FR2840402A1 - ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE - Google Patents
ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE Download PDFInfo
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- FR2840402A1 FR2840402A1 FR0206761A FR0206761A FR2840402A1 FR 2840402 A1 FR2840402 A1 FR 2840402A1 FR 0206761 A FR0206761 A FR 0206761A FR 0206761 A FR0206761 A FR 0206761A FR 2840402 A1 FR2840402 A1 FR 2840402A1
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- envelope
- explosive charge
- mpa
- resilience
- elongation rate
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- 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
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
-
- 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
- F42B12/24—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction with grooves, recesses or other wall weakenings
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Powder Metallurgy (AREA)
Abstract
Le secteur technique de l'invention est celui des enveloppes génératrices d'éclats pour charge explosive.L'enveloppe (2) selon l'invention est caractérisée en ce qu'elle est réalisée en un alliage de tungstène ayant une résilience supérieure à 120 J/ cm2, un taux d'allongement supérieur à 10% et une résistance à la rupture supérieure à 930 Mpa.The technical sector of the invention is that of envelopes generating splinters for explosive charge. The envelope (2) according to the invention is characterized in that it is made of a tungsten alloy having a resilience greater than 120 J / cm2, an elongation rate greater than 10% and a breaking strength greater than 930 Mpa.
Description
ss
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Le domaine technique de ltinvention est celui des The technical field of the invention is that of
enveloppes generatrices d'eclats pour charge explosive. shrapnel-generating envelopes for explosive charges.
Les charges explosives connues comportent generalement une enveloppe en acier, fragilisee ou non' ou encore une enveloppe comprenant des eclats preformes (billes ou The known explosive charges generally comprise a steel envelope, weakened or not, or else an envelope comprising preformed fragments (balls or
parallelepipedes) disposes entre deux etuls. parallelepipedes) arranged between two etuls.
Les brevets FR2807156, US5544589 et EP918206 decrivent The patents FR2807156, US5544589 and EP918206 describe
des enveloppes generatrices d' eclats connues. envelopes generating known fragments.
L'accroissement de la resistance des cibles conduit a rechercher une augmentation de lefficacite terminale des The increase in the resistance of the targets leads to seek an increase in the terminal efficiency of the
charges explosives.explosive charges.
Une tel. le augmentation peut et re obtenue par Such and such. the increase can and re obtained by
l' augmentation de la masse et de l'efficacite des eclats. increasing the mass and efficiency of the flakes.
Les eclats vent d'autant plus efficaces que leur IS geometric est maitrisee. Il est facile de maltriser la The flakes are all the more effective as their IS geometric is mastered. It's easy to subdue the
geometric en mettant en muvre des eclats preformes. geometric by using preformed flakes.
Cependant une telle solution est penalisante du point de vue du cout car la structure de la charge explosive est complexe, et comprend notamment des etuis de maintien des However, such a solution is penalizing from the point of view of cost because the structure of the explosive charge is complex, and in particular includes cases for holding the
eclats.bursts.
Une telle solution conduit egalement a definir des enveloppes multi couches. On reduit ainsi la masse du chargement explosif emporte et le rendement, done l'efficacite terminale en raison de la diminution de la Such a solution also leads to defining multi-layer envelopes. This reduces the mass of the explosive charge carried and the yield, therefore the terminal efficiency due to the decrease in the
vitesse des eclats.burst speed.
L'efficacite peut egalement etre accrue par une Efficiency can also be increased by
augmentation de la densite des eclats. increased density of flakes.
Cependant les materiaux denses (tungstene, uranium) qui vent habituellement mis en muvre dans les projectiles explosifs ne permettent pas d'engendrer des eclats de taille However, dense materials (tungsten, uranium), which are usually used in explosive projectiles, do not generate large fragments.
et masse suffisante.and sufficient mass.
Le brevet EP113833 decrit ainsi un projectile explosif comportant un corps en tungstene. Cependant les eclats engendres par un tel projectile ne vent pas homogenes et comprennent notamment une poussiere de tungstene n'ayant pas Patent EP113833 thus describes an explosive projectile comprising a tungsten body. However, the fragments generated by such a projectile are not homogeneous and include in particular a tungsten dust having no
d'effet perforant.perforating effect.
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C'est le but de l' invention que de proposer une enveloppe generatrice d' eclats ayant une efficacite amelioree par It is the aim of the invention to propose a casing generating splinters having an efficiency improved by
rapport aux enveloppes connues.compared to known envelopes.
Ainsi linvention a pour objet une enveloppe generatrice S d' eclats pour charge explosive, enveloppe caracterisee en ce quielle est realisee en un alliage de tungstene ayant une resilience superieure a 120 J/cm2, un taux d'allongement superieur a 10% et une resistance a la rupture superieure a Thus, the subject of the invention is an envelope S generating flakes for explosive charge, an envelope characterized in that it is made of a tungsten alloy having a resilience greater than 120 J / cm2, an elongation rate greater than 10% and a resistance at break greater than
930 Mpa.930 Mpa.
D'une facon preferee, lenveloppe sera realisee en un alliage de tungstene ayant une resilience superieure ou egale a 200 J/cm2, un taux dallongement superieur ou egal a 22% et Preferably, the envelope will be made of a tungsten alloy having a resilience greater than or equal to 200 J / cm2, an elongation rate greater than or equal to 22% and
une resistance a la rupture superieure ou egale a 1000 Mpa. a tensile strength greater than or equal to 1000 Mpa.
L'enveloppe pourra etre realisee en un alliage de tungstene ayant: une resilience de 380 J/cm2, un taux d'allongement de 35% et une resistance a la rupture de 1020 Mpa, ou bien une resilience de 320 J/cm2, un taux d 7 allongement de 30% et une resistance a la rupture de 1060 Mpa, ou bien une resilience de 200 J/cm2 r un taux d'allongement de 22G The envelope can be made of a tungsten alloy having: a resilience of 380 J / cm2, an elongation rate of 35% and a breaking strength of 1020 Mpa, or a resilience of 320 J / cm2, a rate of 7 elongation of 30% and a tensile strength of 1060 Mpa, or a resilience of 200 J / cm2 r an elongation rate of 22G
et une resistance a la rupture de 1150 Mpa. and a breaking strength of 1150 Mpa.
Avantageusement l' epaisseur de l' enveloppe sera comprise Advantageously, the thickness of the envelope will be understood
entre 2 mm et mm.between 2 mm and mm.
L'enveloppe pourra porter un reseau de lignes de fragilisationO Cette fragllisation pourra etre realisee sur une profondeur comprise entre 2% et 50 % de liepaisseur de ltenveloppe L' invention a egalement pour objet une charge explosive generatrice d' eclats incorporant une telle enveloppe ainsi The envelope can carry a network of lines of embrittlement. This embrittlement can be carried out over a depth of between 2% and 50% of the thickness of the envelope. The invention also relates to an explosive charge generating fragments incorporating such an envelope as well.
qutune munition comprenant une telle charge explosive. an ammunition comprising such an explosive charge.
La charge selon l' invention a une efficacite superieure a celle des charges a eclats connues car elle engendre des The charge according to the invention has a higher efficiency than that of known flash charges because it generates
eclats homogenes et de masse superieure. homogeneous flakes and of higher mass.
Par ailleurs elle incorpore une enveloppe generatrice declats pouvant avoir une geometric simple, facilitant ainsi In addition it incorporates a generator generator envelope which can have a simple geometric, thus facilitating
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la mise en muvre industrielle, et permettant l'emport d'une masse de chargement explosif importante' ce qui accrolt la vitesse des eclats, done leur efficaciteO Ainsi la charge explosive generatrice d' eclats selon S l' invention comprend un chargement explosif dispose dans une enveloppe generatrice dieclats ainsi qu'au moins un initiateur pour ce chargement, elle est caracterisee en ce que ltenveloppe generatrice d'eclats est realisee en un alliage de tungstene ayant une resilience superieure a 120 J/cm2, un taux d'allongement superieur a 10% et une resistance a la rupture superieure a 930 Mpa De preference, l'enveloppe sera realisee en un alliage de tungstene ayant une resilience superieure ou egale a 200 J/cm2, un taux d'allongement superieur ou egal a 22% et une industrial implementation, and allowing the carrying of a large explosive charge mass' which increases the speed of the fragments, therefore their efficiency. Thus the explosive charge generating fragments according to the invention comprises an explosive charge placed in a flash generator envelope as well as at least one initiator for this loading, it is characterized in that the chip generator envelope is made of a tungsten alloy having a resilience greater than 120 J / cm2, an elongation rate greater than 10% and a tensile strength greater than 930 Mpa Preferably, the envelope will be made of a tungsten alloy having a resilience greater than or equal to 200 J / cm2, an elongation rate greater than or equal to 22% and a
resistance a la rupture superieure ou egale a 1000 Mpa. tensile strength greater than or equal to 1000 Mpa.
L'enveloppe pourra etre realisee en un alliage de tungstene ayant: une resilience de 380 J/cm2, un taux d'allongement de 35% et une resistance a la rupture de 1020 Mpa, ou bien une resilience de 320 J/cm2/ un taux d'allongement de 30% et une resistance a la rupture de 1060 Mpa, ou bien une resilience de 200 J/cm2 F un taux d'allongement de 22% The envelope can be made of a tungsten alloy having: a resilience of 380 J / cm2, an elongation rate of 35% and a breaking strength of 1020 Mpa, or a resilience of 320 J / cm2 / un elongation rate of 30% and a tensile strength of 1060 Mpa, or a resilience of 200 J / cm2 F an elongation rate of 22%
et une resistance a la rupture de 1150 Mpa. and a breaking strength of 1150 Mpa.
L'enveloppe generatrice d' eclats pourra avoir une epaisseur comprise entre 2 mm et 8 mm et porter un reseau de The fragment-generating envelope may have a thickness of between 2 mm and 8 mm and carry a network of
lignes de fragilisation.lines of weakness.
La fragilisation pourra etre realisee sur une profondeur comprise entre 2% et 50% de l'epaisseur de l'enveloppe Avantageusement l'enveloppe pourra etre fermee par au moins un couvercle presentant une portee cylindrique au niveau de laquelle elle est positionnee, couvercle dont l'enveloppe sera rendue solidaire par des vis transversales, The embrittlement can be carried out over a depth between 2% and 50% of the thickness of the envelope Advantageously the envelope can be closed by at least one cover having a cylindrical bearing at the level of which it is positioned, cover including the envelope will be made integral by transverse screws,
par soudure laser ou par brasage.by laser welding or by soldering.
De preference au moins un couvercle sera realise en un materiau de densite inferieure a celle du materisu Preferably at least one cover will be made of a material with a density lower than that of the material.
d'enveloppe, par exemple en acier inoxydable. casing, for example stainless steel.
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La munition selon linvention est caracterisee en ce que l'enveloppe assure la liaison mecanique entre une partie avant et une partie arriere de la munition formant ainsi une The munition according to the invention is characterized in that the envelope provides the mechanical connection between a front part and a rear part of the ammunition thus forming a
partie de la structure du corps de munition. part of the structure of the ammunition body.
s Ltinvention sera mieux comprise a la lecture de la s The invention will be better understood on reading the
description qui va suivre de modes particuliers de description which follows of particular modes of
realisation' description faite en reference aux figures realization 'description made with reference to the figures
annexees et dans lesquelles o - la figure 1 est une coupe longitudinale d'une charge explosive selon un premier mode de realisation de 1 inventionr - la figure 2 est une coupe longitudinale d'une charge explosive selon un deuxieme mode de realisation de 1' invention' - la figure 3 est une coupe longitudinale d'une charge explosive selon un troisieme mode de realisation de 1 invention, - les figures 4 et 5 vent des vues externes d'une charge selon l' invention montrant la geometric des lignes de fragilisation, - la figure 6 montre en demi coupe longitudinale partielle une munition incorporant une charge selon annexed and in which o - Figure 1 is a longitudinal section of an explosive charge according to a first embodiment of the inventionr - Figure 2 is a longitudinal section of an explosive charge according to a second embodiment of the invention '- Figure 3 is a longitudinal section of an explosive charge according to a third embodiment of the invention, - Figures 4 and 5 are external views of a charge according to the invention showing the geometric lines of weakness, - Figure 6 shows in partial longitudinal half section a munition incorporating a charge according to
l' invention.the invention.
La figure 1 montre une charge explosive 1 comprenant une 2s enveloppe 2 fermee a chaque extremite par un couvercle 3 et 5 Figure 1 shows an explosive charge 1 comprising a 2s envelope 2 closed at each end by a cover 3 and 5
et renfermant un chargement explosif 4. and containing an explosive charge 4.
Le couvercle 5 porte un detonateur 6 ainsi qu'un ou plusieurs relais de detonation 7 de masse et forme appropriees. Conformement a l' invention l'enveloppe 2 est realisee en un alliage de tungstene ayant une resilience superieure a 120 J/cm2, un taux d'allongement superieur a 10% et une resistance a la rupture superieure a 930 MPa (mega pascals). La densite de l'alliage de tungstene sera comprise entre 3s 17 et 18,8, ce qui correspond a un taux de tungstene compris The cover 5 carries a detonator 6 as well as one or more detonation relays 7 of suitable mass and shape. In accordance with the invention, the casing 2 is made of a tungsten alloy having a resilience greater than 120 J / cm2, an elongation rate greater than 10% and a tensile strength greater than 930 MPa (mega pascals). The density of the tungsten alloy will be between 3s 17 and 18.8, which corresponds to a tungsten rate included
entre 90% et 98%.between 90% and 98%.
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L'epaisseur de l 7 enveloppe 2 sera de preference comprise entre 2 et 8 mm. Cette epaisseur sera bien entendu determinee The thickness of the envelope 7 will preferably be between 2 and 8 mm. This thickness will of course be determined
en fonction du calibre de la charge consideree. depending on the size of the load considered.
Les couvercles 3 et 5 seront de preference realises en un S materiau ayant une densite inferieure a celle du materisu d'enveloppe. En effet, si ces couvercles participant au confinement du chargement explosif 4, les eclats ou fragments qu'ils engendrent ne participant pas a l'efficacite de la charge lo Les couvercles seront done realises de facon a etre les plus legers possibles ce qui ameliorera le rapport masse efficace sur masse totale de la charge explosive 1. On pourra ainsi realiser les couvercles 3 et 5 en alliage d'aluminium The covers 3 and 5 will preferably be made of a material S having a density lower than that of the envelope material. Indeed, if these covers participating in the confinement of the explosive charge 4, the fragments or fragments which they generate do not participate in the effectiveness of the charge lo The covers will therefore be made in order to be as light as possible which will improve the effective mass to total mass ratio of the explosive charge 1. It will thus be possible to produce the covers 3 and 5 in aluminum alloy
en titane ou en acier, par exemple en acier inoxydable. made of titanium or steel, for example stainless steel.
Le choix de materiau d'enveloppe 2 propose par ltinvention permet d'une facon surprenante d 7 assurer une fragmentation naturelle de l'enveloppe en alliage de tungstene sous la forme declats relativement homogenes d'environ 0r5 grammes a 8 grammes de masse selon l'alliage mis en oeuvre. Cette derriere valeur (8 g) correspond a une charge de 90 mm de calibre ayant une enveloppe de 4 mm d'epaisseur. Pratiquement aucune poussiere de tungstene n'est The choice of envelope material 2 proposed by the invention makes it possible, surprisingly, to ensure a natural fragmentation of the envelope of tungsten alloy in the form of relatively homogeneous fragments of approximately 0.5 grams to 8 grams of mass depending on the alloy used. This last value (8 g) corresponds to a 90 mm load of caliber with a 4 mm thick envelope. Virtually no tungsten dust is
done engendree par la detonation.done by the detonation.
Il en resulte une efficacite perforante importante pour 2s la charge et un rapport de la masse efficace de la charge sur This results in a significant perforating efficiency for 2s the load and an effective mass ratio of the load on
la masse totale qui est important.the total mass which is important.
On a ainsi realise un certain nombre d'essais comparatifs de materiaux en fabriquant des enveloppes de charge presentant un rapport masse a projeter sur masse d'explosif egal a quatre. Toutes les enveloppes ont ete chargees en hexolite 60/40 (60% d'hexogene, 40% de tolite). Les resultats des essais vent resumes dans le tableau suivant: 3s A number of comparative tests of materials were thus carried out by manufacturing charge envelopes having a mass ratio to be projected onto mass of explosive equal to four. All the envelopes were loaded with 60/40 hexolite (60% hexogene, 40% tolerance). The results of the wind tests summarized in the following table: 3s
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N du Resilience Allongement Resistance Masse moyenne materiau (J/cm2) (%) a la des eclats teste rupture engendres (en (Mega milligramme) Pascal) N of Resilience Elongation Resistance Average mass of material (J / cm2) (%) at the level of the bursts tested rupture generated (in (Mega milligram) Pascal)
1 120 25 935 551,120 25,935 55
2 320 30 1060 742,320 30 1,060 74
3 10 7 600 < 23 10 7 600 <2
4 85 20 720 < 24 85 20 720 <2
60 15 730 < 260 15 730 <2
6 380 35 1020 736 380 35 1020 73
7 200 22 1150 757,200 22 1,150 75
8 200 14 1300 638,200 14 1,300 63
Les enveloppes ont ete realisees par frittage sous compression isostatique d'une poudre comprenant au moins 90% de tungstene ainsi que des materiaux d'addition et ayant une densite apres frittage comprise entre 17 et 18,8. Les materiaux presentant de telles caracteristiques mecaniques peuvent aisement etre obtenus aupres des industrial s special i s es dans la mi s e en muvre du tungstene fritte. On const at e que seul s les echantil lons present ant a la fois une resilience superieure a 120 J/cm2, un taux d'allongement superieur a 10% et une resistance a la rupture superieure a 930 Mpa permettent d'obtenir des eclats The envelopes were produced by sintering under isostatic compression of a powder comprising at least 90% of tungsten as well as addition materials and having a density after sintering of between 17 and 18.8. Materials exhibiting such mechanical characteristics can easily be obtained from special industrialists in the sintered tungsten process. It was found that only if the samples present at the same time have a resilience greater than 120 J / cm2, an elongation rate greater than 10% and a tensile strength greater than 930 Mpa make it possible to obtain splinters.
homogenes en fragmentation naturelle. homogeneous in natural fragmentation.
IS Les masses moyenne des eclats vent particulierement interessantes (superieures a 70 mg) avec des alliages presentant a la fois une resilience superieure a 200 J/cm2, un taux d'allongement superieur a 22% et une resistance a la IS The average masses of shards of wind are particularly interesting (greater than 70 mg) with alloys having at the same time a resilience greater than 200 J / cm2, a rate of elongation greater than 22% and a resistance to
rupture superieure a 1000 Mpa.breaking greater than 1000 Mpa.
Les meilleurs alliages vent coux des echantillons: N 2 resilience 320 J/cm2, allongement 30%, resistance a la The best wind and sample alloys: N 2 resilience 320 J / cm2, elongation 30%, resistance to
rupture 1060 Mpa.breaking 1060 Mpa.
N 6 resilience 380 J/cm2/ allongement 35%, resistance a la N 6 resilience 380 J / cm2 / elongation 35%, resistance to
rupture 1020 Mpa.breaking 1020 Mpa.
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N 7 resilience 200 J/cm2 F allongement 22%' resistance a la N 7 resilience 200 J / cm2 F elongation 22% 'resistance to
rupture 1150 Mpa.breaking 1150 Mpa.
Les resultats obtenus vent surprenants compte tenu des enseignements de l'art anterieur qui proposent des S projectiles a enveloppe tungstene fournissant un melange d' eclats et de poussiere de tungstene et pouvant apporter un effet de souffle (ou incendiaire sur les reservoirs de carburant) ce qui est generalement l'effet principal The results obtained are surprising given the teachings of the prior art which propose S projectiles with a tungsten envelope providing a mixture of fragments and tungsten dust and which can bring a blast (or incendiary effect on the fuel tanks) this which is usually the main effect
recherche avec de tels projectiles.research with such projectiles.
En fait les charges connues a ce j our et concues pour projeter des eclats de tungstene a capacite perforante mettent tonj ours en muvre des eclats preformes (billes ou cubes) disposes entre deux enveloppes de protection. Une enveloppe interne est en particulier necessaire pour amortir IS l'onde de choc engendree par lexplosif et empecher la In fact, the charges known today and designed to project tungsten flakes with perforating capacity, put your preformed flakes (balls or cubes) placed between two protective envelopes. An internal envelope is in particular necessary to absorb IS the shock wave generated by the explosive and to prevent the
destruction des eclats preformes.destruction of preformed shards.
Les charges connues vent done de realisation complexe et couteuse et elles ont une efficacite reduite par l' obligation qui est faite d'amortir les effete de londe de choc sur les The known loads therefore have complex and costly realization and they have a reduced efficiency by the obligation which is made to absorb the effects of the shockwave on the
eclats preformes.preformed chips.
L'enveloppe generatrice d'eclats 2 selon l' invention permet done de simplifier considerablement l' architecture de la charge explosive. En effet l'enveloppe est realisee en un materiau homogene dont l'epaisseur raisonnable (2 a 8 mm 2s selon calibre) permet un emport en explosif consequent et une The shrapnel-generating envelope 2 according to the invention therefore makes it possible to considerably simplify the architecture of the explosive charge. In fact, the envelope is made of a homogeneous material whose reasonable thickness (2 to 8 mm 2s depending on the caliber) allows a significant explosive load and a
efficacite optimale.optimal efficiency.
L'enveloppe 2 decrite a la figure 1 est ici realisee sous la forme d'un tube cylindrique d'axe 8. Toute autre geometric d'enveloppe serait evidemment possible. On pourra notamment realiser l'enveloppe sous la forme d'un corps de projectile (par exemple d'obus de gros calibre ou de bombe air / sol) presentant un profil externe aerodynamique. Ce profil pourra etre monobloc et eventuellement ferme au niveau de sa partie The envelope 2 described in FIG. 1 is here produced in the form of a cylindrical tube of axis 8. Any other envelope geometric would obviously be possible. In particular, the envelope may be produced in the form of a projectile body (for example of large caliber shells or an air / ground bomb) having an aerodynamic external profile. This profile may be in one piece and possibly closed at the level of its part.
avant ogivee.before warhead.
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Les figures 2, 3, 4 et 5 montrent des variantes de l' invention dans laquelle on a realise sur l'enveloppe 2 Figures 2, 3, 4 and 5 show variants of the invention in which we carried out on the envelope 2
generatrice d' eclats un reseau 9 de lignes de fragilisation. generator of shards a network 9 of lines of weakness.
La figure 2 montre un reseau 9 de lignes de fragilisation S obtenues par usinage de rainures sur la surface externe de l'enveloppe. La figure 3 montre un reseau 9 obtenu par traitement FIG. 2 shows a network 9 of weakening lines S obtained by machining grooves on the external surface of the envelope. FIG. 3 shows a network 9 obtained by treatment
thermique localise de la surface externe de l'enveloppe. thermal localizes from the outer surface of the envelope.
Echauffement ou usinage seront dans tous les cas realises suivant un reseau 9 comprenant des lignes: droites 10 (paralleles a l'axe 8 de la charge) et circulaires 11 (centrees sur ltaxe 8 de la charge) (voir la figure 4) ou Heating or machining will in all cases be carried out according to a network 9 comprising lines: straight lines 10 (parallel to the axis 8 of the load) and circular lines 11 (centered on the axis 8 of the load) (see FIG. 4) or
helicoidales 12 (figure 5).helicoidales 12 (Figure 5).
De tel. s reseaux de fragil i sat ion vent bien connus de l'Homme du Metier. Ils peuvent egalement etre realises sur la Like. s fragile networks are well known to those skilled in the art. They can also be performed on the
surface interne de l'enveloppe.inner surface of the envelope.
Le traitement thermique ou mecanique pourra etre effectue par laser, bombardement electronique, traitement de surface The thermal or mechanical treatment can be carried out by laser, electronic bombardment, surface treatment
localise (tel qu'une carburation).localizes (such as carburetion).
Un tel reseau permet de maltriser de facon plus precise la geometric, done la masse des eclats engendres par la charge. On pourra par exemple se reporter au brevet FR2438686 qul decrit differents procedes de fragilisation d'enveloppes de Such a network makes it possible to more precisely control the geometric, therefore the mass of fragments generated by the charge. We can for example refer to patent FR2438686 which describes various methods of weakening envelopes of
charges explosives en acier.steel explosive charges.
Ces procedes vent adaptables a la charge a enveloppe These procedures are adaptable to the envelope load
tungstene selon l' invention.tungsten according to the invention.
Le s parametres de la fragi l i sation seront bi en entendu adaptes par l'Homme du Metier en fonction de la nature du materiau mis en uvre et des dimensions de la charge a fabriquer. Il suffira pour une charge a enveloppe tungstene selon l' invention de realiser une fragilisation sur une profondeur The parameters of the fragi l i sation will of course be adapted by the skilled person depending on the nature of the material used and the dimensions of the load to be manufactured. It will suffice for a tungsten envelope load according to the invention to achieve embrittlement over a depth
comprise entre 2% et 50 % de l'epaisseur de l'enveloppe. between 2% and 50% of the thickness of the envelope.
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Dans le cas d'un usinage on realisera done des rainures sur une profondeur comprise entre 2% et 50% de l'epaisseur de l'enveloppe. Dans le cas de traitement thermique on realisera un echauffement localise provoquant un recuit du materiau sur une profondeur comprise entre 2% et 10% de lepaisseur de l'enveloppe. La figure 6 montre une munition incorporant une charge In the case of machining, grooves will therefore be made over a depth of between 2% and 50% of the thickness of the envelope. In the case of heat treatment, localized heating will be carried out, causing the material to be annealed over a depth of between 2% and 10% of the thickness of the envelope. Figure 6 shows ammunition incorporating a charge
explosive 1 selon l' invention.explosive 1 according to the invention.
L'enveloppe 2 porte un reseau 9 de fragilisation par traitement thermique ou de surface et elle est fermee a chaque extremite par un couvercle 3, 5 Ce mode de fragilisation est ici prefere a l'usinage afin de ne pas degrader la resistance mecanique de l'enveloppe 2 a la flexionO Chaque couvercle presente une portee cylindrique 13, 15 qui recoit lenveloppe 2. L'enveloppe 2 est rendue solidaire des couvercles par des vis transversales 14 (dons seul laxe est ici represente)O L' axe des vis est dispose a une distance D de l ' extremite de l'enveloppe 2 qui est superieure ou egale au diametre des vis cela afin de ne pas fragiliser de facon excessive The envelope 2 carries a network 9 of embrittlement by heat or surface treatment and it is closed at each end by a cover 3, 5 This mode of embrittlement is here preferred for machining so as not to degrade the mechanical resistance of the 'casing 2 to flexionO Each cover has a cylindrical bearing surface 13, 15 which receives the casing 2. The casing 2 is made integral with the covers by transverse screws 14 (only the axis is shown here) OL' the axis of the screws is arranged at a distance D from the end of the casing 2 which is greater than or equal to the diameter of the screws, so as not to weaken excessively
l'enveloppe au niveau des vis de fixation 14. the casing at the level of the fixing screws 14.
Il serait egalement possible d' assurer la solidarisation de l'enveloppe 2 et des couvercles par soudure laser ou bien par brasage. La soudure ou le brasage sera realise au droit des portees cylindriques 13 et 15 par exemple suivant la It would also be possible to secure the casing 2 and the covers by laser welding or by brazing. Welding or brazing will be carried out in line with the cylindrical bearings 13 and 15 for example according to the
direction des axes 14.direction of axes 14.
On pourra pour cela realiser les couvercles en acier We can do this with steel covers
comportant du nickel par exemple en acier inoxydable. comprising nickel, for example stainless steel.
L'alliage de tungstene incorporant lui aussi du nickel, la fusion de cet element a la fois dans l'enveloppe et dans le The tungsten alloy also incorporating nickel, the fusion of this element both in the envelope and in the
couvercle lors d'une soudure laser assurera le brasage. cover during laser welding will ensure soldering.
La munition representee a la figure 6 comprend une partie avant 16 (qui renferme par exemple un autodirecteur et/ou un i 2840402 detecteur de cible) ainsi quune partie arriere 17 qui The ammunition represented in FIG. 6 comprises a front part 16 (which contains for example a seeker and / or a target detector) as well as a rear part 17 which
renferme par exemple un propulseur.contains, for example, a propellant.
Les parties avant 16 et arriere 17 vent rendues solidaires du couvercle avant 3, ou arriere 5 respectivement' s par des moyens de fixation non representes (vissage, soudage). Conformement a l' invention ltenveloppe 2 liee aux couvercles 3 et 5 assure la liaison mecanique entre la partie avant 16 et la partie arriere 17 de la munition. L'enveloppe 2 forme ainsi a elle seule un troncon de la structure du corps de la munitionO Une telle disposition est rendue possible grace a l'enveloppe selon l' invention dont la tenue mecanique (notamment a la flexion) est suffisante pour assurer une IS telle liaison tout en assurant cependant la formation d'eclats souhaitesO Par ailleurs le couvercle arriere 5 qui porte le detonateur 6 comporte une portee cylindrique 15 ayant le meme diametre que l'enveloppe 2 et la partie arriere 17. Ainsi les efforts axiaux vent transmis directement de l'enveloppe 2 a The front 16 and rear 17 parts are made integral with the front cover 3, or rear 5 respectively by means of fixing means which are not shown (screwing, welding). In accordance with the invention, the envelope 2 linked to the covers 3 and 5 provides the mechanical connection between the front part 16 and the rear part 17 of the ammunition. The envelope 2 thus alone forms a section of the structure of the body of the munitionO Such an arrangement is made possible thanks to the envelope according to the invention, the mechanical strength (in particular of bending) is sufficient to ensure IS such a connection while ensuring, however, the formation of desired splinters. Furthermore, the rear cover 5 which carries the detonator 6 has a cylindrical bearing surface 15 having the same diameter as the casing 2 and the rear part 17. Thus the axial forces are transmitted directly of envelope 2 a
la partie arriere 17 sans contraindre le couvercle arriere 5. the rear part 17 without constraining the rear cover 5.
