EP2327952B1 - Gefechtskopf mit Tandemhohlladung - Google Patents
Gefechtskopf mit Tandemhohlladung Download PDFInfo
- Publication number
- EP2327952B1 EP2327952B1 EP10290614.6A EP10290614A EP2327952B1 EP 2327952 B1 EP2327952 B1 EP 2327952B1 EP 10290614 A EP10290614 A EP 10290614A EP 2327952 B1 EP2327952 B1 EP 2327952B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- screen
- charge
- load
- cylindrical zone
- warhead
- 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.)
- Active
Links
- 239000000463 material Substances 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims description 5
- 230000015572 biosynthetic process Effects 0.000 claims description 2
- 230000000977 initiatory effect Effects 0.000 description 11
- 239000007789 gas Substances 0.000 description 9
- 230000000694 effects Effects 0.000 description 7
- 238000000576 coating method Methods 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 239000011248 coating agent Substances 0.000 description 4
- 230000035939 shock Effects 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 239000011324 bead Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000006262 metallic foam Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
- F42B12/16—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge in combination with an additional projectile or charge, acting successively on the target
- F42B12/18—Hollow charges in tandem arrangement
Definitions
- the technical field of the invention is that of the military heads comprising formed charges mounted in tandem.
- tandem charges are well known. They combine a front formed load and a rear formed load which are separated from each other by intercharging protection means.
- the charges are initiated in sequence with a delay of the order of a few hundred microseconds or even of the order of a millisecond between the two charges.
- tandem loads can counter the shields equipped with reactive overprotection.
- the front load makes it possible to initiate the reactive shielding, and the rear charge perforates the main shield once it is no longer protected by its reactive protection.
- the known charges all include an intercharging protection which makes it possible to protect the rear charge during the detonation of the front load.
- This protection most often comprises a screen, more or less solid, which is secured to the envelope of the load and the vents arranged in the case of the load and which allow to radially evacuate the gases generated by the initiation front load.
- the patent FR2540238 thus describes a tandem load head in which an intercharge protection is made in the form of one or more partitions integral with the outer wall of the military head.
- the wall is also weakened by streaks, which allows it to burst under the effect of the shock wave.
- Such protection is particularly cumbersome, the multiplication of screens and fragmentable areas leading to the elongation of the intercharging space.
- this patent describes a metal disc interposed between the front sleeve and the deformable tube, this thin disc has little effect in absorbing the impact but only prevents the penetration of gas or splinters inside the tube. deformable.
- the patent EP1531316 describes a tandem head in which the front load and the rear load are separated by a wall pierced by a passage for the jet of the rear load.
- This partition also comprises a sealing cap applied to a damping material.
- Such a structure also does not allow to achieve a compact military head.
- the patent FR2581749 which forms a starting point for the present invention, describes a specific tandem head incorporating a thruster between front load and rear load, the thruster acting as intercharging screen.
- the patent DE4126793 finally proposes a military head with tandem charges in which the rear load is translated with respect to the case by the effect of the gases of the front load, gases that are otherwise deflected around the rear load by the conical profile of a screen.
- the object of the invention is to provide a military head with tandem loads, in which head, the overall length of the head remains reduced, but the protection of the rear load against the effects of the front load is nevertheless ensured.
- the subject of the invention is a tandem-loaded military head comprising a front load disposed remotely from a rear load, and an intercharging protection means interposed between the two loads and comprising a means of connection with controlled deformation, a military head.
- the intercharging protection means comprises at least a first metal screen which is arranged between the front load and the rear load, the first screen which comprises a solid central part to which is attached the controlled strain deformation means which is constituted by a thinned cylindrical zone comprising at least one groove for initiating a deformation of said cylindrical zone, thinned cylindrical zone which is integral with the caliber of the envelope of the rear charge and which covers the latter.
- the intercharging protection means may comprise a second metal screen interposed between the front load and the first screen, the second screen which is integral with a ferrule connecting the two loads.
- the second screen may have a conical profile, the top of the cone of which will be directed towards the front load, the first screen being formed of a simple integral conical cowling of the thin cylindrical zone, the conicity of the second screen being identical to that of the first screen.
- a layer of a deformable material may advantageously be interposed between the first and the second screen.
- the ferrule may include at least one vent.
- a tandem charge military head 1 according to the invention comprises a front load 2 which is arranged at a distance from a rear load 3.
- Each load 2 and 3 is a charge formed, that is to say it comprises an explosive charge on which is applied a concave coating 2a, 3a which generates a jet at high speed during the initiation of the load.
- the coatings may be conical. But any other concave shape (portion of sphere, paraboloid ...) could be implemented.
- the choice of the geometry of the coating depends on the desired performance for the fillers 2 and 3.
- the coatings 2a, 3a will generally be made of a ductile metallic material, for example copper.
- the figure 1 shows in partial section the rear load 3, which allows to see the coating 3a and the explosive charge 3b contained in a cylindrical envelope 3c.
- the front load 2 is not cut but is represented by dotted its coating 2a.
- the front load 2 and the rear load 3 are arranged in a case 4 (or ferrule) which makes it possible to connect the charges to one another.
- the case 4 has a rear portion 4a slightly larger than that of the rear load 3 and a front portion 4b the caliber of the front load 2.
- the rear load 3 is fixed to the shell 4 at radial shims 7.
- the loads 2 and 3 are secured to the shell 4 (and shims 7) by any appropriate means, for example by radial pins (not shown ).
- the rear portions 4a and 4b before the ferrule 4 are connected by a conical portion 4c.
- the ferrule 4 further includes vents 5, regularly distributed angularly, and which can radially evacuate a portion of the gases generated during the initiation of the load before 2. Such a known arrangement can partially protect the rear load 3 .
- the military head 1 finally comprises a means 6 for intercharging protection which is interposed between the front load 2 and the rear load 3.
- This intercharging protection means 6 comprises at least a first metal screen 8 which is secured to the envelope 3c of the rear load 3 by a controlled deformation linkage means.
- the metal screen 8 has a conical profile whose cone apex is directed towards the front load 2.
- the controlled deformation binding means is constituted here by a thin cylindrical zone (or wall) 9 which cap the envelope 3c of the rear charge 3.
- This cylindrical zone 9 further comprises a groove 10 which makes it possible to initiate a deformation of said cylindrical zone 9.
- the cylindrical zone 9 comes into axial abutment against a shim 7 of the rear load 3.
- the cylindrical zone 9 may be glued to the envelope 3c of the rear load or it may be threaded to this envelope.
- the circular groove 10 extends, inside the cavity 12 delimited by the screen 8, by a bead 11.
- the screen 8 extended by the cylindrical zone 9 thus constitutes a housing which caps the front of the rear load 3. This housing delimits a volume whose dimensions after deformation of the cylindrical zone 9 are however controlled and which are defined by design so as to allow the formation of the jet of the rear load 3.
- the massive conical portion of the screen 8 receives during the initiation of the load before 2 the pressure of the generated gases and the rear projections (chips ...) from the front load. This solid part transmits the received shock to the thinned cylindrical zone 9 which will deform plastically by absorbing the mechanical energy received.
- the rear charge 3 is therefore protected despite the relatively small distance between the two charges.
- the conical profile of the screen 8 ensures a deflection of the gases which are evacuated by the vents 5.
- the circular groove 10 has the effect of initiating and directing the plastic deformation of the cylindrical zone 9.
- the latter instead of splitting longitudinally will rather crash, practically accordion.
- the figure 2 shows the configuration of the screen 8 and the cylindrical zone 9 after initiation of the front load.
- the solid portion 8 of the screen has moved in the direction F while the cylindrical portion 9 has remained in abutment on the wedges 7.
- the cylindrical zone 9 has then crashed.
- the residual length L2 of the protection means 6 is less than half that of the initial length L1.
- a screen 8 with a thickness of 5 to 8 mm associated with a cylindrical zone 9 with a thickness of 2 to 3 mm provides effective protection with an intercharging distance of the order of 2 calibres of the rear charge.
- the cylindrical zone is reduced by about 50 to 70% of its initial length.
- the figure 3 thus shows a second embodiment of the invention in which the protection means 6 comprises a second metal screen 13 which is interposed between the front load 2 and the first screen 8.
- This second screen 13 is made integral with the ferrule 4 connecting the two loads by shearable pins 14.
- the first screen 8 is of relatively small thickness.
- the taper of the cowling 8 is identical to that of the internal profile 15 of the second screen 13.
- This layer may cover the entire conical surface of the screens or more simply (as shown here) have the shape of a washer.
- a deformable material it will be possible to choose a metallic honeycomb (for example based on aluminum) or even a porous metal foam, for example porous aluminum.
- Such reinforced protection makes it possible to obtain compact military heads (intercharging distance of between 1 and 3 calibres of the rear load) while putting in place a front load 2 of relatively large size (from 70 to 90% of the load size). back).
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Image-Pickup Tubes, Image-Amplification Tubes, And Storage Tubes (AREA)
Claims (6)
- Gefechtskopf (1) mit Tandemhohlladung, umfassend eine vordere Ladung (2), welche beabstandet von einer hinteren Ladung (3) angeordnet ist, und ein Zwischenladung-Schutzmittel (6), welches zwischen die beiden Ladungen eingefügt ist und ein Verbindungsmittel (9) mit kontrollierter Deformation umfasst, wobei der Gefechtskopf dadurch gekennzeichnet ist, dass das Zwischenladung-Schutzmittel (6) mindestens einen ersten Metallschirm (8) umfasst, welcher zwischen der vorderen Ladung (2) und der hinteren Ladung (3) angeordnet ist, wobei an dem ersten Schirm (8) das Verbindungsmittel mit kontrollierter Deformation befestigt ist, welches von einem zylindrischen, dünner werdenden Bereich (9) gebildet wird, welcher mindestens eine Einkerbung (10) aufweist, welche es ermöglicht, eine Deformation des genannten zylindrischen Bereichs (9) einzuleiten, wobei der dünner werdende zylindrische Bereich fest mit der Ummantelung (3c) der hinteren Ladung (3) verbunden und in deren Kaliber ist und diese Letztere überdeckt; wobei der erste Schirm und der zylindrische Bereich (9) ein Gehäuse bilden, welches ein Volumen abgrenzt, das die Bildung des Strahls der hinteren Ladung begünstigt.
- Gefechtskopf nach Anspruch 1, dadurch gekennzeichnet, dass der erste Schirm (8) einen zentralen, massiven Abschnitt umfasst, an welchem der zylindrische, dünner werdende Bereich (9) befestigt ist.
- Gefechtskopf nach Anspruch 1, dadurch gekennzeichnet, dass das Zwischenladung-Schutzmittel einen zweiten Metallschirm (13) umfasst, welcher zwischen der vorderen Ladung (2) und dem ersten Schirm (8) eingefügt ist, wobei der zweite Schirm (13) fest mit einer die beiden Ladungen verbindenden Hülse (4) verbunden ist.
- Gefechtskopf nach Anspruch 3, dadurch gekennzeichnet, dass der zweite Schirm (13) ein konisches Profil aufweist, dessen Scheitel des Kegels zur vorderen Ladung (2) ausgerichtet ist, wobei der erste Schirm (8) aus einer einfachen, konischen Abdeckung gebildet ist, welche fest mit dem zylindrischen, dünnen Bereich (9) verbunden ist, wobei die Konizität des zweiten Schirms (13) mit jener des ersten Schirms (8) identisch ist.
