GB982257A - Improvements in or relating to discharge tubes for projectiles - Google Patents
Improvements in or relating to discharge tubes for projectilesInfo
- Publication number
- GB982257A GB982257A GB1955/62A GB195562A GB982257A GB 982257 A GB982257 A GB 982257A GB 1955/62 A GB1955/62 A GB 1955/62A GB 195562 A GB195562 A GB 195562A GB 982257 A GB982257 A GB 982257A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- chamber
- pipe
- air
- pressure
- 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
- F41F3/08—Rocket or torpedo launchers for marine torpedoes
Landscapes
- Engineering & Computer Science (AREA)
- Ocean & Marine Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Safety Valves (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
982,257. Torpedo launching tubes. PINTSCH BAMAG A.G. Jan. 18, 1962 [Jan. 18, 1961], No. 1955/62. Heading B7A. A tube 1 for launching torpedoes, depth charges and mines has a rear closure 2 in which is a storage chamber for gas under pressure fed to the chamber through a movable pipe connected to a gas reservoir, the pipe connection being provided with shut-off means and means being provided to vent the chamber to the tube. In Fig. 1, the closure 2 comprises two bowl-shaped members connected by a sealing ring 5, the closure being pivotally mounted on hinge members 6, 7 and secured in the closing position by engagement of a rotatable ring 9 with projections on the ring 5. Compressed air is led into the closure through a pipe 11, which may pass through one or more of the hinge members 6, 7. In the supply pipe is a shut-off valve 12 and a pressure gauge 14 and a relief valve 13 may also be provided. An outlet nozzle 18 for the chamber 2 has a distributer 20 and is closed by a spring-supported member 21 of a piston-type valve 17 and the valve chamber is closed by a cover 19 from which a pipe 24 leads to a control valve 25. As air enters the chamber, it passes into the valve 17 through ports 23 and leaks through a port 26 to equalize pressure on both sides of the member 21. Pressure within the chamber 2 may be relieved by a pipe 15 furnished with a check-valve 16, the pipe 15 also being used to drain away moisture. When sufficient pressure has been built up in the chamber 2, and a torpedo is to be launched, the valve 25 is opened by pushing a control member 28 to vent the pipe 24 to a pipe 27. The sudden drop in pressure beneath the valve member 21 opens the valve 17 and allows air to flow through the nozzle 18 and so eject the torpedo. The valve 25 may be replaced by a valve which is opened by a pull. In a modification, Fig. 3, the outlet 18a is closed by a dished diaphragm 31a supported by a diaphragm 31b, the space between the diaphragms being in communication through ports 33 and an annular chamber 34 with a pipe 35 leading to a control valve 36. Valve 36 is connected by a pipe 24a to the cover 19a of the valve chamber 17a as in the first embodiment. With the members of the valve 36 in the positions shown, the pipe 35 communicates with the ambient air. To launch a torpedo, after the chamber 2a has been charged, during which charging air leaks into the valve chamber 17a through ports 23a, the valve stem 39 is pushed inwards so that the pipes 24a and 35 are in communication. Pressurized air then causes the diaphragm 31a to rupture, and the lower diaphragm 31b, then being initially loaded, ruptures also and allows air to escape into the discharge tube. To recharge the tube, the ring 31 carrying the diaphragms is changed after removal of an annular nut 32.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEP26405A DE1147866B (en) | 1961-01-18 | 1961-01-18 | Discharge tube for torpedoes, mines, etc. like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB982257A true GB982257A (en) | 1965-02-03 |
Family
ID=7370460
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1955/62A Expired GB982257A (en) | 1961-01-18 | 1962-01-18 | Improvements in or relating to discharge tubes for projectiles |
Country Status (3)
Country | Link |
---|---|
US (1) | US3108562A (en) |
DE (1) | DE1147866B (en) |
GB (1) | GB982257A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1131708A (en) * | 1965-05-19 | 1968-10-23 | Svenska Flygmotor Aktienbolage | Improvements in apparatus for launching torpedoes from a submarine tube |
DE3122631A1 (en) * | 1981-06-06 | 1982-12-23 | Krupp Mak Maschinenbau Gmbh, 2300 Kiel | "BLOWOUT DEVICE FOR EXHAUST PIPES AND DRAIN PIPES FROM SUBMARINE" |
US5199302A (en) * | 1991-09-26 | 1993-04-06 | The United States Of America As Represented By The Secretary Of The Navy | Torpedo tube differential pressure transducer |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US556058A (en) * | 1896-03-10 | Valve for steam-guns | ||
AT46225B (en) * | 1908-07-04 | 1911-02-10 | Carlo Zanic | Lancing device for torpedoes. |
US1033993A (en) * | 1910-09-20 | 1912-07-30 | Gregory C Davison | Launching torpedoes. |
US1161182A (en) * | 1914-12-01 | 1915-11-23 | Lake Torpedo Boat Company Of Maine | Torpedo-expulsion tube. |
GB256960A (en) * | 1925-08-11 | 1926-10-14 | Fried Krupp Germaniawerft Ag | Improvements in under-water torpedo-tubes |
NL36793C (en) * | 1932-05-11 | |||
DE622831C (en) * | 1933-08-30 | 1935-12-07 | Ingenieurskantoor Voor Scheeps | Underwater torpedo ejection device |
US2581758A (en) * | 1946-08-20 | 1952-01-08 | Ind Ideas Inc | Harpoon cannon |
-
1961
- 1961-01-18 DE DEP26405A patent/DE1147866B/en active Pending
-
1962
- 1962-01-18 GB GB1955/62A patent/GB982257A/en not_active Expired
- 1962-01-18 US US167105A patent/US3108562A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE1147866B (en) | 1963-04-25 |
US3108562A (en) | 1963-10-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4444085A (en) | Pneumatic launcher system | |
US3800656A (en) | Launching device for projectiles | |
US4185538A (en) | Simplified air system for underwater rocket launching | |
US4523538A (en) | Torpedo launcher | |
US2581758A (en) | Harpoon cannon | |
ES407357A1 (en) | Vehicle safety device | |
US3070112A (en) | Automatic control valve for use in connection with the raising of sunken bodies | |
US2740259A (en) | Apparatus for converting gas pressure to hydraulic pressure | |
GB982257A (en) | Improvements in or relating to discharge tubes for projectiles | |
US7237353B1 (en) | Muzzle break with gas relief membrane for an underwater gun | |
US3735747A (en) | Underwater compressed-gas gun | |
US20190219356A1 (en) | Valve system for air gun | |
CN112304626A (en) | Gas impact test system and pressure curve control method | |
RU2544253C1 (en) | Method of missile takeoff from transporter-launcher container and device for its implementation | |
US1639665A (en) | Depth charge and like submarine explosive body | |
CN104127972A (en) | Piston type water-based fire-extinguishing agent fire extinguisher | |
US2841953A (en) | System for pressurizing the fluid propellant tank of a self-propelled missile | |
US1324772A (en) | Office | |
US2974619A (en) | Fluid control system for torpedoes | |
GB1479432A (en) | Safety device for the compensation of leaks or losses of inert gas pressure contained inside vessel tanks | |
US2447651A (en) | Control mechanism | |
CN204767108U (en) | Fire extinguisher of piston river system fire extinguishing agent | |
US1445936A (en) | Vent valve for torpedoes | |
GB892019A (en) | Pressure vessel unit | |
SU698629A1 (en) | Automatic unit for extinguishing fire in tank |