EP0626555B1 - Practice projectile and method for fabrication - Google Patents

Practice projectile and method for fabrication Download PDF

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Publication number
EP0626555B1
EP0626555B1 EP94401117A EP94401117A EP0626555B1 EP 0626555 B1 EP0626555 B1 EP 0626555B1 EP 94401117 A EP94401117 A EP 94401117A EP 94401117 A EP94401117 A EP 94401117A EP 0626555 B1 EP0626555 B1 EP 0626555B1
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EP
European Patent Office
Prior art keywords
projectile
segments
sectors
projectile according
holding means
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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.)
Expired - Lifetime
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EP94401117A
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German (de)
French (fr)
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EP0626555A1 (en
Inventor
Jean-Marie Godefroy
Philippe Maillard
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Manurhin Defense SA
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Manurhin Defense SA
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/12Projectiles or missiles
    • F42B8/14Projectiles or missiles disintegrating in flight or upon impact

Definitions

  • the technical field of the present invention is that of ammunition and exercise projectiles and more particularly that of projectiles which disintegrate at the exit of the barrel of a weapon.
  • ammunition of exercise one distinguishes generally those which are intended to reproduce the real ballistics of a war projectile, but on a reduced distance and those which are intended to reproduce only the environment suitable for shooting (noise, recoil, fumes ).
  • the first type of ammunition for practice can be illustrated by the patents FR2509457, on which the preambles of independent claims 1 and 11 are based, and DE734429, which both describe a projectile comprising a body formed by the assembly of several segments.
  • This projectile is intended to reproduce the actual ballistics of a war projectile over a certain distance. It thus comprises means which make it possible to secure the joining of the different segments over part of the trajectory. It requires the installation of a shooting safety template and cannot be used to reproduce only the shooting environment.
  • This charge must in particular be sufficiently dense and compact to ensure the mechanical strength of the projectile, but it must still be easily dispersed at the exit of the barrel of the weapon.
  • the document DE3819251 describes a bullet whose body is formed from several bonded metal sectors which remain integral on the trajectory and only separate on impact on a target.
  • the projectile according to the invention is inexpensive and does not degrade the barrel of the weapon. It also has excellent storage behavior even in the harshest climatic environments.
  • the invention also relates to a particularly advantageous manufacturing method for such an exercise projectile.
  • the subject of the invention is an exercise projectile comprising a body formed by the assembly of several sectors and a base having a housing intended to receive the different sectors, projectile characterized in that the sectors are made of a material of the type thermoplastic and in that it comprises means ensuring maintenance of the assembly of the sectors during the handling phases, means designed so as to release the sectors at the exit of the barrel of a weapon when the projectile is fired.
  • the holding means can comprise a cap surrounding a front part of the projectile.
  • the cap can carry a bead which penetrates into an annular groove arranged on the sectors and ensures the fixing of the cap on the latter.
  • the first group of sectors delimits dwellings in which the other sectors are arranged, and the latter which constitute a second group of sectors are held together with the previous ones by a cover.
  • the second group of sectors can be formed in one piece with the cover.
  • the sectors are welded two by two along their external contact edges.
  • the different sectors are produced by a single molding operation, all of them connected in a star by their tapered ends.
  • an exercise projectile 1 according to a first embodiment of the invention comprises a body 2 formed by the assembly of six identical sectors 3a, 3b, 3c, 3d, 3e and 3f.
  • Each sector is delimited by two intersecting planes 4a, 4b which form an angle of 60 °.
  • each sector is in contact with two neighboring sectors at its intersecting planes.
  • the absence of empty space between the sectors ensures excellent rigidity of the projectile.
  • the projectile also includes a base 5 which has a housing 6 intended to receive the sectors 3.
  • the base 5 carries an annular bulge 7 which constitutes a belt intended to come to seal the propellant gases in the barrel of the weapon.
  • the base also carries an annular groove 8 intended to allow the projectile to be secured to a propellant charge case (not shown).
  • the base 5 has an internal rim 9 which penetrates into a groove 10 arranged on the body 2. This rim secures the base and the body.
  • the main function of the base is to seal the propellant gases in the barrel, on the one hand thanks to the belt 7, and on the other hand thanks to the bottom wall 11 of the base which prevents gases from entering between the different sectors.
  • the sectors and the base are made of a plastic material of the thermoplastic type. These elements are obtained for example by injection. This material allows the projectile to withstand the various temperature and humidity constraints encountered during storage.
  • thermoplastic materials can be considered. We can for example choose from the following materials: Polyethylene, Polyamide, Polypropylene, Polystyrene, Polycarbonate, Polyphenylene Oxide and Acrylonitrile Butadiene Styrene.
  • the projectile comprises means ensuring maintenance of the assembly of the sectors during the transport and handling phases.
  • these means comprise a welding point 12 which secures the various sectors at a front part 13 of the projectile.
  • This welding can be carried out by locally heating the front part 13 of the projectile.
  • the holding means are designed so as to free the sectors at the outlet of the barrel of a weapon when the projectile is fired.
  • the mechanical strength of the weld is not sufficient to withstand the stresses developed during firing.
  • the sectors Due to the lightness of the plastic, the sectors are quickly braked after their separation at the outlet of the tube. They will be dispersed a short distance from the weapon (of the order of 50 m for a caliber of 20 millimeters).
  • the holding in the tube is excellent because the sectors constitute a rigid projectile body, the bursting at the exit of the barrel of the weapon is guaranteed because the holding means are sized for this purpose.
  • the barrel of the weapon is not deteriorated by the sectors and the energy of the latter after dispersion is insufficient to deteriorate the optics or to injure the servants of the weapon.
  • Such a projectile is inexpensive to produce.
  • the holding means can be constituted solely by the base itself which will then have a sufficient length to ensure the maintenance of the sectors.
  • FIGS. 2a and 2b show a second embodiment in which the holding means comprise a sleeve 14 made of a plastic material of the heat-shrinkable type. Such a material is known to those skilled in the art. It is thus possible to set up a sleeve with a diameter greater than that of the body 2, then to heat this sleeve to reduce its diameter so that it comes to bear tightly on the body 2.
  • Figures 3a and 3b show a third embodiment in which the holding means comprise a cap 15 made of plastic (for example of the same type as that constituting the body).
  • the cap 15 completely surrounds the front part of the projectile. It has at its rear part a bead 16 which enters an annular groove 17 arranged on the sectors 3. The bead ensures the fixing of the cap 15 on the sectors constituting the projectile body.
  • the cap is assembled by elastic deformation of the latter.
  • the thickness of the cap will be defined as a function of the resistance desired for the connecting means. It will be possible in particular to provide incipient fractures on the cap, for example longitudinal thinning regularly distributed angularly.
  • the cap is a connecting means making it possible to provide mechanical resistance to environmental stresses which is better than that of the welding point described above.
  • the cap also has the advantage of preventing humidity or dust from entering between the sectors.
  • FIGS. 4a and 4b show a fourth embodiment in which the holding means comprise on the one hand a cover 15 made of plastic material and on the other hand projections 18, integral with the different sectors and which cooperate with grooves 19 arranged on the sectors.
  • the grooves 19 have a shape complementary to those of the projections 18.
  • the cap is identical to that described with reference to Figures 3a and 3b and will not be described in more detail.
  • Each sector 3 carries a groove 19 on one of its intersecting planes 4a and a projection 18 on the other intersecting plane 4b.
  • Grooves and projections extend substantially over the entire length of each sector as can be seen in FIG. 4a.
  • Figures 5a and 5b show a fifth embodiment in which the holding means comprise on the one hand a cap 15 (identical to that described with reference to Figures 3a and 3b) and on the other hand a central area 20 which is formed in one piece with the three sectors 3a, 3c and 3e and which extends over substantially the entire length of the latter.
  • the first group of sectors delimits housings 21 in which the sectors 3b, 3d and 3f are arranged (which constitute what will be called hereinafter the second group of sectors).
  • the cap allows the first and second group of sectors to be joined together.
  • FIGS. 6a and 6b show a sixth embodiment similar to the previous one but in which the second group of sectors (which is made up of sectors 3b, 3d and 3f) is formed in one piece with the cover 15.
  • the first group of sectors consisting of sectors 3a, 3c and 3e connected by the central area 20, is therefore housed inside the cover 15 which carries the second group of sectors.
  • connection means will be modulated by varying the dimensions of the central zone 20 and the thickness of the cap 15 opposite the first group of sectors.
  • Figures 7a and 7b show a seventh embodiment of a projectile according to the invention.
  • This embodiment is a variant of the mode described with reference to Figures 1a and 1b.
  • the body 2 of the projectile 1 is further formed by the assembly of six identical sectors 3a, 3b, 3c, 3d, 3e and 3f.
  • the sectors are all joined at their tapered ends by a plastic connection 22 obtained by molding with the sectors.
  • the sectors are also welded two by two along the external contact edges 23 of the intersecting planes 4a, 4b.
  • These longitudinal welds 24 extend along the body 2 of the projectile from its front part 13 to the annular bulge 7 of the base 5. They are obtained by heating the body 2 along the external contact edges 23 of the intersecting planes 4a, 4b.
  • the welds 24 also extend radially over a certain thickness towards the inside of the projectile.
  • a base 5 receives the sectors 3 in a housing 6.
  • This variant has the advantage of ensuring good mechanical strength of the assembly of the sectors during transport or loading phases of the weapon.
  • FIG. 8 schematizes the different stages of a method of manufacturing the projectile according to this latter embodiment.
  • step A all the sectors intended to form the projectile body are produced (step A), by a single molding operation in a suitable mold not shown.
  • step B The sectors are then grouped together (step B) so as to constitute the projectile body 2.
  • a front zone 2a of the body 2 is placed inside a tool 26 intended to heat its external surface (step C).
  • the tool 26 comprises for this purpose a housing of shape complementary to that of the front zone 2a of the projectile body, thus the heat is imparted uniformly over the entire external surface of the front zone 2a.
  • the tool 26 is defined so as to bring the front zone 2a to a temperature sufficient to locally melt the material of the sectors, which makes it possible to weld them along their edges of external contact 23.
  • heating tool 26 we could for example use an electric oven connected to an energy source 25.
  • a person skilled in the art will choose the welding temperature and the duration for which the projectile body is maintained at this temperature depending on the one hand on the characteristics of the thermoplastic material used. and on the other hand the thickness desired for the welds 24 (therefore the mechanical strength of the connecting means).
  • the thickness of the weld increases with the duration during which the projectile body is maintained at the temperature considered.
  • step D1 After the body 2 has cooled, it is removed from the tool 26 (step D1).
  • the sketch D1 no longer represents the separations between sectors on the projectile body, the welds 24 in fact give the front part 2a of the body a smooth external surface.
  • a base 5 is also produced by molding (step D2).
  • step E the projectile body 2 and the base 5 are assembled.
  • This manufacturing process is particularly economical and suitable for mass production of the projectiles according to the invention.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

