EP2426455A1 - Method for compressing an explosive material in the body of a projectile and tool for implementing such a method - Google Patents
Method for compressing an explosive material in the body of a projectile and tool for implementing such a method Download PDFInfo
- Publication number
- EP2426455A1 EP2426455A1 EP11290343A EP11290343A EP2426455A1 EP 2426455 A1 EP2426455 A1 EP 2426455A1 EP 11290343 A EP11290343 A EP 11290343A EP 11290343 A EP11290343 A EP 11290343A EP 2426455 A1 EP2426455 A1 EP 2426455A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- guide
- punch
- compression
- bead
- head
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 45
- 239000000463 material Substances 0.000 title claims abstract description 28
- 238000000034 method Methods 0.000 title claims abstract description 19
- 238000007906 compression Methods 0.000 claims abstract description 65
- 230000006835 compression Effects 0.000 claims abstract description 62
- 239000011324 bead Substances 0.000 claims abstract description 55
- 238000007790 scraping Methods 0.000 claims description 4
- 238000004080 punching Methods 0.000 claims 1
- 238000005266 casting Methods 0.000 description 3
- 238000010079 rubber tapping Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 208000031968 Cadaver Diseases 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/025—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by compacting
Definitions
- the technical field of the invention is that of methods for compressing explosive materials in the projectile bodies as well as tools associated with such processes.
- casting is the preferred method.
- the advantage of explosive compression processes is that they allow the projectiles to be loaded relatively quickly. Indeed, the explosive is set up by dosing the material in the powdered and non-liquid state and it is not necessary, when the compression is carried out at ambient temperature, to carry out heat treatments for cooling the load such as the usual casting processes impose it.
- the explosive material in powder form is compressed by means of a compression punch directly into the projectile body and through a rear opening of this body.
- the object of the invention is to propose a method, and the associated tooling, for compressively loading a projectile body or military head having one or more internal circular beads.
- the subject of the invention is a method of compressing an explosive material in a projectile body or military head through a rear opening of this body, a method employing at least one compression punch, characterized in that the compression is carried out in several successive steps, each compression step being carried out by using a particular tooling associating a compression punch and a punch guide, guide interposed between the punch and the body, at minus a first punch guide having a defined length such that this guide can come into contact with an internal bead of the body or at least in the immediate vicinity of this bead, the internal diameter of the guide being less than or equal to the diameter of the bead .
- the second guide may be disposed within the bore of the first guide.
- the invention also relates to a tool for compressing an explosive material in a projectile body or military head through a rear opening of the body, a tool comprising a support for holding the body and at least one punch of compression mounted sliding relative to the support, tooling which is characterized in that it comprises at least one cylindrical guide for the sliding punch, guide interposed between the body and the punch, the guide having a length such that it can come into contact on an internal bead of the body or at least in the immediate vicinity of this bead, the inner diameter of the guide being less than or equal to the diameter of the bead.
- This compression tooling may comprise a set of at least two punch guides of different lengths, the punch may also be equipped with at least two different compression heads.
- the compression tool may comprise at least a second guide longer than the first guide and thus to guide a compression punch beyond the inner bead.
- the second guide may be disposed within the bore of the first guide.
- the punch head may include an end shoulder for scraping the inner surface of the guide.
- the punch may also include at least one circular groove behind the head.
- a compression tool 1 for an explosive material comprises a support 2 ensuring the maintenance of a body 3 of a projectile.
- This support 2 is secured to a frame (not shown) of a compression machine.
- the support 2 comprises a cylindrical bore 2a which receives the projectile body 3.
- the bore 2a is extended by a concave surface 4 which has a shape complementary to that of the nose 3a of the body 3.
- the body 3 is firmly maintained by the support 2, both radially and axially.
- the support 2 is capped at its rear by a sleeve 5 to which it is fixed by screws or radial pins 6.
- the sleeve has an internal counterbore 7 which constitutes a stop bearing against the rear 3b of the body 3 to level of the opening 8 of the latter.
- the positioning holes of the pins 6 in the support 2 are arranged on the tool so that when placing these pins 6, the countersink 7 is actually in abutment against the rear 3b of the body.
- the sleeve 5 has an axial bore 9 which has the same diameter as the internal bore 3c of the projectile body 3.
- the axial bore 9 opens into an opening 10 of larger diameter and is threaded to receive a guide as will be described later.
- the sleeve 5 finally carries radial vents 11 which allow the evacuation of air during the positioning of the sleeve 5 on the support 2.
- the body 3 of the projectile has a particular internal profile which here comprises two circular beads 12a, 12b. These beads 12a, 12b are intended to strengthen the structure of the body 3 of the projectile. They oppose against the passage of a compression punch of the explosive which would be the internal diameter of the bore 3c of the body 3.
- a cylindrical tubular guide 13 is disposed in the bore 9 of the sleeve 5. This guide slides when it is placed on the bore 3c of the body 3 of the projectile up to come into contact on the first bead 12a or at least in the immediate vicinity of this bead.
- the internal diameter of the bore 13a of the guide 13 is less than or equal to the inner diameter (d) of the bead 12a (here substantially equal). Thus, when a punch 14 is slid inside the guide 13, this punch no longer interferes with the bead 12a.
- the punch that slides inside the guide does not interfere with the bead and the length of the guide is sufficient to guide the punch during compression.
- the end of the guide must also be as close as possible to the bead to limit the risk of introducing explosive between guide and bead during loading.
- the guide 13 is secured to the support 2 by means of the sleeve 5 and is interposed between the body 3 of the projectile and the punch 14.
- the guide 13 thus ensures the guiding of the punch 14 as usually done the body of the projectile when the latter is devoid of bulges. This avoids any risk of buckling of the punch and prevents the rise of the explosive material along the punch body 14.
- the guide 13 comprises an enlarged rear head 15 which is threaded and is housed in the tapping 10 of the sleeve 5. It is thus ensured a rigid positioning of the guide 13 relative to the assembly formed by the support 2 and the sleeve 5.
- Punch 14 is attached at its back to the compression machine (not shown). The latter exerts a force on the punch 14 and the head 16 of the punch 14 is then applied against the explosive charge (not shown in this example). figure 2 ) to achieve its compression in the body 3.
- the head 16 of the punch 14 comprises a conical portion 16a which terminates in a spherical portion 16b.
- the shape of the end of the head 16 of the punch is defined so as to ensure a transfer of the axial compression force along non-axial directions towards the wall of the body 3.
- the compression force that the head 16 provides to the explosive material is oriented perpendicularly to the walls of the head 16.
- the shape of the head 16 will therefore be chosen as a function of the maximum depth of penetration of the punch 14 inside the body 3 and in particular the distance maximum then separating the head 16 from the wall of the body 3.
- the head 16 of the punch 14 has an end shoulder 16c in the form of a circular ring between the conical portion 16a and the cylindrical body of the punch 14.
- This shoulder is a scraper for scraping the inner surface of the guide 13 during the advance of the punch. This scraping makes it possible to push towards the inside of the body 3 the explosive material which could be adhering to the inner wall 13a of the guide 13.
- the punch 14 has a circular groove 17 behind the head 16. This groove 17 completes the scraper 16c and makes it possible to trap during the movement of the punch 14 the explosive material that may be on the inner cylindrical surface 13a of the guide 13.
- the annular surfaces 17a and 17b delimiting the groove 17 are also scrapers which lead to the groove 17 the explosive material present on the cylindrical surface of the guide.
- the figure 3a shows a first step of the method according to the invention.
- the first guide 13.1 is chosen with a length such that it can come into contact with the first inner bead 12a of the body 3 (or at least in the immediate vicinity of this bead).
- a first volume 18.1 of an explosive material in the powdery state is then placed at the bottom of the body 3 of the projectile.
- the compressible explosives are well known to those skilled in the art.
- the patent can be consulted FR2801883 which describes a compressible explosive. This explosive is introduced using a metering hopper (not shown) that is positioned in the guide 13.1.
- a first punch 14.1 is then introduced into the guide 13.1. This punch is secured to a compression machine (not shown) which exerts on the punch 14.1 an effort F.
- the head 16.1 of the punch 14.1 is then applied against the explosive charge to achieve its compression in the body 3.
- a head 16.1 having a conical profile at acute apex angle was chosen.
- the axial compression force F will be decomposed into compression forces along directions G perpendicular to the cone walls of the head 16.1.
- the shape of the head 16.1 will thus ensure compression forces well distributed around the punch 14.1 and to the inner wall of the body 3.
- the compressive force exerted on the first volume of explosive material 18.1 will also cause it to rise along the punch 14.1 to the first bead 12a (annular zone 18a).
- the figure 3b shows a second step of the compression process according to the invention.
- a second guide 13.2 which is fixed in the same way as the previous one to the sleeve 5 but which is shorter than the first guide and is therefore no longer in abutment against the first bead 12a.
- This second guide is also the diameter of the bore of the body 3 and is therefore interposed between the punch 14.2 and the body 3.
- a second punch 14.2 is used whose head 16.2 is different from the first head 16.1.
- This head 16.2 has a conical portion having an obtuse apex angle.
- the second volume of compressed explosive material 18.2 is less for this second compression step and the compression forces must then be distributed either to the nose 3a of the body 3 but rather to the upper interface 18.1a of the first volume of explosive 18.1 tablet.
- the second head 16.2 comprises (just like the first head 16.1) an annular scraper 16c.
- the figure 3c finally shows a third step of the method according to the invention.
- This guide 13.3 is fixed in the same way as the two previous guides. It is also the diameter of the bore of the body 3 and is therefore interposed between a third punch 14.3 and the body 3.
- the third punch 14.3 has a head 16.3 having a different profile.
- the profile of the head 16.3 is spherical.
- the bore of the body at the level of the third layer 18.3 of explosive material is indeed cylindrical without beads and the compression forces can be closer to the axial direction.
- the profile of the head 16.3 of the punch 14.3 may change depending on the desired shape for the external surface of the explosive charge.
- the guides 13.1, 13.2 and 13.3 make it possible to guiding the punches 14.1, 14.2 and 14.3 despite the presence of the beads.
- the guides also allow to channel the explosive. No interference between the punch and the bead is to be feared because the guide diameter of the punch in the guide is less than or equal to the diameter (d) of the bead.
- the lengths of the guides make it possible to progressively fill the body 3 of the projectile with the explosive.
- figure 3a a method in which it is sufficient, during the first compression step, to position the first guide directly in contact (or in the immediate vicinity) with the first bead 12a. This is possible if the distance between the end of the head 16.1 of the punch 14.1 and the bottom of the body 3 is not too large relative to the internal diameter of the body 3 (distance between 1 and 2 times the size).
- the figure 4 shows thus another embodiment of the tool according to the invention, wherein a second guide 13.1b is disposed within the bore of the first guide 13.1a.
- the first guide comprises a tapping 19 arranged in the threaded rear head 15 of the first guide 13.1a.
- the tapping 19 receives a threaded head 20 secured to the second guide 13.1b.
- the tapping 19 receives a threaded head 20 secured to the second guide 13.1b.
- the first guide 13.1a is positioned in contact (or in the immediate vicinity) with the first bead 12a. It has an internal bore whose diameter is equal to the inner diameter of the bead 12a.
- the second guide 13.1b has an outer diameter equal to the inner diameter of the first guide 13.1a. This second guide 13.1b is longer than the first guide 13.1a and extends here beyond the second inner bead 12b of the projectile body 3.
- the compression punch 14.1 is guided by the second guide 13.1b beyond the first inner bead 12a and also beyond the second inner bead 12b.
- this second embodiment of the invention makes it possible to perform compressions in bodies of projectiles or military heads comprising a large number of beads and even adjacent beads of the front end of the body.
Abstract
Description
Le domaine technique de l'invention est celui des procédés de compression des matériaux explosifs dans les corps de projectile ainsi que des outillages associés à de tels procédés.The technical field of the invention is that of methods for compressing explosive materials in the projectile bodies as well as tools associated with such processes.
Il est classique de réaliser un chargement d'un corps de projectile par compression. Ceci est plus particulièrement mis en oeuvre pour réaliser les chargements de projectiles de moyen calibre (calibre compris entre 20mm et 75mm) ou bien pour charger des têtes militaires.It is conventional to perform a loading of a projectile body by compression. This is more particularly used to carry out the projectiles of medium caliber (caliber between 20mm and 75mm) or to load military heads.
Pour les obus de gros calibre, on a plutôt recours aux procédés de chargement par coulée.For larger shells, casting is the preferred method.
Les procédés de compression d'explosif présentent comme avantage de permettre un chargement relativement rapide des projectiles. En effet l'explosif est mis en place par dosage du matériau à l'état pulvérulent et non liquide et il n'est pas nécessaire, lorsque la compression est effectuée à température ambiante, de procéder à des traitements thermiques de refroidissement du chargement comme les procédés de coulée habituels l'imposent.The advantage of explosive compression processes is that they allow the projectiles to be loaded relatively quickly. Indeed, the explosive is set up by dosing the material in the powdered and non-liquid state and it is not necessary, when the compression is carried out at ambient temperature, to carry out heat treatments for cooling the load such as the usual casting processes impose it.
Avec les procédés de compression connus, on comprime à l'aide d'un poinçon de compression le matériau explosif à l'état pulvérulent directement dans le corps de projectile et au travers d'une ouverture arrière de ce corps.With the known compression methods, the explosive material in powder form is compressed by means of a compression punch directly into the projectile body and through a rear opening of this body.
Une telle opération est facilitée par le fait que la surface interne des corps de projectile est généralement cylindrique sur sensiblement toute la hauteur du projectile. Un poinçon de compression peut donc être guidé sur une partie du corps du projectile lors de la compression.Such an operation is facilitated by the fact that the inner surface of the projectile bodies is generally cylindrical over substantially the entire height of the projectile. A compression punch can therefore be guided on part of the body of the projectile during compression.
Il est cependant parfois nécessaire de réaliser des corps de projectile ou de têtes militaires comportant des bourrelets internes circulaires plus ou moins longs, par exemple pour renforcer le corps de projectile ou bien lui donner des caractéristiques de fragmentation particulières.However, it is sometimes necessary to make projectile bodies or military heads with circular inner beads more or less long, for example to strengthen the projectile body or give it particular fragmentation characteristics.
Dans ce cas il n'est plus possible de charger l'explosif par compression et seule la coulée permet de remplir complètement le volume interne du corps de projectile avec le matériau explosif. Des traitements thermiques ou cycles de refroidissement sont alors nécessaires pour assurer l'homogénéité du chargement (éviter les retassures).In this case it is no longer possible to load the explosive by compression and only the casting can completely fill the internal volume of the projectile body with the explosive material. Heat treatments or cooling cycles are then necessary to ensure the homogeneity of the loading (avoid the shrinkage).
L'invention a pour but de proposer un procédé, et l'outillage associé, permettant de charger par compression un corps de projectile ou de tête militaire comportant un ou plusieurs bourrelets circulaires internes.The object of the invention is to propose a method, and the associated tooling, for compressively loading a projectile body or military head having one or more internal circular beads.
Ainsi, l'invention a pour objet un procédé de compression d'un matériau explosif dans un corps de projectile ou de tête militaire au travers d'une ouverture arrière de ce corps, procédé mettant en oeuvre au moins un poinçon de compression, procédé caractérisé en ce qu'on procède à la compression en plusieurs étapes successives, chaque étape de compression étant conduite en mettant en oeuvre un outillage particulier associant un poinçon de compression et un guide de poinçon, guide s'interposant entre le poinçon et le corps, au moins un premier guide de poinçon ayant une longueur définie de telle sorte que ce guide puisse venir en contact sur un bourrelet interne du corps ou tout au moins à proximité immédiate de ce bourrelet, le diamètre interne du guide étant inférieur ou égal au diamètre du bourrelet.Thus, the subject of the invention is a method of compressing an explosive material in a projectile body or military head through a rear opening of this body, a method employing at least one compression punch, characterized in that the compression is carried out in several successive steps, each compression step being carried out by using a particular tooling associating a compression punch and a punch guide, guide interposed between the punch and the body, at minus a first punch guide having a defined length such that this guide can come into contact with an internal bead of the body or at least in the immediate vicinity of this bead, the internal diameter of the guide being less than or equal to the diameter of the bead .
On pourra avantageusement fixer avant chaque étape de compression une tête à l'extrémité du poinçon, tête ayant un profil adapté au profil interne du corps contre lequel est réalisée la compression.It is advantageous to fix before each compression step a head at the end of the punch, head having a profile adapted to the internal profile of the body against which the compression is performed.
On pourra éventuellement prévoir au moins un deuxième guide, deuxième guide plus long que le premier guide et permettant ainsi de guider un poinçon de compression au-delà d'un bourrelet interne.It may optionally provide at least a second guide, second guide longer than the first guide and thus to guide a compression punch beyond an inner bead.
Le deuxième guide pourra être disposé à l'intérieur de l'alésage du premier guide.The second guide may be disposed within the bore of the first guide.
L'invention a également pour objet un outillage de compression d'un matériau explosif dans un corps de projectile ou de tête militaire au travers d'une ouverture arrière de ce corps, outillage comprenant un support de maintien du corps et au moins un poinçon de compression monté coulissant par rapport au support, outillage qui est caractérisé en ce qu'il comprend au moins un guide cylindrique pour le poinçon coulissant, guide s'interposant entre le corps et le poinçon, guide ayant une longueur telle qu'il puisse venir en contact sur un bourrelet interne du corps ou tout au moins à proximité immédiate de ce bourrelet, le diamètre interne du guide étant inférieur ou égal au diamètre du bourrelet.The invention also relates to a tool for compressing an explosive material in a projectile body or military head through a rear opening of the body, a tool comprising a support for holding the body and at least one punch of compression mounted sliding relative to the support, tooling which is characterized in that it comprises at least one cylindrical guide for the sliding punch, guide interposed between the body and the punch, the guide having a length such that it can come into contact on an internal bead of the body or at least in the immediate vicinity of this bead, the inner diameter of the guide being less than or equal to the diameter of the bead.
Cet outillage de compression pourra comprendre un jeu d'au moins deux guides de poinçon de longueurs différentes, le poinçon pouvant par ailleurs être équipé d'au moins deux têtes de compression différentes.This compression tooling may comprise a set of at least two punch guides of different lengths, the punch may also be equipped with at least two different compression heads.
L'outillage de compression pourra comprendre au moins un deuxième guide plus long que le premier guide et permettant ainsi de guider un poinçon de compression au-delà du bourrelet interne.The compression tool may comprise at least a second guide longer than the first guide and thus to guide a compression punch beyond the inner bead.
Le deuxième guide pourra être disposé à l'intérieur de l'alésage du premier guide.The second guide may be disposed within the bore of the first guide.
Selon une variante de réalisation, la tête du poinçon pourra comporter un épaulement d'extrémité permettant le raclage de la surface interne du guide.According to an alternative embodiment, the punch head may include an end shoulder for scraping the inner surface of the guide.
Le poinçon pourra par ailleurs comporter au moins une gorge circulaire en arrière de la tête.The punch may also include at least one circular groove behind the head.
L'invention sera mieux comprise à la lecture du complément de description qui va suivre de différents modes de réalisation, description faite en référence aux dessins annexés et dans lesquels :
- la
figure 1 montre un exemple de réalisation du support de l'outillage selon l'invention, support sur lequel est positionné un corps de projectile, - la
figure 2 montre le même support après positionnement du guide ainsi que d'un poinçon de compression, - les
figures 3a ,3b et3c montrent trois étapes successives du procédé de compression selon l'invention, et - la
figure 4 montre un autre mode de réalisation de l'outillage selon l'invention, mode dans lequel un deuxième guide est disposé dans le premier guide.
- the
figure 1 shows an exemplary embodiment of the support of the tool according to the invention, support on which is positioned a projectile body, - the
figure 2 shows the same support after positioning the guide as well as a compression punch, - the
figures 3a ,3b and3c show three successive steps of the compression process according to the invention, and - the
figure 4 shows another embodiment of the tool according to the invention, wherein a second guide is disposed in the first guide.
En se reportant à la
Le support 2 est coiffé à sa partie arrière par un manchon 5 auquel il est fixé par des vis ou bien des goupilles radiales 6. Le manchon comporte un lamage interne 7 qui constitue une butée venant en appui contre l'arrière 3b du corps 3 au niveau de l'ouverture 8 de ce dernier. Les trous de positionnement des goupilles 6 dans le support 2 sont disposés sur l'outillage de telle sorte que lors de la mise en place de ces goupilles 6, le lamage 7 soit effectivement en appui contre l'arrière 3b du corps.The
Le manchon 5 comporte un alésage axial 9 qui a même diamètre que l'alésage interne 3c du corps 3 de projectile. L'alésage axial 9 débouche dans une ouverture 10 de plus grand diamètre et qui est taraudée pour recevoir un guide comme cela sera décrit par la suite.The
Le manchon 5 porte enfin des évents radiaux 11 qui permettent l'évacuation de l'air lors du positionnement du manchon 5 sur le support 2.The
On remarque sur la
En considérant la
Le diamètre interne de l'alésage 13a du guide 13 est inférieur ou égal au diamètre interne (d) du bourrelet 12a (ici sensiblement égal). Ainsi lorsque l'on glisse un poinçon 14 à l'intérieur du guide 13, ce poinçon n'interfère plus avec le bourrelet 12a.The internal diameter of the
On a précisé "tout au moins à proximité immédiate du bourrelet". En effet, en fonction de la forme en section du bourrelet 12a (rectangulaire, trapézoïdale ou arrondie) et compte tenu du fait que le guide 13 est en butée contre le manchon 5, il n'est pas toujours possible d'amener le guide 13 en contact avec le bourrelet 12a. Un intervalle réduit peut donc subsister entre l'extrémité du guide et le bourrelet.It has been specified "at least in the immediate vicinity of the bead". Indeed, depending on the sectional shape of the
Ce qui est important cependant c'est que le poinçon qui glisse à l'intérieur du guide n'interfère pas avec le bourrelet et que la longueur du guide soit suffisante pour assurer le guidage du poinçon lors de la compression. L'extrémité du guide doit par ailleurs être la plus proche possible du bourrelet pour limiter les risques d'introduire de l'explosif entre guide et bourrelet lors du chargement.What is important however is that the punch that slides inside the guide does not interfere with the bead and the length of the guide is sufficient to guide the punch during compression. The end of the guide must also be as close as possible to the bead to limit the risk of introducing explosive between guide and bead during loading.
Le guide 13 est solidaire du support 2 par l'intermédiaire du manchon 5 et il s'interpose entre le corps 3 du projectile et le poinçon 14. Le guide 13 assure ainsi le guidage du poinçon 14 comme le fait habituellement le corps du projectile lorsque ce dernier est dépourvu de bourrelets. On évite ainsi tout risque de flambage du poinçon et on empêche les remontées du matériau explosif le long du corps de poinçon 14.The
On remarque sur la
Le poinçon 14 est fixé à sa partie arrière à la machine de compression (non représentée). Cette dernière exerce un effort sur le poinçon 14 et la tête 16 du poinçon 14 est alors appliquée contre le chargement explosif (non représenté sur cette
On remarque sur la
En effet, l'effort de compression que la tête 16 fournit au matériau explosif est orienté perpendiculairement aux parois de la tête 16.Indeed, the compression force that the
La forme de la tête 16 sera donc choisie en fonction de la profondeur d'enfoncement maximale du poinçon 14 à l'intérieur du corps 3 et en particulier de la distance maximale qui séparera alors la tête 16 de la paroi du corps 3.The shape of the
On remarque aussi sur la
Cet épaulement constitue un racloir permettant le raclage de la surface interne du guide 13 lors de l'avance du poinçon. Ce raclage permet de repousser vers l'intérieur du corps 3 le matériau explosif qui pourrait être adhérent à la paroi interne 13a du guide 13.This shoulder is a scraper for scraping the inner surface of the
On remarque aussi sur la
Les surfaces annulaires 17a et 17b délimitant la gorge 17 constituent, elles aussi, des racloirs qui conduisent vers la gorge 17 le matériau explosif présent sur la surface cylindrique du guide.The
On pourra ainsi prévoir plusieurs gorges circulaires sur le poinçon 14.We can thus provide several circular grooves on the
Le procédé de compression selon l'invention va maintenant être décrit en référence aux
La
Avant la mise en place de l'explosif on fixe un premier guide 13.1 au manchon 5 par vissage. Le premier guide 13.1 est choisi avec une longueur telle qu'il puisse venir en contact sur le premier bourrelet interne 12a du corps 3 (ou tout au moins à proximité immédiate de ce bourrelet).Before placing the explosive is fixed a first guide 13.1 to the
On dispose ensuite un premier volume 18.1 d'un matériau explosif à l'état pulvérulent au fond du corps 3 du projectile. Les explosifs comprimables sont bien connus de l'Homme du Métier. On pourra consulter par exemple le brevet
On introduit ensuite un premier poinçon 14.1 dans le guide 13.1. Ce poinçon est solidaire d'une machine de compression (non représentée) qui exerce sur le poinçon 14.1 un effort F.A first punch 14.1 is then introduced into the guide 13.1. This punch is secured to a compression machine (not shown) which exerts on the punch 14.1 an effort F.
Lors de l'introduction du poinçon 14.1 son racloir 16c va repousser vers le corps 3 le matériau explosif pouvant se trouver sur la paroi interne du guide 13.1.When the punch 14.1 is inserted, its
La tête 16.1 du poinçon 14.1 est alors appliquée contre le chargement explosif pour réaliser sa compression dans le corps 3. Pour cette première étape de compression on a choisi une tête 16.1 ayant un profil conique à angle au sommet aigu. L'effort de compression axial F va se décomposer en des efforts de compression suivant des directions G perpendiculaires aux parois du cône de la tête 16.1. La forme de la tête 16.1 va ainsi assurer des efforts de compression bien répartis tout autour du poinçon 14.1 et vers la paroi interne du corps 3.The head 16.1 of the punch 14.1 is then applied against the explosive charge to achieve its compression in the
Par réaction, l'effort de compression exercé sur le premier volume de matériau explosif 18.1 va aussi provoquer sa remontée le long du poinçon 14.1 jusqu'au premier bourrelet 12a (zone annulaire 18a).By reaction, the compressive force exerted on the first volume of explosive material 18.1 will also cause it to rise along the punch 14.1 to the
L'Homme du Métier définira la géométrie de la tête 16.1 en fonction des dimensions du corps 3 et de la profondeur d'enfoncement maximale du poinçon 14.1.Those skilled in the art will define the geometry of the head 16.1 according to the dimensions of the
La
Au cours de cette deuxième étape on dispose dans le corps 3 du projectile un deuxième guide 13.2 qui se fixe de la même façon que le précédent au manchon 5 mais qui est plus court que le premier guide et ne se trouve donc plus en butée contre le premier bourrelet 12a. Ce deuxième guide est lui aussi au diamètre de l'alésage du corps 3 et s'interpose donc entre le poinçon 14.2 et le corps 3.During this second step, there is disposed in the
Par ailleurs on utilise alors un deuxième poinçon 14.2 dont la tête 16.2 est différente de la première tête 16.1. Cette tête 16.2 comporte une partie conique présentant un angle au sommet obtus. En effet, le deuxième volume de matériau explosif 18.2 comprimé est moindre pour cette deuxième étape de compression et les efforts de compression doivent être alors répartis non plus vers l'ogive 3a du corps 3 mais plutôt vers l'interface supérieure 18.1a du premier volume d'explosif 18.1 comprimé.In addition, a second punch 14.2 is used whose head 16.2 is different from the first head 16.1. This head 16.2 has a conical portion having an obtuse apex angle. Indeed, the second volume of compressed explosive material 18.2 is less for this second compression step and the compression forces must then be distributed either to the
La deuxième tête 16.2 comporte (tout comme la première tête 16.1) un racloir annulaire 16c.The second head 16.2 comprises (just like the first head 16.1) an
La
Au cours de cette étape on positionne un troisième guide 13.3 plus court que le deuxième guide 13.2. Ce guide 13.3 se fixe de la même façon que les deux guides précédents. Il est lui aussi au diamètre de l'alésage du corps 3 et s'interpose donc entre un troisième poinçon 14.3 et le corps 3.During this step we position a third guide 13.3 shorter than the second guide 13.2. This guide 13.3 is fixed in the same way as the two previous guides. It is also the diameter of the bore of the
Le troisième poinçon 14.3 comporte une tête 16.3 ayant un profil différent. Ici le profil de la tête 16.3 est sphérique. L'alésage du corps au niveau de la troisième couche 18.3 de matériau explosif est en effet cylindrique sans bourrelets et les efforts de compression peuvent se rapprocher de la direction axiale.The third punch 14.3 has a head 16.3 having a different profile. Here the profile of the head 16.3 is spherical. The bore of the body at the level of the third layer 18.3 of explosive material is indeed cylindrical without beads and the compression forces can be closer to the axial direction.
Le profil de la tête 16.3 du poinçon 14.3 peut évoluer en fonction de la forme désirée pour la surface externe du chargement explosif.The profile of the head 16.3 of the punch 14.3 may change depending on the desired shape for the external surface of the explosive charge.
On voit donc que grâce à l'invention il est possible de conduire une compression de matériau explosif à l'intérieur d'un corps 3 de projectile (ou de tête militaire) comportant des bourrelets internes, et ce quelles que soient les dimensions des bourrelets 12a et 12b.It can therefore be seen that, thanks to the invention, it is possible to conduct a compression of explosive material inside a projectile body (or military head) 3 comprising internal rolls, regardless of the dimensions of the
Les guides 13.1, 13.2 et 13.3 permettent d'assurer un guidage des poinçons 14.1, 14.2 et 14.3 malgré la présence des bourrelets. Les guides permettent aussi de canaliser l'explosif. Aucune interférence entre le poinçon et le bourrelet n'est à craindre car le diamètre de guidage du poinçon dans le guide est inférieur ou égal au diamètre (d) du bourrelet.The guides 13.1, 13.2 and 13.3 make it possible to guiding the punches 14.1, 14.2 and 14.3 despite the presence of the beads. The guides also allow to channel the explosive. No interference between the punch and the bead is to be feared because the guide diameter of the punch in the guide is less than or equal to the diameter (d) of the bead.
Les longueurs des guides, différentes d'une étape à l'autre, permettent de remplir progressivement le corps 3 du projectile avec l'explosif.The lengths of the guides, different from one stage to another, make it possible to progressively fill the
En fonction de la géométrie du corps 3 et du nombre de bourrelets 12a et 12b il sera possible de faire varier le nombre de guides et de poinçons ainsi que la géométrie des têtes des poinçons.Depending on the geometry of the
On a ainsi précédemment décrit (
Lorsque cette distance est plus grande ou que le nombre de bourrelets est plus important, il peut être nécessaire d'amener le poinçon 14.1 plus en avant dans le corps 3.When this distance is greater or the number of beads is greater, it may be necessary to bring the punch 14.1 further forward in the
La
Le taraudage 19 reçoit une tête filetée 20 solidaire du deuxième guide 13.1b. Ainsi après montage les deux guides 13.1a et 13.1b sont solidaires l'un de l'autre ainsi que du manchon 5.The tapping 19 receives a threaded
Le premier guide 13.1a est positionné en contact (ou à proximité immédiate) avec le premier bourrelet 12a. Il a un alésage interne dont le diamètre est égal au diamètre interne du bourrelet 12a. Le deuxième guide 13.1b a un diamètre externe égal au diamètre interne du premier guide 13.1a. Ce deuxième guide 13.1b est plus long que le premier guide 13.1a et il s'étend ici au-delà du deuxième bourrelet interne 12b du corps 3 de projectile.The first guide 13.1a is positioned in contact (or in the immediate vicinity) with the
Le poinçon de compression 14.1 est guidé par le deuxième guide 13.1b au-delà du premier bourrelet interne 12a et également au-delà du deuxième bourrelet interne 12b.The compression punch 14.1 is guided by the second guide 13.1b beyond the first
Avec ce mode de réalisation, on peut donc réaliser une compression de l'explosif sans être gêné par la présence des bourrelets internes.With this embodiment, it is therefore possible to compress the explosive without being hindered by the presence of the internal beads.
Après une première étape de compression dans laquelle l'explosif comprimé remontera jusqu'au deuxième bourrelet 12b, on retirera le deuxième guide 13.1b et on pourra procéder à une deuxième étape de compression d'explosif avec un poinçon qui sera alors guidé directement par le premier guide 13.1a.After a first compression step in which the compressed explosive will go up to the
La configuration de l'outillage lors de cette deuxième étape est pratiquement celle de la
On voit donc que ce second mode de réalisation de l'invention permet d'effectuer des compressions dans des corps de projectiles ou têtes militaires comprenant un grand nombre de bourrelets et même des bourrelets voisins de l'extrémité avant du corps.It can thus be seen that this second embodiment of the invention makes it possible to perform compressions in bodies of projectiles or military heads comprising a large number of beads and even adjacent beads of the front end of the body.
A titre de variante de ce second mode de réalisation, il serait bien entendu possible de définir un outillage dans lequel le guide utilisé lors de la première étape serait monobloc. On pourra alors considérer la
Il sera cependant nécessaire de prévoir un guide ayant la forme du guide 13.1a pour une étape de compression ultérieure.It will however be necessary to provide a guide in the form of the guide 13.1a for a subsequent compression step.
Dans tous les modes de réalisation précédents il est possible de prévoir un outillage dans lequel il n'y a pas de manchon 5. Les guides sont alors simplement positionnés dans le corps de projectile.In all the previous embodiments it is possible to provide a tool in which there is no
Claims (10)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1003503A FR2964188B1 (en) | 2010-09-01 | 2010-09-01 | METHOD OF COMPRESSING AN EXPLOSIVE MATERIAL IN A PROJECTILE BODY AND TOOLING FOR PERFORMING SUCH A METHOD |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2426455A1 true EP2426455A1 (en) | 2012-03-07 |
EP2426455B1 EP2426455B1 (en) | 2014-12-17 |
Family
ID=43858010
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20110290343 Active EP2426455B1 (en) | 2010-09-01 | 2011-07-28 | Method for compressing an explosive material in the body of a projectile and tool for implementing such a method |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2426455B1 (en) |
ES (1) | ES2529772T3 (en) |
FR (1) | FR2964188B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108955426A (en) * | 2018-06-13 | 2018-12-07 | 河南北方红阳机电有限公司 | A kind of thin-wall case warhead compound charge method with deep fuse hole |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN113804067B (en) * | 2021-09-14 | 2023-05-09 | 四川航天川南火工技术有限公司 | General initiating explosive device dress presses frock |
CN113790640A (en) * | 2021-09-16 | 2021-12-14 | 太原师范学院 | Fuel press-fitting mold for cylindrical thin-wall structure projectile body and using method thereof |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE41318C (en) * | W. LORENZ in Karlsruhe i. B | Process and tools for compressing powder or other compressible substances in hollow bodies of all kinds, such as cartridge cases, tubes, matrices, cans, etc. in a radial, lateral or inclined direction from the inside of the hollow body towards the wall of the same | ||
DE733070C (en) * | 1940-11-17 | 1943-03-18 | Rheinmetall Borsig Ag | Device for injecting explosives into projectiles |
US2373799A (en) * | 1942-11-04 | 1945-04-17 | Frank C Wilson | Bomb loading press |
US2395898A (en) * | 1943-08-13 | 1946-03-05 | John C Mohr | Pressing device |
FR2801883A1 (en) | 1999-12-06 | 2001-06-08 | Giat Ind Sa | Low-sensitivity compressible explosive composition for use in medium caliber ammunition, comprising oxynitrotriazole, hexogen or octogen, aluminum powder and optionally graphite powder |
-
2010
- 2010-09-01 FR FR1003503A patent/FR2964188B1/en not_active Expired - Fee Related
-
2011
- 2011-07-28 ES ES11290343.0T patent/ES2529772T3/en active Active
- 2011-07-28 EP EP20110290343 patent/EP2426455B1/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE41318C (en) * | W. LORENZ in Karlsruhe i. B | Process and tools for compressing powder or other compressible substances in hollow bodies of all kinds, such as cartridge cases, tubes, matrices, cans, etc. in a radial, lateral or inclined direction from the inside of the hollow body towards the wall of the same | ||
DE733070C (en) * | 1940-11-17 | 1943-03-18 | Rheinmetall Borsig Ag | Device for injecting explosives into projectiles |
US2373799A (en) * | 1942-11-04 | 1945-04-17 | Frank C Wilson | Bomb loading press |
US2395898A (en) * | 1943-08-13 | 1946-03-05 | John C Mohr | Pressing device |
FR2801883A1 (en) | 1999-12-06 | 2001-06-08 | Giat Ind Sa | Low-sensitivity compressible explosive composition for use in medium caliber ammunition, comprising oxynitrotriazole, hexogen or octogen, aluminum powder and optionally graphite powder |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108955426A (en) * | 2018-06-13 | 2018-12-07 | 河南北方红阳机电有限公司 | A kind of thin-wall case warhead compound charge method with deep fuse hole |
CN108955426B (en) * | 2018-06-13 | 2020-11-17 | 河南北方红阳机电有限公司 | Composite powder charging method for thin-wall shell warhead with deep communication hole |
Also Published As
Publication number | Publication date |
---|---|
FR2964188B1 (en) | 2012-08-17 |
ES2529772T3 (en) | 2015-02-25 |
EP2426455B1 (en) | 2014-12-17 |
FR2964188A1 (en) | 2012-03-02 |
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