Il n'est plus necessaire avec l'enveloppe selon l' invention de realiser un corps de munition assurant la tenue mecanique structurale de la munition et a l'interieur duquel serait disposee une enveloppe generatrice d'eclats preformes. L'enveloppe selon l' invention permet done la realisation de munitions de structure mecanique extremement simple. 1i 2840402 It is no longer necessary with the envelope according to the invention to produce an ammunition body ensuring the structural mechanical hold of the ammunition and inside which would be an envelope generating preformed shards. The envelope according to the invention therefore allows the production of ammunition of extremely simple mechanical structure. 1i 2840402
Claims (14)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0206761A FR2840402B1 (en) | 2002-05-31 | 2002-05-31 | ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE |
EP03291266A EP1367357A1 (en) | 2002-05-31 | 2003-05-27 | Fragmenting hull and war head ammunition comprising such a hull |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0206761A FR2840402B1 (en) | 2002-05-31 | 2002-05-31 | ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2840402A1 true FR2840402A1 (en) | 2003-12-05 |
FR2840402B1 FR2840402B1 (en) | 2004-07-16 |
Family
ID=29415183
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0206761A Expired - Fee Related FR2840402B1 (en) | 2002-05-31 | 2002-05-31 | ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE |
Country Status (2)
Country | Link |
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EP (1) | EP1367357A1 (en) |
FR (1) | FR2840402B1 (en) |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2401483A (en) * | 1940-07-31 | 1946-06-04 | Mallory & Co Inc P R | Projectile and method of making the same |
FR2480427A1 (en) * | 1980-04-09 | 1981-10-16 | Michel Gerard | Noise making cover for bombs - has hollow spaces filled with material of similar density and or hardness to cover wall |
EP0063927A2 (en) * | 1981-04-23 | 1982-11-03 | Norman Allen | Explosive small arms projectile |
EP0113833A2 (en) | 1983-01-18 | 1984-07-25 | Rheinmetall GmbH | Projectile with explosive and incendiary action |
EP0392084A2 (en) * | 1989-04-08 | 1990-10-17 | Rheinmetall GmbH | Projectile |
EP0407288A1 (en) * | 1989-07-03 | 1991-01-09 | Manurhin Defense | Training projectile for an automatically or hand-operated firearm |
US5544589A (en) | 1991-09-06 | 1996-08-13 | Daimler-Benz Aerospace Ag | Fragmentation warhead |
EP0918206A2 (en) | 1997-11-21 | 1999-05-26 | Diehl Stiftung & Co. | Fragmentation casing for ammunition |
FR2807156A1 (en) | 2000-03-30 | 2001-10-05 | Commissariat Energie Atomique | PYROTECHNIC CHARGE WITH DUAL OPERATION |
-
2002
- 2002-05-31 FR FR0206761A patent/FR2840402B1/en not_active Expired - Fee Related
-
2003
- 2003-05-27 EP EP03291266A patent/EP1367357A1/en not_active Ceased
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2401483A (en) * | 1940-07-31 | 1946-06-04 | Mallory & Co Inc P R | Projectile and method of making the same |
FR2480427A1 (en) * | 1980-04-09 | 1981-10-16 | Michel Gerard | Noise making cover for bombs - has hollow spaces filled with material of similar density and or hardness to cover wall |
EP0063927A2 (en) * | 1981-04-23 | 1982-11-03 | Norman Allen | Explosive small arms projectile |
EP0113833A2 (en) | 1983-01-18 | 1984-07-25 | Rheinmetall GmbH | Projectile with explosive and incendiary action |
EP0392084A2 (en) * | 1989-04-08 | 1990-10-17 | Rheinmetall GmbH | Projectile |
EP0407288A1 (en) * | 1989-07-03 | 1991-01-09 | Manurhin Defense | Training projectile for an automatically or hand-operated firearm |
US5544589A (en) | 1991-09-06 | 1996-08-13 | Daimler-Benz Aerospace Ag | Fragmentation warhead |
EP0918206A2 (en) | 1997-11-21 | 1999-05-26 | Diehl Stiftung & Co. | Fragmentation casing for ammunition |
FR2807156A1 (en) | 2000-03-30 | 2001-10-05 | Commissariat Energie Atomique | PYROTECHNIC CHARGE WITH DUAL OPERATION |
Also Published As
Publication number | Publication date |
---|---|
EP1367357A1 (en) | 2003-12-03 |
FR2840402B1 (en) | 2004-07-16 |
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