EP0401114A1 - Holding device for a projectile in relation to a telescoped ammunition case - Google Patents

Holding device for a projectile in relation to a telescoped ammunition case Download PDF

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Publication number
EP0401114A1
EP0401114A1 EP90401448A EP90401448A EP0401114A1 EP 0401114 A1 EP0401114 A1 EP 0401114A1 EP 90401448 A EP90401448 A EP 90401448A EP 90401448 A EP90401448 A EP 90401448A EP 0401114 A1 EP0401114 A1 EP 0401114A1
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EP
European Patent Office
Prior art keywords
projectile
holding device
ring
cap
integral
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP90401448A
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German (de)
French (fr)
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EP0401114B1 (en
Inventor
Michel Desevaux
Pierre Ducros
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Giat Industries SA
Original Assignee
Direction General pour lArmement DGA
Giat Industries SA
Etat Francais
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Publication of EP0401114A1 publication Critical patent/EP0401114A1/en
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Publication of EP0401114B1 publication Critical patent/EP0401114B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/18Caseless ammunition; Cartridges having combustible cases
    • F42B5/184Caseless ammunition; Cartridges having combustible cases telescopic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/06Sub-calibre projectiles having sabots; Sabots therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/045Cartridges, i.e. cases with charge and missile of telescopic type

Definitions

  • the present invention relates to a device for holding a projectile relative to the casing of a telescoped type of munition.
  • Telescoped ammunition which has been the subject of numerous developments in recent years, is characterized by the fact that the projectile is located inside the casing containing the propellant charge instead of being projecting relatively to the latter.
  • the main advantage of such an arrangement is that it allows, for equal ballistic performances, to define shorter munitions which allows the design of more compact weapons or at higher rates of fire.
  • Such ammunition is complex because it requires the assembly of several fine mechanical parts, moreover the transition between the combustion of the first charge and that of the second charge is difficult to control, which risks reducing the efficiency of the charge. therefore propellant ammunition performance.
  • Patent US4770098 proposes an ammunition in which a ring comes to close the front part of the sleeve, this plastic ring has a bore whose diameter is slightly smaller than that of the projectile.
  • the ring also makes it possible to position the projectile relative to the casing therefore also relative to the barrel of the weapon, a certain number of holes make it possible to play on the stiffness of the ring and thus on the minimum pressure necessary for setting in motion of the projectile .
  • Such a concept of ammunition is particularly interesting because it makes it possible to produce ammunition of the telescoped type with a single propellant charge.
  • the ring is not sufficient to hold the projectile and this is how radial ribs are provided on the internal surface of the sleeve, the function of which is to support the projectile by its rear part.
  • Patent GB1310607 shows a telescoped munition comprising a casing comprising radial ribs ensuring the support of the projectile, as well as a plug ensuring sealing and allowing the projectile to be held axially relative to the casing.
  • the projectile is placed in a bore of this solid charge and is held radially by it, a washer ensures the axial positioning of the projectile and is bonded to the propellant charge.
  • the washer is not secured to the projectile, which implies that in the event of a fracture of the propellant blocks, following mechanical stresses of placing in position, the projectile will no longer be held radially.
  • Patent US4015527 shows an ammunition also comprising several molded propellant charge blocks arranged in a combustible envelope which is not closed by a ring.
  • the subject of the invention is a device for holding a projectile relative to the casing of a telescoped type of ammunition, comprising at least one annular ring fitted to the casing and in which the projectile is disposed, and a cap. fitted inside the ring, holding device characterized in that the cap is integral with the projectile at the front part of the latter.
  • the cap may be integral with the shoe.
  • the cap may be made integral with the projectile at the level of the ballistic warhead.
  • the holding device according to the invention may also include means ensuring the support of the projectile on the envelope at its rear part.
  • these support means comprise a wedge secured to the projectile at its rear part.
  • the means ensuring the support of the projectile comprise at least three tabs, integral with the ring at its rear part, regularly spaced from one another and extending in an axial direction.
  • the envelope has at least one bulge at its internal surface and the wedge comes to bear on this bulge.
  • the wedge will preferably include at least three arms regularly spaced from each other, it may be integral with the shoe or the tail.
  • a telescoped munition 1 of the type described in patent US4770098 comprises a casing 2, preferably made of plastic material, and closed at a rear end by a base 5, also made of plastic material, which carries an ignition device 6 of known type.
  • the envelope contains a propellant charge 7, it is closed at its front end by an annular ring 3 also made of plastic.
  • the ring 2 is thus a means for holding the projectile relative to the envelope, therefore relative to the weapon. As such, it therefore ensures correct positioning of the projectile opposite the barrel of the weapon (not shown).
  • a projectile 4 which is here of the gyrostabilized type, is disposed in a housing 9, cylindrical or slightly conical, of the ring.
  • the sealing belt 8 has a diameter greater than that of the cylindrical housing, and thus achieves a localized deformation of the ring.
  • Figure 2 shows a telescoped munition integrating a first embodiment of the holding means according to the invention.
  • the length of the ring 3 has been reduced, which has made it possible to increase the mass of propellant charge.
  • the rear face of the ring which is in contact with the load, thus arrives substantially at the level of the conical front part of the projectile.
  • the projectile 4 carries at its front part a cap 10, which has an internal profile corresponding to the external profiles of the ballistic warhead 11 and of the external surface 12 of the front part of the projectile.
  • the cap 10 is made integral with the projectile by bonding, it comprises an internal crown 10a and an external crown 10b connected by radial partitions 10c and by a conical partition 10d (see Figure 2A), the cap is exploded at the outlet of the tube of the weapon under the effect of centrifugal force.
  • the cap 10 is adjusted tightly in the cylindrical housing 9 of the ring 3, this so as to ensure the initial confinement of the propellant charge as well as the gas tightness before the forcing of the belt 8 inside the cylindrical housing 9 .
  • Such a configuration made it possible to maintain the projectile with a ring of reduced dimensions, and therefore with a maximum propellant charge mass, while retaining a socket with a cylindrical internal profile.
  • the ring 3 will preferably have a length as it is in contact with at least 50% of the external surface of the cap.
  • FIG. 3 shows another embodiment of the holding means according to the invention.
  • the front ring has the minimum length compatible with its resistance to pressure.
  • the holding means here comprises, in addition to the ring 3 and the cap 10, a shim 13 made of plastic secured to the projectile 4 at its rear part.
  • This wedge has three arms 13a, 13b, 13c regularly spaced (see Figure 3B) which are formed by the juxtaposition of three identical arcs.
  • the wedge could also be in one piece.
  • the wedge 13 completes the front cover, the contact surface with the ring is insufficient to avoid possible tilting of the projectile.
  • the wedge / cap / ring assembly constitutes the means for holding the projectile relative to the shell of the ammunition.
  • Figure 3A shows the projectile when it leaves the envelope, it is then in the barrel of the weapon 21 shown schematically.
  • the wedge 13 is stopped then broken by the ring 3, it is ejected from the envelope after the projectile without disturbing the trajectory thereof or the operation of the weapon.
  • Figure 4 shows another embodiment of the invention, in which the ring 3 has at its rear part three legs 14 regularly spaced (see Figure 4A). The projectile is then supported at its front part by the cap 10, and at its rear part by the lugs 14 of the ring 3.
  • Figure 5 shows another variant of the invention in which the casing 2 of the ammunition carries three bulges 19 regularly distributed, the projectile is then still supported at its front part by the cap 10, and at its part rear by the bulges 19 of the casing 2 (see Figure 5A).
  • FIGS. 6 to 8 show other embodiments of the holding means according to the invention intended for a telescoped munition in which the projectile 4 is of the sub-calibrated type stabilized by a stabilizer 17, and comprises a sub-projectile 16, integral with a shoe 15, consisting of several elements (in general three), a known sealing means not shown, for example a silicone coating, ensures gas tightness at the separations between the elements of the shoe.
  • the cap 10 is integral with the shoe 15 at a circular groove 18 thereof.
  • the cap provides sealing against propellant gases inside the barrel of the weapon and thus plays the role of belt.
  • the cap 10 made of plastic is injected onto the aluminum alloy shoe already equipped with the sub-projectile 16.
  • the ring 3 will preferably have a length such that it is in contact with at least 50% of the external surface of the cap.
  • the projectile shown in Figure 6 has a shoe of the pusher type, in order to gain even more volume for the propellant charge it is possible to design an ammunition in which the shoe is of the "tractor" type, that is to say as the resultant of the forces exerted on the shoe by the propellant gases has a point of application well in front of the center of gravity of the sub-projectile.
  • projectiles driven by a tractor shoe are very sensitive to transverse pressure waves and in this case it will be essential to provide a wedging means at the rear part of the projectile so as to prevent it from tilting, regardless of the length of the projectile. relative contact between the ring and the cap.
  • annular block 13 made of plastic material and comprising three regularly spaced arms 13a, 13b, 13c is made integral with the shoe at the rear part of the latter, (see FIG. 7a).
  • the shoe carries for this purpose three extensions 20 on which the shim 13 adjusts.
  • the connection between the shoe and the shim will be made by threading, gluing or tight adjustment.
  • the wedge will be broken when the extensions pass inside the ring, the wedge will then be ejected following the shoe and will not disturb the trajectory of the sub-projectile.
  • the extensions 20 will guide the projectile inside the barrel of the weapon.
  • the fit is of the tight type and the annular part of the shim 13 therefore has here a conical internal profile 22 on which the external edges of the fins of the tail unit 17 come to bear.
  • the wedge has, as in the previous variant, three regularly spaced arms 13a, 13b, 13c (see Figure 8A), the guidance is thus ensured without the need to reduce the volume of the propellant charge.
  • the mounting of the wedge on the tail will be carried out by passing the sub-projectile inside the latter and thereby achieving a deformation of the wedge by the fins.
  • the wedge will be further broken during the passage inside the ring and it will be ejected following the shoe, without disturbing the trajectory of the sub-projectile.
  • the projectile, carrying cap and ring and possibly one or more shims is first made integral with the envelope, then the propellant charge is introduced from the rear of the envelope, the base being put in place last. .