Le domaine technique de la présente invention est celui des munitions et projectiles d'exercice et plus particulièrement celui des projectiles qui se désintègrent à la sortie du tube d'une arme.The technical field of the present invention is that of ammunition and exercise projectiles and more particularly that of projectiles which disintegrate at the exit of the barrel of a weapon.

Parmi les munitions d'exercice on distingue généralement celles qui sont destinées à reproduire la balistique réelle d'un projectile de guerre, mais sur une distance réduite et celles qui sont destinées à reproduire uniquement l'environnement propre au tir (bruit, recul, fumées...).Among the ammunition of exercise one distinguishes generally those which are intended to reproduce the real ballistics of a war projectile, but on a reduced distance and those which are intended to reproduce only the environment suitable for shooting (noise, recoil, fumes ...).

Le premier type de munitions d'exercice peut être illustré par les brevets FR2509457, sur lequel reposent les préambules des revendications indépendantes 1 et 11, et DE734429, qui décrivent tous deux un projectile comprenant un corps formé par l'assemblage de plusieurs segments. Ce projectile est destiné à reproduire la balistique réelle d'un projectile de guerre sur une certaine distance. Il comporte ainsi des moyens qui permettent d'assurer la solidarisation des différents segments sur une partie de la trajectoire. Il impose la mise en place d'un gabarit de sécurité de tir et ne peut être utilisé pour reproduire uniquement l'environnement du tir.The first type of ammunition for practice can be illustrated by the patents FR2509457, on which the preambles of independent claims 1 and 11 are based, and DE734429, which both describe a projectile comprising a body formed by the assembly of several segments. This projectile is intended to reproduce the actual ballistics of a war projectile over a certain distance. It thus comprises means which make it possible to secure the joining of the different segments over part of the trajectory. It requires the installation of a shooting safety template and cannot be used to reproduce only the shooting environment.

Si on considère maintenant les munitions destinées à reproduire l'environnement d'un tir, on connaît les munitions dites "à blanc" qui ne comportent pas de projectile. Ces munitions ont pour inconvénient d'imposer l'adjonction sur l'arme de dispositifs auxiliaires pour permettre en particulier le réarmement.If we now consider the ammunition intended to reproduce the environment of a shooting, we know the so-called "blank" ammunition which does not comprise a projectile. The disadvantage of these munitions is that they require the addition of auxiliary devices to the weapon, in particular to enable rearming.

