EP3114424B1 - Decoy cartridge for aircraft - Google Patents

Decoy cartridge for aircraft Download PDF

Info

Publication number
EP3114424B1
EP3114424B1 EP15715684.5A EP15715684A EP3114424B1 EP 3114424 B1 EP3114424 B1 EP 3114424B1 EP 15715684 A EP15715684 A EP 15715684A EP 3114424 B1 EP3114424 B1 EP 3114424B1
Authority
EP
European Patent Office
Prior art keywords
sheath
envelope
plug
composition
pyrotechnic
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.)
Active
Application number
EP15715684.5A
Other languages
German (de)
French (fr)
Other versions
EP3114424A1 (en
Inventor
Thierry SECCO
Cyril LEOQUET
Marc Pignol
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.)
Etienne LaCroix Tous Artifices SA
Original Assignee
Etienne LaCroix Tous Artifices SA
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 Etienne LaCroix Tous Artifices SA filed Critical Etienne LaCroix Tous Artifices SA
Publication of EP3114424A1 publication Critical patent/EP3114424A1/en
Application granted granted Critical
Publication of EP3114424B1 publication Critical patent/EP3114424B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J2/00Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic or acoustic waves
    • F41J2/02Active targets transmitting infrared radiation
    • 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
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/70Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies for dispensing radar chaff or infrared material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B4/00Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
    • F42B4/26Flares; Torches
    • 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
    • F42B5/145Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances
    • F42B5/15Cartridges, i.e. cases with charge and missile for dispensing gases, vapours, powders, particles or chemically-reactive substances for creating a screening or decoy effect, e.g. using radar chaff or infrared material

Description

La présente invention concerne le domaine des leurres, notamment pour la protection des aéronefs, tels qu'avions et/ou hélicoptères.The present invention relates to the field of lures, in particular for the protection of aircraft, such as aircraft and / or helicopters.

Différents dispositifs destinés à former des leurres, notamment dans le domaine infrarouge ont déjà été proposés. On trouvera des exemples de dispositifs connus dans les documents GB 2 300 035 , DE 100 65 816 , DE 34 43 778 et US 2 868 129 . Le document GB 2300035 forme un point de départ pour le préambule de la revendication indépendante 1.Various devices for forming lures, especially in the infrared range have already been proposed. Examples of known devices can be found in the documents GB 2,300,035 , DE 100 65 816 , DE 34 43 778 and US 2,868,129 . The document GB 2300035 forms a starting point for the preamble of independent claim 1.

Les documents précités décrivent des systèmes comprenant une gaine en matière plastique qui loge une charge destinée à former leurre. Les moyens décrits dans les documents précités à base d'une gaine en matière plastique pour contenir la charge, ont cependant globalement été abandonnés ces derniers temps au profit d'une solution très différente de confinement de la charge à base d'un film, le plus souvent en aluminium, enroulé sur la charge. Comme on le verra par la suite l'utilisation d'un film en aluminium enroulé sur la charge a en effet été considérée comme offrant des avantages.The aforementioned documents describe systems comprising a plastic sheath which houses a charge intended to form a lure. The means described in the aforementioned documents based on a plastic sheath for containing the load, however, have generally been abandoned in recent times in favor of a very different solution for confining the film-based filler, the more often aluminum, wound on the load. As will be seen later the use of an aluminum film wound on the load has indeed been considered to offer advantages.

Dans toutes les architectures des cartouches de leurrage air de différents calibres et formes (rond, carré, rectangulaire), destinées à équiper et protéger les avions et les hélicoptères contre des missiles à autodirecteur infrarouge, on trouve ainsi aujourd'hui une enveloppe adhésive en papier tramé ou aluminium, plié et entourant un corps de radiation (composition pyrotechnique infrarouge comprimée appelée aussi « bloc infrarouge ») contribuant à l'allumage et la mise en régime de celui-ci.In all architectures of air decoy cartridges of different calibers and shapes (round, square, rectangular), designed to equip and protect planes and helicopters against missiles with infrared homing, we find today an adhesive paper envelope wafer or aluminum, folded and surrounding a body of radiation (compressed infrared pyrotechnic composition also called "infrared block") contributing to the ignition and the setting regime thereof.

La présente invention a pour objectif de perfectionner les dispositifs connus du type illustré sur la figure 1 annexée.The present invention aims to improve the known devices of the type illustrated on the figure 1 attached.

On a en effet proposé et utilisé depuis de nombreuses années des dispositifs formant leurre par émission d'un rayonnement infrarouge conformes à la figure 1 annexée.For many years, lure-emitting devices have been proposed and used for emitting infrared radiation in accordance with the figure 1 attached.

On aperçoit sur la figure 1 une cartouche comprenant deux parties principales : un ensemble 10 comprenant une douille 11 et un impulseur 12, d'une part, et un ensemble 20 destiné à être éjecté, d'autre part.We can see on the figure 1 a cartridge comprising two main parts: an assembly 10 comprising a sleeve 11 and a impeller 12, on the one hand, and an assembly 20 intended to be ejected, on the other hand.

L'ensemble formé de la douille 11 et de l'impulseur 12 est conçu pour être rendu solidaire d'un chargeur lui-même intégré à un lanceur.The assembly formed of the sleeve 11 and the impeller 12 is designed to be secured to a loader itself integrated with a launcher.

L'ensemble 10 reste dans le chargeur après tir.Set 10 remains in the magazine after firing.

L'ensemble éjecté 20 comprend :

  • un ensemble 21 formant corps de radiation (bloc infrarouge),
  • un ensemble 22 formant partie pyrotechnique équipé d'une charge d'allumage 23 et d'un tiroir de sécurité 24 intégrant un doigt d'armement assurant une rupture de chaîne pyrotechnique tant que l'ensemble éjecté 20 n'est pas sortie de la douille 11.
  • un couvercle de fermeture 25 placé à l'avant du bloc infrarouge 21, et
  • une enveloppe 26 adhésive en papier tramé ou aluminium pliée pour entourer le bloc infrarouge 21 et assurer également une liaison mécanique et étanche avec l'ensemble partie pyrotechnique 22 et le couvercle de fermeture 25.
The ejected assembly 20 comprises:
  • a set 21 forming a body of radiation (infrared block),
  • an assembly 22 forming a pyrotechnic part equipped with an ignition charge 23 and a safety slide 24 integrating an arming finger ensuring a pyrotechnic chain break until the ejected assembly 20 is out of the socket 11.
  • a closure cover 25 placed at the front of the infrared block 21, and
  • an envelope 26 of folded aluminum paper or folded to surround the infrared block 21 and also provide a mechanical and sealed connection with the pyrotechnic assembly 22 and the closure cover 25.

Le dispositif illustré sur la figure 1 fonctionne comme suit :The device illustrated on the figure 1 works as follows:

La mise à feu de l'impulseur 12 entraîne l'éjection de l'ensemble éjecté 20 hors de la douille 11 et l'initiation de la charge d'allumage 23 de l'ensemble partie pyrotechnique 22.The ignition of the impeller 12 causes the ejection 20 to be ejected from the socket 11 and the initiation of the ignition charge 23 of the pyrotechnic unit 22.

Une fois l'ensemble éjecté 20 complètement sorti de la douille 11, le tiroir de sécurité 24 se libère (il n'y a plus de rupture de chaîne pyrotechnique) et ainsi la charge d'allumage 23 peut initier le bloc infrarouge 21.Once the ejected assembly 20 is completely out of the socket 11, the safety slide 24 is released (there is no longer a pyrotechnic chain break) and thus the ignition charge 23 can initiate the infrared block 21.

L'enveloppe adhésive 26 en papier tramé ou aluminium confine le bloc 21 pour assurer une mise en régime et une mise en pression du bloc infrarouge 21.The adhesive envelope 26 made of ruled paper or aluminum confines the block 21 to ensure that the infrared block 21 is put into operation and put under pressure.

L'enveloppe adhésive 26 en papier tramé ou aluminium se déchire ou se disloque à la fin de la mise en régime.The adhesive envelope 26 of screen paper or aluminum tears or dislocates at the end of the startup.

Le corps de radiation 21 peut ainsi rayonner et émettre une signature infrarouge simulant celle des avions ou hélicoptères.The radiation body 21 can thus radiate and emit an infrared signature simulating that of airplanes or helicopters.

L'utilisation d'une enveloppe 26 formée d'un papier en aluminium permet d'adapter la répartition de l'enveloppe sur le corps de radiation, par exemple en cumulant localement si on le désire plusieurs couches de papier, pour moduler le confinement du corps de radiation et permet donc une bonne reproductibilité des courbes de rayonnement recherchéesThe use of an envelope 26 formed of an aluminum paper makes it possible to adapt the distribution of the envelope on the body of radiation, for example by locally combining, if desired, several layers of paper, to modulate the confinement of the radiation body and thus allows good reproducibility of the desired radiation curves

Il a été constaté par ailleurs que la réalisation de l'enveloppe 26 en papier d'aluminium permet une déchirure facile lors de la mise en oeuvre, pour laisser le corps de radiation visible.It has also been found that the realization of the envelope 26 of aluminum foil allows easy tearing during the implementation, to leave the radiation body visible.

Cependant jusqu'à ce jour il s'est avéré nécessaire de procéder manuellement à l'enroulement du papier d'aluminium formant l'enveloppe sur le corps de radiation, en raison d'une part de la nature du corps de radiation concerné, pour éviter tout risque d'initiation intempestive à la fabrication, et d'autre part pour garantir une application parfaite de l'enveloppe sur l'intégralité de la surface du corps de radiation afin d'éviter une initiation par l'extérieur du corps de radiation bien que tiroir 24 soit toujours en position de sécurité.However, until today, it has been necessary to manually wind the aluminum foil forming the envelope on the radiation body, partly because of the nature of the radiation body in question. avoid any risk of inadvertent initiation to manufacture, and secondly to ensure a perfect application of the envelope on the entire surface of the body of radiation to prevent initiation from outside the body of radiation although drawer 24 is always in the safety position.

De fait la moindre déchirure à la fabrication, dans l'enveloppe 26, est susceptible de conduire à un allumage du corps de radiation, par l'extérieur, à travers une telle déchirure, même si l'ensemble 20 devant être éjecté est toujours dans la douille 11, en position de sécurité du tiroir 24.In fact, the slightest tear in the manufacturing process, in the envelope 26, is likely to lead to an ignition of the radiation body, from the outside, through such a tear, even if the assembly 20 to be ejected is still in the bushing 11, in the safety position of the drawer 24.

L'enroulement manuel du papier d'aluminium permet un contrôle visuel de la qualité de l'enroulement.The manual winding of the aluminum foil allows a visual check of the quality of the winding.

Cependant l'on ne peut totalement exclure le risque de déchirure de l'enveloppe lorsque l'ensemble 20 est engagé dans la douille 11.However, the risk of tearing of the envelope when the assembly 20 is engaged in the sleeve 11 can not be totally excluded.

Dans ce contexte la présente invention a en particulier pour objectif

  • d'améliorer la maîtrise de la reproductibilité de la mise en régime du pain,
  • d'améliorer la robustesse de la conception en terme sécuritaire, et
  • de réduire significativement les coûts de production.
In this context, the present invention particularly aims at
  • to improve the control of the reproducibility of the setting in regime of the bread,
  • to improve the robustness of the design in terms of security, and
  • significantly reduce production costs.

Ces buts sont atteints selon l'invention grâce à un dispositif formant leurre infrarouge selon la revendication indépendante 1, le dispositif comprenant :

  • une partie pyrotechnique d'amorçage,
  • une composition adaptée pour émettre un rayonnement dans le domaine infrarouge, et
  • une enveloppe de protection de la composition, formée d'une gaine en matière plastique,
l'un au moins d'un corps de partie pyrotechnique d'initiation et/ou d'un bouchon d'obturation de la gaine possédant une gorge annulaire qui débouche sur sa périphérie extérieure, caractérisé en ce que la gorge annulaire communique avec au moins un canal longitudinal lequel débouche sur une extrémité du corps ou du bouchon pour recevoir un ruban de colle polymérisable assurant le collage du corps et/ou du bouchon sur la gaine.These objects are achieved according to the invention by means of an infrared lure device according to independent claim 1, the device comprising:
  • a pyrotechnic priming part,
  • a composition adapted to emit radiation in the infrared range, and
  • a protective cover of the composition, formed of a plastic sheath,
at least one of a pyrotechnic initiation body and / or a plug of the sheath having an annular groove which opens out at its outer periphery, characterized in that the annular groove communicates with at least one a longitudinal channel which opens on one end of the body or plug to receive a polymerizable adhesive tape ensuring the bonding of the body and / or plug on the sheath.

L'enveloppe est de préférence, une enveloppe rigide profilée formée par extrusion.The casing is preferably a shaped rigid casing formed by extrusion.

D'autres caractéristiques, buts et avantages de la présente invention apparaîtront à la lecture de la description détaillée qui va suivre et au regard des dessins annexés donnés à titre d'exemple non limitatifs et sur lesquels :

  • la figure 1 représente une vue en coupe éclatée d'un dispositif conforme à l'état de la technique,
  • la figure 2 représente une vue générale en perspective avant l'assemblage d'un premier mode de réalisation conforme à la présente invention,
  • la figure 3 représente une vue générale similaire en perspective avant l'assemblage d'un second mode de réalisation conforme à la présente invention,
  • la figure 4 représente une vue générale similaire en perspective avant l'assemblage d'un troisième mode de réalisation conforme à la présente invention,
  • la figure 5 représente une variante de réalisation conforme à la présente invention selon laquelle le bouchon de fermeture est intégré à l'enveloppe en matière plastique, et
  • les figures 6, 7, 8 et 9 représentent respectivement une vue en perspective et une vue en coupe longitudinale d'un corps de partie pyrotechnique d'initiation et une vue en perspective et une vue en coupe longitudinale d'un bouchon conformes à l'invention, adaptés pour faciliter le collage desdits corps de partie pyrotechnique et bouchon sur une gaine.
Other characteristics, objects and advantages of the present invention will appear on reading the detailed description which follows and with reference to the appended drawings given by way of non-limiting example and in which:
  • the figure 1 represents an exploded sectional view of a device according to the state of the art,
  • the figure 2 represents a general perspective view before the assembly of a first embodiment according to the present invention,
  • the figure 3 represents a similar general perspective view before assembling a second embodiment according to the present invention,
  • the figure 4 represents a similar general perspective view before assembling a third embodiment according to the present invention,
  • the figure 5 represents an alternative embodiment according to the present invention according to which the closure cap is integrated in the plastic envelope, and
  • the Figures 6, 7, 8 and 9 represent respectively a perspective view and a longitudinal sectional view of a part body pyrotechnic initiation and a perspective view and a longitudinal sectional view of a plug according to the invention, adapted to facilitate the bonding of said pyrotechnic body and plug body on a sheath.

On retrouve sur la figure 2, un dispositif formant leurre qui comprend un ensemble 110 comprenant une douille 111 associée à un impulseur 112 et un partie 120 destinée à être éjectée.We find on the figure 2 , a lure device which comprises an assembly 110 comprising a bushing 111 associated with an impeller 112 and a portion 120 intended to be ejected.

La douille 111 équipée de l'impulseur 112, de préférence formé d'un initiateur électrique, est adaptée pour être placée/coopèrer avec un lanceur. Sa structure est classique en soi et ne sera donc pas décrite plus en détail par la suite.The bushing 111 equipped with the impeller 112, preferably formed of an electric initiator, is adapted to be placed / co-operate with a launcher. Its structure is classic in itself and will not be described in more detail later.

La partie 120 destinée à être éjectée, comprend un pain 121 de composition adaptée pour émettre un rayonnement infrarouge lors de sa combustion.The portion 120 intended to be ejected comprises a bread 121 of composition adapted to emit infrared radiation during its combustion.

Le pain 121 est placé dans une gaine en matière plastique 130 conforme à l'invention.The bread 121 is placed in a plastic sheath 130 according to the invention.

La gaine 130 est de préférence formée d'un tube de section droite constante dont la paroi latérale est continue, pleine, sans ouverture en dehors de ses extrémités axiales débouchantes.The sheath 130 is preferably formed of a tube of constant cross section whose side wall is continuous, solid, without opening out of its axial ends open.

Cette gaine 130 est obturée à l'avant par un bouchon 140 et à l'arrière par une partie pyrotechnique d'initiation 150. Celle-ci comporte de préférence un tiroir de sécurité 160 susceptible d'occuper deux positions : d'une part une position de sécurité tant que l'ensemble 120 est logé dans la douille 111 et d'autre part une position de libération lorsque l'ensemble 120 est sorti de la douille 111.This sheath 130 is closed at the front by a stopper 140 and at the rear by a pyrotechnic initiation portion 150. The latter preferably comprises a safety slide 160 capable of occupying two positions: on the one hand a safety position as the assembly 120 is housed in the sleeve 111 and secondly a release position when the assembly 120 is out of the sleeve 111.

En position de sécurité le tiroir 160 est sollicité élastiquement en appui contre la paroi interne de la douille 111. Ne pouvant se déplacer transversalement à l'axe longitudinal de l'ensemble 120 en raison de son appui sur la surface interne de la douille 111, il assure une rupture dans le canal de transmission d'initiation entre l'impulseur 112 et le corps ou pain 121.In the safety position, the slide 160 is resiliently biased against the inner wall of the sleeve 111. It can not move transversely to the longitudinal axis of the assembly 120 because of its support on the inner surface of the sleeve 111, it ensures a break in the initiation transmission channel between the impeller 112 and the body or bread 121.

En revanche lorsque l'ensemble 120 est éjecté hors de la douille par des gaz de propulsion produits par l'impulseur 112, le tiroir 160 n'ayant plus d'appui en regard est déplacé (comme schématisé sur la figure 2) et autorise alors une transmission d'initiation vers le pain 121.On the other hand, when the assembly 120 is ejected from the socket by propulsion gases produced by the impeller 112, the slide 160 having no support in view is moved (as schematized on the figure 2 ) and then authorizes an initiation transmission to the bread 121.

Une fois le pain 121 placé dans la gaine 130, celle-ci est collée d'une part sur la partie pyrotechnique 150 et d'autre part sur le bouchon de fermeture 140. Le pain 121 est alors parfaitement confiné et l'on évite en toute sécurité tout risque d'allumage intempestif par l'extérieur du pain 121.Once the bread 121 placed in the sheath 130, it is glued on the one hand on the pyrotechnic part 150 and on the other hand on the closure cap 140. The bread 121 is then perfectly confined and is avoided by safely any risk of inadvertent ignition from outside the bread 121.

L'on notera que la présente invention permet de s'affranchir de l'enroulement manuel de la feuille d'aluminium et permet par conséquent un processus d'assemblage automatisable et industrialisable, notamment pour l'insertion du pain 121 dans la douille 111 et le collage de la gaine 130 sur la partie pyrotechnique 150 et sur le bouchon 140.It should be noted that the present invention makes it possible to dispense with the manual winding of the aluminum foil and therefore allows an automated and industrially usable assembly process, in particular for the insertion of the bread 121 into the bushing 111 and the gluing of the sheath 130 on the pyrotechnic part 150 and on the cap 140.

Le fonctionnement du dispositif conforme à l'invention reste globalement identique à celui du dispositif antérieur illustré sur la figure 1.The operation of the device according to the invention remains globally identical to that of the prior device illustrated in FIG. figure 1 .

Lors de la sortie de l'ensemble 120 hors de la douille 111, suite à une sollicitation de l'impulseur 112, le déplacement du tiroir 160 autorise l'alignement d'une pastille de transmission de feu avec le bloc 121 de composition IR.Upon the exit of the assembly 120 from the sleeve 111, following a bias of the impeller 112, the movement of the slide 160 allows the alignment of a fire transmission chip with the block 121 IR composition.

La composition Infrarouge 121 est alors allumée.The Infrared 121 composition is then lit.

Selon la nature et l'épaisseur de la gaine 130, celle-ci est soit détruite soit déplacée relativement au pain 121 de sorte que le rayonnement infrarouge recherché est pleinement obtenu.Depending on the nature and thickness of the sheath 130, it is either destroyed or moved relative to the bread 121 so that the desired infrared radiation is fully achieved.

On notera à l'examen de la figure 2 que le pain 121 est de préférence rainuré longitudinalement pour assurer une canalisation des gaz d'initiation et assurer un allumage du pain 121 sur toute sa longueur.It will be noted in the examination of figure 2 that the bread 121 is preferably longitudinally grooved to ensure a channeling of the initiation gases and ensure ignition of the bread 121 over its entire length.

Plus précisément selon le mode de réalisation particulier illustré sur la figure 2, le pain 121 est muni d'une série de rainures 122 sur deux faces opposées, par exemple 3 rainures 122 sur respectivement chacune de deux faces opposées.More precisely according to the particular embodiment illustrated on the figure 2 , the bread 121 is provided with a series of grooves 122 on two opposite faces, for example 3 grooves 122 on respectively each of two opposite faces.

Selon la variante illustrée sur la figure 3, le pain 121 est muni d'une ou plusieurs rainures 122 sur chacune de ses quatre faces.According to the variant illustrated on the figure 3 , the bread 121 is provided with one or more grooves 122 on each of its four faces.

La gaine 130 est formée de préférence en polystyrène, ABS (acrylonitrile butadiène styrène), polypropylène, polyéthylène ou PA6.6 (polyamide 6.6).The sheath 130 is preferably formed of polystyrene, ABS (acrylonitrile butadiene styrene), polypropylene, polyethylene or PA6.6 (polyamide 6.6).

Plus précisément selon l'invention le matériau composant la gaine 130 est avantageusement transparent aux ultraviolets (UV) pour permettre l'application d'un rayonnement ultraviolets à travers la gaine afin d'assurer la polymérisation d'une colle permettant la fixation de la gaine sur le corps 150 de la partie pyrotechnique d'initiation et/ou du bouchon 140.More specifically according to the invention the material constituting the sheath 130 is advantageously transparent to ultraviolet (UV) to allow the application of ultraviolet radiation through the sheath to ensure the polymerization of an adhesive for fixing the sheath on the body 150 of the pyrotechnic initiation part and / or the stopper 140.

Comme indiqué précédemment selon l'invention la gaine 130 est de préférence formée d'un tube de section droite constante dont la paroi latérale est continue, pleine, sans ouverture en dehors de ses extrémités axiales débouchantes.As indicated above according to the invention the sheath 130 is preferably formed of a tube of constant cross-section whose side wall is continuous, solid, without opening outside its axial ends open.

On a représenté sur les figures annexées des gaines 130 formées d'un tube rectiligne de section droite constante carrée. En conséquence le pain 121 a une géométrie identique, homothétique en dimensions pour définir un jeu suffisant pour permettre l'engagement du pain 121 dans la gaine 130.Appended figures are shown sheaths 130 formed of a rectilinear tube of constant square cross section. As a result, the bread 121 has an identical geometry, homothetic in dimensions to define a sufficient clearance to allow the engagement of the bread 121 in the sheath 130.

L'utilisation d'une gaine en matière plastique de section carrée s'avère plus fiable que l'enroulement d'un film en aluminium sur une charge de section carrée. En effet un enroulement de film en aluminium présente des faiblesses au niveau de ses arêtes de la section carrée, que ne présente pas une gaine formée par exemple par extrusion, moulage ou soufflage.The use of a square section plastic sheath is more reliable than winding an aluminum film on a square section load. Indeed an aluminum film winding has weaknesses at its edges of the square section, that does not present a sheath formed for example by extrusion, molding or blowing.

Bien entendu l'invention n'est pas limitée à ce mode de réalisation. On peut envisager de réaliser des gaines 130 ayant toute autre section, par exemple une section droite polygonale différente, ou circulaire.Of course, the invention is not limited to this embodiment. It is conceivable to make sheaths 130 having any other section, for example a polygonal cross section that is different or circular.

Par ailleurs l'on peut réaliser des gaines 130 ayant une épaisseur variable sur leur longueur pour maîtriser le front de montée du rayonnement et sa reproductibilité.Furthermore, sheaths 130 having a variable thickness along their length can be produced to control the rising edge of the radiation and its reproducibility.

L'homme de l'art comprendra aisément que l'utilisation d'une gaine réalisée par matière plastique, par exemple par moulage ou extrusion, permet d'éviter tout risque de déchirure et permet de réduire les coûts de production par rapport à l'état de la technique.Those skilled in the art will readily understand that the use of a sheath made of plastic, for example by molding or extrusion, avoids any risk of tearing and reduces production costs compared to the state of the art.

Selon une autre caractéristique avantageuse de la présente invention, la gaine 130 est réalisée en un matériau optiquement transparent, au moins dans le domaine infrarouge et dans le domaine ultraviolets. Ainsi la gaine ne perturbe aucunement la diffusion du rayonnement infrarouge émis par le pain 121.According to another advantageous characteristic of the present invention, the sheath 130 is made of an optically transparent material, at least in the infrared range and in the ultraviolet range. Thus the sheath does not disturb the diffusion of the infrared radiation emitted by the bread 121.

Des tests réalisés par les inventeurs ont en effet démontré que l'utilisation d'une gaine 130 en matériau transparent aux infrarouges, ne perturbe aucunement la diffusion du rayonnement infrarouge, que ce soit dans la phase de montée en puissance ou en régime d'entretien de l'émission et ce quel que soit le comportement de la gaine 130, c'est-à-dire que la gaine 130 soit éjectée ou détruite par explosion.Tests carried out by the inventors have in fact demonstrated that the use of a sheath 130 of infrared-transparent material does not disturb the diffusion of the infrared radiation, whether in the power-up or maintenance phase. of the emission and whatever the behavior of the sheath 130, that is to say that the sheath 130 is ejected or destroyed by explosion.

Les inventeurs ont de plus déterminé qu'il est avantageux de prévoir un jeu, par exemple de 0,5mm entre le pain 121 et la gaine 130. Ainsi le dispositif conforme à l'invention autorise sans risque un certain gonflement du pain 121, possible sous l'effet du vieillissement ou des conditions climatiques. A cet égard l'utilisation d'une gaine 130 en matière plastique est un avantage important par rapport à l'état de la technique utilisant une enveloppe en aluminium dans la mesure où une telle enveloppe en aluminium ne tolère pratiquement pas de gonflement du pain 121, et se déchire lors des premières déformations du pain 121.The inventors have further determined that it is advantageous to provide a clearance, for example of 0.5 mm between the bread 121 and the sheath 130. Thus the device according to the invention safely allows a certain swelling of the bread 121, possible under the effect of aging or weather conditions. In this respect, the use of a sheath 130 of plastic material is an important advantage over the state of the art using an aluminum casing since such an aluminum casing practically does not tolerate swelling of the bread. , and tears during the first deformations of bread 121.

On a représenté sur la figure 5 une variante de réalisation selon laquelle le bouchon de fermeture 140 est venu de matière sur la gaine 130. Une telle gaine 130 intégrant le bouchon 140 peut par exemple être formée par soufflage.We have shown on the figure 5 an alternative embodiment according to which the closure cap 140 is integral with the sheath 130. Such a sheath 130 incorporating the cap 140 may for example be formed by blowing.

On a représenté sur la figure 4 une variante de réalisation de la gaine 130 comportant une série de rainurages sur sa surface externe pour faciliter l'éclatement de la gaine sous la pression des gaz générés par le pain 121.We have shown on the figure 4 an alternative embodiment of the sheath 130 having a series of grooves on its outer surface to facilitate the bursting of the sheath under the pressure of the gases generated by the bread 121.

De nombreuses configurations de rainurage peuvent être prévues à cet effet.Many grooving configurations can be provided for this purpose.

Selon le mode de réalisation particulier illustré sur la figure 4, non limitatif, la gaine 130 comprend une rainure longitudinale 132 sur chacune de ses faces, par exemple à mi largeur, et une série de rainures transversales 134. L'homme de l'art comprendra que la présence des rainures 132 et 134 formant des amorces de rupture, permet de faciliter la découpe de la gaine 130 en segments de faibles dimensions et ainsi l'éclatement de la gaine 130.According to the particular embodiment illustrated on the figure 4 , not limiting, the sheath 130 comprises a longitudinal groove 132 on each of its faces, for example half width, and a series of transverse grooves 134. Those skilled in the art will understand that the presence of the grooves 132 and 134 forming breaking primers, facilitates the cutting of the sheath 130 into small segments and thus the bursting of the sheath 130.

On a représenté sur les figures 6, 7, 8 et 9 un mode de réalisation particulier du corps 150 de la partie pyrotechnique d'initiation et du bouchon 140, adaptée pour faciliter le collage desdits corps 150 et bouchon 140 sur la gaine 130.We have shown on Figures 6, 7, 8 and 9 a particular embodiment of the body 150 of the pyrotechnic initiation portion and the cap 140, adapted to facilitate the bonding of said bodies 150 and cap 140 on the sheath 130.

Plus précisément selon le mode de réalisation illustré sur les figures 6 et 7, le corps 150 possède une gorge annulaire 152 qui débouche sur toute sa périphérie extérieure et qui communique avec deux canaux longitudinaux 154, 156 lesquels débouchent eux-mêmes sur l'extrémité du corps 150 destinée à être placée à l'intérieur de la gaine 130.More precisely according to the embodiment illustrated on the Figures 6 and 7 , the body 150 has an annular groove 152 which opens out over its entire outer periphery and which communicates with two longitudinal channels 154, 156 which open themselves on the end of the body 150 intended to be placed inside the sheath 130 .

De même selon le mode de réalisation illustré sur les figures 8 et 9, le bouchon 140 possède une gorge annulaire 142 qui débouche sur toute sa périphérie extérieure et qui communique avec deux canaux longitudinaux 144, 146 lesquels débouchent eux-mêmes sur l'extrémité du bouchon 140 destinée à être placée à l'extérieur de la gaine 130.Similarly according to the embodiment illustrated on the Figures 8 and 9 , the plug 140 has an annular groove 142 which opens out over its entire outer periphery and which communicates with two longitudinal channels 144, 146 which open themselves on the end of the plug 140 intended to be placed outside the sheath 130 .

Lors du montage, le corps 150 est introduit dans la gaine 130. Une colle polymérisable est introduite dans les canaux 154 et 156 grâce à un outil engagé dans la gaine 130, afin de remplir la gorge 152. Ainsi le ruban de colle contenu dans la gorge 152 vient au contact de la surface interne de la gaine 130. La colle peut être polymérisée à ce stade de l'assemblage ou ultérieurement, par exemple par irradiation UV à travers la gaine 130.During assembly, the body 150 is introduced into the sheath 130. A polymerizable adhesive is introduced into the channels 154 and 156 by means of a tool engaged in the sheath 130, to fill the groove 152. Thus, the adhesive tape contained in the The groove 152 comes into contact with the inner surface of the sheath 130. The glue can be polymerized at this stage of the assembly or subsequently, for example by UV irradiation through the sheath 130.

Une fois l'ensemble 120 comprenant le pain 121 placé dans la gaine 130, le bouchon 140 peut être mis en place sur l'extrémité de la gaine 130. De façon similaire à l'opération réalisée pour le corps 150, une colle polymérisable est introduite dans les canaux 144 et 146 accessibles sur l'extérieur, grâce à un outil approprié, afin de remplir la gorge 142. Ainsi le ruban de colle contenu dans la gorge 142 vient au contact de la surface interne de la gaine 130. La colle peut être polymérisée à ce stade de l'assemblage ou ultérieurement, par exemple par irradiation UV à travers la gaine 130.Once the assembly 120 comprising the bread 121 placed in the sheath 130, the stopper 140 can be put in place on the end of the Sheath 130. Similarly to the operation performed for the body 150, a polymerizable adhesive is introduced into the channels 144 and 146 accessible on the outside, by means of a suitable tool, to fill the groove 142. Thus the ribbon The adhesive contained in the groove 142 comes into contact with the inner surface of the sheath 130. The adhesive may be polymerized at this stage of the assembly or subsequently, for example by UV irradiation through the sheath 130.

L'homme de l'art comprendra que les moyens de collage du corps 150 et du bouchon 140 décrits ci-dessus en regard des figures 6 à 9 permettent un assemblage simple, économique et fiable.Those skilled in the art will understand that the means for bonding the body 150 and the cap 140 described above with respect to the Figures 6 to 9 allow a simple, economical and reliable assembly.

Ces moyens sont particulièrement adaptés à une gaine 130 en ABS (acrylonitrile butadiène styrène), bien que l'invention ne soit pas limitée à l'utilisation de ce matériau particulier.These means are particularly suitable for a sheath 130 of ABS (acrylonitrile butadiene styrene), although the invention is not limited to the use of this particular material.

La colle polymérisable utilisée dans le cadre de la présente invention peut faire l'objet de nombreuses variantes.The polymerizable adhesive used in the context of the present invention may be subject to numerous variants.

A titre d'exemple non limitatif, il peut s'agir de VITRALIT®, notamment de VITRALIT® UV 4050 qui est une colle à base d'acrylate.By way of non-limiting example, it may be VITRALIT®, especially VITRALIT® UV 4050 which is an acrylate-based glue.

En variante le corps 150 et/ou le bouchon 140 peuvent ne comprendre qu'un seul canal longitudinal 154 ou 156, respectivement 144, 146.In a variant, the body 150 and / or the stopper 140 may comprise only one longitudinal channel 154 or 156, respectively 144, 146.

Les essais réalisés ont montré que les moyens précités permettent une bonne tenue mécanique de l'ensemble sous les accélérations appliquées lors du lancement et notamment que l'application d'un rayonnement UV pour assurer la polymérisation de la colle n'altère pas les propriétés mécaniques et optiques de la gaine 130. Ainsi l'invention permet d'assurer un cordon d'étanchéité et une tenue mécanique assurant la sécurité et permettant la mise en pression du pain en fonctionnement.The tests carried out have shown that the aforementioned means allow a good mechanical strength of the assembly under the accelerations applied during the launch and in particular that the application of UV radiation to ensure the polymerization of the glue does not alter the mechanical properties and optical sheath 130. Thus the invention ensures a sealing bead and a mechanical strength ensuring safety and allowing the pressurizing of bread in operation.

A titre d'exemple non limitatif, la gaine 130 peut avoir une épaisseur de l'ordre de 0,5 à 0,9mm.By way of non-limiting example, the sheath 130 may have a thickness of the order of 0.5 to 0.9 mm.

Un premier effet technique obtenu selon l'invention est l'amélioration de la sécurité par rapport aux enveloppes en aluminium antérieures du fait de la suppression du risque de déchirure avant l'initiation.A first technical effect obtained according to the invention is the improvement of safety compared to aluminum envelopes earlier because of the elimination of the risk of tearing before initiation.

Un deuxième effet technique obtenu selon l'invention résulte du jeu autorisé selon l'invention, et interdit par la technique d'enroulement antérieur, qui permet un gonflement dans le temps de la composition IR.A second technical effect obtained according to the invention results from the authorized clearance according to the invention, and prohibited by the prior winding technique, which allows a swelling in time of the IR composition.

Un troisième effet technique obtenu selon l'invention résulte du confinement mécanique du pain 121 opéré par la gaine 130 et impossible avec une enveloppe en papier aluminium enroulé dès lors que les contraintes appliquées par le pain 121 dépassent un certain seuil.A third technical effect obtained according to the invention results from the mechanical confinement of the bread 121 operated by the sheath 130 and impossible with an envelope of wrapped aluminum foil as soon as the stresses applied by the bread 121 exceed a certain threshold.

Des essais réalisés par les inventeurs ont également démontré que l'utilisation d'une gaine 130 en matière plastique est totalement compatible avec l'environnement pyrotechnique impliqué et en particulier que l'utilisation d'une telle gaine 130 en matière plastique ne risque pas de conduire à un niveau de charge électrostatique susceptible d'induire une initiation intempestive des éléments ou compositions pyrotechniques intervenant dans le dispositif.Tests carried out by the inventors have also demonstrated that the use of a plastic sheath 130 is fully compatible with the pyrotechnic environment involved and in particular that the use of such a sheath 130 of plastic material does not risk lead to an electrostatic charge level likely to induce inadvertent initiation of pyrotechnic elements or compositions involved in the device.

Par ailleurs la gaine 130 en matière plastique masque moins la flamme du pain infrarouge 121 qu'un papier en aluminium traditionnel. En effet du fait de sa tenue mécanique en pression à plus d'un bar, la gaine 130 se sépare et éclate plus facilement qu'un papillotage en aluminium qui est collé sur le pain 121 et qui a tendance à rester coller sur ce pain 121. La conséquence positive résultant de l'invention est une meilleure maîtrise de l'allumage et une meilleure reproductibilité de l'allumage.Moreover, the sheath 130 made of plastic mask less the flame of infrared bread 121 than a traditional aluminum paper. Indeed, because of its mechanical strength under pressure at more than one bar, the sheath 130 separates and bursts more easily than an aluminum spraying which is stuck on the bread 121 and which tends to stick on the bread 121 The positive consequence resulting from the invention is a better control of the ignition and a better reproducibility of the ignition.

Claims (12)

  1. A device forming an infrared decoy comprising:
    - a triggering pyrotechnic portion (150), housed in a body of pyrotechnic initiation portion,
    - a composition (121) adapted to emit radiation in the infrared range,
    - an envelope (130) for protecting the composition (121), formed from a sheath made of plastic material, and
    - a closure plug (140) which blocks the sheath at the front,
    wherein one at least of the body (150) of the pyrotechnic initiation portion and/or of the plug (140) for blocking the sheath (130) has an annular recess (152, 142) which leads to its outer periphery, characterized in that the annular recess (152, 142) communicates with at least one longitudinal channel (154, 156; 144, 146) which leads to one end of the body (150) or of the plug (140) to receive a ribbon of polymerizable glue providing for gluing the body (150) and/or the plug (140) to the sheath (130).
  2. The device according to claim 1, characterized in that the envelope (130) is a rigid profiled envelope formed by extrusion, molding or blowing.
  3. The device according to one of claims 1 or 2, characterized in that the envelope (130) is made of a material chosen in the group comprising the following plastic materials: polystyrene, ABS (acrylonitrile butadiene styrene), polypropylene, polyethylene or PA6.6 (polyamide 6.6).
  4. The device according to one of claims 1 to 3, characterized in that the envelope (130) is made of an optically transparent plastic material, at least in the infrared range.
  5. The device according to one of claims 1 to 4, characterized in that the envelope (130) is made of an optically transparent plastic material, at least in the ultraviolet range.
  6. The device according to one of claims 1 to 5, characterized in that the envelope (130) defines a clearance on the order of 0.5 mm around the composition (121) .
  7. The device according to one of claims 1 to 6, characterized in that the envelope (130) is made in one piece with a closure plug (140).
  8. The device according to one of claims 1 to 7, characterized in that the envelope (130) has a variable thickness.
  9. The device according to one of claims 1 to 8, characterized in that the envelope (130) has a thickness on the order of 0.5 to 0.9 mm.
  10. The device according to one of claims 1 to 9, characterized in that the sheath (130) comprises a series of grooves (132, 134) forming rupture initiators on its outer surface.
  11. The device according to one of claims 1 to 10, characterized in that the composition (121) is longitudinally grooved to ensure channeling of the initiation gases.
  12. The device according to one of claims 1 to 11, characterized in that the sheath (130) has a straight square section.
EP15715684.5A 2014-03-03 2015-03-02 Decoy cartridge for aircraft Active EP3114424B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1451687A FR3018112B1 (en) 2014-03-03 2014-03-03 AIRCRAFT SANDING CARTRIDGE
PCT/EP2015/054329 WO2015132212A1 (en) 2014-03-03 2015-03-02 Decoy cartridge for aircraft

Publications (2)

Publication Number Publication Date
EP3114424A1 EP3114424A1 (en) 2017-01-11
EP3114424B1 true EP3114424B1 (en) 2018-01-10

Family

ID=51260962

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15715684.5A Active EP3114424B1 (en) 2014-03-03 2015-03-02 Decoy cartridge for aircraft

Country Status (7)

Country Link
US (1) US10001351B2 (en)
EP (1) EP3114424B1 (en)
KR (1) KR102237804B1 (en)
FR (1) FR3018112B1 (en)
IL (1) IL247530B (en)
SG (1) SG11201607300UA (en)
WO (1) WO2015132212A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3018112B1 (en) * 2014-03-03 2018-04-20 Etienne Lacroix Tous Artifices S.A. AIRCRAFT SANDING CARTRIDGE
US10330449B2 (en) * 2015-07-24 2019-06-25 Raytheon Company Dispenser and dispensing system for radar jamming material
US10962337B2 (en) * 2019-09-03 2021-03-30 Imi Systems Ltd. Cartridge for providing delayed chaff for use as a decoy for RF radars
RU2764417C1 (en) * 2021-03-16 2022-01-17 Федеральное государственное бюджетное учреждение "Центральный научно-исследовательский испытательный институт инженерных войск имени Героя Советского Союза генерал-лейтенанта инженерных войск Д.М. Карбышева" Министерства обороны Российской Федерации Heat target simulator
RU2770205C1 (en) * 2021-06-15 2022-04-14 Федеральное государственное бюджетное учреждение "Центральный научно-исследовательский испытательный институт инженерных войск имени Героя Советского Союза генерал-лейтенанта инженерных войск Д.М. Карбышева" Министерства обороны Российской Федерации Radar-thermal simulator of moving military vehicles

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2436751A (en) * 1945-02-19 1948-02-24 Eureka Williams Corp Discharger
US2868129A (en) * 1956-08-10 1959-01-13 Thomas H Johnson Flare device
US3399621A (en) * 1968-01-05 1968-09-03 George H. Schillreff Underwater flare
US3596599A (en) * 1968-12-09 1971-08-03 Gen Dynamics Corp Pyrotechnic assembly
US3901152A (en) * 1971-11-17 1975-08-26 Dow Chemical Co Flare article
US4171669A (en) * 1978-02-13 1979-10-23 The United States Of America As Represented By The Secretary Of The Navy Decoy flare
FR2490333B1 (en) * 1980-09-12 1986-05-02 Lacroix E Tous Artifices CARTRIDGE HAVING PYROTECHNIC USEFUL LOAD WITH SECURITY
FR2501360B1 (en) * 1981-03-09 1986-11-21 Lacroix E Tous Artifices CARTRIDGE WITH PYROTECHNICALLY OPERATING USEFUL LOAD EXPLOSING AFTER REBOUND
DE3443778A1 (en) * 1983-04-05 1988-05-19 Haley & Weller Ltd Pyrotechnic mixture for producing a radiation barrier screen, process for its preparation and device for discharging a pyrotechnic mixture
US4791870A (en) * 1983-04-05 1988-12-20 Haley & Weller Limited Pyrotechnic assembly
DE3515166A1 (en) * 1985-04-26 1986-10-30 Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen THROWING BODY FOR THE DISPLAY OF AN INFRARED SURFACE SPOTLIGHT
GB2300035B (en) * 1993-07-29 1997-09-24 Lacroix Soc E An infrared decoy cartridge, and decoy apparatus including such a cartridge
US5561259A (en) * 1994-10-13 1996-10-01 Alliant Techsystems Inc. Decoy flare with sequencer ignition
US5763818A (en) * 1995-06-30 1998-06-09 Thiokol Corporation Illuminant igniter pellet ignition system for use in a decoy flare
US6170399B1 (en) * 1997-08-30 2001-01-09 Cordant Technologies Inc. Flares having igniters formed from extrudable igniter compositions
EP1342047B1 (en) * 2000-12-13 2006-02-22 The Secretary of State for Defence Infra-red emitting decoy flare
DE10065816B4 (en) * 2000-12-27 2009-04-23 Buck Neue Technologien Gmbh Ammunition for generating a fog
US6634301B1 (en) * 2002-09-26 2003-10-21 The United States Of America As Represented By The Secretary Of The Navy Enclosed ignition flare igniter
US7640858B1 (en) * 2004-01-23 2010-01-05 Kilgore Flares Company, Llc Stacked pellet flare assembly and methods of making and using the same
US7992496B2 (en) * 2005-04-28 2011-08-09 Alloy Surfaces Company, Inc. Decoys for infra-red radiation seeking missiles and methods of producing and using the same
AU2006330065B2 (en) * 2005-04-28 2011-12-01 Alloy Surfaces Company, Inc. Decoys for infra-red radiation seeking missiles and methods of producing and using the same
US20080093418A1 (en) * 2005-06-22 2008-04-24 Weihs Timothy P Multifunctional Reactive Composite Structures Fabricated From Reactive Composite Materials
US7469640B2 (en) * 2006-09-28 2008-12-30 Alliant Techsystems Inc. Flares including reactive foil for igniting a combustible grain thereof and methods of fabricating and igniting such flares
US9194669B2 (en) * 2011-11-04 2015-11-24 Orbital Atk, Inc. Flares with a consumable weight and methods of fabrication and use
US20150323296A1 (en) * 2013-10-01 2015-11-12 Omnitek Partners Llc Countermeasure Flares
US11920910B2 (en) * 2014-02-26 2024-03-05 Northrop Grumman Systems Corporation Compositions usable as flare compositions, countermeasure devices containing the flare compositions, and related methods
FR3018112B1 (en) * 2014-03-03 2018-04-20 Etienne Lacroix Tous Artifices S.A. AIRCRAFT SANDING CARTRIDGE
US10173944B2 (en) * 2014-10-16 2019-01-08 Northrop Grumman Innovations Systems, Inc. Compositions usable as flare compositions, countermeasure devices containing the flare compositions, and related methods

Also Published As

Publication number Publication date
KR102237804B1 (en) 2021-04-08
FR3018112B1 (en) 2018-04-20
EP3114424A1 (en) 2017-01-11
KR20160140690A (en) 2016-12-07
US10001351B2 (en) 2018-06-19
IL247530A0 (en) 2016-11-30
FR3018112A1 (en) 2015-09-04
US20170074626A1 (en) 2017-03-16
WO2015132212A1 (en) 2015-09-11
IL247530B (en) 2020-04-30
SG11201607300UA (en) 2016-10-28

Similar Documents

Publication Publication Date Title
EP3114424B1 (en) Decoy cartridge for aircraft
EP0906556B1 (en) Non-lethal projectile
EP2079980B1 (en) Device for the deconfinement of an ammunition casing
EP0389358B1 (en) Opening system for spreading wings on a projectile
WO1993013382A1 (en) Bullet fragment retaining socket tube for rifle grenades
EP1181498B1 (en) Igniter tube for artillery ammunition
WO2005098346A1 (en) Radiation-emitting device, which is intended in particular for infrared radiation
EP2962060B1 (en) Munition with modifiable explosive capability
EP0594482B1 (en) Case for a propellant charge
FR2509457A1 (en) SHORT TRAJECTORY PROJECTILE
FR2960055A1 (en) GUIDED MUNITION PROTECTED BY AERODYNAMIC COIFFE
EP1693645B1 (en) Artillery projectile having a driving band
EP1582321A1 (en) Device for the cutting of an automotive structure
FR2765961A1 (en) INFRARED LURE ROCKET FOR HELICOPTER
WO2008037713A1 (en) Stabilized projectile used over a trajectory, particularly decoy
WO2006122984A1 (en) Radiation-emitting device for protecting aircraft
FR2886003A1 (en) Cartridge for launching radiation-emitting projectiles from aircraft has launching piston that separates from projectile as it leaves launch tube
FR2610085A1 (en) Infrared emitter, especially for use as a decoy, and infrared decoy-launching cartridge for using it
FR2800867A1 (en) Liquid-firing cartridge, for disarming booby-trapped package, has plastic container of water inside case, cut open as it is fired
EP2103896A1 (en) Paillet and detonator without primary explosive comprising such a paillet
BE824041A (en) CARTRIDGE FOR THE DISPERSION OF ELECTROMAGNETIC LURES.
FR2867556A1 (en) Infrared ray transmitting device for use in civilian aircraft, has projectile comprising block placed on non metallic envelop, and piston placed in booster tube between projectile and propulsion load using ring
FR2712686A1 (en) Propulsion/ignition unit, esp. for tear-gas grenade
FR2873198A1 (en) Riot control grenade for police force, has cylindrical dispersion container housed inside cylindrical envelope, where container and envelope are made up of flexible or semi-rigid thermoplastic material
FR2567197A1 (en) Powder propulsion unit for projectile fired in a launching tube

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: 20160930

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20170808

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

GRAL Information related to payment of fee for publishing/printing deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR3

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAR Information related to intention to grant a patent recorded

Free format text: ORIGINAL CODE: EPIDOSNIGR71

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

INTC Intention to grant announced (deleted)
AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

INTG Intention to grant announced

Effective date: 20171204

RIN1 Information on inventor provided before grant (corrected)

Inventor name: SECCO, THIERRY

Inventor name: LEOQUET, CYRIL

Inventor name: PIGNOL, MARC

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: AT

Ref legal event code: REF

Ref document number: 962878

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180115

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: DE

Ref legal event code: R096

Ref document number: 602015007463

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 4

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20180110

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 962878

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180110

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180110

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

Ref country code: FI

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: 20180110

Ref country code: CY

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: 20180110

Ref country code: NO

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: 20180410

Ref country code: HR

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: 20180110

Ref country code: LT

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: 20180110

Ref country code: ES

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: 20180110

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: 20180510

Ref country code: LV

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: 20180110

Ref country code: SE

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: 20180110

Ref country code: AT

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: 20180110

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: 20180410

Ref country code: RS

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: 20180110

Ref country code: PL

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: 20180110

Ref country code: GR

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: 20180411

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

Ref country code: MT

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: 20180110

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602015007463

Country of ref document: DE

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180110

Ref country code: IT

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: 20180110

Ref country code: EE

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: 20180110

Ref country code: AL

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: 20180110

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

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

Ref country code: DK

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: 20180110

Ref country code: SK

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: 20180110

Ref country code: MC

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: 20180110

Ref country code: SM

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: 20180110

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20180331

26N No opposition filed

Effective date: 20181011

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

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: 20180302

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

Ref country code: IE

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

Effective date: 20180302

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: 20180331

Ref country code: SI

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: 20180110

Ref country code: CH

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

Effective date: 20180331

Ref country code: BE

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

Effective date: 20180331

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180110

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

Ref country code: PT

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: 20180110

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

Ref country code: HU

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

Effective date: 20150302

Ref country code: MK

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

Effective date: 20180110

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

Ref country code: FR

Payment date: 20230320

Year of fee payment: 9

Ref country code: CZ

Payment date: 20230223

Year of fee payment: 9

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230426

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

Ref country code: DE

Payment date: 20240307

Year of fee payment: 10

Ref country code: CZ

Payment date: 20240219

Year of fee payment: 10

Ref country code: GB

Payment date: 20240325

Year of fee payment: 10