FR2400182A1 - Missile portion mechanical manoeuvring system - has chisel cutting cable and device releasing locking mechanism from missile - Google Patents
Missile portion mechanical manoeuvring system - has chisel cutting cable and device releasing locking mechanism from missileInfo
- Publication number
- FR2400182A1 FR2400182A1 FR7604997A FR7604997A FR2400182A1 FR 2400182 A1 FR2400182 A1 FR 2400182A1 FR 7604997 A FR7604997 A FR 7604997A FR 7604997 A FR7604997 A FR 7604997A FR 2400182 A1 FR2400182 A1 FR 2400182A1
- Authority
- FR
- France
- Prior art keywords
- missile
- locking mechanism
- machine
- launcher
- cable
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C14/00—Mechanical fuzes characterised by the ammunition class or type
- F42C14/04—Mechanical fuzes characterised by the ammunition class or type for torpedoes, marine mines or depth charges
Landscapes
- Engineering & Computer Science (AREA)
- Ocean & Marine Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Earth Drilling (AREA)
Abstract
Une fois un engin lancé par un véhicule lanceur, on désire manoeuvrer dans l'engin un organe quand il est à une distance prédéterminée du lanceur. Le système comprend une cisaille 1 solidaire du lanceur 2, un organe de déclenchement 7 capable de manoeuvrer un organe de l'engin 4 et un dispositif mécanique 5 à trois états, un état de repos initial, un état de travail et un état de repos initial. Un câble 9, initialement lové dans un touret 3 relie la cisaille 1 à l'organe 7 en passant à travers le dispositif 5. Une fois le câble 9 tendu, il déclenche l'organe 7, puis successivement fait passer le dispositif 5 au travail, est coupé par la cisaille 1 et se détache avec le dispositif 5 à l'etat final. Utilisable pour assurer l'armement d'engins, notamment de mines lancées par des sous-marins.Once a machine has been launched by a launcher vehicle, it is desired to maneuver an organ in the machine when it is at a predetermined distance from the launcher. The system comprises a shear 1 integral with the launcher 2, a trigger member 7 capable of maneuvering a member of the machine 4 and a mechanical device 5 with three states, an initial rest state, a working state and a resting state initial. A cable 9, initially coiled in a reel 3 connects the shears 1 to the member 7 by passing through the device 5. Once the cable 9 is stretched, it triggers the member 7, then successively makes the device 5 go to work. , is cut by the shears 1 and comes off with the device 5 in the final state. Can be used to ensure the arming of devices, in particular mines launched by submarines.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7604997A FR2400182A1 (en) | 1976-02-24 | 1976-02-24 | Missile portion mechanical manoeuvring system - has chisel cutting cable and device releasing locking mechanism from missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7604997A FR2400182A1 (en) | 1976-02-24 | 1976-02-24 | Missile portion mechanical manoeuvring system - has chisel cutting cable and device releasing locking mechanism from missile |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2400182A1 true FR2400182A1 (en) | 1979-03-09 |
| FR2400182B1 FR2400182B1 (en) | 1983-02-18 |
Family
ID=9169487
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7604997A Granted FR2400182A1 (en) | 1976-02-24 | 1976-02-24 | Missile portion mechanical manoeuvring system - has chisel cutting cable and device releasing locking mechanism from missile |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2400182A1 (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3158124A (en) * | 1962-07-24 | 1964-11-24 | Chevillon Manuel | Missile launching apparatus |
| US3701331A (en) * | 1968-11-08 | 1972-10-31 | Us Navy | Mooring line cutter system |
| US3703874A (en) * | 1970-07-15 | 1972-11-28 | Us Navy | Flexible hose wire payout system |
-
1976
- 1976-02-24 FR FR7604997A patent/FR2400182A1/en active Granted
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3158124A (en) * | 1962-07-24 | 1964-11-24 | Chevillon Manuel | Missile launching apparatus |
| US3701331A (en) * | 1968-11-08 | 1972-10-31 | Us Navy | Mooring line cutter system |
| US3703874A (en) * | 1970-07-15 | 1972-11-28 | Us Navy | Flexible hose wire payout system |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2400182B1 (en) | 1983-02-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ER | Errata listed in the french official journal (bopi) | ||
| ST | Notification of lapse |