On connaît également les munitions dites "break up" qui tirent un projectile comportant un chargement en poudre d'acier ou de tungstène disposé à l'intérieur d'une enveloppe fragile. Ce projectile éclate à la sortie du tube sous l'effet des forces d'inertie centrifuge. Les brevets US3338167 et CH445341 décrivent de telles munitions, qui présentent l'avantage de pouvoir être tirées sans modifier l'arme.We also know the so-called "break up" munitions which fire a projectile comprising a load of steel or tungsten powder placed inside a fragile envelope. This projectile bursts at the exit of the tube under the effect of centrifugal forces of inertia. The patents US3338167 and CH445341 describe such ammunition, which has the advantage of being able to be fired without modifying the weapon.

Cependant un projectile "break up" présente des inconvénients. Tout d'abord il est d'un coût important, car il nécessite la réalisation d'un chargement en poudre métallique présentant des caractéristiques mécaniques bien définies.However, a "break up" projectile has drawbacks. First of all, it is of significant cost, because it requires the production of a metal powder charge having well defined mechanical characteristics.

Ce chargement doit en particulier être suffisamment dense et compact pour assurer la tenue mécanique du projectile, mais il doit quand même se disperser facilement à la sortie du tube de l'arme.This charge must in particular be sufficiently dense and compact to ensure the mechanical strength of the projectile, but it must still be easily dispersed at the exit of the barrel of the weapon.

La tenue au stockage d'un tel chargement est aléatoire et il arrive ainsi que les poudres métalliques s'oxydent, ce qui nuit au comportement du projectile dans le tube et à la sortie de ce dernier.The storage behavior of such a load is random and it happens that the metal powders oxidize, which affects the behavior of the projectile in the tube and at the exit of the latter.

De plus on constate fréquemment que ces projectiles éclatent à l'intérieur du tube de l'arme, provoquant ainsi une détérioration rapide de celui-ci.In addition, it is frequently observed that these projectiles burst inside the barrel of the weapon, thus causing rapid deterioration of the latter.

Enfin la poudre dense qui se trouve dispersée au voisinage de la bouche de l'arme risque de venir dégrader les optiques de visée, voire même de blesser les personnels.Finally, the dense powder which is dispersed in the vicinity of the muzzle of the weapon risks damaging the sighting optics, or even injuring personnel.

Le document DE3819251 décrit une balle dont le corps est formé de plusieurs secteurs métalliques collés qui restent solidaires sur trajectoire et ne se séparent qu'à l'impact sur une cible.The document DE3819251 describes a bullet whose body is formed from several bonded metal sectors which remain integral on the trajectory and only separate on impact on a target.

C'est le but de l'invention que de proposer un projectile d'exercice se désintégrant à la sortie du tube de l'arme mais ne présentant pas les inconvénients des projectiles "Break up" selon l'état de la technique.It is the object of the invention to provide an exercise projectile disintegrating at the outlet of the barrel of the weapon but not having the drawbacks of "break up" projectiles according to the state of the art.

Ainsi le projectile selon l'invention est peu coûteux et ne dégrade pas le tube de l'arme. Il présente également une excellente tenue au stockage même dans les environnements climatiques les plus sévères.Thus the projectile according to the invention is inexpensive and does not degrade the barrel of the weapon. It also has excellent storage behavior even in the harshest climatic environments.

L'invention a également pour objet un procédé de fabrication particulièrement avantageux pour un tel projectile d'exercice.The invention also relates to a particularly advantageous manufacturing method for such an exercise projectile.

Ainsi l'invention a pour objet un projectile d'exercice comprenant un corps formé par l'assemblage de plusieurs secteurs et un culot présentant un logement destiné à recevoir les différents secteurs, projectile caractérisé en ce que les secteurs sont réalisés en une matière du type thermoplastique et en ce qu'il comporte des moyens assurant un maintien de l'assemblage des secteurs pendant les phases de manipulation, moyens conçus de façon à libérer les secteurs à la sortie du tube d'une arme lors du tir du projectile.Thus the subject of the invention is an exercise projectile comprising a body formed by the assembly of several sectors and a base having a housing intended to receive the different sectors, projectile characterized in that the sectors are made of a material of the type thermoplastic and in that it comprises means ensuring maintenance of the assembly of the sectors during the handling phases, means designed so as to release the sectors at the exit of the barrel of a weapon when the projectile is fired.

Selon divers mode de réalisation les moyens de maintien peuvent comprendre une coiffe entourant une partie avant du projectile.According to various embodiments, the holding means can comprise a cap surrounding a front part of the projectile.

La coiffe peut porter un bourrelet qui pénètre dans une gorge annulaire aménagée sur les secteurs et assure la fixation de la coiffe sur ces derniers.The cap can carry a bead which penetrates into an annular groove arranged on the sectors and ensures the fixing of the cap on the latter.

Selon divers modes de réalisation, les moyens de maintien peuvent comprendre:

  • un manchon entourant une partie avant du projectile, manchon réalisé en un matériau thermorétractable,
  • au moins un point de soudure entre deux secteurs contigus,
  • au moins une saillie solidaire d'un secteur et coopérant avec une rainure aménagée sur un secteur contigu au précédent, rainure ayant une forme complémentaire de celle de la saillie,
  • une zone centrale formée d'une seule pièce avec au moins deux secteurs régulièrement répartis angulairement et formant un premier groupe de secteurs.
According to various embodiments, the holding means can comprise:
  • a sleeve surrounding a front part of the projectile, sleeve made of a heat-shrinkable material,
  • at least one weld point between two contiguous sectors,
  • at least one projection integral with a sector and cooperating with a groove arranged on a sector contiguous to the previous one, groove having a shape complementary to that of the projection,
  • a central zone formed in one piece with at least two sectors regularly distributed angularly and forming a first group of sectors.

Dans ce dernier cas, le premier groupe de secteurs délimite des logements dans lesquels sont disposés les autres secteurs, et ces derniers qui constituent un deuxième groupe de secteurs sont maintenus solidaires des précédents par une coiffe.In the latter case, the first group of sectors delimits dwellings in which the other sectors are arranged, and the latter which constitute a second group of sectors are held together with the previous ones by a cover.

Le deuxième groupe de secteurs peut être formé d'une seule pièce avec la coiffe.The second group of sectors can be formed in one piece with the cover.

Selon un mode particulier de réalisation, les secteurs sont soudés deux par deux le long de leurs arêtes de contact externes.According to a particular embodiment, the sectors are welded two by two along their external contact edges.

L'invention a également pour objet un procédé de fabrication d'un projectile comportant les étapes suivantes:

  • regroupement des secteurs de façon à constituer le corps de projectile,
  • positionnement d'au moins une zone avant du corps de projectile dans un outillage destiné à chauffer sa surface externe à une température suffisante pour faire fondre localement le matériau des secteurs et les souder le long de leurs arêtes de contact externe,
  • refroidissement du corps,
  • assemblage du corps de projectile et du culot.
The subject of the invention is also a method of manufacturing a projectile comprising the following steps:
  • regrouping of the sectors so as to constitute the projectile body,
  • positioning of at least one front zone of the projectile body in a tool intended to heat its external surface to a temperature sufficient to locally melt the material of the sectors and weld them along their edges of external contact,
  • body cooling,
  • assembly of the projectile body and the base.

Selon une variante avantageuse, on réalise par une seule opération de moulage les différents secteurs, tous reliés en étoile par leurs extrémités effilées.According to an advantageous variant, the different sectors are produced by a single molding operation, all of them connected in a star by their tapered ends.

L'invention sera mieux comprise à la lecture de la description qui va suivre de divers modes de réalisation description faite en référence aux dessins annexés et dans lesquels:

  • les figures 1a et 1b représentent un projectile suivant un premier mode de réalisation de l'invention, la figure 1a étant une coupe longitudinale axiale et la figure 1b une coupe transversale suivant le plan AA de la figure 1a,
  • les figures 2a et 2b représentent un projectile suivant un deuxième mode de réalisation de l'invention, la figure 2b étant une coupe transversale suivant le plan BB de la figure 2a,
  • les figures 3a et 3b représentent un projectile suivant un troisième mode de réalisation de l'invention, la figure 3b étant une coupe transversale suivant le plan CC de la figure 3a,
  • les figures 4a et 4b représentent un projectile suivant un quatrième mode de réalisation de l'invention, la figure 4b étant une coupe transversale suivant le plan DD de la figure 4a et la figure 4a étant une coupe suivant le plan EE de la figure 4b,
  • les figures 5a et 5b représentent un projectile suivant un cinquième mode de réalisation de l'invention, la figure 5b étant une coupe transversale suivant le plan FF de la figure 5a et la figure 5a étant une coupe suivant le plan GG de la figure 5b,
  • les figures 6a et 6b représentent un projectile suivant un sixième mode de réalisation de l'invention, la figure 6b étant une coupe transversale suivant le plan HH de la figure 6a et la figure 6a étant une coupe suivant le plan II de la figure 6b.
  • les figures 7a et 7b représentent un projectile suivant un septième mode de réalisation de l'invention, la figure 7b étant une coupe transversale suivant le plan JJ de la figure 7a et la figure 7a étant une coupe suivant le plan KK de la figure 7b.
  • la figure 8 schématise les différentes étapes d'un procédé de fabrication du projectile selon les figures 7a et 7b.
The invention will be better understood on reading the description which follows of various embodiments, description made with reference to the appended drawings and in which:
  • FIGS. 1a and 1b represent a projectile according to a first embodiment of the invention, FIG. 1a being an axial longitudinal section and FIG. 1b a transverse section along the plane AA of FIG. 1a,
  • FIGS. 2a and 2b represent a projectile according to a second embodiment of the invention, FIG. 2b being a cross section along the plane BB of FIG. 2a,
  • FIGS. 3a and 3b represent a projectile according to a third embodiment of the invention, FIG. 3b being a cross section along the plane CC of FIG. 3a,
  • FIGS. 4a and 4b represent a projectile according to a fourth embodiment of the invention, FIG. 4b being a cross section along the plane DD of FIG. 4a and FIG. 4a being a section along the plane EE of FIG. 4b,
  • FIGS. 5a and 5b represent a projectile according to a fifth embodiment of the invention, FIG. 5b being a cross section along the plane FF of FIG. 5a and FIG. 5a being a section along the plane GG of FIG. 5b,
  • Figures 6a and 6b show a projectile according to a sixth embodiment of the invention, Figure 6b being a cross section along the plane HH of Figure 6a and Figure 6a being a section along the plane II of Figure 6b.
  • Figures 7a and 7b show a projectile according to a seventh embodiment of the invention, Figure 7b being a cross section along the plane JJ of Figure 7a and Figure 7a being a section along the plane KK of Figure 7b.
  • FIG. 8 schematizes the different stages of a method of manufacturing the projectile according to FIGS. 7a and 7b.

En se reportant aux figures 1a et 1b, un projectile d'exercice 1 selon un premier mode de réalisation de l'invention comprend un corps 2 formé par l'assemblage de six secteurs identiques 3a, 3b, 3c, 3d, 3e et 3f.Referring to Figures 1a and 1b, an exercise projectile 1 according to a first embodiment of the invention comprises a body 2 formed by the assembly of six identical sectors 3a, 3b, 3c, 3d, 3e and 3f.

Chaque secteur est délimité par deux plans sécants 4a, 4b qui forment un angle de 60°. Ainsi, après assemblage, chaque secteur se trouve en contact avec deux secteurs voisins au niveau de ses plans sécants. L'absence d'espace vide entre les secteurs assure une excellente rigidité du projectile.Each sector is delimited by two intersecting planes 4a, 4b which form an angle of 60 °. Thus, after assembly, each sector is in contact with two neighboring sectors at its intersecting planes. The absence of empty space between the sectors ensures excellent rigidity of the projectile.

Le projectile comporte également un culot 5 qui présente un logement 6 destiné à recevoir les secteurs 3. Le culot 5 porte un renflement annulaire 7 qui constitue une ceinture destinée à venir réaliser l'étanchéité aux gaz propulsifs dans le tube de l'arme. Le culot porte également un sillon annulaire 8 destiné à permettre la solidarisation du projectile sur un étui de charge propulsive (non représenté).The projectile also includes a base 5 which has a housing 6 intended to receive the sectors 3. The base 5 carries an annular bulge 7 which constitutes a belt intended to come to seal the propellant gases in the barrel of the weapon. The base also carries an annular groove 8 intended to allow the projectile to be secured to a propellant charge case (not shown).

Le culot 5 présente un rebord interne 9 qui pénètre dans une gorge 10 aménagée sur le corps 2. Ce rebord assure la solidarisation du culot et du corps.The base 5 has an internal rim 9 which penetrates into a groove 10 arranged on the body 2. This rim secures the base and the body.

La fonction principale du culot est d'assurer l'étanchéité aux gaz propulsifs dans le tube de l'arme, cela d'une part grâce à la ceinture 7, et d'autre part grâce à la paroi de fond 11 du culot qui empêche les gaz de pénétrer entre les différents secteurs.The main function of the base is to seal the propellant gases in the barrel, on the one hand thanks to the belt 7, and on the other hand thanks to the bottom wall 11 of the base which prevents gases from entering between the different sectors.

Les secteurs et le culot sont réalisés en une matière plastique du type thermoplastique. Ces éléments sont obtenus par exemple par injection. Ce matériau permet une bonne tenue du projectile aux différentes contraintes de température et d'humidité rencontrées au cours du stockage.The sectors and the base are made of a plastic material of the thermoplastic type. These elements are obtained for example by injection. This material allows the projectile to withstand the various temperature and humidity constraints encountered during storage.

Différentes matières thermoplastiques peuvent être envisagées. On pourra par exemple choisir parmi les matériaux suivants: Polyéthylène, Polyamide, Polypropylène, Polystyrène, Polycarbonate, Polyphenylène Oxyde et Acrylonitrile Butadiène Styrène.Different thermoplastic materials can be considered. We can for example choose from the following materials: Polyethylene, Polyamide, Polypropylene, Polystyrene, Polycarbonate, Polyphenylene Oxide and Acrylonitrile Butadiene Styrene.

Le projectile comporte des moyens assurant un maintien de l'assemblage des secteurs pendant les phases de transport et manipulation.The projectile comprises means ensuring maintenance of the assembly of the sectors during the transport and handling phases.

Ces moyens permettent de garantir la tenue du projectile aux vibrations et autres contraintes mécaniques rencontrées lors du transport ou du chargement de l'arme.These means make it possible to guarantee the resistance of the projectile to vibrations and other mechanical stresses encountered during transport or loading of the weapon.

Selon le premier mode de réalisation décrit ici, ces moyens comprennent un point de soudure 12 qui solidarise les différents secteurs au niveau d'une partie avant 13 du projectile.According to the first embodiment described here, these means comprise a welding point 12 which secures the various sectors at a front part 13 of the projectile.

Cette soudure pourra être réalisée en chauffant localement la partie avant 13 du projectile.This welding can be carried out by locally heating the front part 13 of the projectile.

Les moyens de maintien sont conçus de façon à libérer les secteurs à la sortie du tube d'une arme lors du tir du projectile. La tenue mécanique de la soudure n'est pas suffisante pour résister aux contraintes développées lors du tir.The holding means are designed so as to free the sectors at the outlet of the barrel of a weapon when the projectile is fired. The mechanical strength of the weld is not sufficient to withstand the stresses developed during firing.

Après rupture de la soudure les secteurs peuvent s'écarter, ils restent cependant maintenus par le tube de l'arme, mais ils s'écartent à la sortie de ce dernier par suite des efforts aérodynamiques qui s'exercent sur le projectile (efforts auxquels s'ajoutera la force centrifuge dans le cas du tir à partir d'une arme à tube rayé).After rupture of the weld the sectors can deviate, they remain however maintained by the barrel of the weapon, but they deviate at the exit of this last owing to the aerodynamic forces which are exerted on the projectile (forces to which centrifugal force will be added in the case of shooting from a rifle with a rifled tube).

On voit ainsi que par un dimensionnement approprié des moyens de maintien, il est possible de concevoir un projectile d'exercice destiné au tir dans un tube lisse. Les projectiles connus de type "break up", et qui sont cités dans le préambule, ne peuvent au contraire être rompus que lors du tir dans un tube rayé.It is thus seen that by an appropriate dimensioning of the holding means, it is possible to design an exercise projectile intended for shooting in a smooth tube. On the contrary, the known “break up” type projectiles, which are mentioned in the preamble, can only be broken when firing in a striped tube.

Du fait de la légèreté de la matière plastique, les secteurs sont rapidement freinés après leur séparation à la sortie du tube. Ils se trouveront dispersés à une faible distance de l'arme (de l'ordre de 50 m pour un calibre de 20 millimètres).Due to the lightness of the plastic, the sectors are quickly braked after their separation at the outlet of the tube. They will be dispersed a short distance from the weapon (of the order of 50 m for a caliber of 20 millimeters).

On voit donc les avantages apportés par l'invention sur les munitions connues du type "Break up": la tenue dans le tube est excellente car les secteurs constituent un corps de projectile rigide, l'éclatement à la sortie du tube de l'arme est garanti car les moyens de maintien sont dimensionnés à cet effet. Le tube de l'arme n'est pas détérioré par les secteurs et l'énergie de ces derniers après dispersion est insuffisante pour détériorer les optiques ou pour blesser les servants de l'arme.We therefore see the advantages provided by the invention on the known ammunition of the "Break up" type: the holding in the tube is excellent because the sectors constitute a rigid projectile body, the bursting at the exit of the barrel of the weapon is guaranteed because the holding means are sized for this purpose. The barrel of the weapon is not deteriorated by the sectors and the energy of the latter after dispersion is insufficient to deteriorate the optics or to injure the servants of the weapon.

Le montage du projectile est réalisé de la façon suivante:

  • les secteurs sont assemblés de façon à constituer le corps 2, qui est ensuite disposé dans un outillage présentant une forme complémentaire,
  • le culot est mis en place sur la partie arrière du corps par déformation élastique,
  • le projectile est retiré de l'outillage et la soudure 12 est réalisée par chauffage de la partie avant 13.
The assembly of the projectile is carried out as follows:
  • the sectors are assembled so as to constitute the body 2, which is then placed in a tool having a complementary shape,
  • the base is placed on the rear part of the body by elastic deformation,
  • the projectile is removed from the tool and the welding 12 is carried out by heating the front part 13.

Un tel projectile est peu coûteux à réaliser.Such a projectile is inexpensive to produce.

A titre de variante les moyens de maintien peuvent être constitués uniquement par le culot lui même qui présentera alors une longueur suffisante pour assurer le maintien des secteurs.As a variant, the holding means can be constituted solely by the base itself which will then have a sufficient length to ensure the maintenance of the sectors.

Dans les autres modes de réalisation qui vont être maintenant décrits en référence aux figures 2 à 6, certains éléments constitutifs du projectile porteront les mêmes numéros que ceux décrits en référence aux figures 1a et 1b.In the other embodiments which will now be described with reference to Figures 2 to 6, some constituent elements of the projectile will bear the same numbers as those described with reference to FIGS. 1a and 1b.

Ces éléments ne seront pas décrits plus en détail lorsqu'ils sont structurellement identiques à ceux décrits précédemment.These elements will not be described in more detail when they are structurally identical to those described above.

Les figures 2a et 2b montrent un deuxième mode de réalisation dans lequel les moyens de maintien comprennent un manchon 14 réalisé en une matière plastique du type thermorétractable. Un tel matériau est connu de l'homme du métier. Il est possible ainsi de mettre en place un manchon d'un diamètre supérieur à celui du corps 2, puis de chauffer ce manchon pour réduire son diamètre de telle façon qu'il vienne en appui serré sur le corps 2.FIGS. 2a and 2b show a second embodiment in which the holding means comprise a sleeve 14 made of a plastic material of the heat-shrinkable type. Such a material is known to those skilled in the art. It is thus possible to set up a sleeve with a diameter greater than that of the body 2, then to heat this sleeve to reduce its diameter so that it comes to bear tightly on the body 2.

Il est possible avec cette variante de moduler de façon précise la résistance des moyens de liaison en jouant sur la longueur du manchon 14.With this variant, it is possible to precisely modulate the resistance of the connecting means by varying the length of the sleeve 14.

Les figures 3a et 3b montrent un troisième mode de réalisation dans lequel les moyens de maintien comprennent une coiffe 15 réalisée en matière plastique (par exemple du même type que celle constituant le corps).Figures 3a and 3b show a third embodiment in which the holding means comprise a cap 15 made of plastic (for example of the same type as that constituting the body).

La coiffe 15 entoure complètement la partie avant du projectile. Elle comporte à sa partie arrière un bourrelet 16 qui pénètre dans une gorge annulaire 17 aménagée sur les secteurs 3. Le bourrelet assure la fixation de la coiffe 15 sur les secteurs constituant le corps de projectile. Le montage de la coiffe s'effectue par déformation élastique de cette dernière.The cap 15 completely surrounds the front part of the projectile. It has at its rear part a bead 16 which enters an annular groove 17 arranged on the sectors 3. The bead ensures the fixing of the cap 15 on the sectors constituting the projectile body. The cap is assembled by elastic deformation of the latter.

On définira l'épaisseur de la coiffe en fonction de la résistance souhaitée pour les moyens de liaison. Il sera possible en particulier de prévoir des amorces de ruptures sur la coiffe, par exemple des amincissements longitudinaux régulièrement répartis angulairement.The thickness of the cap will be defined as a function of the resistance desired for the connecting means. It will be possible in particular to provide incipient fractures on the cap, for example longitudinal thinning regularly distributed angularly.

La coiffe est un moyen de liaison permettant d'assurer une tenue mécanique aux contraintes d'environnement qui est meilleure que celle du point de soudure décrit précédemment.The cap is a connecting means making it possible to provide mechanical resistance to environmental stresses which is better than that of the welding point described above.

La coiffe présente également pour avantage d'empêcher l'humidité ou bien les poussières de pénétrer entre les secteurs.The cap also has the advantage of preventing humidity or dust from entering between the sectors.

Les figures 4a et 4b montrent un quatrième mode de réalisation dans lequel les moyens de maintien comprennent d'une part une coiffe 15 réalisée en matière plastique et d'autre part des saillies 18, solidaires des différents secteurs et qui coopèrent avec des rainures 19 aménagées sur les secteurs. Les rainures 19 ont une forme complémentaire de celles des saillies 18.FIGS. 4a and 4b show a fourth embodiment in which the holding means comprise on the one hand a cover 15 made of plastic material and on the other hand projections 18, integral with the different sectors and which cooperate with grooves 19 arranged on the sectors. The grooves 19 have a shape complementary to those of the projections 18.

La coiffe est identique à celle décrite en référence aux figures 3a et 3b et ne sera pas décrite plus en détail.The cap is identical to that described with reference to Figures 3a and 3b and will not be described in more detail.

Chaque secteur 3 porte une rainure 19 sur un de ses plans sécants 4a et une saillie 18 sur l'autre plan sécant 4b.Each sector 3 carries a groove 19 on one of its intersecting planes 4a and a projection 18 on the other intersecting plane 4b.

Rainures et saillies s'étendent sensiblement sur toute la longueur de chaque secteur comme cela est visible sur la figure 4a.Grooves and projections extend substantially over the entire length of each sector as can be seen in FIG. 4a.

On pourra jouer à la fois sur les dimensions des saillies 18 et sur l'épaisseur de la coiffe 15 pour moduler la résistance des moyens de liaison.We can play with both the dimensions of the projections 18 and the thickness of the cap 15 to modulate the resistance of the connecting means.

Rainures et saillies permettent également d'améliorer la tenue mécanique aux contraintes d'environnement de l'assemblage des secteurs.Grooves and projections also make it possible to improve the mechanical resistance to environmental constraints of the assembly of the sectors.

Il est possible à titre de variante de ne pas prévoir de coiffe 15 et d'assurer le maintien des secteurs uniquement au moyen des saillies 18 et des rainures 19.It is possible, as a variant, not to provide a cover 15 and to ensure the maintenance of the sectors only by means of the projections 18 and the grooves 19.

Les figures 5a et 5b montrent un cinquième mode de réalisation dans lequel les moyens de maintien comprennent d'une part une coiffe 15 (identique à celle décrite en référence aux figures 3a et 3b) et d'autre part une zone centrale 20 qui est formée d'une seule pièce avec les trois secteurs 3a, 3c et 3e et qui s'étend sur sensiblement toute la longueur de ces derniers.Figures 5a and 5b show a fifth embodiment in which the holding means comprise on the one hand a cap 15 (identical to that described with reference to Figures 3a and 3b) and on the other hand a central area 20 which is formed in one piece with the three sectors 3a, 3c and 3e and which extends over substantially the entire length of the latter.

Ces trois secteurs sont régulièrement répartis angulairement, ils forment ce qui sera appelé par la suite le premier groupe de secteurs.These three sectors are regularly distributed angularly, they form what will be called hereinafter the first group of sectors.

Le premier groupe de secteur délimite des logements 21 dans lesquels sont disposés les secteurs 3b, 3d et 3f (qui constituent ce qui sera appelé par la suite le deuxième groupe de secteurs).The first group of sectors delimits housings 21 in which the sectors 3b, 3d and 3f are arranged (which constitute what will be called hereinafter the second group of sectors).

La coiffe permet de rendre solidaires le premier et le deuxième groupe de secteurs.The cap allows the first and second group of sectors to be joined together.

Il est possible de jouer sur les dimensions de la zone centrale 20, ainsi que sur l'épaisseur de la coiffe pour moduler la résistance des moyens de liaison.It is possible to play on the dimensions of the central zone 20, as well as on the thickness of the cap to modulate the resistance of the connecting means.

Les figures 6a et 6b montrent un sixième mode de réalisation analogue au précédent mais dans lequel le deuxième groupe de secteurs (qui est constitué des secteurs 3b, 3d et 3f) est formé d'une seule pièce avec la coiffe 15.FIGS. 6a and 6b show a sixth embodiment similar to the previous one but in which the second group of sectors (which is made up of sectors 3b, 3d and 3f) is formed in one piece with the cover 15.

Le premier groupe de secteurs, constitué par les secteurs 3a, 3c et 3e reliés par la zone centrale 20, se loge donc à l'intérieur de la coiffe 15 qui porte le deuxième groupe de secteurs.The first group of sectors, consisting of sectors 3a, 3c and 3e connected by the central area 20, is therefore housed inside the cover 15 which carries the second group of sectors.

Ce mode particulier de réalisation permet un montage particulièrement aisé du projectile puisque seules deux opérations sont nécessaires:

  • mise en place du premier groupe de secteurs dans la coiffe,
  • fixation du culot.
This particular embodiment allows a particularly easy mounting of the projectile since only two operations are necessary:
  • establishment of the first group of sectors in the cap,
  • fixing the base.

On modulera la résistance des moyens de liaison en jouant sur les dimensions de la zone centrale 20 et sur l'épaisseur de la coiffe 15 en regard du premier groupe de secteurs.The resistance of the connection means will be modulated by varying the dimensions of the central zone 20 and the thickness of the cap 15 opposite the first group of sectors.

Il sera en particulier possible d'aménager sur la coiffe 15 des amorces de ruptures longitudinales disposées dans le prolongement des plans sécants 4a et 4b des secteurs du deuxième groupe.It will in particular be possible to arrange on the cap 15 primers for longitudinal breaks arranged in the extension of the intersecting planes 4a and 4b of the sectors of the second group.

D'autres variantes sont possibles sans sortir du cadre de l'invention. Ainsi il est possible de combiner entre eux les différents moyens de maintien décrits précédemment. Par exemple:

  • associer soudure 12 et manchon thermorétractable 14,
  • associer les saillies 18 et rainures 19 avec une soudure ou un manchon thermorétractable,
  • remplacer, dans la variante des figures 5a et 5b, la coiffe par une soudure ou un manchon thermorétractable.
Other variants are possible without departing from the scope of the invention. Thus it is possible to combine together the different holding means described above. For example:
  • combine welding 12 and heat-shrinkable sleeve 14,
  • associate the projections 18 and grooves 19 with a weld or a heat-shrinkable sleeve,
  • replace, in the variant of FIGS. 5a and 5b, the cap with a weld or a heat-shrinkable sleeve.

Les figures 7a et 7b montrent un septième mode de réalisation d'un projectile selon l'invention.Figures 7a and 7b show a seventh embodiment of a projectile according to the invention.

Ce mode de réalisation est une variante du mode décrit en référence aux figures 1a et 1b.This embodiment is a variant of the mode described with reference to Figures 1a and 1b.

Le corps 2 du projectile 1 est encore formé par l'assemblage de six secteurs identiques 3a, 3b, 3c, 3d, 3e et 3f.The body 2 of the projectile 1 is further formed by the assembly of six identical sectors 3a, 3b, 3c, 3d, 3e and 3f.

Les secteurs sont tous solidaires au niveau de leurs extrémités effilées par une liaison 22 en matière plastique obtenue par moulage avec les secteurs.The sectors are all joined at their tapered ends by a plastic connection 22 obtained by molding with the sectors.

Les secteurs sont également soudés deux par deux le long des arêtes de contact externes 23 des plans sécants 4a, 4b.The sectors are also welded two by two along the external contact edges 23 of the intersecting planes 4a, 4b.

Ces soudures longitudinales 24 s'étendent le long du corps 2 du projectile depuis sa partie avant 13 jusqu'au renflement annulaire 7 du culot 5. Elles sont obtenues en chauffant le corps 2 le long des arêtes de contact externes 23 des plans sécants 4a, 4b.These longitudinal welds 24 extend along the body 2 of the projectile from its front part 13 to the annular bulge 7 of the base 5. They are obtained by heating the body 2 along the external contact edges 23 of the intersecting planes 4a, 4b.

Les soudures 24 s'étendent aussi radialement sur une certaine épaisseur vers l'intérieur du projectile.The welds 24 also extend radially over a certain thickness towards the inside of the projectile.

Elles constituent les moyens de maintien de l'assemblage des secteurs et leur épaisseur est choisie par l'homme du métier en fonction de la résistance mécanique souhaitée pour ces moyens de maintien.They constitute the means for maintaining the assembly of the sectors and their thickness is chosen by a person skilled in the art as a function of the mechanical strength desired for these holding means.

Comme dans les variantes précédentes, un culot 5 reçoit les secteurs 3 dans un logement 6.As in the previous variants, a base 5 receives the sectors 3 in a housing 6.

Cette variante présente l'avantage d'assurer une bonne tenue mécanique de l'assemblage des secteurs au cours de phases de transport ou de chargement de l'arme.This variant has the advantage of ensuring good mechanical strength of the assembly of the sectors during transport or loading phases of the weapon.

Elle permet également, avec un nombre de pièces réduit donc un faible coût de fabrication, d'empêcher l'humidité ou bien les poussières de pénétrer entre les secteurs. Les soudures longitudinales jouent ainsi le même rôle que la coiffe 15 décrite dans les modes de réalisation précédents.It also makes it possible, with a reduced number of parts therefore a low manufacturing cost, to prevent humidity or else dust from entering between the sectors. Longitudinal welds thus play the same role that the cap 15 described in the previous embodiments.

La figure 8 schématise les différentes étapes d'un procédé de fabrication du projectile selon ce dernier mode de réalisation.FIG. 8 schematizes the different stages of a method of manufacturing the projectile according to this latter embodiment.

On fabrique tout d'abord (étape A), par une seule opération de moulage dans un moule approprié non représenté, tous les secteurs destinés à former le corps de projectile.Firstly, all the sectors intended to form the projectile body are produced (step A), by a single molding operation in a suitable mold not shown.

Les différents secteurs 3a, 3b, 3c, 3d, 3e et 3f sont ainsi tous reliés en étoile par la liaison 22 au niveau de leurs extrémités effilées.The different sectors 3a, 3b, 3c, 3d, 3e and 3f are thus all connected in a star shape by the link 22 at their tapered ends.

On regroupe ensuite les secteurs (étape B) de façon à constituer le corps 2 de projectile.The sectors are then grouped together (step B) so as to constitute the projectile body 2.

Une zone avant 2a du corps 2 est placée à l'intérieur d'un outillage 26 destiné à chauffer sa surface externe (étape C).A front zone 2a of the body 2 is placed inside a tool 26 intended to heat its external surface (step C).

L'outillage 26 comporte à cet effet un logement de forme complémentaire de celle de la zone avant 2a du corps de projectile, ainsi la chaleur est communiquée de façon homogène sur l'ensemble de la surface externe de la zone avant 2a.The tool 26 comprises for this purpose a housing of shape complementary to that of the front zone 2a of the projectile body, thus the heat is imparted uniformly over the entire external surface of the front zone 2a.

L'outillage 26 est défini de façon à porter la zone avant 2a à une température suffisante pour faire fondre localement le matériau des secteurs, ce qui permet de les souder le long de leurs arêtes de contact externe 23.The tool 26 is defined so as to bring the front zone 2a to a temperature sufficient to locally melt the material of the sectors, which makes it possible to weld them along their edges of external contact 23.

Différentes technologies peuvent être utilisées pour l'outillage chauffant 26. On pourra par exemple utiliser un four électrique relié à une source d'énergie 25.Different technologies can be used for the heating tool 26. We could for example use an electric oven connected to an energy source 25.

On pourrait également utiliser un four dans lequel circulerait un fluide caloporteur, ou encore tremper des manchons outillages 26 portant le corps de projectile dans un bain thermostaté.One could also use an oven in which a heat transfer fluid would circulate, or alternatively dip tool sleeves 26 carrying the projectile body in a thermostatically controlled bath.

L'homme du métier choisira la température de soudure et la durée pendant laquelle le corps de projectile est maintenu à cette température en fonction, d'une part des caractéristiques de la matière thermoplastique utilisée et d'autre part de l'épaisseur souhaitée pour les soudures 24 (donc de la résistance mécanique des moyens de liaison).A person skilled in the art will choose the welding temperature and the duration for which the projectile body is maintained at this temperature depending on the one hand on the characteristics of the thermoplastic material used. and on the other hand the thickness desired for the welds 24 (therefore the mechanical strength of the connecting means).

On note en effet que pour une température de chauffage donnée, l'épaisseur de la soudure croît avec la durée pendant laquelle le corps de projectile est maintenu à la température considérée.It is in fact noted that for a given heating temperature, the thickness of the weld increases with the duration during which the projectile body is maintained at the temperature considered.

Après refroidissement du corps 2, il est retiré de l'outillage 26 (étape D1).After the body 2 has cooled, it is removed from the tool 26 (step D1).

Le croquis D1 ne représente plus les séparations entre secteurs sur le corps de projectile, les soudures 24 donnent en effet à la partie avant 2a du corps une surface externe lisse.The sketch D1 no longer represents the separations between sectors on the projectile body, the welds 24 in fact give the front part 2a of the body a smooth external surface.

Un culot 5 est réalisé par ailleurs par moulage (étape D2).A base 5 is also produced by molding (step D2).

On assemble enfin le corps 2 de projectile et le culot 5 (étape E).Finally, the projectile body 2 and the base 5 are assembled (step E).

Ce procédé de fabrication est particulièrement économique et adapté à une production en grande série des projectiles selon l'invention.This manufacturing process is particularly economical and suitable for mass production of the projectiles according to the invention.

Claims (12)

  1. A practice projectile (1) comprising a body (2) formed by assembling several segments (3) and a base (5) having a housing (6) designed to accommodate these segments, characterised in that the segments are made of a thermo-plastic type material and in that it comprises means to hold the segment (3) assembly together during the handling phases, means designed so as to free the segments upon exiting from the barrel of a weapon during firing of the projectile.
  2. A projectile according to Claim 1, characterised in that the holding means comprise a nose cap (15) surrounding a front part of the projectile (1).
  3. A projectile according to Claim 2, characterised in that the nose cap (15) has a flange (16) which penetrates into a ring-shaped groove (17) arranged on the segments (3) thereby fastening the nose cap to the latter.
  4. A projectile according to Claim 1, characterised in that the holding means comprise a sleeve (14) surrounding a front part of the projectile (1), a sleeve made of a heat-shrinkable material.
  5. A projectile according to one of Claims 1 to 4, characterised in that the holding means comprise at least one protrusion (18) integral with a segment and working in conjunction with a groove (19) arranged on a contiguous segments to the previous one, a groove of a matching shape to that of the protrusion.
  6. A projectile according to one of Claims 1 to 5, characterised in that the holding means comprise a central section (20) formed in a single piece with at least t<o segments evenly distributed at an angle and forming a first group of segments.
  7. A projectile according to Claim 6, characterised in that the first group of segments marks out housing (21) in which the other segments are placed, the latter, which form a second group of segments, being joined to the former by means of a nose cap (15).
  8. A projectile according to Claim 7, characterised in that the second group of segments is formed in a single piece with the nose cap (15).
  9. A projectile according to Claim 1, characterised in that the holding means comprise at least one spot weld (12) between two contiguous segments (3).
  10. A projectile according to Claim 9, characterised in that the segments (3) are welded two by two along their outer contact edges (23).
  11. A production process for a projectile according to Claim 10, characterised by the following steps :
    - the segments (3) are grouped together so as to form the projectile body,
    - at least a front section (2a) of the projectile body is placed in a tooling (26) designed to heat its outer surface to a high enough temperature to make the constitutive material of the segments (3) melt locally and weld them along their outer contact edges (23),
    - the body (2) is cooled,
    - the projectile body (2) and the base (5) are assembled.
  12. A production process according to Claim 11, characterised in that the various segments (3) are made in a single operation by casting and are joined together in a star shape by their tips.
EP94401117A 1993-05-25 1994-05-19 Practice projectile and method for fabrication Expired - Lifetime EP0626555B1 (en)

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FR9306183A FR2705772B1 (en) 1993-05-25 1993-05-25 Exercise projectile.
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US9921040B2 (en) * 2012-05-22 2018-03-20 Darren Rubin Longitudinally sectioned firearms projectiles
US9255775B1 (en) * 2012-05-22 2016-02-09 Darren Rubin Longitudinally sectioned firearms projectiles
US10670379B2 (en) 2012-05-22 2020-06-02 Darren Rubin Longitudinally sectioned firearms projectiles
US9212876B1 (en) * 2013-08-30 2015-12-15 The United States Of America As Represented By The Secretary Of The Army Large caliber frangible projectile
US20160018200A1 (en) * 2014-05-02 2016-01-21 Andrey Sharudenko Bullet with separable elements
LU92734B1 (en) * 2015-06-05 2016-12-06 Securinov Sa HIGH ELASTIC DEFORMATION KINETIC PROJECTILE
US10330448B2 (en) * 2015-12-16 2019-06-25 Ruag Ammotec Ag Fragmentation projectile and method for its manufacturing
US10036619B2 (en) * 2016-01-11 2018-07-31 Lehigh Defense, LLC Armor-piercing cavitation projectile
CN109141129B (en) * 2018-09-17 2020-06-16 北京机械设备研究所 Processing device for thermal shrinkage of projectile body

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Also Published As

Publication number Publication date
US5505137A (en) 1996-04-09
EP0626555A1 (en) 1994-11-30
GR3019807T3 (en) 1996-07-31
SG43301A1 (en) 1997-10-17
FR2705772A1 (en) 1994-12-02
ES2086989T3 (en) 1996-07-01
FR2705772B1 (en) 1995-08-11
DE69400093T2 (en) 1996-07-25
DE69400093D1 (en) 1996-04-18

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