FR2496252A1 - Multiple stage hollow charge - has conical stages of differing sizes and taper acting in forward and rear directions - Google Patents

Multiple stage hollow charge - has conical stages of differing sizes and taper acting in forward and rear directions Download PDF

Info

Publication number
FR2496252A1
FR2496252A1 FR8026635A FR8026635A FR2496252A1 FR 2496252 A1 FR2496252 A1 FR 2496252A1 FR 8026635 A FR8026635 A FR 8026635A FR 8026635 A FR8026635 A FR 8026635A FR 2496252 A1 FR2496252 A1 FR 2496252A1
Authority
FR
France
Prior art keywords
stage
hollow charge
perforating
stages
retro
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
Application number
FR8026635A
Other languages
French (fr)
Other versions
FR2496252B1 (en
Inventor
Simone De Montrigaud
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SERAT
Original Assignee
SERAT
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SERAT filed Critical SERAT
Priority to FR8026635A priority Critical patent/FR2496252B1/en
Publication of FR2496252A1 publication Critical patent/FR2496252A1/en
Application granted granted Critical
Publication of FR2496252B1 publication Critical patent/FR2496252B1/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04Projectiles, 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
    • F42B12/10Projectiles, 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
    • F42B12/16Projectiles, 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
    • F42B12/18Hollow charges in tandem arrangement

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

The hollow charge has a cover shape formed by revolution of an opposed conical section solid (10-14). The slope may be regular and define several perforation stages. The thickness of all parts of the revolution elements can be the same or varied. Each element of the generated shape forms one stage of working of the hollow charge. From rear to front, the first rear stage (J1 N1) acting forward, is followed by a first intermediate stage (J13) acting rearwards and so on.

Description

Cette invention est relative à des perfectionnements apportés aux charges creuses. On sait que les charges creuses connues comportent géné- ralement un revêtement de révolution en cuivre de forme géométrique simple: par exemple, cane (génératrice droite), ou de profil curviligne (par exemple, revêtement ogival ou "tulipe").  This invention relates to improvements made to shaped charges. It is known that the known shaped charges generally comprise a coating of revolution in copper of simple geometric shape: for example, cane (straight generator), or of curvilinear profile (for example, ogival coating or "tulip").

Dans le but d'augmenter l'efficacité de ces charges, on a imaginé d'additionner des effets de charges disposées les unes derrière les autres, par exemple comme décrit et revendiqué par la Demanderesse dans ses brevets français
- n" 75 14 091, du 6 mai 1975
- n" 77 35 320, du 24 novembre 1977, et sa première Addition,
- n" 80 23 444, du 3 novembre 1980.
In order to increase the efficiency of these charges, it has been imagined to add effects of charges arranged one behind the other, for example as described and claimed by the Applicant in its French patents
- No. 75 14 091, of May 6, 1975
- No 77 35 320 of 24 November 1977 and its first Addition,
- No 80 23 444, of 3 November 1980.

Ces dispositions imposent d'avoir deux ou plusieurs charges, des revêtements distincts et des systèmes de retard entre les amorçages des charges successives (retards pyrotechniques ou électroniques). These provisions require having two or more charges, separate coatings and delay systems between the initiation of successive charges (pyrotechnic or electronic delays).

La présente invention apporte un nouveau progrès, en augmentant la masse du jet produit sans augmenter le calibre. The present invention brings a new progress, by increasing the mass of the jet produced without increasing the caliber.

Selon l'invention, on augmente la masse du jet en prévoyant un unique revêtement de révolution, ledit revêtement étant généré par une ligne brisée ou courbe composée d'éléments rectilignes à plusieurs maxima et minima, de révolution autour de l'axe longitudinal du projectile, définissant les étages de fonctionnement perforant de l'ensemble. According to the invention, the mass of the jet is increased by providing a single coating of revolution, said coating being generated by a broken or curved line composed of rectilinear elements with several maxima and minima, of revolution around the longitudinal axis of the projectile , defining the perforating operating stages of the assembly.

Le nombre d'éléments du revêtement à génératrice en ligne brisée ou courbe selon l'invention n'est pas limité ; il peut hêtre supérieur à 2. The number of elements of the broken or curved line generator coating according to the invention is not limited; it can be more than 2.

Les divers caractéristiques et avantages de l'invention ressortiront des exemples décrits ci-après. The various characteristics and advantages of the invention will emerge from the examples described below.

I1 est bien précisé qutil s'agit uniquement d'exemples, et que tous autres modes de construction, disposition, formes, proportions, peuvent être utilisés sans sortir du cadre de l'invention. It is clearly stated that these are only examples, and that all other modes of construction, arrangement, shapes, proportions, can be used without departing from the scope of the invention.

Au cours de cette description, on se réfère aux dessins annexés, sur lesquels
- la Figure 1 est une vue schématique, en élévation, d'un premier exemple de réalisation dtune charge creuse selon l'invention;
- les Figures 2 et 3 sont des vues schématiques partielles, en élé vation, illustrant deux variantes du revêtement de la charge creuse selon l'invention ; et,
- la Figure 4 est une vue schématique, en élévation, d'une variante du revêtement comportant des éléments courbes.
In the course of this description, reference is made to the appended drawings, in which
- Figure 1 is a schematic view, in elevation, of a first embodiment of a hollow charge according to the invention;
- Figures 2 and 3 are partial schematic views, in elevation, illustrating two variants of the coating of the shaped charge according to the invention; and,
- Figure 4 is a schematic view, in elevation, of a variant of the coating comprising curved elements.

En se référant à la Figure 1, on y a représenté schematiquement une tete à charge creuse comportant trois étages perforants (exemple non limitatif) selon l'invention. Elle comprend un revêtement 1 en ligne brisée selon l'invention, des explosifs principaux 2, 2' et 2" des trois étages perforants successifs 10, 11 et 12. L'étage arrière 10 comprend, en outre, un écran 4 et un amorçage 5. Une enveloppe 6 et une ogive 7 achèvent la construction. Referring to Figure 1, there is shown schematically a hollow charge head comprising three perforating stages (non-limiting example) according to the invention. It comprises a coating 1 in a broken line according to the invention, main explosives 2, 2 ′ and 2 ″ from the three successive perforating stages 10, 11 and 12. The rear stage 10 further comprises a screen 4 and a priming 5. An envelope 6 and a warhead 7 complete the construction.

Le revêtement 1 en ligne brisée selon l'invention comprend cinq éléments rectilignes P1 à P5 (ce nombre n'étant pas limitatif), et quatre discontinuités d à d4 (ce nombre n'étant pas limitatif). The coating 1 in broken line according to the invention comprises five rectilinear elements P1 to P5 (this number not being limiting), and four discontinuities d to d4 (this number not being limiting).

Ce revetement 1 définit les trois étages perforants précités 10, 11 et 12 de fonctionnement selon l'invention (non limitatif). This coating 1 defines the three aforementioned perforating stages 10, 11 and 12 of operation according to the invention (not limiting).

On voit, sur la Figure 1, qu'après initiation de l'amorçage 5, une onde torique est formée dans l'explosif 2 par l'écr-an 4, et attaque la fraction
P1 du premier étage 10 perforant du revêtement selon l'invention.
We see, in Figure 1, that after initiation of the priming 5, an O-wave is formed in the explosive 2 by the screen 4, and attacks the fraction
P1 of the first stage 10 perforating the coating according to the invention.

La partie P1 du revêtement 1 selon l'invention produit un premier jet J1 et un noyau N1. The part P1 of the coating 1 according to the invention produces a first jet J1 and a core N1.

Le deuxième étage perforant 11 du revetement 1 selon l'invention fonctionne comme le premier étage perforant 10. Cet étage 11 perforant comprend la fraction P3 dudit revêtement 1, un explosif principal 2', et il forme un jet J2 (+ noyau N2) qui doit compléter, selon l'invention, le jet J1 de l'étage précédent 10. The second perforating stage 11 of the coating 1 according to the invention functions like the first perforating stage 10. This perforating stage 11 comprises the fraction P3 of said coating 1, a main explosive 2 ', and it forms a jet J2 (+ core N2) which must complete, according to the invention, the jet J1 of the previous stage 10.

Selon l'invention, on intercale entre ces deux étages perforants 10 et 1 1 un chargement annulaire 3 en explosif moins rapide que les explosifs 2 et 2' desdits étages perforants 10 et 11. Ce chargement 3 entoure la partie
P2 du revetement à génératrice en ligne brisée selon l'invention.On réalise ainsi un ensemble intermédiaire 13 (explosif 3 et fraction P2 du revetement 1) qui forme, selon l'invention, d'une part une charge creuse à effet dirigé vers l'arrière, et qui, d'autre part, assure l'excitation du deuxième étage perforant 1 1 (revêtement P3 et explosif 2') par l'intermédiaire dudit explosif
3 3 dudit étage ou ensemble intermédiaire explosif 1 3 selon l'invention, moins rapide, d'où, intrinsèquement, compte tenu des dimensions (longueur e) dudit ensemble ou étage 13, un retard de fonctionnement du deuxième étage perforant 11 par rapport au premier étage perforant 10.
According to the invention, an annular charge 3 of explosive slower than explosives 2 and 2 ′ of said perforating stages 10 and 11 is interposed between these two perforating stages 10 and 1 1. This charging 3 surrounds the part
P2 of the coating with a broken line generator according to the invention. This produces an intermediate assembly 13 (explosive 3 and fraction P2 of the coating 1) which, according to the invention, forms on the one hand a hollow charge with an effect directed towards the 'rear, and which, on the other hand, ensures the excitation of the second perforating stage 1 1 (P3 coating and explosive 2') via said explosive
3 3 of said explosive intermediate stage or assembly 1 3 according to the invention, slower, hence, intrinsically, taking into account the dimensions (length e) of said assembly or stage 13, an operating delay of the second perforating stage 11 relative to the first perforating stage 10.

Ainsi, et selon l'invention, ce dispositif d'un jet "rétro" J13, agissant en sens inverse, freine le noyau N1 du premier étage perforant 10 et l'empeche de gener l'addition des jets J1 et J2 des deux étages perforants 10 et 11 (J1 passant naturellement avant J2, par la chronométrie meme du fonctionnement de la charge selon l'invention). Thus, and according to the invention, this device of a “retro” jet J13, acting in the opposite direction, brakes the core N1 of the first perforating stage 10 and prevents it from generating the addition of the jets J1 and J2 of the two stages perforators 10 and 11 (J1 passing naturally before J2, even by the timing of the operation of the load according to the invention).

On voit donc que, selon l'invention, le revêtement 1 à génératrice en ligne brisée et la succession d'étages de chargement engendrant des jets additionnés successifs lancés vers l'avant, avec interposition, entre deux étages successifs perforants de ce type, d'un étage inverse ou "rétro", permet à la fois, selon l'invention: - de retarder l'effet perturbateur de étage de rang n par rapport à l'étage
de rang n + ; - d'assurer en meme temps, avec un retard convenable, la détonation de
l'étage de rang n + 1 après celle de l'étage de rang n.
It can therefore be seen that, according to the invention, the coating 1 with a broken line generator and the succession of loading stages generating successive added jets launched forward, with interposition, between two successive perforating stages of this type, d 'a reverse or "retro" stage, allows both, according to the invention: - to delay the disturbing effect of stage of rank n with respect to the stage
of rank n +; - ensure at the same time, with a suitable delay, the detonation of
the stage of row n + 1 after that of the stage of row n.

En poursuivant l'examen de la Figure 1, on trouve en continuant vers la gauche, en regardant cette Figure - un étage intermédiaire 14 (explosif "plus lent" 3', fraction P4 du revete-
ment 1, longueur 1,, jet à effet inverse J );
14 - un troisième étage perforant 12 (explosif plus rapide 2", fraction P5 du
revêtement 1, jet J3 et noyau N3).
Continuing the examination of Figure 1, we find continuing to the left, looking at this Figure - an intermediate stage 14 (explosive "slower" 3 ', fraction P4 of the coating-
ment 1, length 1 ,, reverse jet J);
14 - a third perforating stage 12 (faster explosive 2 ", fraction P5 of
coating 1, jet J3 and core N3).

Comme décrit précédemment pour le premier étage intermédiaire 13, le second étage intermédiaire 14 assure, selon l'invention, l'excitation du troisième étage perforant 12 (par son explosif 3' plus lent), et compte tenu de sa longueur g1, de manière que les noyaux N1 et N2 ne viennent pas perturber l'addition au jet J3 du troisième étage perforant 12 des jets successifs J1 et J2 des deux étages perforants précédents 10 et 11. As described above for the first intermediate stage 13, the second intermediate stage 14 ensures, according to the invention, the excitation of the third perforating stage 12 (by its explosive 3 'slower), and taking into account its length g1, so that the cores N1 and N2 do not disturb the addition to the jet J3 of the third perforating stage 12 of the successive jets J1 and J2 of the two preceding perforating stages 10 and 11.

Cette combinaison d'effets permet d'obtenir, avec le revetement engendré par une ligne brisée selon l'invention, un jet plus long et de masse plus importante qu'un jet de charge creuse classique. This combination of effects makes it possible to obtain, with the coating generated by a broken line according to the invention, a longer jet and of greater mass than a conventional hollow charge jet.

Les pentes o( des éléments de la ligne brisée engendrant, par révolution autour de l'axe du projectile, le revetement selon l'invention, peuvent etre répétitives (Figure 2) ou non répétitives (Figure 3), sans sortir du cadre de l'invention. The slopes o (elements of the broken line generating, by revolution around the axis of the projectile, the coating according to the invention, can be repetitive (Figure 2) or non-repetitive (Figure 3), without departing from the scope of the 'invention.

Sur la Figure 4, on a représente une variante du revêtement selon l'invention, dont la génératrice comporte des éléments courbes, C1 à C5. In Figure 4, there is shown a variant of the coating according to the invention, the generator of which comprises curved elements, C1 to C5.

L'épaisseur du revêtenJent selon l'inventjon peut etre constante dans ses éléments en ligne brisée ou courbe, ou variable, ou différente, sans sortir du cadre de l'invention
Naturellement, selon les explosifs utilisés, on peut avoir recours, sans sortir du cadre de l'invention, à des éléments pyrotechniques avec ou sans retard, pour compléter, améliorer ou modifier l'amorçage de l'explo- sif d'un étage de rang n + 1 par l'intervention de l'explosif d'un étage inter médiaire à partir de l'explosif d'un étage de rang n.
The thickness of the coating according to the invention can be constant in its elements in a broken or curved line, or variable, or different, without departing from the scope of the invention
Naturally, depending on the explosives used, pyrotechnic elements can be used, without departing from the scope of the invention, with or without delay, to complete, improve or modify the initiation of the explosive of a stage of rank n + 1 by the intervention of the explosive of an intermediate stage from the explosive of a stage of rank n.

Claims (11)

REVENDICATIONS 1 - Charge creuse comportant un revêtement de révolution carac térisé en ce qu'il est engendré par une génératrice en ligne brisée ou courbe composée d'éléments rectilignes ou non et à pentes répétitives ou non, définissant plusieurs étages de fonctionnement perforant de l'ensemble. 1 - Hollow charge comprising a coating of revolution characterized in that it is generated by a broken or curved line generator composed of rectilinear elements or not and with repetitive slopes or not, defining several stages of perforating operation of the assembly . 2 - Charge creuse selon la revendication 1, caractérisée en ce que ledit revetement est engendré par une génératrice en ligne brisée à éléments courbes, à plusieurs maxima et minima, définissant plusieurs étages de fonctionnement perforant , quelles que soient les concavités ou convexités des éléments courbes de la génératrice. 2 - Hollow charge according to claim 1, characterized in that said coating is generated by a broken line generator with curved elements, at several maxima and minima, defining several stages of perforating operation, whatever the concavities or convexities of the curved elements of the generator. 3 - Charge creuse comportant un revêtement selon l'une des revendications précédentes, caractérisée en ce que les épaisseurs des éléments de la génératrice sont constantes, ou différentes, ou encore variables, le long de chaque élément. 3 - Hollow charge comprising a coating according to one of the preceding claims, characterized in that the thicknesses of the elements of the generator are constant, or different, or even variable, along each element. 4 - Charge creuse comportant un revetement selon l'une quelconque des revendications précédentes, caractérisée en ce que chaque élément de la génératrice correspond à un étage de fonctionnement de la charge creuse. 4 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that each element of the generator corresponds to an operating stage of the hollow charge. 5 - Charge creuse comportant un revêtement selon l'une quelconque des revendications précédentes, caractérisée en ce qu'en parcourant le projectile de l'arrière vers l'avant, le premier étage arrière perforant agissant vers l'avant est suivi d'un premier étage intermédiaire agissant vers l'ar rière,(avec effet dit "rétro"), lui-même suivi d'un deuxième étage perforant agissant aussi vers l'avant, et ainsi de suite. 5 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that by traversing the projectile from rear to front, the first rear perforating stage acting towards the front is followed by a first intermediate stage acting towards the rear, (with so-called "retro" effect), itself followed by a second perforating stage acting also towards the front, and so on. 6 - Charge creuse comportant un revetement selon l'une quelconque des revendications précédentes, caractérisée en ce que chaque étage perforant à effet "rétro" correspond au chargement en explosif non obligatoirement identique (vitesse de détonation, puissance) à celui de l'étage qui le précède ou lui succède. 6 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that each perforating stage with "retro" effect corresponds to the loading of explosive which is not necessarily identical (detonation speed, power) to that of the stage which precedes or succeeds it. 7 - Charge creuse comportant un revêtement selon l'une quelconque des revendications précédentes, caractérisée en ce que les étages perforants agissant vers l'avant comportent des chargements en explosif plus rapide, alors que les étages intermédiaires , à effet "rétro" agissant vers l'arrière, comportent des chargements en explosif plus lent. 7 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that the perforating stages acting towards the front have faster explosive charges, while the intermediate stages, with a "retro" effect acting towards the 'rear, have slower explosive charges. 8 - Charge creuse comportant un revêtement selon l'une quelconque des revendications précédentes, caractérisée en ce qu'un étage de rang n + 1 perforant agissant vers l'avant, chargé en explosif plus rapide, est amorcé par l'étage, aussi perforant, agissant vers l'avant, de rang n, également chargé en explosif plus rapide à par l'intermédiaire de l'étage intermédiaire à effet "rétro" agissant vers l'arrière, intercalé entre ces deux étages n et n + 1 , par simple continuité de la détonation et contact direct des explosifs rapide (rang n), puis plus lent, intermédiaire "rétro", et enfin rapide avant (rang n + 1).  8 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that a stage of row n + 1 piercing acting forward, charged with faster explosive, is initiated by the stage, also piercing , acting forwards, of rank n, also charged with faster explosive through the intermediate stage with "retro" effect acting towards the rear, interposed between these two stages n and n + 1, by simple continuity of detonation and direct contact with explosives fast (row n), then slower, intermediate "retro", and finally fast before (row n + 1). 9 - Charge creuse comportant un revêtement selon l'une quelconque des revendications précédentes, caractérisée en ce que l'effet dirigé vers l'arrière, ou "rétro", de l'étage intermédiaire, retarde l'arrivée du noyau de l'étage précédent, de rang n, de manière que le jet dudit étage perforant de rang n vienne à l'avant du jet de l'étage perforant de rang n + 1, en permettant donc d!additionner ces deux jets, et ainsi de proche en proche pour tous les étages de la charge. 9 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that the rearward or "retro" effect of the intermediate stage delays the arrival of the core of the stage previous, of rank n, so that the jet of said perforating stage of rank n comes to the front of the jet of the perforating stage of rank n + 1, thus making it possible to add these two jets, and thus close in close for all stages of the load. 10 - Charge creuse comportant un revetement selon l'une quelconque des revendications précédentes, caractérisée en ce que la chronométrie des étages, et notamment celle de l'effet retardateur "rétro" d'un étage intermédiaire, est réglée par la combinaison des longueurs des étages successifs intermédiaires à effet "rétro" et des vitesses de détonation en explosif desdits étages successifs. 10 - Hollow charge comprising a coating according to any one of the preceding claims, characterized in that the timing of the stages, and in particular that of the "retro" retarding effect of an intermediate stage, is regulated by the combination of the lengths of the successive intermediate stages with a "retro" effect and explosive detonation rates of said successive stages. 11 - Charge creuse selon l'une quelconque des revendications précédentes, caractérisée en ce qu'elle comporte un élément pyrotechnique particulier, éventuellement complété par un retard, pour assurer, modifier, compléter l'amorçage du chargement d'un étage perforant de rang n + 1 à partir de l'étage perforant de rang n, par l'intermédiaire du chargement de l'étage intermédiaire à effet "rétro".  11 - Hollow charge according to any one of the preceding claims, characterized in that it comprises a particular pyrotechnic element, possibly supplemented by a delay, to ensure, modify, complete the initiation of the loading of a perforating stage of rank n + 1 from the perforating stage of row n, via the loading of the intermediate stage with "retro" effect.
FR8026635A 1980-12-16 1980-12-16 IMPROVEMENTS TO HOLLOW CHARGES Expired FR2496252B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8026635A FR2496252B1 (en) 1980-12-16 1980-12-16 IMPROVEMENTS TO HOLLOW CHARGES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8026635A FR2496252B1 (en) 1980-12-16 1980-12-16 IMPROVEMENTS TO HOLLOW CHARGES

