FR2487966A1 - IMPROVEMENTS ON COATINGS FOR FORMED EXPLOSIVE CHARGES - Google Patents
IMPROVEMENTS ON COATINGS FOR FORMED EXPLOSIVE CHARGES Download PDFInfo
- Publication number
- FR2487966A1 FR2487966A1 FR8017029A FR8017029A FR2487966A1 FR 2487966 A1 FR2487966 A1 FR 2487966A1 FR 8017029 A FR8017029 A FR 8017029A FR 8017029 A FR8017029 A FR 8017029A FR 2487966 A1 FR2487966 A1 FR 2487966A1
- Authority
- FR
- France
- Prior art keywords
- charge
- coating according
- hollow
- coatings
- copper
- 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
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/032—Shaped or hollow charges characterised by the material of the liner
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Forging (AREA)
- Powder Metallurgy (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
REVETEMENT A BASE DE CUIVRE POUR CHARGE EXPLOSIVE FORMEE, TELLE QUE CHARGE CREUSE, CHARGE A ASSIETTE DEFORMABLE, CARACTERISE PAR UNE ADDITION DE METAL NOBLE TEL QUE: ARGENT, OR, PLATINE.COPPER BASED COATING FOR SHAPED EXPLOSIVE LOAD, SUCH AS HOLLOW LOAD, DEFORMABLE PLATE LOAD, CHARACTERIZED BY AN ADDITION OF NOBLE METAL SUCH AS: SILVER, GOLD, PLATINUM.
Description
1 24879661 2487966
Pour la constitution des revêtements pour charges explosives for- For the construction of coatings for explosive charges
mées (charges creuses, charges creuses "à assiette déformable" lançant un noyau, dit "self-forging"), on utilise généralement des matériaux denses, ductiles, malléables, supportant sans rupture des déformations très rapides sous l'effet des ultra-pressions engendrées par la détonation. Ainsi, le tantale prend une place grandissante dans la technique des mées (hollow charges, hollow charges "with deformable base" launching a core, called "self-forging"), dense, ductile, malleable materials are generally used, supporting very rapid deformations without breaking under the effect of ultra-pressures generated by the detonation. Thus, tantalum is taking an increasing place in the technique of
"assiettes déformables" ("self forging"), alors que le cuivre conserve tou- "self-forging", while copper still retains
jours, par ses qualités propres, sa place prépondérante dans la technique days, by its own qualities, its preponderant place in the technique
des charges creuses.shaped charges.
Cependant, même dans le cas du cuivre, et dès l'origine des charges However, even in the case of copper, and from the origin of the charges
creuses modernes très performantes (4 à 5 calibres, lère et 2ème généra- modern high performance hollow (4 to 5 calibers, 1st and 2nd generation)
tions, double décennie des années 50 et 60), on s'est rapidement orienté vers le cuivre de très haute pureté (à 99,99 %), de plus désoxygéné, ce qui lui permet de supporter, sans fissuration ni crique, les déformations inhérentes au phénomène ultra rapide du fonctionnement, qualité d'ailleurs vérifiée, lot tions, double decade of the 50s and 60s), we quickly turned to very high purity copper (99.99%), more oxygen-free, which allows it to withstand, without cracking or cracking, deformations inherent in the ultra-fast phenomenon of operation, quality verified, lot
par lot, par des épreuves très particulières de pliage. by batch, by very specific folding tests.
La présente invention propose une amélioration du cuivre pour re- The present invention provides an improvement in copper for
vêtement de charges explosives formées, ayant pour objet d'en augmenter à la fois la densité et la capacité de déformation sans rupture, fissure, crique, etc... On obtient ainsi une augmentation de la longueur du jet, un relèvement garment of explosive charges formed, the purpose of which is to increase both the density and the capacity of deformation without rupture, crack, crack, etc. An increase in the length of the jet is thus obtained, an increase
de sa masse spécifique et de sa continuité, d'o amélioration directe du pou- of its specific mass and its continuity, o direct improvement of the
voir perforant et de l'effet terminal. see perforating and terminal effect.