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

Abstract

The technical field of the invention is that of ammunition of the telescopic type. …<??>The invention provide a device for holding a projectile (4) in relation to the casing (2) of an ammunition (1) of the telescopic type, comprising at least one annular ring (3) which is fitted in the casing (2) and in which the projectile (4) is arranged, this holding device being characterised in that it also comprises a cap (10) fitted into the ring (3) and integral with the projectile (4) in the region of the front part of the latter. …<??>The invention is used for the production of medium-calibre ammunition. …<IMAGE>…

Description

La présente invention concerne un dispositif de maintien d'un projectile relativement à l'enveloppe d'une munition du type télescopée.The present invention relates to a device for holding a projectile relative to the casing of a telescoped type of munition.

Les munitions télescopées, qui ont fait l'objet de nombreux développement au cours de ces dernières années, sont caractérisées par le fait que le projectile se trouve disposé à l'intérieur de la douille contenant la charge propulsive au lieu d'être en saillie relativement à cette dernière.Telescoped ammunition, which has been the subject of numerous developments in recent years, is characterized by the fact that the projectile is located inside the casing containing the propellant charge instead of being projecting relatively to the latter.

Le principal avantage d'une telle disposition est qu'elle permet, à performances balistiques égales, de définir des munitions plus courtes ce qui autorise la conception d'armes plus compactes ou à cadences de tir plus élevées.The main advantage of such an arrangement is that it allows, for equal ballistic performances, to define shorter munitions which allows the design of more compact weapons or at higher rates of fire.

Mais la mise au point de telles munitions se heurte à un certain nombre de problèmes.However, the development of such ammunition faces a number of problems.

Ainsi le projectile ne se trouve plus à poste dans le tube de l'arme lorsque la munition est disposée dans la chambre, c'est la pression due à la combustion des gaz de la charge propulsive qui va dans un premier temps amener le projectile à poste, puis dans un deuxième temps le pousser à l'intérieur du tube.Thus the projectile is no longer in position in the barrel of the weapon when the ammunition is placed in the chamber, it is the pressure due to the combustion of the gases of the propellant charge which will initially bring the projectile to post, then push it inside the tube.

Afin de garder les mêmes performances balistiques que celles d'une munition classique, on est amené à remplir la douille de la munition de la plus grande quantité possible de poudre propulsive, ce qui impose la présence d'une couche annulaire de cette poudre autour du projectile.In order to keep the same ballistic performances as those of a conventional ammunition, it is necessary to fill the cartridge case of the ammunition with the greatest possible quantity of propellant powder, which imposes the presence of an annular layer of this powder around the projectile.

Lors de la mise à feu il est à craindre que les gaz de combustion devancent le projectile avant que celui-ci n'ait suffisamment pénétré dans le tube pour pouvoir assurer une étanchéité.When firing there is a risk that the combustion gases will get ahead of the projectile before it has penetrated the tube enough to be able to seal.

Différentes solutions ont été envisagées pour éviter un tel phénomène, citons pour mémoire le brevet US4604954 qui décrit une munition dans laquelle une première charge de poudre propulsive, contenue dans un petit cylindre, agit uniquement sur le projectile par l'intermédiaire d'un piston coulissant dans ce cylindre, la charge principale qui entoure le projectile ne se trouve allumée que lorsque ce-dernier à pénétré dans le tube de l'arme.Various solutions have been envisaged to avoid such a phenomenon, let us cite for memory the patent US4604954 which describes an ammunition in which a first charge of propellant powder, contained in a small cylinder, acts only on the projectile by means of a sliding piston in this cylinder, the main charge surrounding the projectile is only lit when the latter has entered the barrel of the weapon.

Une telle munition est complexe car elle requiert l'assemblage de plusieurs pièces de mécanique fine, de plus la transition entre la combustion de la première charge et celle de la deuxième charge est délicate à maîtriser, ce qui risque de diminuer le rendement de la charge propulsive donc les performances de la munition.Such ammunition is complex because it requires the assembly of several fine mechanical parts, moreover the transition between the combustion of the first charge and that of the second charge is difficult to control, which risks reducing the efficiency of the charge. therefore propellant ammunition performance.

Le brevet US4770098 propose une munition dans laquelle une bague vient fermer la partie avant de la douille, cette bague en matière plastique comporte un alésage dont le diamètre est légèrement inférieur à celui du projectile.Patent US4770098 proposes an ammunition in which a ring comes to close the front part of the sleeve, this plastic ring has a bore whose diameter is slightly smaller than that of the projectile.

Celui-ci se trouve donc immobilisé par la bague qui réalise ainsi une étanchéité aux gaz de combustion de la charge propulsive.It is therefore immobilized by the ring which thus seals the combustion gases of the propellant charge.

La bague permet également de positionner le projectile relativement à la douille donc également relativement au tube de l'arme, un certain nombre de trous permettent de jouer sur la raideur de la bague et ainsi sur la pression minimale nécessaire à la mise en mouvement du projectile.The ring also makes it possible to position the projectile relative to the casing therefore also relative to the barrel of the weapon, a certain number of holes make it possible to play on the stiffness of the ring and thus on the minimum pressure necessary for setting in motion of the projectile .

Un tel concept de munition est particulièrement intéressant car il permet de réaliser une munition du type télescopée avec une seule charge propulsive.Such a concept of ammunition is particularly interesting because it makes it possible to produce ammunition of the telescoped type with a single propellant charge.

Cependant la bague ne suffit pas à maintenir le projectile et c'est ainsi qu'il est prévu des nervures radiales sur la surface interne de la douille dont la fonction est de soutenir le projectile par sa partie arrière.However, the ring is not sufficient to hold the projectile and this is how radial ribs are provided on the internal surface of the sleeve, the function of which is to support the projectile by its rear part.

Ces nervures réduisent le volume disponible pour la poudre et risquent de perturber la régularité de l'allumage.These ribs reduce the volume available for the powder and risk disturbing the regularity of the ignition.

Il serait tentant de supprimer les nervures mais cela imposerait alors de prévoir une bague présentant une importante surface de contact avec le projectile, ce qui ne peut être accepté car une bague de longueur trop importante réduirait le volume disponible pour la poudre.It would be tempting to remove the ribs but this would then require providing a ring having a large contact surface with the projectile, which cannot be accepted because a ring of too long length would reduce the volume available for the powder.

Le brevet GB1310607 montre une munition telescopée comprennant une enveloppe comportant des nervures radiales assurant le soutien du projectile, ainsi qu'un bouchon assurant l'étanchéité et permettant un maintien axial du projectile relativement à l'enveloppe.Patent GB1310607 shows a telescoped munition comprising a casing comprising radial ribs ensuring the support of the projectile, as well as a plug ensuring sealing and allowing the projectile to be held axially relative to the casing.

Cette disposition présente les mêmes inconvénients que celle du brevet US4770098, les nervures assurent le maintien radial et limitent le volume disponible pour la charge propulsive.This arrangement has the same drawbacks as that of patent US4770098, the ribs provide radial support and limit the volume available for the propellant charge.

Le brevet US3575112 décrit une munition telescopée comprennant plusieurs éléments de charge propulsive moulée.US Pat. No. 3,575,112 describes a telescoped munition comprising several molded propellant charge elements.

Le projectile est disposé dans un alésage de cette charge solide et se trouve maintenu radialement par elle, une rondelle assure le positionement axial du projectile et est collée à la charge propulsive.The projectile is placed in a bore of this solid charge and is held radially by it, a washer ensures the axial positioning of the projectile and is bonded to the propellant charge.

La rondelle n'est pas solidaire du projectile ce qui implique qu'en cas de fracture des blocs propulsifs, suite aux contraintes mécaniques de mise à poste, le projectile ne se trouvera plus maintenu radialement.The washer is not secured to the projectile, which implies that in the event of a fracture of the propellant blocks, following mechanical stresses of placing in position, the projectile will no longer be held radially.

Celà est d'autant plus gênant que cette munition ne comporte pas d'enveloppe contenant la charge propulsive et que la rondelle est collée sur la charge elle-même qui risque de se fracturer.This is all the more annoying that this munition does not have an envelope containing the propellant charge and that the washer is stuck on the charge itself which risks fracturing.

Le brevet US4015527 montre une munition comportant également plusieurs blocs de charge propulsive moulée disposés dans une enveloppe combustible qui n'est pas fermée par une bague.Patent US4015527 shows an ammunition also comprising several molded propellant charge blocks arranged in a combustible envelope which is not closed by a ring.

C'est le but de l'invention de proposer un dispositif de maintien d'un projectile relativement à l'enveloppe d'une munition du type télescopée qui ne présente pas de tels inconvénients.It is the object of the invention to provide a device for holding a projectile relative to the casing of a telescoped type of munition which does not have such drawbacks.

Ainsi l'invention a pour objet un dispositif de maintien d'un projectile relativement à l'enveloppe d'une munition du type télescopée, comprenant au moins une bague annulaire ajustée à l'enveloppe et dans laquelle est disposé le projectile, et une coiffe ajustée à l'intérieur de la bague, dispositif de maintien caractérisé en ce que la coiffe est solidaire du projectile au niveau de la partie avant de ce-dernier.Thus, the subject of the invention is a device for holding a projectile relative to the casing of a telescoped type of ammunition, comprising at least one annular ring fitted to the casing and in which the projectile is disposed, and a cap. fitted inside the ring, holding device characterized in that the cap is integral with the projectile at the front part of the latter.

Dans le cas où le projectile est du type sous-calibré, stabilisé par empennage, et disposé à l'intérieur d'un sabot au calibre, la coiffe pourra être solidaire du sabot.In the case where the projectile is of the sub-calibrated type, stabilized by empennage, and placed inside a shoe of caliber, the cap may be integral with the shoe.

Dans le cas où le projectile est du type gyrostabilisé et comporte une ogive balistique, la coiffe pourra être rendue solidaire du projectile au niveau de l'ogive balistique.In the case where the projectile is of the gyro-stabilized type and comprises a ballistic warhead, the cap may be made integral with the projectile at the level of the ballistic warhead.

Le dispositif de maintien selon l'invention pourra comprendre également des moyens assurant l'appui du projectile sur l'enveloppe au niveau de sa partie arrière.The holding device according to the invention may also include means ensuring the support of the projectile on the envelope at its rear part.

Selon un mode particulier de réalisation, ces moyens d'appui comprennent une cale solidaire du projectile au niveau de sa partie arrière.According to a particular embodiment, these support means comprise a wedge secured to the projectile at its rear part.

Selon un autre mode de réalisation les moyens assurant l'appui du projectile comprennent au moins trois pattes, solidaires de la bague au niveau de sa partie arrière, régulièrement espacées les unes des autres et s'étendant dans une direction axiale.According to another embodiment, the means ensuring the support of the projectile comprise at least three tabs, integral with the ring at its rear part, regularly spaced from one another and extending in an axial direction.

Selon une variante, l'enveloppe comporte au moins un renflement au niveau de sa surface interne et la cale vient en appui sur ce renflement.According to a variant, the envelope has at least one bulge at its internal surface and the wedge comes to bear on this bulge.

La cale comportera de préférence au moins trois bras régulièrement espacés les uns des autres, elle pourra être solidaire du sabot ou bien de l'empennage.The wedge will preferably include at least three arms regularly spaced from each other, it may be integral with the shoe or the tail.

L'invention sera mieux comprise à la lecture de la description qui va suivre de modes particuliers de réalisation, description faite en regard des dessins annexés dans lesquels:

  • La Figure 1 est une représentation en coupe axiale d'une munition télescopée selon l'état de la technique.
  • Les Figures 2 à 8 montrent différentes munitions télescopées intégrant différents modes de réalisation du moyen de maintien selon l'invention.
  • La Figure 2A est une vue frontale de la coiffe.
  • La Figure 3A représente la munition de la Figure 3 après mise à feu de la charge propulsive, lorsque le projectile s'apprête à quitter l'enveloppe.
  • La Figure 3B montre un détail de la Figure 3.
  • La Figure 4A est une coupe suivant le plan A-A de la Figure 4.
  • La Figure 5A est une coupe suivant le plan B-B de la Figure 5.
  • La Figure 7A est une coupe suivant le plan C-C de la Figure 7.
  • La Figure 8A est une vue frontale de la cale seule qui est utilisée dans la variante de la Figure 8.
The invention will be better understood on reading the description which follows of particular embodiments, description made with reference to the appended drawings in which:
  • Figure 1 is an axial sectional representation of a telescoped munition according to the prior art.
  • Figures 2 to 8 show different telescoped ammunition integrating different embodiments of the holding means according to the invention.
  • Figure 2A is a front view of the cap.
  • Figure 3A shows the ammunition of Figure 3 after firing of the propellant charge, when the projectile is about to leave the envelope.
  • Figure 3B shows a detail of Figure 3.
  • Figure 4A is a section along the plane AA of Figure 4.
  • Figure 5A is a section along the plane BB of Figure 5.
  • Figure 7A is a section along the plane CC of Figure 7.
  • Figure 8A is a front view of the sole block which is used in the variant of Figure 8.

En se reportant à la Figure 1, une munition télescopée 1 du type de celle décrite dans le brevet US4770098 comprend une enveloppe 2, réalisée de façon préférentielle en matière plastique, et fermée à une extrémité arrière par un culot 5, également en matière plastique, qui porte un dispositif d'allumage 6 de type connu.Referring to FIG. 1, a telescoped munition 1 of the type described in patent US4770098 comprises a casing 2, preferably made of plastic material, and closed at a rear end by a base 5, also made of plastic material, which carries an ignition device 6 of known type.

L'enveloppe contient une charge propulsive 7, elle est fermée à son extrémité avant par une bague annulaire 3 réalisée également en matière plastique.The envelope contains a propellant charge 7, it is closed at its front end by an annular ring 3 also made of plastic.

La bague 2 est ainsi un moyen de maintien du projectile relativement à l'enveloppe, donc relativement à l'arme. A ce titre elle assure donc un positionnement correct du projectile en regard du tube de l'arme (non représenté).The ring 2 is thus a means for holding the projectile relative to the envelope, therefore relative to the weapon. As such, it therefore ensures correct positioning of the projectile opposite the barrel of the weapon (not shown).

Un projectile 4, qui est ici du type gyrostabilisé, est disposé dans un logement 9, cylindrique ou légèrement conique, de la bague.A projectile 4, which is here of the gyrostabilized type, is disposed in a housing 9, cylindrical or slightly conical, of the ring.

L'ajustement du projectile et de la bague est du type serré, la ceinture d'étanchéité 8 présente un diamètre supérieur à celui du logement cylindrique, et réalise ainsi une déformation localisée de la bague.The adjustment of the projectile and the ring is of the tight type, the sealing belt 8 has a diameter greater than that of the cylindrical housing, and thus achieves a localized deformation of the ring.

Un tel ajustement permet d'assurer que la mise en mouvement du projectile n'intervienne que lorsque un certain niveau de pression est atteint à l'intérieur de l'enveloppe.Such an adjustment makes it possible to ensure that the setting in motion of the projectile does not intervene until a certain level of pressure is reached inside the envelope.

La Figure 2 montre une munition télescopée intégrant un premier mode de réalisation du moyen de maintien selon l'invention.Figure 2 shows a telescoped munition integrating a first embodiment of the holding means according to the invention.

La longueur de la bague 3 a été réduite ce qui a permis d'augmenter la masse de charge propulsive.The length of the ring 3 has been reduced, which has made it possible to increase the mass of propellant charge.

La face arrière de la bague, qui se trouve en contact avec la charge, arrive ainsi sensiblement au niveau de la partie avant conique du projectile.The rear face of the ring, which is in contact with the load, thus arrives substantially at the level of the conical front part of the projectile.

Le projectile 4 porte à sa partie avant une coiffe 10, qui présente un profil interne correspondant aux profils extérieurs de l'ogive balistique 11 et de la surface externe 12 de la partie avant du projectile.The projectile 4 carries at its front part a cap 10, which has an internal profile corresponding to the external profiles of the ballistic warhead 11 and of the external surface 12 of the front part of the projectile.

La coiffe 10 est rendue solidaire du projectile par collage, elle comprend une couronne interne 10a et une couronne externe 10b reliées par des cloisons radiales 10c et par une cloison conique 10d (voir Figure 2A), la coiffe est éclatée à la sortie du tube de l'arme sous l'effet de la force centrifuge.The cap 10 is made integral with the projectile by bonding, it comprises an internal crown 10a and an external crown 10b connected by radial partitions 10c and by a conical partition 10d (see Figure 2A), the cap is exploded at the outlet of the tube of the weapon under the effect of centrifugal force.

La coiffe 10 est ajustée serrée dans le logement cylindrique 9 de la bague 3, cela de façon à assurer le confinement initial de la charge propulsive ainsi que l'étanchéité aux gaz avant le forcement de la ceinture 8 à l'intérieur du logement cylindrique 9.The cap 10 is adjusted tightly in the cylindrical housing 9 of the ring 3, this so as to ensure the initial confinement of the propellant charge as well as the gas tightness before the forcing of the belt 8 inside the cylindrical housing 9 .

Une telle configuration a permis d'assurer le maintien du projectile avec une bague de dimensions réduites, et donc avec une masse de charge propulsive maximale, tout en conservant une douille au profil interne cylindrique.Such a configuration made it possible to maintain the projectile with a ring of reduced dimensions, and therefore with a maximum propellant charge mass, while retaining a socket with a cylindrical internal profile.

Pour éviter au moment de la mise à feu les inconvénients dûs éventuellement à des ondes de pressions transversales qui risqueraient de provoquer un léger basculement du projectile et une mauvaise mise à poste dans le tube de l'arme, la bague 3 aura de préférence une longueur telle qu'elle se trouve en contact avec au moins 50% de la surface externe de la coiffe.To avoid at the time of firing the disadvantages possibly due to waves of transverse pressures which would risk causing a slight tilting of the projectile and a bad setting in the barrel of the weapon, the ring 3 will preferably have a length as it is in contact with at least 50% of the external surface of the cap.

La Figure 3 montre un autre mode de réalisation du moyen de maintien selon l'invention.Figure 3 shows another embodiment of the holding means according to the invention.

On a ici recherché à augmenter encore la masse de charge propulsive contenue dans l'enveloppe, ainsi la bague avant présente la longueur minimale compatible avec sa tenue à la pression.Here we sought to further increase the mass of propellant charge contained in the envelope, so the front ring has the minimum length compatible with its resistance to pressure.

Le moyen de maintien comprend ici, en plus de la bague 3 et de la coiffe 10, une cale 13 en matière plastique solidaire du projectile 4 au niveau de sa partie arrière.The holding means here comprises, in addition to the ring 3 and the cap 10, a shim 13 made of plastic secured to the projectile 4 at its rear part.

Cette cale comporte trois bras 13a, 13b, 13c régulièrement espacés (voir Figure 3B) qui sont constitués par la juxtaposition de trois arcs identiques.This wedge has three arms 13a, 13b, 13c regularly spaced (see Figure 3B) which are formed by the juxtaposition of three identical arcs.

La cale pourrait également être monobloc.The wedge could also be in one piece.

L'extrémité des bras vient en appui sur la surface cylindrique interne de l'enveloppe 2.The end of the arms bears on the internal cylindrical surface of the casing 2.

Dans ce mode particulier de réalisation, la cale 13 vient compléter la coiffe avant dont la surface de contact avec la bague est insuffisante pour éviter un éventuel basculement du projectile. L'ensemble cale/coiffe/bague constitue le moyen de maintien du projectile relativement à l'enveloppe de la munition.In this particular embodiment, the wedge 13 completes the front cover, the contact surface with the ring is insufficient to avoid possible tilting of the projectile. The wedge / cap / ring assembly constitutes the means for holding the projectile relative to the shell of the ammunition.

La Figure 3A montre le projectile au moment où il sort de l'enveloppe, il se trouve alors dans le tube de l'arme 21 représenté schématiquement. La cale 13 est arrêtée puis brisée par la bague 3, elle est éjectée de l'enveloppe après le projectile sans perturber la trajectoire de celui-ci ni le fonctionnement de l'arme.Figure 3A shows the projectile when it leaves the envelope, it is then in the barrel of the weapon 21 shown schematically. The wedge 13 is stopped then broken by the ring 3, it is ejected from the envelope after the projectile without disturbing the trajectory thereof or the operation of the weapon.

La Figure 4 représente un autre mode de réalisation de l'invention, dans lequel la bague 3 présente à sa partie arrière trois pattes 14 régulièrement espacées (voir Figure 4A). Le projectile est alors soutenu au niveau de sa partie avant par la coiffe 10, et au niveau de sa partie arrière par les pattes 14 de la bague 3.Figure 4 shows another embodiment of the invention, in which the ring 3 has at its rear part three legs 14 regularly spaced (see Figure 4A). The projectile is then supported at its front part by the cap 10, and at its rear part by the lugs 14 of the ring 3.

Il est possible de réduire la longueur de la partie cylindrique de la bague à sa valeur minimale admissible, ce qui permet d'accroître la masse de charge propulsive contenue dans l'enveloppe, le soutien de la partie arrière du projectile étant assuré par les pattes de la bague, on évite ainsi le montage d'une cale sur le projectile.It is possible to reduce the length of the cylindrical part of the ring to its minimum admissible value, which makes it possible to increase the mass of propellant charge contained in the envelope, the support of the rear part of the projectile being provided by the legs of the ring, this avoids mounting a shim on the projectile.

La Figure 5 montre une autre variante de l'invention dans laquelle l'enveloppe 2 de la munition porte trois renflements 19 régulièrement répartis, le projectile est alors encore soutenu au niveau de sa partie avant par la coiffe 10, et au niveau de sa partie arrière par les renflements 19 de l'enveloppe 2 (voir Figure 5A).Figure 5 shows another variant of the invention in which the casing 2 of the ammunition carries three bulges 19 regularly distributed, the projectile is then still supported at its front part by the cap 10, and at its part rear by the bulges 19 of the casing 2 (see Figure 5A).

Les Figures 6 à 8 montrent d'autres modes de réalisation du moyen de maintien selon l'invention destinés à une munition télescopée dans laquelle le projectile 4 est du type sous-calibré stabilisé par un empennage 17, et comprend un sous-projectile 16, solidaire d'un sabot 15, constitué de plusieurs éléments (en général trois), un moyen d'étanchéité connu non représenté, par exemple un revêtement silicone, assure l'étanchéité aux gaz au niveau des séparations entre les éléments du sabot.FIGS. 6 to 8 show other embodiments of the holding means according to the invention intended for a telescoped munition in which the projectile 4 is of the sub-calibrated type stabilized by a stabilizer 17, and comprises a sub-projectile 16, integral with a shoe 15, consisting of several elements (in general three), a known sealing means not shown, for example a silicone coating, ensures gas tightness at the separations between the elements of the shoe.

En se reportant à la Figure 6, la coiffe 10 est solidaire du sabot 15 au niveau d'une gorge circulaire 18 de celui-ci.Referring to Figure 6, the cap 10 is integral with the shoe 15 at a circular groove 18 thereof.

La coiffe réalise l'étanchéité aux gaz propulsifs à l'intérieur du tube de l'arme et joue ainsi le rôle de ceinture.The cap provides sealing against propellant gases inside the barrel of the weapon and thus plays the role of belt.

Dans ce mode particulier de réalisation, la coiffe 10 réalisée en matière plastique, est injectée sur le sabot en alliage d' aluminium déjà équipé du sous-projectile 16.In this particular embodiment, the cap 10 made of plastic, is injected onto the aluminum alloy shoe already equipped with the sub-projectile 16.

Afin d'éviter au moment de la mise à feu les inconvénients dûs éventuellement à des ondes de pressions transversales qui risqueraient de provoquer un léger basculement du projectile et une mauvaise mise à poste dans le tube de l'arme, la bague 3 aura de préférence une longueur telle qu'elle se trouve en contact avec au moins 50% de la surface externe de la coiffe.In order to avoid at the time of firing the inconveniences possibly due to waves of transverse pressures which would risk causing a slight tilting of the projectile and a bad setting in the barrel of the weapon, the ring 3 will preferably have a length such that it is in contact with at least 50% of the external surface of the cap.

Si on souhaite réduire les dimensions de la bague, il sera nécessaire de prévoir une cale à la partie arrière du projectile comme cela a déjà été décrit précédemment.If it is desired to reduce the dimensions of the ring, it will be necessary to provide a spacer at the rear part of the projectile as has already been described previously.

Les efforts aérodynamiques qui s'exerceront sur le sabot et la coiffe à la sortie du tube de l'arme provoqueront la rupture de la coiffe et la libération du sous-projectile.The aerodynamic forces which will be exerted on the hoof and the cap at the exit of the barrel of the weapon will cause the rupture of the cap and the release of the sub-projectile.

Le projectile représenté Figure 6 comporte un sabot du type pousseur, afin de gagner encore plus de volume pour la charge propulsive il est possible de concevoir une munition dans laquelle le sabot est du type "tracteur", c'est à dire tel que la résultante des efforts exercés sur le sabot par les gaz propulsifs ait un point d'application bien en avant du centre de gravité du sous-projectile.The projectile shown in Figure 6 has a shoe of the pusher type, in order to gain even more volume for the propellant charge it is possible to design an ammunition in which the shoe is of the "tractor" type, that is to say as the resultant of the forces exerted on the shoe by the propellant gases has a point of application well in front of the center of gravity of the sub-projectile.

Cependant des projectiles entraînés par un sabot tracteur sont très sensibles aux ondes de pression transversales et il sera dans ce cas indispensable de prévoir un moyen de calage à la partie arrière du projectile de façon à empêcher son basculement, et cela quelle que soit la longueur de contact relatif entre la bague et la coiffe.However, projectiles driven by a tractor shoe are very sensitive to transverse pressure waves and in this case it will be essential to provide a wedging means at the rear part of the projectile so as to prevent it from tilting, regardless of the length of the projectile. relative contact between the ring and the cap.

Ainsi sur la Figure 7, une cale 13 annulaire en matière plastique et comportant trois bras régulièrement espacés 13a, 13b, 13c est rendue solidaire du sabot à la partie arrière de ce-dernier, (voir Figure 7a). Le sabot porte à cet effet trois prolongements 20 sur lesquels vient s'ajuster la cale 13. La solidarisation entre le sabot et la cale sera faite par filetage, collage ou ajustement serré.Thus in FIG. 7, an annular block 13 made of plastic material and comprising three regularly spaced arms 13a, 13b, 13c is made integral with the shoe at the rear part of the latter, (see FIG. 7a). The shoe carries for this purpose three extensions 20 on which the shim 13 adjusts. The connection between the shoe and the shim will be made by threading, gluing or tight adjustment.

La cale sera rompue au moment du passage des prolongements à l'intérieur de la bague, la cale sera alors éjectée à la suite du sabot et ne perturbera pas la trajectoire du sous-projectile.The wedge will be broken when the extensions pass inside the ring, the wedge will then be ejected following the shoe and will not disturb the trajectory of the sub-projectile.

Les prolongements 20 assureront le guidage du projectile à l'intérieur du tube de l'arme.The extensions 20 will guide the projectile inside the barrel of the weapon.

Sur la Figure 8 la cale 13 est rendue solidaire du projectile au niveau de l'empennage.In Figure 8 the wedge 13 is made integral with the projectile at the tail.

L'ajustement est du type serré et la partie annulaire de la cale 13 présente donc ici un profil interne conique 22 sur lequel viennent en appui les bords externes des ailettes de l'empennage 17.The fit is of the tight type and the annular part of the shim 13 therefore has here a conical internal profile 22 on which the external edges of the fins of the tail unit 17 come to bear.

La cale présente comme dans la variante précédente trois bras régulièrement espacés 13a, 13b, 13c (voir Figure 8A), le guidage est ainsi assuré sans qu'il soit nécessaire de diminuer le volume du chargement propulsif.The wedge has, as in the previous variant, three regularly spaced arms 13a, 13b, 13c (see Figure 8A), the guidance is thus ensured without the need to reduce the volume of the propellant charge.

Le montage de la cale sur l'empennage s'effectuera en faisant passer le sous-projectile à l'intérieur de celle-ci et en réalisant ainsi une déformation de la cale par les ailettes.The mounting of the wedge on the tail will be carried out by passing the sub-projectile inside the latter and thereby achieving a deformation of the wedge by the fins.

La cale sera encore brisée lors du passage à l'intérieur de la bague et elle sera ejectée à la suite du sabot, sans perturber la trajectoire du sous-projectile.The wedge will be further broken during the passage inside the ring and it will be ejected following the shoe, without disturbing the trajectory of the sub-projectile.

Enfin il convient de noter que la fabrication et le chargement de ces différentes munitions est particulièrement aisé, il suffit de prévoir un culot 5, métallique ou non, qui soit distinct de l'enveloppe 2.Finally, it should be noted that the manufacture and loading of these different munitions is particularly easy, it suffices to provide a base 5, metallic or not, which is distinct from the envelope 2.

Ainsi le projectile, portant coiffe et bague et éventuellement une ou plusieurs cales est dans un premier temps rendu solidaire de l'enveloppe, puis le chargement propulsif est introduit par l'arrière de l'enveloppe, le culot étant mis en place en dernier lieu.Thus the projectile, carrying cap and ring and possibly one or more shims is first made integral with the envelope, then the propellant charge is introduced from the rear of the envelope, the base being put in place last. .

Claims (10)

1-Dispositif de maintien d'un projectile (4) relativement à l'enveloppe (2) d'une munition (1) du type télescopée, comprenant au moins une bague annulaire (3) ajustée à l'enveloppe (2) et dans laquelle est disposé le projectile (4), et une coiffe (10) ajustée à l'intérieur de la bague (3), dispositif de maintien caractérisé en ce que la coiffe est solidaire du projectile (4) au niveau de la partie avant de ce-dernier.1-Device for holding a projectile (4) relative to the casing (2) of a munition (1) of the telescoped type, comprising at least one annular ring (3) adjusted to the casing (2) and in which is disposed the projectile (4), and a cap (10) fitted inside the ring (3), holding device characterized in that the cap is integral with the projectile (4) at the front part of this last. 2-Dispositif de maintien selon la revendication 1 et plus particulièrement destiné à une munition dans laquelle le projectile (4) est du type sous-calibré et comprend un sous-projectile (16), stabilisé par un empennage (17) et disposé à l'intérieur d'un sabot (15) au calibre, caractérisé en ce que la coiffe (10) est solidaire du sabot.2-holding device according to claim 1 and more particularly intended for ammunition in which the projectile (4) is of the sub-calibrated type and comprises a sub-projectile (16), stabilized by a tail (17) and disposed at the interior of a shoe (15) caliber, characterized in that the cap (10) is integral with the shoe. 3-Dispositif de maintien selon la revendication 1 et plus particulièrement destiné à une munition dans laquelle le projectile (4) est du type gyrostabilisé et comporte une ogive balistique (11), caractérisé en ce que la coiffe (10) est rendue solidaire du projectile (4) au niveau de l'ogive balistique (11).3-holding device according to claim 1 and more particularly intended for an ammunition in which the projectile (4) is of the gyrostabilized type and comprises a ballistic warhead (11), characterized in that the cap (10) is made integral with the projectile (4) at the level of the ballistic warhead (11). 4-Dispositif de maintien selon une des revendications 1 à 3, caractérisé en ce qu'il comprend également des moyens (13, 14, 19) assurant l'appui du projectile (4) sur l'enveloppe (2) au niveau de sa partie arrière.4-holding device according to one of claims 1 to 3, characterized in that it also comprises means (13, 14, 19) ensuring the support of the projectile (4) on the envelope (2) at its rear part. 5-Dispositif de maintien selon la revendication 4, caractérisé en ce que les moyens assurant l'appui compren­nent une cale (13) solidaire du projectile (4) au niveau de sa partie arrière.5-holding device according to claim 4, characterized in that the means ensuring the support comprise a wedge (13) integral with the projectile (4) at its rear part. 6-Dispositif de maintien selon une des revendications 4 ou 5, caractérisé en ce que les moyens assurant l'appui du projectile comprennent au moins trois pattes (14), solidaires de la bague (3) au niveau de sa partie arrière, régulièrement espacées les unes des autres et s'étendant dans une direction axiale.6-holding device according to one of claims 4 or 5, characterized in that the means ensuring the support of the projectile comprise at least three tabs (14), integral with the ring (3) at its rear part, regularly spaced from each other and extending in an axial direction. 7-Dispositif de maintien selon la revendication 5, caractérisé en ce que les moyens assurant l'appui du projectile comprennent au moins un renflement (19) porté par l'enveloppe (2) au niveau de sa surface interne.7-holding device according to claim 5, characterized in that the means ensuring the support of the projectile comprise at least one bulge (19) carried by the casing (2) at its internal surface. 8-Dispositif de maintien selon une des revendications 5 à 7, caractérisé en ce que la cale (13) comporte au moins trois bras (13a, 13b, 13c) régulièrement espacés les uns des autres.8-holding device according to one of claims 5 to 7, characterized in that the wedge (13) comprises at least three arms (13a, 13b, 13c) regularly spaced from each other. 9-Dispositif de maintien selon les revendications 2 et 8, caractérisé en ce que la cale (13) est solidaire du sabot (15).9-holding device according to claims 2 and 8, characterized in that the wedge (13) is integral with the shoe (15). 10-Dispositif de maintien selon les revendications 2 et 8, caractérisé en ce que la cale (13) est solidaire de l'empennage (17).10-holding device according to claims 2 and 8, characterized in that the wedge (13) is integral with the tail (17).
EP90401448A 1989-06-01 1990-05-31 Holding device for a projectile in relation to a telescoped ammunition case Expired - Lifetime EP0401114B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8907231 1989-06-01
FR8907231A FR2647890A1 (en) 1989-06-01 1989-06-01 DEVICE FOR MAINTAINING A PROJECTILE RELATING TO THE ENVELOPE OF TELESCOPED MUNITION

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EP0401114A1 true EP0401114A1 (en) 1990-12-05
EP0401114B1 EP0401114B1 (en) 1993-07-28

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EP (1) EP0401114B1 (en)
DE (1) DE69002402T2 (en)
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FR2679991B1 (en) * 1991-07-31 1993-10-29 Giat Industries IMPROVEMENTS PROVIDED FOR AMMUNITION IN PARTICULAR OF THE TELESCOPE TYPE.
FR2702553B1 (en) * 1993-03-12 1995-04-28 Giat Ind Sa Telescoped type ammunition.
FR2717569B1 (en) * 1994-03-16 1996-05-10 Giat Ind Sa Device for igniting a propellant charge.
FR2763392B1 (en) * 1997-05-15 1999-06-11 Giat Ind Sa BOX FOR PROPULSIVE CHARGE
US20050016413A1 (en) * 2003-07-25 2005-01-27 Giat Industries Sub-calibred projectiles with multiple supports
US10508891B2 (en) * 2017-12-12 2019-12-17 Quint Gregory Tibeau Stoppage-inducing ammunition cartridge

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Also Published As

Publication number Publication date
DE69002402D1 (en) 1993-09-02
US5163165A (en) 1992-11-10
EP0401114B1 (en) 1993-07-28
FR2647890A1 (en) 1990-12-07
FR2647890B1 (en) 1994-04-22
DE69002402T2 (en) 1994-01-13

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