GB1375691A - - Google Patents
Info
- Publication number
- GB1375691A GB1375691A GB4764964A GB4764964A GB1375691A GB 1375691 A GB1375691 A GB 1375691A GB 4764964 A GB4764964 A GB 4764964A GB 4764964 A GB4764964 A GB 4764964A GB 1375691 A GB1375691 A GB 1375691A
- Authority
- GB
- United Kingdom
- Prior art keywords
- setting
- fuze
- controller
- counts
- control device
- 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
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C11/00—Electric fuzes
- F42C11/06—Electric fuzes with time delay by electric circuitry
-
- G—PHYSICS
- G04—HOROLOGY
- G04G—ELECTRONIC TIME-PIECES
- G04G15/00—Time-pieces comprising means to be operated at preselected times or after preselected time intervals
- G04G15/003—Time-pieces comprising means to be operated at preselected times or after preselected time intervals acting only at one preselected time or during one adjustable time interval
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Air Bags (AREA)
Abstract
1375691 Fuze setting arrangement TELEFUNKEN PATENTVERWERTUNGS GmbH 23 Nov 1964 [21 March 1964] 47649/64 Heading F3A In a rocket or missile fuze setting arrangement, the fuze controller is coupled to the setting device by inductive or capacitive means or directly by wires. The controller is mounted with the fuze, and is expendable. The input setting signals are supplied before launching to the setting device by three rotary step switches which are adjusted externally so as to provide the required predetermined firing signal to the fuze primer at a desired time interval of the launching. The input signals are supplied in the form of a binary decimal code and are converted to a digital code, within the controller, prior to application to the control device. The use of a digital code facilitates the simple fabrication of the expendable control devices. The control device comprises a known digital counter which counts the pulses from a master clock. During the acceptance of the control signal, the control device counts upwards and then subsequenty counts downwards, to the starting or primer firing signal, supervised by a master clock, in steps of 0À1 second. Conversion from the binary decimal code to the digital system is effected by a known form of switching matrix. Fault indication is provided at the setting device when no setting signal is developed after a complete setting sequence.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DET0025872 | 1964-03-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1375691A true GB1375691A (en) | 1974-11-27 |
Family
ID=7552365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4764964A Expired GB1375691A (en) | 1964-03-21 | 1964-11-23 |
Country Status (4)
| Country | Link |
|---|---|
| DE (1) | DE977992C (en) |
| FR (1) | FR1605376A (en) |
| GB (1) | GB1375691A (en) |
| IT (1) | IT984503B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2333220A1 (en) * | 1975-11-25 | 1977-06-24 | Mefina Sa | ELECTRONIC IGNITION DEVICE FOR PROJECTILE ROCKET |
| FR2431673A1 (en) * | 1978-07-21 | 1980-02-15 | Thomson Brandt | Rocket launcher with inductive connection to rockets - includes seven parallel tubes of synthetic material surrounded by induction windings |
| EP0252821A1 (en) * | 1986-07-08 | 1988-01-13 | Thomson-Brandt Armements | Transmission process and system for an initiation order to an apparatus aboard an engine |
| WO1990003549A1 (en) * | 1988-09-20 | 1990-04-05 | Cableries & Trefileries De Cossonay | Device for arming and timing a rocket for ammunition to be fired by a launcher, particularly an automatic launcher |
| US4928570A (en) * | 1986-07-08 | 1990-05-29 | Thomson Brandt Armements | Method and system for transmitting a command to start up a device on board a missile |
| US10845175B2 (en) | 2017-08-17 | 2020-11-24 | Luis Eduardo Tobón Trujillo | Electromechanical contact fuse for multipurpose aircraft ammunition |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2653452C3 (en) * | 1976-11-25 | 1983-11-17 | Diehl GmbH & Co, 8500 Nürnberg | Electronic ignition circuit |
| DE3317376A1 (en) * | 1983-05-13 | 1984-11-15 | Diehl GmbH & Co, 8500 Nürnberg | Safety circuit for a projectile fuzing circuit |
| CH676882A5 (en) * | 1988-09-30 | 1991-03-15 | Eidgenoess Munitionsfab Thun |
-
1964
- 1964-03-21 DE DE1964977992 patent/DE977992C/de not_active Expired
- 1964-11-23 GB GB4764964A patent/GB1375691A/en not_active Expired
- 1964-12-11 IT IT2648764A patent/IT984503B/en active
-
1965
- 1965-02-19 FR FR6248A patent/FR1605376A/fr not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2333220A1 (en) * | 1975-11-25 | 1977-06-24 | Mefina Sa | ELECTRONIC IGNITION DEVICE FOR PROJECTILE ROCKET |
| FR2431673A1 (en) * | 1978-07-21 | 1980-02-15 | Thomson Brandt | Rocket launcher with inductive connection to rockets - includes seven parallel tubes of synthetic material surrounded by induction windings |
| EP0252821A1 (en) * | 1986-07-08 | 1988-01-13 | Thomson-Brandt Armements | Transmission process and system for an initiation order to an apparatus aboard an engine |
| FR2601484A1 (en) * | 1986-07-08 | 1988-01-15 | Thomson Brandt Armements | METHOD AND SYSTEM FOR TRANSMITTING AN ORDER FOR STARTING A DEVICE ON BOARD A DEVICE |
| US4928570A (en) * | 1986-07-08 | 1990-05-29 | Thomson Brandt Armements | Method and system for transmitting a command to start up a device on board a missile |
| WO1990003549A1 (en) * | 1988-09-20 | 1990-04-05 | Cableries & Trefileries De Cossonay | Device for arming and timing a rocket for ammunition to be fired by a launcher, particularly an automatic launcher |
| US10845175B2 (en) | 2017-08-17 | 2020-11-24 | Luis Eduardo Tobón Trujillo | Electromechanical contact fuse for multipurpose aircraft ammunition |
Also Published As
| Publication number | Publication date |
|---|---|
| DE977992C (en) | 1974-12-19 |
| FR1605376A (en) | 1975-02-28 |
| IT984503B (en) | 1974-11-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| CSNS | Application of which complete specification have been accepted and published, but patent is not sealed |