is pivotally mounted on the extension 6 and is urged by a spring, the member 8 has an extension which co-operates with a notched wheel 20 to arrest the return of the member 8 for a period of time sufficient to enable the ejection of the case, releasing of the case is effected mechanically, the case has a removable end having a plug therein and a cup connected thereto which engages the blast-pipe of the projectile, the case is provided with contact rings which are connected to an electrically-operated detonator, projectile-retaining means comprises a cup which is shrunk on to the blast-pipe of the projectile and tongues on a connecting member which engage the rear end of the case, projectileretaining means comprises a cup which is shrunk on to the blast-pipe of the projectile and is connected to the end of the case by a screw, projectible-retaining means comprises a plug which forms the end of the case and is forced into the blast-pipe of the projectile, folded-back stabilizer fins of the projectile have studs which are received in slots in the wall of the case, the folded-back fins are engaged by a fork carried by the case, and the folded-back fins are engaged by rivets mounted in the wall of the case, the rivets each having a machined portion which engages the fins and each having a hole therein through which a wire is passed so as to connect them together. The control device includes a firing distributer selector for the successive firing of the three projectiles. The selector is housed in the grip 24, Fig. 1, of the weapon which also contains an electromagnetic generator 25, Fig. 9, and which carries a safety device 26 and a trigger 23. The generator is connected to the electrically-operated detonators of the three projectiles.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH750870A CH524802A (en) | 1970-05-21 | 1970-05-21 | Set including an infantry weapon and its ammunition |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1340386A true GB1340386A (en) | 1973-12-12 |
Family
ID=4326227
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1476271*[A Expired GB1340386A (en) | 1970-05-21 | 1971-05-13 | Combination of and infantry weapon and its ammunition |
Country Status (6)
Country | Link |
---|---|
US (1) | US3780616A (en) |
CH (1) | CH524802A (en) |
DE (1) | DE2125149C3 (en) |
FR (1) | FR2091471A5 (en) |
GB (1) | GB1340386A (en) |
SE (1) | SE388682B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5239909A (en) * | 1989-09-15 | 1993-08-31 | Short Brothers Plc | Missile weapon system |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE407712B (en) * | 1975-09-12 | 1979-04-09 | Bofors Ab | DEVICE AT AMMUNITION MAGAZINE |
FR2492083A1 (en) * | 1980-10-14 | 1982-04-16 | Serat | ANTICHAR ROCKET LAUNCHER |
DE3048596A1 (en) * | 1980-12-23 | 1982-07-01 | Dynamit Nobel Ag, 5210 Troisdorf | One man anti tank weapon - has firing tube, shell and charges formed as disposable integral unit separate from pistol grip |
US4376405A (en) * | 1981-03-05 | 1983-03-15 | The United States Of America As Represented By The Secretary Of The Army | Automatic hard-soft rocket detent system |
FR2520860A1 (en) * | 1982-01-29 | 1983-08-05 | Lacroix E | Base and launch tube for movable shell casing - comprises cylindrical support with inwardly projecting peg to latch in groove in shell |
FR2529659A1 (en) * | 1982-07-02 | 1984-01-06 | Brandt Francois | RETRACTABLE BRAKE CANON |
JP2002521645A (en) * | 1998-07-27 | 2002-07-16 | ピエクソン アーゲー | Self-defense device |
FI121553B (en) * | 2008-01-31 | 2010-12-31 | Patria Weapon Systems Oy | The support means for supporting a grenade in a weapon pipe and the method of attaching a support member to a grenade |
EP2161531B1 (en) * | 2008-09-04 | 2014-01-29 | Saab AB | Countermass weapon |
FR2965609B1 (en) * | 2010-10-01 | 2017-02-10 | Mbda France | LAUNCH-MUNITION AND ANALOGUE ARM SYSTEM WITH A TUBULAR EXTENSION |
CN105486493B (en) * | 2014-09-17 | 2017-12-22 | 北京强度环境研究所 | A kind of Hold down and release simulation test device and its application method |
ITUB20151126A1 (en) * | 2015-05-26 | 2016-11-26 | Myhre Tito Waage | DEVICE FOR LAUNCHING HAND GRENADE |
AU2019288728A1 (en) | 2018-06-23 | 2021-01-14 | Genentech, Inc. | Methods of treating lung cancer with a pd-1 axis binding antagonist, a platinum agent, and a topoisomerase ii inhibitor |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL154575B (en) * | 1949-07-14 | Gross Hans | DRIVE DEVICE FOR A ROLLING SHUTTER, SUNSHADE OR THE LIKE. | |
US2836105A (en) * | 1953-09-01 | 1958-05-27 | Jr Robert A Doak | Contact type latch and firing mechanism for rocket launcher |
FR1112975A (en) * | 1954-10-22 | 1956-03-21 | Soc Tech De Rech Ind | Reaction projectile improvements |
FR95452E (en) * | 1954-10-22 | 1971-01-15 | Soc Tech De Rech Ind | Improvements to reaction projectiles. |
US2920533A (en) * | 1957-10-07 | 1960-01-12 | Musser C Walton | Self-ejecting breech |
US2966827A (en) * | 1959-01-27 | 1961-01-03 | Leo M Harvey | Rocket launcher |
US3005386A (en) * | 1960-01-22 | 1961-10-24 | Musser C Walton | Cartridge case ejecting mechanism |
US3030864A (en) * | 1960-05-03 | 1962-04-24 | Musser C Walton | Self-ejecting breech |
NL278018A (en) * | 1961-11-13 | |||
US3296929A (en) * | 1963-10-16 | 1967-01-10 | Bofors Ab | Missiles |
DE1428642A1 (en) * | 1964-12-28 | 1968-11-28 | Dynamit Nobel Ag | Fixing missiles in their launcher |
DE1578001A1 (en) * | 1965-08-06 | 1969-10-23 | Dynamit Nobel Ag | Device for holding rockets in their launching device |
US3494249A (en) * | 1968-05-01 | 1970-02-10 | Norris Industries | Weapon system including a launcher of the rocket launcher type and a projectile of the rocket type |
US3677131A (en) * | 1970-12-16 | 1972-07-18 | Norris Industries | Disposable projectile launcher of the recoilless type |
-
1970
- 1970-05-21 CH CH750870A patent/CH524802A/en not_active IP Right Cessation
-
1971
- 1971-05-10 US US00141700A patent/US3780616A/en not_active Expired - Lifetime
- 1971-05-11 FR FR7117033A patent/FR2091471A5/fr not_active Expired
- 1971-05-13 GB GB1476271*[A patent/GB1340386A/en not_active Expired
- 1971-05-18 SE SE7106456A patent/SE388682B/en unknown
- 1971-05-21 DE DE2125149A patent/DE2125149C3/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5239909A (en) * | 1989-09-15 | 1993-08-31 | Short Brothers Plc | Missile weapon system |
Also Published As
Publication number | Publication date |
---|---|
CH524802A (en) | 1972-06-30 |
FR2091471A5 (en) | 1972-01-14 |
DE2125149B2 (en) | 1980-07-10 |
DE2125149A1 (en) | 1971-12-09 |
SE388682B (en) | 1976-10-11 |
US3780616A (en) | 1973-12-25 |
DE2125149C3 (en) | 1981-06-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |