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 PDFInfo
- 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
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- 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.)
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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
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- 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
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)
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 |
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FR (1) | FR2496252B1 (en) |
Cited By (3)
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)
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 |
-
1980
- 1980-12-16 FR FR8026635A patent/FR2496252B1/en not_active Expired
Patent Citations (8)
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)
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 |
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