Conformément à l'invention, le cuivre du revêtement comporte une In accordance with the invention, the copper in the coating has a
addition d'un métal noble tel que: argent, or, platine. Les capacités de dé- addition of a noble metal such as: silver, gold, platinum. The capabilities of
formation de ces métaux nobles et leur densité donnent à l'alliage ainsi formé, formation of these noble metals and their density give the alloy thus formed,
selon l'invention, les caractéristiques précisément recherchées, comme rap- according to the invention, the characteristics precisely sought, such as
pelé plus haut, pour relever le pouvoir perforant de l'effet terminal d'une peeled higher, to raise the perforating power of the terminal effect of a
charge explosive formée.explosive charge formed.
La teneur de l'addition en métal noble peut d'ailleurs être modérée The content of the noble metal addition can also be moderate
sans sortir du cadre de l'invention, elle peut être de quelques % seulement. without departing from the scope of the invention, it may be only a few%.
Des revêtements en métal noble ont d'ailleurs été déjà réalisés dans le passé. Mais le prix de ces métaux ne permet pas d'y avoir recours pour les produits de série, même s'il s'agit de missiles tactiques. Par contre l'alliage à base de cuivre, avec addition d'argent ou d'or ou de platine, tout 224P 7 'w7 5 ? en restant d'un prix raisonnable, procure tous les avantages et les progrès In addition, noble metal coatings have been made in the past. But the price of these metals does not allow them to be used for serial products, even if they are tactical missiles. On the other hand, the copper-based alloy, with the addition of silver or gold or platinum, all 224P 7 'w7 5? remaining reasonably priced, provides all the benefits and progress
évoqués plus haut.mentioned above.
S'y ajoute la possibilité d'adapter, par les procédés métallurgiques et mécaniques classiques (traitement thermique, corroyage, fluotournage, emboutissage, etc...), les caractéristiques de l'alliage: granulométrie, Added to this is the possibility of adapting, by conventional metallurgical and mechanical processes (heat treatment, wrinkling, flow forming, stamping, etc.), the characteristics of the alloy: particle size,
dureté, allongement, striction, limite élastique, etc..., au cas précis d'em- hardness, elongation, necking, elastic limit, etc ..., in the specific case of em-
ploi: revêtement de charge creuse ou assiette déformable, calibre, épais- bend: hollow load coating or deformable plate, caliber, thick-
seur, forme, chargement en explosif, nature de l'explosif, forme d'onde de sor, shape, explosive charge, nature of the explosive, waveform of
détonation, etc...detonation, etc ...
3 24879663 2487966
Claims (4)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8017029A FR2487966B1 (en) | 1980-08-01 | 1980-08-01 | IMPROVEMENTS ON COATINGS FOR FORMED EXPLOSIVE CHARGES |
GB8122764A GB2081428B (en) | 1980-08-01 | 1981-07-23 | Claddings for shaped explosive charges |
IT68042/81A IT1144438B (en) | 1980-08-01 | 1981-07-27 | REFINEMENTS FOR COATINGS FOR EXPLOSIVE CHARGES FORMED |
DE19813129530 DE3129530A1 (en) | 1980-08-01 | 1981-07-27 | COATS FOR SHAPED EXPLOSIVE CHARGES |
CH495381A CH645976A5 (en) | 1980-08-01 | 1981-07-30 | COATING FOR SHAPED EXPLOSIVE CHARGE. |