Publications (2)

Publication Number Publication Date
FR2496252A1 true FR2496252A1 (en) 1982-06-18
FR2496252B1 FR2496252B1 (en) 1987-03-20

Family

ID=9249128

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8026635A Expired FR2496252B1 (en) 1980-12-16 1980-12-16 IMPROVEMENTS TO HOLLOW CHARGES

Country Status (1)

Country Link
FR (1) FR2496252B1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2583156A1 (en) * 1985-06-07 1986-12-12 Thomson Brandt Armements Hollow-charge head intended for piercing armour protected by active pre-armour
FR2856788A1 (en) * 2003-06-24 2004-12-31 Giat Ind Sa Multiple-effect munition with shaped explosive charges, primer systems and fragmentation casing, includes second annular explosive charge initiated by second primer system
US20230052273A1 (en) * 2020-01-21 2023-02-16 Saab Ab Shaped charge assembly

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB645611A (en) * 1943-08-10 1950-11-01 Ici Ltd Improvements in or relating to devices intended to effect the penetration of an object by the detonation of an explosive charge on the exterior thereof, for military andlike uses
FR1066178A (en) * 1951-09-12 1954-06-02 Luvo Ltd Improvements made to shaped explosive projectiles
FR1161445A (en) * 1956-08-30 1958-08-29 Improvements to the characteristics and constitution of shaped charges
US2856850A (en) * 1954-03-22 1958-10-21 Joseph H Church Shaped charge
FR1177197A (en) * 1957-06-06 1959-04-21 Converging sheet shaped explosive charge
CH397468A (en) * 1960-02-23 1965-08-15 Bofors Ab Shaped charge
US3416449A (en) * 1966-12-07 1968-12-17 Army Usa Tandem effect anti-tank projectile
US4004515A (en) * 1971-01-25 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Sequential jet shaped charge

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB645611A (en) * 1943-08-10 1950-11-01 Ici Ltd Improvements in or relating to devices intended to effect the penetration of an object by the detonation of an explosive charge on the exterior thereof, for military andlike uses
FR1066178A (en) * 1951-09-12 1954-06-02 Luvo Ltd Improvements made to shaped explosive projectiles
US2856850A (en) * 1954-03-22 1958-10-21 Joseph H Church Shaped charge
FR1161445A (en) * 1956-08-30 1958-08-29 Improvements to the characteristics and constitution of shaped charges
FR1177197A (en) * 1957-06-06 1959-04-21 Converging sheet shaped explosive charge
CH397468A (en) * 1960-02-23 1965-08-15 Bofors Ab Shaped charge
US3416449A (en) * 1966-12-07 1968-12-17 Army Usa Tandem effect anti-tank projectile
US4004515A (en) * 1971-01-25 1977-01-25 The United States Of America As Represented By The Secretary Of The Navy Sequential jet shaped charge

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2583156A1 (en) * 1985-06-07 1986-12-12 Thomson Brandt Armements Hollow-charge head intended for piercing armour protected by active pre-armour
FR2856788A1 (en) * 2003-06-24 2004-12-31 Giat Ind Sa Multiple-effect munition with shaped explosive charges, primer systems and fragmentation casing, includes second annular explosive charge initiated by second primer system
US20230052273A1 (en) * 2020-01-21 2023-02-16 Saab Ab Shaped charge assembly
EP4094037A4 (en) * 2020-01-21 2023-09-27 Saab Ab Shaped charge assembly

Also Published As

Publication number Publication date
FR2496252B1 (en) 1987-03-20

Similar Documents

Publication Publication Date Title
CH642446A5 (en) HOLLOW LOAD.
WO1988009477A1 (en) Improved perforating projectile
EP3102906B1 (en) Hollow charge and use for separating two floors of an aeronautical vehicle or for the neutralization thereof
FR2545923A1 (en) PROJECTILE ENSURING THE DRILLING OF SHIELDS
EP0053855B1 (en) Rotor for a centrifugal sling weapon
EP0221218A1 (en) Shaped-charge war heads in tandem arrangement
FR2552870A1 (en) Improvements to warheads with shaped charges mounted in tandem
FR2496252A1 (en) Multiple stage hollow charge - has conical stages of differing sizes and taper acting in forward and rear directions
FR2520102A1 (en) HOLLOW LOAD, IN PARTICULAR FOR MISSILE
CH635422A5 (en) EXPLOSIVE CHARGE.
EP0561085B1 (en) Method using a hollow charge for perforating an armour which is protected by a reactive pre-armour
FR2616217A1 (en) SYSTEM FOR MAINTAINING MULTIPLE LOADS EMBEDDED IN A PROJECTILE ROTATING AROUND ITS LONGITUDINAL AXIS
FR2805607A1 (en) EXPLOSIVE CHARGE FOR A PROJECTILE HEAD
BE512346A (en)
EP0084007A1 (en) Dual stage penetrator bomb
EP0437992A1 (en) Explosive charge creating a plurality of plugs and/or jets
FR2679994A1 (en) Device for igniting the propulsive charge of a munition, especially a telescoped munition, and munition initiated by such an igniting device
FR2563903A1 (en) BREAKING LOAD
FR2728674A1 (en) CARTRIDGE WITH SOCKET AND ARROW PROJECTILE
FR2552869A1 (en) Warhead with sequential hollow charges
EP0138640A1 (en) Explosive charge for military use
FR2576405A1 (en) COMBAT HEAD WITH A TAPERED CONE-SHAPED COVER
FR2540238A1 (en) Improvements made to double hollow charges
FR2552871A1 (en) Anti-tank projectile acting at the deviation speed
FR2706997A1 (en) Device for protecting an armoured structure from high energy projectiles

Legal Events

Date Code Title Description
ST Notification of lapse