- Gefechtskopf nach Anspruch 4, dadurch gekennzeichnet, dass eine Schicht (16) aus einem verformbaren Material zwischen den ersten (8) und den zweiten Schirm (13) eingefügt ist.
- Gefechtskopf nach einem der Ansprüche 3 bis 5, dadurch gekennzeichnet, dass die Hülse (4) mindestens ein Entlüftungsloch (5) umfasst.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0905693A FR2953009A1 (fr) | 2009-11-26 | 2009-11-26 | Tete militaire a charges en tandem |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2327952A1 EP2327952A1 (de) | 2011-06-01 |
EP2327952B1 true EP2327952B1 (de) | 2015-09-09 |
Family
ID=42246221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10290614.6A Active EP2327952B1 (de) | 2009-11-26 | 2010-11-18 | Gefechtskopf mit Tandemhohlladung |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2327952B1 (de) |
FR (1) | FR2953009A1 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2775320C1 (ru) * | 2022-01-25 | 2022-06-29 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Проникающий в преграду зонд |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102018005258B4 (de) * | 2018-07-02 | 2023-02-02 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Tandem-Ladung für einen Flugkörper und schockabweisende Kappe für eine Hauptladung einer Tandem-Ladung |
DE102018006741B4 (de) * | 2018-08-24 | 2022-06-15 | TDW Gesellschaft für verteidigungstecchnische Wirksysteme mbH | Tandem-Ladung für einen Flugkörper |
DE102020001784A1 (de) | 2020-03-17 | 2021-09-23 | Diehl Defence Gmbh & Co. Kg | Geschoss, Wirkmittelanordnung und Verfahren |
DE102023000642B3 (de) | 2023-02-22 | 2024-01-25 | Bundesrepublik Deutschland, vertr. durch das Bundesministerium der Verteidigung, vertr. durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr | Gefechtskopf mit einer Vorhohlladung und einer Haupthohlladung |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2552870B1 (fr) * | 1980-10-24 | 1987-02-13 | France Etat Armement | Perfectionnement aux tetes militaires a charges formees montees en tandem |
FR2540238B1 (fr) * | 1983-01-27 | 1987-01-16 | Serat | Perfectionnements apportes aux charges creuses doubles |
FR2559896B1 (fr) | 1984-02-20 | 1987-09-25 | France Etat Armement | Retard d'initiation pour tete militaire a charges formees montees en tandem |
FR2577037B1 (fr) | 1985-01-31 | 1987-11-13 | France Etat Armement | Tete militaire a charges formees montees en tandem |
FR2581749B1 (fr) * | 1985-05-10 | 1987-10-02 | France Etat Armement | Projectile antichar |
DE3601051C1 (en) | 1986-01-16 | 1987-06-11 | Messerschmitt Boelkow Blohm | Warhead |
IL81097A (en) * | 1986-12-25 | 1991-06-10 | Israel Defence | Two-stage shaped charge projectile |
DE3740412C1 (de) * | 1987-11-28 | 1996-04-25 | Rheinmetall Ind Gmbh | Gefechtskopf |
DE4126793C1 (de) * | 1991-08-14 | 1994-05-11 | Deutsche Aerospace | Tandemgefechtskopf |
EP1531316A1 (de) * | 2003-11-11 | 2005-05-18 | RUAG Munition | Struktur eines Geschosses |
-
2009
- 2009-11-26 FR FR0905693A patent/FR2953009A1/fr active Pending
-
2010
- 2010-11-18 EP EP10290614.6A patent/EP2327952B1/de active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2775320C1 (ru) * | 2022-01-25 | 2022-06-29 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Проникающий в преграду зонд |
Also Published As
Publication number | Publication date |
---|---|
FR2953009A1 (fr) | 2011-05-27 |
EP2327952A1 (de) | 2011-06-01 |
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