[go: up one dir, main page]

EP1728042A1 - Fragmentable grenade - Google Patents

Fragmentable grenade

Info

Publication number
EP1728042A1
EP1728042A1 EP05739413A EP05739413A EP1728042A1 EP 1728042 A1 EP1728042 A1 EP 1728042A1 EP 05739413 A EP05739413 A EP 05739413A EP 05739413 A EP05739413 A EP 05739413A EP 1728042 A1 EP1728042 A1 EP 1728042A1
Authority
EP
European Patent Office
Prior art keywords
projectiles
grenade
sheet
grenade according
web
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
EP05739413A
Other languages
German (de)
French (fr)
Other versions
EP1728042B1 (en
Inventor
Tanguy Catherine
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.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to PL05739413T priority Critical patent/PL1728042T3/en
Priority to SI200530120T priority patent/SI1728042T1/en
Publication of EP1728042A1 publication Critical patent/EP1728042A1/en
Application granted granted Critical
Publication of EP1728042B1 publication Critical patent/EP1728042B1/en
Priority to CY20071101632T priority patent/CY1107110T1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/32Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/22Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
    • F42B12/24Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction with grooves, recesses or other wall weakenings

Definitions

  • the present invention relates to an improvement to the grenades used, for example in conjunction with tear gas, for dispersing crowds.
  • International application WO 97/18435 discloses a pomegranate of this type, fragmentable into several projectiles of kinetic energy sufficiently weak not to cause serious injury to persons affected thereby.
  • This grenade has an inner sheath and nonmetallic projectiles individually secured to this sheath and surrounded by a heat-shrinkable envelope.
  • Such a grenade requires the unitary manufacture of the projectiles, then their assembly on the inner sheath, which has repercussions on the cost of manufacture.
  • the outer shell may hinder the dispersion of the projectiles.
  • the invention meets this need by proposing a new fragmentable grenade, comprising: an explosive charge, a sheet of elastically deformable projectiles interconnected by material bridges integrally molded with the projectiles, this sheet surrounding the charge and being configured to to allow, during the explosion of this one, the separation and the dispersion of the projectiles.
  • a new fragmentable grenade comprising: an explosive charge, a sheet of elastically deformable projectiles interconnected by material bridges integrally molded with the projectiles, this sheet surrounding the charge and being configured to to allow, during the explosion of this one, the separation and the dispersion of the projectiles.
  • the presence of the projectile sheet simplifies the manufacture of the grenade, since the projectiles do not have to be manufactured or assembled individually.
  • the sheet can still be used to optimize the volume of the grenade, that is to say, for the same external size to increase the mass of the projectiles, or mass projectiles equal, reduce the caliber of the grenade.
  • the sheet comprises two assembled edges, preferably by gluing.
  • the grenade can thus comprise half-projectiles assembled along an assembly line.
  • the projectiles thus reconstituted may have ballistic characteristics very similar to those of the other projectiles of the sheet, which are monohthical.
  • the material bridges may be located on the outside of the web.
  • the material bridges may be located on the inside of the web or elsewhere.
  • the thickness of the bridges of material may be chosen according to the mechanical characteristics of the material used to mold the sheet and may represent less than 10%, better less than 5% of the maximum thickness of the projectiles.
  • the projectile web may be devoid of openwork, or alternatively may include openings, including openings extending between the material bridges. The projectiles are advantageously devoid of sharp edges, so as to limit the risk of serious injury during impact.
  • the projectiles have radially inner and outer faces each at least partially substantially in the form of cylinder portions and, between them, substantially planar and radial faces.
  • the web defines an inner housing in which the explosive charge is placed.
  • the grenade may include a detonator and a device for retarding ignition.
  • the inner housing can house the detonator and the possible ignition retarder, which is sold in the trade under the name of "self-timer igniter plug" and can have a screw or clip interface for launching manual of the grenade if it is equipped with a lever equipped with a safety pin, ie the launching with a firearm, generally a rifle, if it is equipped with a cap of self-propulsion and d a percussion primer.
  • the inner housing may have at its axial ends enlarged portions, and one of them can receive at least partially the detonator.
  • the elastically deformable material in which the projectiles are made may have a hardness of, for example, between 20 and 55 Shore A, in particular between 35 and 45 Shore A, or even about 40 Shore A, and be for example FEPDM, or any another suitable elastomer, natural or synthetic.
  • the material used may optionally be supplemented with chemicals intended to improve the physical or chemical qualities, during manufacture or after.
  • the elastically deformable material may, for example, comprise a filler of a compound making it possible to reduce the coefficient of friction of the grenade, for example graphite or PTFE.
  • the elastically deformable material may also include, where appropriate, metal particles or not, a composite material or plastic.
  • the added particles may, for example, make it possible to increase or reduce the density of the projectiles, for example they may make it possible to reduce the elasticity of the elastically deformable material, which may, for example, make it easier to break the bridges of material during the explosion of the load, for example an elastically deformable material having particles having dynamic characteristics comparable to those of biological tissues may be used, for example using materials similar to those usually used for cosmetic surgery prostheses, or exhibiting
  • At least one projectile may contain an agent, for example a powder, a liquid or a gas, intended to produce a physiological effect, for example CS or capsicum, This agent may for example be contained, in particular at encapsulated state, in a cavity defined by at least one projectile.
  • the grenade can be configured to be launched with a grenade launcher.
  • its firing can be caused for example by the impact on the target or on the ground.
  • the firing can be linked to a pyrotechnic chain triggering the shot of the grenade launcher.
  • the grenade may further include, if necessary, a guide shoe or overscaling to improve the coefficient of friction and the rear seal.
  • a shoe can also be used to launch grenades of an undersized caliber with an existing grenade launcher, configured to launch grenades of a higher caliber.
  • the invention further relates, independently or in combination with the foregoing, to a method of manufacturing a projectile web comprising the following step: molding with an elastically deformable material, in particular a natural or synthetic elastomer, a projectile layer with between them material bridges bringing them together.
  • an elastically deformable material in particular a natural or synthetic elastomer
  • a projectile layer with between them material bridges bringing them together.
  • the projectile sheets can each be monolithic.
  • Each web may have been molded flat, being for example of generally rectangular shape, then rolled and glued edge to edge, the two edges before gluing each comprising for example a row of half-projectiles.
  • a projectile sheet used to make a grenade can be molded in one piece with an annular shape in an elastically deformable material, then demolded by its elasticity, for example by externally applying a pressure lower than the existing pressure on the inner side of the projectile sheet, or by applying internally an overpressure. If appropriate, whatever the molding process used, the web may be dipped in a bath of a compound to reduce the coefficient of friction of the pomegranate, for example PTFE or the like.
  • the invention also relates to a method of assembling a fragmentable grenade, comprising: providing a sheet of projectiles connected by material bridges integrally molded with the projectiles, - the placement of an explosive charge in an inner housing defined by the tablecloth.
  • FIG. perspective view, schematic and partial, of a fragmentable grenade according to the invention FIG. 2 represents in isolation and in perspective a sheet of projectiles used to manufacture the grenade of FIG. 1
  • FIG. 3 is a partial, schematic transverse section of the projectile sheet of FIG. 1
  • FIG. represents in isolation in longitudinal section the projectile layer of FIG. 1.
  • FIG. 1 shows a fragmentable grenade 1 comprising a sheet 4 of projectiles 5 interconnected by material bridges 6, integrally molded with the projectiles 5.
  • the sheet 4 surrounds an explosive charge 2, contained in a tube 3, and known per se.
  • the sheet 4 is configured to allow, during the explosion of the load 2, the separation and the dispersion of the projectiles 5.
  • FIG. 2 shows separately the sheet 4 of projectiles, on the inner side and 5.
  • the sheet 4 has, when flattened for the purposes of observation, a generally rectangular shape and comprises for example three rows of projectiles 5, each of which comprises five projectiles. 5 integers and two half projectiles 5a, 5b.
  • the grenade 1 comprises thus three stages of projectiles each comprising six projectiles distributed circumferentially, as can be seen in Figure 4, eighteen projectiles in total. Of course, it is not beyond the scope of the present invention when the grenade comprises a different number of projectiles, for example between twelve and twenty four projectiles.
  • the material bridges 6 are located on the outside of the grenade 1. Their thickness e represents in the example considered less than 5% of the maximum thickness E of the projectiles, in this case about 4% of the maximum thickness E , as can be seen in Figure 3.
  • each projectile 5 has in cross section, as illustrated in FIG. 3, radially outer 11 and inner 12 substantially concentric sides joined by substantially radial sides 13 and 14 converging towards the center of the grenade 1.
  • the grenade 1 is generally symmetrical with respect to planes containing its longitudinal axis X.
  • the sheet 4 defines an inner housing 15 in which the explosive charge 2 is placed.
  • This inner housing 15 has a first portion 15a, substantially cylindrical, of a first radius Ri, and in this first portion a second enlarged portion 15b, with two substantially cylindrical stages of respective radii R 'and R 2 with
  • the housing 15 further comprises a third enlarged portion 15c, substantially cylindrical, radius R 3 > R 1, intended for example to receive a ring for fixing the explosive charge 2 in the middle of the sheet 4 of projectiles 5.
  • the tube 3 s tightly adjusts in the housing 15, and the ply 4 by deforming elastically can contribute to retain the tube 3 in the grenade 1.
  • the ply 4 is made of an elastically deformable material, which is in the example described a hardness between 20 and 55 Shore A, especially between 35 and 45 Shore A, or even about 40 Shore A.
  • the material used is, for example, FEPDM.
  • the elastically deformable material may comprise a charge of a compound making it possible to reduce the coefficient of friction of the outside of the grenade, for example graphite or PTFE.
  • the elastically deformable material may comprise metal particles, made of composite material or plastic material.
  • At least one of the projectiles may contain an agent such as a powder, a gas or a liquid, intended to produce a physiological effect, in particular CS or capsicum.
  • the material bridges 6 connect the projectiles 5 without forming apertures, but it is not beyond the scope of the present invention when for example the bridges of material 6 define apertures which may for example facilitate the detachment of the projectiles 5 from each other during the explosion of the explosive charge.

Landscapes

  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Medicines That Contain Protein Lipid Enzymes And Other Medicines (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Materials For Medical Uses (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)
  • Catching Or Destruction (AREA)
  • Air Bags (AREA)
  • Breeding Of Plants And Reproduction By Means Of Culturing (AREA)
  • Toys (AREA)
  • Ultra Sonic Daignosis Equipment (AREA)
  • Bridges Or Land Bridges (AREA)
  • Steering Devices For Bicycles And Motorcycles (AREA)
  • Tires In General (AREA)
  • Peptides Or Proteins (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Tents Or Canopies (AREA)

Abstract

The invention relates to a fragmentable grenade ( 1 ) including an explosive charge ( 2 ) and a layer ( 4 ) of projectiles ( 5 ), which are elastically deformable and joined by bridges of material ( 6 ) produced by moulding together with the projectiles ( 5 ). The layer ( 4 ) surrounds the charge ( 2 ) and is designed for enabling the projectiles ( 5 ) to separate and disperse when the charge ( 2 ) explodes.

Description

Grenade fragmentable La présente invention concerne un perfectionnement aux grenades utilisées, par exemple conjointement à des gaz lacrymogènes, pour disperser des foules. On connaît par la demande internationale WO 97/18435 une grenade de ce type, fragmentable en plusieurs projectiles d'énergie cinétique suffisamment faible pour ne pas provoquer de blessures sérieuses aux personnes atteintes par ceux-ci. Cette grenade comporte une gaine intérieure et des projectiles non métalliques solidarisés individuellement à cette gaine et entourés d'une enveloppe thermorétractable. Une telle grenade nécessite la fabrication unitaire des projectiles, puis leur assemblage sur la gaine intérieure, ce qui se répercute sur le coût de fabrication. De plus, l'enveloppe extérieure peut gêner la dispersion des projectiles. Il existe un besoin pour disposer d'une grenade fragmentable plus simple et moins coûteuse à fabriquer. L'invention répond à ce besoin en proposant une nouvelle grenade fragmentable, comportant : une charge explosive, une nappe de projectiles élastiquement déformables reliés entre eux par des ponts de matière venus de moulage avec les projectiles, cette nappe entourant la charge et étant configurée pour permettre, lors de l'explosion de celle-ci, la séparation et la dispersion des projectiles. La présence de la nappe de projectiles permet de simplifier la fabrication de la grenade, puisque les projectiles n'ont plus à être fabriqués ni assemblés individuellement. The present invention relates to an improvement to the grenades used, for example in conjunction with tear gas, for dispersing crowds. International application WO 97/18435 discloses a pomegranate of this type, fragmentable into several projectiles of kinetic energy sufficiently weak not to cause serious injury to persons affected thereby. This grenade has an inner sheath and nonmetallic projectiles individually secured to this sheath and surrounded by a heat-shrinkable envelope. Such a grenade requires the unitary manufacture of the projectiles, then their assembly on the inner sheath, which has repercussions on the cost of manufacture. In addition, the outer shell may hinder the dispersion of the projectiles. There is a need to have a fragmentable grenade that is simpler and less expensive to manufacture. The invention meets this need by proposing a new fragmentable grenade, comprising: an explosive charge, a sheet of elastically deformable projectiles interconnected by material bridges integrally molded with the projectiles, this sheet surrounding the charge and being configured to to allow, during the explosion of this one, the separation and the dispersion of the projectiles. The presence of the projectile sheet simplifies the manufacture of the grenade, since the projectiles do not have to be manufactured or assembled individually.
La nappe peut encore permettre d'optimiser le volume de la grenade, c'est-à-dire pour un même encombrement extérieur d'augmenter la masse des projectiles, ou à masse des projectiles égale, de réduire le calibre de la grenade. Dans une réalisation particulière, la nappe comporte deux bords assemblés, de préférence par collage. La grenade peut ainsi comporter des demi-projectiles assemblés le long d'une ligne d'assemblage. Les projectiles ainsi reconstitués peuvent présenter des caractéristiques balistiques très proches de celles des autres projectiles de la nappe, qui sont monohthiques. Les ponts de matière peuvent être situés du côté extérieur de la nappe. Cela s'avère avantageux pour conférer à la grenade une surface extérieure relativement lisse sans avoir à recourir à une enveloppe thermorétractable rapportée, ce qui est utile notamment en cas d'éjection de la grenade par un lance-grenade. En variante, les ponts de matière peuvent être situés du côté intérieur de la nappe ou ailleurs. L'épaisseur des ponts de matière pourra être choisie en fonction des caractéristiques mécaniques du matériau utilisé pour mouler la nappe et pourra représenter moins de 10 %, mieux moins de 5 % de l'épaisseur maximale des projectiles. La nappe de projectile peut être dépourvue d' ajoure, ou en variante comporter des ajours, notamment des ajours s 'étendant entre les ponts de matière. Les projectiles sont avantageusement dépourvus d'arêtes vives, de manière à limiter le risque de lésions graves lors de l'impact. Dans un exemple de réalisation, les projectiles présentent des faces radialement intérieure et extérieure chacune au moins partiellement sensiblement en forme de portion de cylindre et, entre elles, des faces sensiblement planes et radiales. La nappe définit un logement intérieur dans lequel est placée la charge explosive. La grenade peut comporter un détonateur et un dispositif de retardement de l'allumage. Le logement intérieur peut loger le détonateur et l'éventuel dispositif de retardement de l'allumage, lequel est vendu dans le commerce sous le nom de « bouchon allumeur retardateur » et peut disposer d'une interface à vis ou à clip permettant soit le lancement manuel de la grenade s'il est muni d'un levier équipé d'une goupille de sécurité, soit le lancement avec une arme à feu, généralement un fusil, s'il est muni d'un bouchon d'auto-propulsion et d'une amorce à percussion. Le logement intérieur peut présenter à ses extrémités axiales des portions élargies, et l'une d'elles peut recevoir au moins partiellement le détonateur. Le matériau élastiquement déformable dans lequel les projectiles sont réalisés peut être d'une dureté comprise par exemple entre 20 et 55 Shore A, notamment entre 35 et 45 Shore A, voire de 40 Shore A environ, et être par exemple de FEPDM, ou tout autre élastomère convenable, naturel ou synthétique. Le matériau utilisé peut éventuellement être additionné de produits chimiques destinés à en améliorer les qualités physiques ou chimiques, pendant la fabrication ou après. Le matériau élastiquement déformable peut par exemple comporter une charge d'un composé permettant de <_taιinuer le coefficient de frottement de la grenade, par exemple du graphite ou du PTFE. Le matériau élastiquement déformable peut aussi comporter, le cas échéant, des particules métalliques ou non, en un matériau composite ou en matière plastique. Les particules ajoutées peuvent permettre par exemple d'augmenter ou de (iiniinuer la densité des projectiles. Elles peuvent permettre par exemple de réduire l'élasticité du matériau élastiquement déformable, ce qui peut permettre par exemple de faciliter la rupture des ponts de matière lors de l'explosion de la charge. On pourra par exemple utiliser un matériau élastiquement déformable comportant des particules ayant des caractéristiques dynamiques comparables à celles des tissus biologiques, en utilisant par exemple des matériaux similaires à ceux usuellement utilisés pour les prothèses de chirurgie esthétique, ou présentant des caractéristiques voisines. Au moins un projectile peut contenir un agent, par exemple une poudre, un liquide ou un gaz, destiné à produire un effet physiologique, par exemple du CS ou du capsicum. Cet agent peut par exemple être contenu, notamment à l'état encapsulé, dans une cavité définie par un projectile au moins. La grenade peut être configurée pour pouvoir être lancée à la main et présenter une taille adaptée à cet effet. En variante, la grenade peut être configurée pour être lancée avec un lance-grenade. Dans ce cas, sa mise à feu peut être provoquée par exemple par l'impact sur la cible ou sur le sol. En variante, la mise à feu peut être liée à une chaîne pyrotechnique de déclenchement du coup du lance-grenade. La grenade peut comporter en outre, le cas échéant, un sabot de guidage ou de surcalibrage destiné à améliorer le coefficient de frottement et l'étanchéité arrière. Un tel sabot peut également permettre de lancer des grenades d'un calibre sous-dimensionné avec un lance-grenade existant, configuré pour lancer des grenades d'un calibre supérieur. L'invention a encore pour objet, indépendamment ou en combinaison avec ce qui précède, un procédé de fabrication d'une nappe de projectiles comportant l'étape suivante : mouler avec un matériau élastiquement déformable, notamment un élastomère naturel ou synthétique, une nappe de projectiles avec entre eux des ponts de matière les réunissant. On peut notamment : - mouler en une seule fois une pluralité de nappes de projectiles avec entre eux des ponts de matière les réunissant dans un matériau élastiquement déformable, notamment un élastomère naturel ou synthétique, par exemple quatre nappes à la fois. Les nappes de projectiles peuvent chacune être monolithiques. Chaque nappe peut avoir été moulée à plat, étant par exemple de forme générale rectangulaire, puis roulée et collée bord à bord, les deux bords avant collage comportant par exemple chacun une rangée de demi-projectiles. Chaque nappe individuelle peut ainsi servir à la fabrication ultérieure d'une grenade. Une nappe de projectiles servant à fabriquer une grenade peut encore être moulée en un seul bloc avec une forme annulaire dans un matériau élastiquement déformable, puis démoulée grâce à son élasticité, par exemple en appliquant extérieurement une pression inférieure à la pression existant du côté intérieur de la nappe de projectiles, ou en appliquant intérieurement une surpression. Le cas échéant, quel que soit le procédé de moulage employé, la nappe peut être trempée dans un bain d'un composé permettant de diminuer le coefficient de frottement de la grenade, par exemple du PTFE ou analogue. L'invention a encore pour objet un procédé d'assemblage d'une grenade fragmentable, comportant : la fourniture d'une nappe de projectiles reliés par des ponts de matière venus de moulage avec les projectiles, - le placement d'une charge explosive dans un logement intérieur défini par la nappe. L'invention pourra être mieux comprise à la lecture de la description détaillée qui va suivre, d'un exemple de mise en œuvre non limitatif de celle-ci, et à l'examen du dessin annexé, sur lequel : la figure 1 est une vue en perspective, schématique et partielle, d'une grenade fragmentable conforme à l'invention, la figure 2 représente isolément et en perspective une nappe de projectiles servant à fabrication de la grenade de la figure 1, la figure 3 est une coupe transversale, partielle et schématique, de la nappe de projectiles de la figure 1, et - la figure 4 représente isolément en section longitudinale la nappe de projectiles de la figure 1. On a représenté à la figure 1 une grenade fragmentable 1 comportant une nappe 4 de projectiles 5 reliés entre eux par des ponts de matière 6, venus de moulage avec les projectiles 5. La nappe 4 entoure une charge explosive 2, contenue dans un tube 3, et connue en soi. La nappe 4 est configurée pour permettre, lors de l'explosion de la charge 2, la séparation et la dispersion des projectiles 5. Pour plus de clarté, on a représenté isolément à la figure 2 la nappe 4 de projectiles, du côté intérieur et après une déformation écartant les projectiles 5. Dans l'exemple considéré, la nappe 4 présente, lorsque mise à plat pour les besoins de l'observation, une forme générale rectangulaire et comporte par exemple trois rangées de projectiles 5, chacune desquelles comprenant cinq projectiles 5 entiers et deux demi-projectiles 5a, 5b. Ces derniers sont assemblés l'un à l'autre par collage le long d'une ligne d'assemblage A pour former le logement recevant le tube 3 contenant la charge 2, comme on peut le voir sur la figure 1. La grenade 1 comporte ainsi trois étages de projectiles 5 comportant chacun six projectiles répartis circonférentiellement, comme on peut le voir sur la figure 4, soit dix- huit projectiles au total. Bien entendu, on ne sort pas du cadre de la présente invention lorsque la grenade comporte un nombre différent de projectiles, par exemple entre douze et vingt quatre projectiles. Les ponts de matière 6 sont situés du côté extérieur de la grenade 1. Leur épaisseur e représente dans l'exemple considéré moins de 5 % de l'épaisseur maximale E des projectiles, en l'espèce environ 4 % de l'épaisseur maximale E, comme on peut le voir sur la figure 3. On voit également sur les figures 2 et 3 que les projectiles 5 comportent, dans les coins, des surfaces arrondies 7 permettant d'éviter qu'ils ne blessent gravement les personnes touchées. Chaque projectile 5 présente en section transversale, comme illustré à la figure 3, des côtés radialement extérieur 11 et intérieur 12 sensiblement concentriques, réunis par des côtés 13 et 14 sensiblement radiaux et convergents vers le centre de la grenade 1. Dans l'exemple considéré, une fois la nappe 4 assemblée, la grenade 1 est généralement symétrique par rapport à des plans contenant son axe longitudinal X. La nappe 4 définit un logement intérieur 15 dans lequel est placée la charge explosive 2. Ce logement intérieur 15 présente une première portion 15a, sensiblement cylindrique, d'un premier rayon Ri, et sous cette première portion une deuxième portion élargie 15b, avec deux étages sensiblement cylindriques de rayons respectifs R' et R2 avecThe sheet can still be used to optimize the volume of the grenade, that is to say, for the same external size to increase the mass of the projectiles, or mass projectiles equal, reduce the caliber of the grenade. In a particular embodiment, the sheet comprises two assembled edges, preferably by gluing. The grenade can thus comprise half-projectiles assembled along an assembly line. The projectiles thus reconstituted may have ballistic characteristics very similar to those of the other projectiles of the sheet, which are monohthical. The material bridges may be located on the outside of the web. This is advantageous for giving the pomegranate a relatively smooth outer surface without having to use a heat-shrinkable envelope reported, which is useful especially in case of ejection of the grenade by a grenade launcher. Alternatively, the material bridges may be located on the inside of the web or elsewhere. The thickness of the bridges of material may be chosen according to the mechanical characteristics of the material used to mold the sheet and may represent less than 10%, better less than 5% of the maximum thickness of the projectiles. The projectile web may be devoid of openwork, or alternatively may include openings, including openings extending between the material bridges. The projectiles are advantageously devoid of sharp edges, so as to limit the risk of serious injury during impact. In an exemplary embodiment, the projectiles have radially inner and outer faces each at least partially substantially in the form of cylinder portions and, between them, substantially planar and radial faces. The web defines an inner housing in which the explosive charge is placed. The grenade may include a detonator and a device for retarding ignition. The inner housing can house the detonator and the possible ignition retarder, which is sold in the trade under the name of "self-timer igniter plug" and can have a screw or clip interface for launching manual of the grenade if it is equipped with a lever equipped with a safety pin, ie the launching with a firearm, generally a rifle, if it is equipped with a cap of self-propulsion and d a percussion primer. The inner housing may have at its axial ends enlarged portions, and one of them can receive at least partially the detonator. The elastically deformable material in which the projectiles are made may have a hardness of, for example, between 20 and 55 Shore A, in particular between 35 and 45 Shore A, or even about 40 Shore A, and be for example FEPDM, or any another suitable elastomer, natural or synthetic. The material used may optionally be supplemented with chemicals intended to improve the physical or chemical qualities, during manufacture or after. The elastically deformable material may, for example, comprise a filler of a compound making it possible to reduce the coefficient of friction of the grenade, for example graphite or PTFE. The elastically deformable material may also include, where appropriate, metal particles or not, a composite material or plastic. The added particles may, for example, make it possible to increase or reduce the density of the projectiles, for example they may make it possible to reduce the elasticity of the elastically deformable material, which may, for example, make it easier to break the bridges of material during the explosion of the load, for example an elastically deformable material having particles having dynamic characteristics comparable to those of biological tissues may be used, for example using materials similar to those usually used for cosmetic surgery prostheses, or exhibiting At least one projectile may contain an agent, for example a powder, a liquid or a gas, intended to produce a physiological effect, for example CS or capsicum, This agent may for example be contained, in particular at encapsulated state, in a cavity defined by at least one projectile. have been configured to be hand-launched and have a size suitable for this purpose. Alternatively, the grenade can be configured to be launched with a grenade launcher. In this case, its firing can be caused for example by the impact on the target or on the ground. Alternatively, the firing can be linked to a pyrotechnic chain triggering the shot of the grenade launcher. The grenade may further include, if necessary, a guide shoe or overscaling to improve the coefficient of friction and the rear seal. Such a shoe can also be used to launch grenades of an undersized caliber with an existing grenade launcher, configured to launch grenades of a higher caliber. The invention further relates, independently or in combination with the foregoing, to a method of manufacturing a projectile web comprising the following step: molding with an elastically deformable material, in particular a natural or synthetic elastomer, a projectile layer with between them material bridges bringing them together. In particular, it is possible to: - mold a plurality of projectile layers at one time with material bridges joining them together in an elastically deformable material, in particular a natural or synthetic elastomer, for example four sheets at a time. The projectile sheets can each be monolithic. Each web may have been molded flat, being for example of generally rectangular shape, then rolled and glued edge to edge, the two edges before gluing each comprising for example a row of half-projectiles. Each individual tablecloth can thus be used for the subsequent manufacture of a grenade. A projectile sheet used to make a grenade can be molded in one piece with an annular shape in an elastically deformable material, then demolded by its elasticity, for example by externally applying a pressure lower than the existing pressure on the inner side of the projectile sheet, or by applying internally an overpressure. If appropriate, whatever the molding process used, the web may be dipped in a bath of a compound to reduce the coefficient of friction of the pomegranate, for example PTFE or the like. The invention also relates to a method of assembling a fragmentable grenade, comprising: providing a sheet of projectiles connected by material bridges integrally molded with the projectiles, - the placement of an explosive charge in an inner housing defined by the tablecloth. The invention may be better understood on reading the following detailed description of an example of non-limiting implementation thereof, and on examining the appended drawing, in which: FIG. perspective view, schematic and partial, of a fragmentable grenade according to the invention, FIG. 2 represents in isolation and in perspective a sheet of projectiles used to manufacture the grenade of FIG. 1, FIG. 3 is a partial, schematic transverse section of the projectile sheet of FIG. 1, and FIG. represents in isolation in longitudinal section the projectile layer of FIG. 1. FIG. 1 shows a fragmentable grenade 1 comprising a sheet 4 of projectiles 5 interconnected by material bridges 6, integrally molded with the projectiles 5. The sheet 4 surrounds an explosive charge 2, contained in a tube 3, and known per se. The sheet 4 is configured to allow, during the explosion of the load 2, the separation and the dispersion of the projectiles 5. For clarity, FIG. 2 shows separately the sheet 4 of projectiles, on the inner side and 5. In the example considered, the sheet 4 has, when flattened for the purposes of observation, a generally rectangular shape and comprises for example three rows of projectiles 5, each of which comprises five projectiles. 5 integers and two half projectiles 5a, 5b. These are assembled to one another by gluing along an assembly line A to form the housing receiving the tube 3 containing the load 2, as can be seen in FIG. 1. The grenade 1 comprises thus three stages of projectiles each comprising six projectiles distributed circumferentially, as can be seen in Figure 4, eighteen projectiles in total. Of course, it is not beyond the scope of the present invention when the grenade comprises a different number of projectiles, for example between twelve and twenty four projectiles. The material bridges 6 are located on the outside of the grenade 1. Their thickness e represents in the example considered less than 5% of the maximum thickness E of the projectiles, in this case about 4% of the maximum thickness E , as can be seen in Figure 3. It is also seen in Figures 2 and 3 that the projectiles 5 have, in the corners, rounded surfaces 7 to prevent they seriously hurt the affected people. Each projectile 5 has in cross section, as illustrated in FIG. 3, radially outer 11 and inner 12 substantially concentric sides joined by substantially radial sides 13 and 14 converging towards the center of the grenade 1. In the example considered once the sheet 4 has been assembled, the grenade 1 is generally symmetrical with respect to planes containing its longitudinal axis X. The sheet 4 defines an inner housing 15 in which the explosive charge 2 is placed. This inner housing 15 has a first portion 15a, substantially cylindrical, of a first radius Ri, and in this first portion a second enlarged portion 15b, with two substantially cylindrical stages of respective radii R 'and R 2 with
Rι< R'2 < R2, ce qui permet de loger par exemple le détonateur et un éventuel dispositif de retardement de l'allumage. Le logement 15 comporte encore supérieurement une troisième portion élargie 15c, sensiblement cylindrique, de rayon R3 > Ri, destinée par exemple à recevoir une couronne de fixation de la charge explosive 2 au milieu de la nappe 4 de projectiles 5. Le tube 3 s'ajuste étroitement dans le logement 15, et la nappe 4 en se déformant élastiquement peut contribuer à retenir le tube 3 dans la grenade 1. La nappe 4 est réalisée dans un matériau élastiquement déformable, qui est dans l'exemple décrit d'une dureté comprise entre 20 et 55 Shore A, notamment entre 35 et 45 Shore A, voire de 40 Shore A environ. Le matériau utilisé est par exemple de FEPDM. Le matériau élastiquement déformable peut comporter une charge d'un composé permettant de diminuer le coefficient de frottement de l'extérieur de la grenade, par exemple du graphite ou du PTFE. Le matériau élastiquement déformable peut comporter des particules métalliques, en matériau composite ou en matière plastique. Au moins l'un des projectiles peut contenir un agent tel qu'une poudre, un gaz ou un liquide, destiné à produire un effet physiologique, notamment du CS ou du capsicum. Dans ce qui vient d'être décrit, les ponts de matière 6 relient les projectiles 5 sans former d' ajours, mais on ne sort pas du cadre de la présente invention lorsque par exemple les ponts de matière 6 définissent des ajours qui peuvent par exemple faciliter le détachement des projectiles 5 les uns des autres lors de l'explosion de la charge explosive. Dans toute la description, y compris les revendications, l'expression « comportant un » doit être comprise comme étant synonyme de « comportant au moins un », sauf si le contraire est spécifié. Rι <R ' 2 <R 2 , which allows to house for example the detonator and a possible device for retarding ignition. The housing 15 further comprises a third enlarged portion 15c, substantially cylindrical, radius R 3 > R 1, intended for example to receive a ring for fixing the explosive charge 2 in the middle of the sheet 4 of projectiles 5. The tube 3 s tightly adjusts in the housing 15, and the ply 4 by deforming elastically can contribute to retain the tube 3 in the grenade 1. The ply 4 is made of an elastically deformable material, which is in the example described a hardness between 20 and 55 Shore A, especially between 35 and 45 Shore A, or even about 40 Shore A. The material used is, for example, FEPDM. The elastically deformable material may comprise a charge of a compound making it possible to reduce the coefficient of friction of the outside of the grenade, for example graphite or PTFE. The elastically deformable material may comprise metal particles, made of composite material or plastic material. At least one of the projectiles may contain an agent such as a powder, a gas or a liquid, intended to produce a physiological effect, in particular CS or capsicum. In what has just been described, the material bridges 6 connect the projectiles 5 without forming apertures, but it is not beyond the scope of the present invention when for example the bridges of material 6 define apertures which may for example facilitate the detachment of the projectiles 5 from each other during the explosion of the explosive charge. Throughout the description, including the claims, the phrase "having one" should be understood as being synonymous with "having at least one", unless the opposite is specified.

Claims

REVENDICATIONS
1. Grenade fragmentable (1), comportant : une charge explosive (2), - une nappe (4) de projectiles (5) élastiquement déformables reliés par des ponts de matière (6) venus de moulage avec les projectiles (5), cette nappe (4) entourant la charge (2) et étant configurée pour permettre, lors de l'explosion de la charge (2), la séparation et la dispersion des projectiles (5). 1. fragmentable grenade (1), comprising: an explosive charge (2), - a sheet (4) of projectiles (5) elastically deformable connected by material bridges (6) integrally molded with the projectiles (5), this web (4) surrounding the load (2) and being configured to allow, during the explosion of the load (2), the separation and dispersion of the projectiles (5).
2. Grenade selon la revendication précédente, caractérisée par le fait que la nappe (4) comporte des demi-projectiles (5a, 5b) assemblés le long d'une ligne d'assemblage (A), notamment par collage. 2. Grenade according to the preceding claim, characterized in that the web (4) comprises half-projectiles (5a, 5b) assembled along an assembly line (A), in particular by gluing.
3. Grenade selon l'une des revendications précédentes, caractérisée par le fait que les ponts de matière (6) sont situés du côté extérieur de la nappe (4). 3. Grenade according to one of the preceding claims, characterized in that the material bridges (6) are located on the outside of the web (4).
4. Grenade selon l'une quelconque des revendications précédentes, caractérisée par le fait que l'épaisseur (e) des ponts de matière (6) représente moins de4. Grenade according to any one of the preceding claims, characterized in that the thickness (e) of the bridges of material (6) represents less than
10 %, mieux moins de 5 % de l'épaisseur maximale (E) des projectiles. 10%, better less than 5% of the maximum thickness (E) of the projectiles.
5. Grenade selon l'une quelconque des revendications précédentes, caractérisée par le fait que les projectiles (5) sont dépourvus d'arêtes vives. 5. Grenade according to any one of the preceding claims, characterized in that the projectiles (5) are devoid of sharp edges.
6. Grenade selon l'une quelconque des revendications précédentes, caractérisée par le fait que les projectiles (5) présentent des faces radialement intérieure et extérieure chacune au moins partiellement sensiblement en forme de portion de cylindre et, entre elles, des faces sensiblement planes et radiales. 6. Grenade according to any one of the preceding claims, characterized in that the projectiles (5) have radially inner and outer faces each at least partially substantially cylinder-shaped portion and, between them, substantially flat faces and radials.
7. Grenade selon l'une quelconque des revendications précédentes, caractérisée par le fait que les projectiles (5) définissent un logement intérieur (15) dans lequel est placée la charge (2). 7. Grenade according to any one of the preceding claims, characterized in that the projectiles (5) define an inner housing (15) in which the load (2) is placed.
8. Grenade selon la revendication précédente, caractérisée par le fait que le logement intérieur (15) présente deux portions élargies (15b, 15c) à ses extrémités axiales. 8. Grenade according to the preceding claim, characterized in that the inner housing (15) has two enlarged portions (15b, 15c) at its axial ends.
9. Grenade selon l'une quelconque des revendications précédentes, caractérisée par le fait que le matériau élastiquement déformable dans lequel les projectiles sont réalisés est d'une dureté comprise entre 20 et 55 Shore A, notamment entre 35 et 45 Shore A, voire de 40 Shore A environ. 9. Grenade according to any one of the preceding claims, characterized in that the elastically deformable material in which the projectiles are made has a hardness of between 20 and 55 Shore A, in particular between 35 and 45 Shore A, or even 40 Shore A approx.
10. Grenade selon l'une quelconque des revendications précédentes, caractérisée par le fait qu'elle est dépourvue d'enveloppe extérieure. 10. Grenade according to any one of the preceding claims, characterized in that it is devoid of outer casing.
11. Procédé d'assemblage d'une grenade fragmentable, comportant les étapes suivantes : - fournir une nappe (4) de projectiles (5) reliés par des ponts de matière (6) venus de moulage avec les projectiles, - placer une charge explosive (2) dans un logement intérieur défini par la nappe. 11. A method of assembling a fragmentable grenade, comprising the following steps: - providing a sheet (4) of projectiles (5) connected by material bridges (6) integrally molded with the projectiles, - placing an explosive charge (2) in an inner housing defined by the web.
12. Procédé de fabrication d'une nappe de projectiles, comportant les étapes suivantes : mouler avec un matériau élastiquement déformable, notamment un élastomère naturel ou synthétique, une nappe (4) de projectiles (5) avec entre eux des ponts de matière (6) les réunissant. 12. A method of manufacturing a projectile sheet, comprising the following steps: molding with an elastically deformable material, in particular a natural or synthetic elastomer, a sheet (4) of projectiles (5) with between them material bridges (6). ) bringing them together.
13. Procédé selon la revendication précédente, comportant l'étape suivante : la nappe ayant été moulée avec une forme annulaire, démouler la nappe grâce à son élasticité en appliquant extérieurement une pression inférieure à la pression existant du côté intérieur de la nappe de projectiles, ou en appliquant intérieurement une surpression. 13. The method as claimed in the preceding claim, comprising the following step: the sheet having been molded with an annular shape, demolding the sheet by virtue of its elasticity by externally applying a pressure lower than the pressure existing on the inner side of the sheet of projectiles, or by applying internally an overpressure.
14. Procédé selon l'une des deux revendications précédentes, caractérisé par le fait qu'on trempe la nappe (4) dans un bain d'un composé permettant de diminuer le coefficient de frottement de la grenade. 14. Method according to one of the two preceding claims, characterized in that the quilt (4) is quenched in a bath of a compound to reduce the coefficient of friction of the grenade.
EP05739413A 2004-03-16 2005-03-11 Fragmentable grenade Expired - Lifetime EP1728042B1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
PL05739413T PL1728042T3 (en) 2004-03-16 2005-03-11 Fragmentable grenade
SI200530120T SI1728042T1 (en) 2004-03-16 2005-03-11 Fragmentable grenade
CY20071101632T CY1107110T1 (en) 2004-03-16 2007-12-27 BREAKFAST HANDBALL

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0450527A FR2867849B1 (en) 2004-03-16 2004-03-16 FRAGMENTABLE GRENAGE
PCT/FR2005/050157 WO2005093364A1 (en) 2004-03-16 2005-03-11 Fragmentable grenade

Publications (2)

Publication Number Publication Date
EP1728042A1 true EP1728042A1 (en) 2006-12-06
EP1728042B1 EP1728042B1 (en) 2007-09-26

Family

ID=34896785

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05739413A Expired - Lifetime EP1728042B1 (en) 2004-03-16 2005-03-11 Fragmentable grenade

Country Status (13)

Country Link
US (1) US20080156220A1 (en)
EP (1) EP1728042B1 (en)
AT (1) ATE374353T1 (en)
BR (1) BRPI0508827A (en)
CA (1) CA2559884A1 (en)
CY (1) CY1107110T1 (en)
DE (1) DE602005002639T2 (en)
DK (1) DK1728042T3 (en)
ES (1) ES2296168T3 (en)
FR (1) FR2867849B1 (en)
PL (1) PL1728042T3 (en)
PT (1) PT1728042E (en)
WO (1) WO2005093364A1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2915794B1 (en) * 2007-05-02 2009-07-24 Davey Bickford Snc FRAGMENTATION GRENADE AND METHOD FOR MANUFACTURING A PROJECTILE ASSEMBLY
FR2923004B1 (en) * 2007-10-26 2009-12-04 Applic Des Procedes Lefebvre S FRAGMENTABLE GRENADE IN PROJECTILES OF LOW KINETIC ENERGY.
US9016888B2 (en) * 2008-09-19 2015-04-28 Jersey Tactical Corp. Non combustible, tactical flash device
FR2965910B1 (en) 2010-10-08 2012-11-02 Armement Et D Etudes Alsetex Soc D NON-LETHAL GRENADE
FR2980567B1 (en) * 2011-09-23 2015-09-04 Applic Des Procedes Lefebvre Soc D GRENADE OF MAINTENANCE OF THE ORDER
FR2989457B1 (en) 2012-04-12 2017-03-17 Soc D'armement Et D'etudes Alsetex NON-LETHAL FLAKE GRENADE COMPRISING MEANS FOR MAINTAINING IGNITION PLUG
RU2503920C1 (en) * 2012-12-14 2014-01-10 Открытое акционерное общество "Научно-производственное объединение "Прибор" Fragmentation grenade
WO2016100594A1 (en) * 2014-12-18 2016-06-23 Raytheon Company Explosive device with casing having voids therein
US11054230B1 (en) * 2018-06-14 2021-07-06 The United States Of America As Represented By The Secretary Of The Navy Flexible anti-personnel mine
FR3086746B1 (en) * 2018-10-01 2020-08-28 Nexter Munitions ENVELOPE FOR AMMUNITION AND AMMUNITION INCORPORATING SUCH AN ENVELOPE
US12203732B2 (en) * 2019-09-12 2025-01-21 Carl Salmon Grenade with independently detachable carpel segments
US11300392B1 (en) * 2020-12-21 2022-04-12 Attila G. Zoltan A.Z.G. TRI grenade
DE102022002278A1 (en) 2022-06-23 2023-12-28 Diehl Defence Gmbh & Co. Kg Active body with predetermined breaking points for projectiles

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2564751A (en) * 1945-05-19 1951-08-21 Lawrence H Cook Grenade
US3298308A (en) * 1960-11-11 1967-01-17 Aerojet General Co Composite casing for fragmentationtype explosive weapon and method of forming same
US3263612A (en) * 1961-02-10 1966-08-02 Aerojet General Co Fragmentation type weapon
US4057001A (en) * 1968-04-01 1977-11-08 Martin Marietta Corporation Endless carrier sleeve for discrete fragments
US3580175A (en) * 1968-09-19 1971-05-25 Gerity Schultz Corp Fragmentation explosive device
US4493264A (en) * 1982-12-27 1985-01-15 The United States Of America As Represented By The Secretary Of The Army Elastic fragmentation sleeve
EP0200856B1 (en) * 1985-03-04 1988-09-21 Oregon Etablissement Für Patentverwertung Grenade body, especially for hand grenades
AT387281B (en) * 1985-04-01 1988-12-27 Oregon Ets Patentverwertung SPLITTER BODY FOR GRENADES, ESPECIALLY HAND GRENADES
US4942820A (en) * 1988-11-14 1990-07-24 Sawruk Stephen D Fragmentation device
US5313890A (en) * 1991-04-29 1994-05-24 Hughes Missile Systems Company Fragmentation warhead device
FR2741436B1 (en) * 1995-11-16 1998-01-30 Applic Des Procedes Lefebvre S FRAGMENTABLE GRENADE IN LOW CINETIC ENERGY PROJECTILES

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2005093364A1 *

Also Published As

Publication number Publication date
DK1728042T3 (en) 2008-02-11
DE602005002639T2 (en) 2008-06-19
ATE374353T1 (en) 2007-10-15
FR2867849B1 (en) 2006-07-21
WO2005093364A1 (en) 2005-10-06
DE602005002639D1 (en) 2007-11-08
CA2559884A1 (en) 2005-10-06
PT1728042E (en) 2008-01-09
BRPI0508827A (en) 2007-08-14
PL1728042T3 (en) 2008-03-31
CY1107110T1 (en) 2012-10-24
EP1728042B1 (en) 2007-09-26
ES2296168T3 (en) 2008-04-16
US20080156220A1 (en) 2008-07-03
FR2867849A1 (en) 2005-09-23

Similar Documents

Publication Publication Date Title
EP1728042B1 (en) Fragmentable grenade
CA2145950C (en) Projectile, especially a non-lethal bullet
EP2297545B1 (en) Non-lethal munition
EP0655603B1 (en) Ammunition comprising projectiles connected to each other by means of flexible filaments
EP3818324B1 (en) Biodegradable wadding cup for a shotgun cartridge
WO1997049969A1 (en) Non-lethal projectile
FR2487063A1 (en) BOURRE AND PROJECTILE FOR CARTRIDGE OF HUNTING RIFLE
EP3303983B1 (en) Kinetic and/or incapacitating projectile having high energy absorption
FR2533309A1 (en) IMPROVED PROJECTILE WITH MULTIPLE POSSIBILITIES AND METHODS OF MAKING THE PROJECTILE
EP0407288B1 (en) Training projectile for an automatically or hand-operated firearm
FR2705772A1 (en) Exercise projectile.
EP0728293B1 (en) Close range dual penetration bullet for hunting
EP0664877B1 (en) Sabot with controlled separation of segments for sub-calibre projectiles
EP2650637B1 (en) Nonlethal fragmentation grenade comprising means to hold the igniter plug
EP0268535B1 (en) Slipping obturator ring for projectiles of all calibres
EP2439483B1 (en) Grenade with non-lethal shrapnel
WO2008148983A2 (en) Fragmentation grenade and method for making a set of projectiles
CA2176029C (en) Close range dual penetration bullet for hunting
EP3022519B1 (en) Projectile, in particular ammunition, for a defense launcher
EP1586852A1 (en) Caseless ammuniton and manufacturing method of such an ammunition
FR2711780A1 (en) Cylinder for training in the firing of a revolver and corresponding ogive
FR2712686A1 (en) Propulsion/ignition unit, esp. for tear-gas grenade
FR2791421A1 (en) Hand gun assembly for the firing of deformable projectiles for the non-lethal neutralization of threats and aggressors
WO1999019685A1 (en) Launcher with enhanced tightness for ammunitions comprising a launcher associated with a sub-projectile

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20061016

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

DAX Request for extension of the european patent (deleted)
GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REF Corresponds to:

Ref document number: 602005002639

Country of ref document: DE

Date of ref document: 20071108

Kind code of ref document: P

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: RO

Ref legal event code: EPE

REG Reference to a national code

Ref country code: PT

Ref legal event code: SC4A

Free format text: AVAILABILITY OF NATIONAL TRANSLATION

Effective date: 20071226

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

REG Reference to a national code

Ref country code: GR

Ref legal event code: EP

Ref document number: 20070403846

Country of ref document: GR

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20080113

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: A. BRAUN, BRAUN, HERITIER, ESCHMANN AG PATENTANWAE

REG Reference to a national code

Ref country code: PL

Ref legal event code: T3

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2296168

Country of ref document: ES

Kind code of ref document: T3

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DK

Payment date: 20080326

Year of fee payment: 4

Ref country code: ES

Payment date: 20080130

Year of fee payment: 4

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BG

Payment date: 20080128

Year of fee payment: 4

Ref country code: CZ

Payment date: 20080208

Year of fee payment: 4

Ref country code: EE

Payment date: 20080128

Year of fee payment: 4

Ref country code: FI

Payment date: 20080220

Year of fee payment: 4

Ref country code: IE

Payment date: 20080227

Year of fee payment: 4

Ref country code: LT

Payment date: 20080220

Year of fee payment: 4

Ref country code: LU

Payment date: 20080205

Year of fee payment: 4

Ref country code: MC

Payment date: 20080129

Year of fee payment: 4

Ref country code: PL

Payment date: 20080130

Year of fee payment: 4

Ref country code: PT

Payment date: 20080129

Year of fee payment: 4

Ref country code: SE

Payment date: 20080318

Year of fee payment: 4

Ref country code: SI

Payment date: 20080128

Year of fee payment: 4

Ref country code: SK

Payment date: 20080226

Year of fee payment: 4

REG Reference to a national code

Ref country code: CH

Ref legal event code: PFA

Owner name: CATHERINE, TANGUY

Free format text: CATHERINE, TANGUY#9 RUE DU GATINAIS#77570 CHATEAU LANDON (FR) -TRANSFER TO- CATHERINE, TANGUY#9 RUE DU GATINAIS#77570 CHATEAU LANDON (FR)

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: RO

Payment date: 20080229

Year of fee payment: 4

Ref country code: CY

Payment date: 20080214

Year of fee payment: 4

Ref country code: AT

Payment date: 20080307

Year of fee payment: 4

REG Reference to a national code

Ref country code: HU

Ref legal event code: AG4A

Ref document number: E003090

Country of ref document: HU

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20080528

Year of fee payment: 4

Ref country code: FR

Payment date: 20080125

Year of fee payment: 4

Ref country code: HU

Payment date: 20080228

Year of fee payment: 4

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20080131

Year of fee payment: 4

26N No opposition filed

Effective date: 20080627

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20080122

Year of fee payment: 4

REG Reference to a national code

Ref country code: PT

Ref legal event code: MM4A

Free format text: LAPSE DUE TO NON-PAYMENT OF FEES

Effective date: 20090911

BERE Be: lapsed

Owner name: CATHERINE, TANGUY

Effective date: 20090331

LTLA Lt: lapse of european patent or patent extension

Effective date: 20090311

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: CZ

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: FI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

Ref country code: PT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090911

Ref country code: LT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

EUG Se: european patent has lapsed
GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20090311

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20091001

REG Reference to a national code

Ref country code: EE

Ref legal event code: MM4A

Ref document number: E001869

Country of ref document: EE

Effective date: 20090331

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20091130

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

REG Reference to a national code

Ref country code: SI

Ref legal event code: KO00

Effective date: 20091029

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

Ref country code: EE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

Ref country code: HU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090312

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20091001

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20091001

Ref country code: SK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: SI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090312

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

Ref country code: DK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20091123

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IS

Payment date: 20100215

Year of fee payment: 6

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20090312

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20091002

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090312

REG Reference to a national code

Ref country code: PL

Ref legal event code: LAPE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090312

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20080331

Year of fee payment: 4

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111001

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090311