BE0/205554A BE889823A (en) | 1980-08-01 | 1981-07-31 | IMPROVEMENTS ON COATINGS FOR FORMED EXPLOSIVE CHARGES |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8017029A FR2487966B1 (en) | 1980-08-01 | 1980-08-01 | IMPROVEMENTS ON COATINGS FOR FORMED EXPLOSIVE CHARGES |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2487966A1 true FR2487966A1 (en) | 1982-02-05 |
FR2487966B1 FR2487966B1 (en) | 1986-07-11 |
Family
ID=9244800
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8017029A Expired FR2487966B1 (en) | 1980-08-01 | 1980-08-01 | IMPROVEMENTS ON COATINGS FOR FORMED EXPLOSIVE CHARGES |
Country Status (6)
Country | Link |
---|---|
BE (1) | BE889823A (en) |
CH (1) | CH645976A5 (en) |
DE (1) | DE3129530A1 (en) |
FR (1) | FR2487966B1 (en) |
GB (1) | GB2081428B (en) |
IT (1) | IT1144438B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4498367A (en) * | 1982-09-30 | 1985-02-12 | Southwest Energy Group, Ltd. | Energy transfer through a multi-layer liner for shaped charges |
DE3525613A1 (en) * | 1985-07-18 | 1987-01-22 | Rheinmetall Gmbh | INSERT FOR PUTTING A BLAST CHARGE AND FORMING A ROD-SHAPED PROJECTILE AND METHOD FOR PRODUCING THE INSERT |
FR2599648B1 (en) * | 1986-06-10 | 1995-06-30 | Saint Louis Inst | PROCESS FOR THE MANUFACTURE OF A HOLLOW LOAD COATING |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1086048A (en) * | 1953-07-02 | 1955-02-09 | Soc Tech De Rech Ind | Improvements to coatings for crense loads |
FR1327804A (en) * | 1962-04-09 | 1963-05-24 | Soc Tech De Rech Ind | Improvements to coatings for shaped charges |
US3112700A (en) * | 1959-12-11 | 1963-12-03 | Jr John W Gehring | Eutectic alloy shaped charge liner |
FR1531530A (en) * | 1967-05-22 | 1968-07-05 | Alsetex Soc Alsacienne D Etude | Advanced training in shaped charges |
FR2268242A1 (en) * | 1974-04-17 | 1975-11-14 | Poudres & Explosifs Ste Nale |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2429990B1 (en) * | 1978-06-27 | 1985-11-15 | Saint Louis Inst | EXPLOSIVE FLAT CHARGE |
-
1980
- 1980-08-01 FR FR8017029A patent/FR2487966B1/en not_active Expired
-
1981
- 1981-07-23 GB GB8122764A patent/GB2081428B/en not_active Expired
- 1981-07-27 DE DE19813129530 patent/DE3129530A1/en active Granted
- 1981-07-27 IT IT68042/81A patent/IT1144438B/en active
- 1981-07-30 CH CH495381A patent/CH645976A5/en not_active IP Right Cessation
- 1981-07-31 BE BE0/205554A patent/BE889823A/en not_active IP Right Cessation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1086048A (en) * | 1953-07-02 | 1955-02-09 | Soc Tech De Rech Ind | Improvements to coatings for crense loads |
US3112700A (en) * | 1959-12-11 | 1963-12-03 | Jr John W Gehring | Eutectic alloy shaped charge liner |
FR1327804A (en) * | 1962-04-09 | 1963-05-24 | Soc Tech De Rech Ind | Improvements to coatings for shaped charges |
FR1531530A (en) * | 1967-05-22 | 1968-07-05 | Alsetex Soc Alsacienne D Etude | Advanced training in shaped charges |
FR2268242A1 (en) * | 1974-04-17 | 1975-11-14 | Poudres & Explosifs Ste Nale |
Also Published As
Publication number | Publication date |
---|---|
CH645976A5 (en) | 1984-10-31 |
DE3129530C2 (en) | 1989-12-21 |
GB2081428B (en) | 1984-01-18 |
FR2487966B1 (en) | 1986-07-11 |
DE3129530A1 (en) | 1982-06-03 |
GB2081428A (en) | 1982-02-17 |
BE889823A (en) | 1981-11-16 |
IT1144438B (en) | 1986-10-29 |
IT8168042A0 (en) | 1981-07-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |