EP0292383B1 - Photopyrotechnic priming device, and photopyrotechnic chain using such a device - Google Patents
Photopyrotechnic priming device, and photopyrotechnic chain using such a device Download PDFInfo
- Publication number
- EP0292383B1 EP0292383B1 EP88401203A EP88401203A EP0292383B1 EP 0292383 B1 EP0292383 B1 EP 0292383B1 EP 88401203 A EP88401203 A EP 88401203A EP 88401203 A EP88401203 A EP 88401203A EP 0292383 B1 EP0292383 B1 EP 0292383B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- barrier
- transparent barrier
- charge
- lens
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/10—Initiators therefor
- F42B3/113—Initiators therefor activated by optical means, e.g. laser, flashlight
Definitions
- the present invention relates to the field of initiation of pyrotechnic substances by light beams produced by laser and transported by fibers or optical cables.
- the laser source it is preferably possible to use a triggered pulsed laser.
- a triggered pulsed laser is described in the article by MM. C. CAREL and A.P. JOSSE of Aerospace and MM. M. MORISSON, P. BALDY and J. REFOUVELET from the Tarbes Construction Workshops entitled “Initiation of Explosives by Laser” (communication made at the "international symposium on fundamental and applied pyrotechnics: substances and systems” held on 5 on October 7, 1982 in Arcachon (France)).
- a photopyrotechnic detonator primer is a device charged with primary or secondary explosives which can be initiated under the action of an energy beam such as a laser beam and make it possible to obtain a shock wave. sufficient to initiate another pyrotechnic component charged with explosive.
- pyrotechnic igniters these are devices containing a pyrotechnic substance capable of igniting when it receives a calorific contribution, for example in the form of a laser beam, this flame possibly causing the ignition of another composition. pyrotechnic.
- the object of the present invention is to remedy these drawbacks by proposing a photopyrotechnical initiation device in which the pyrotechnic initiation substance is protected from external aggressions before and during operation.
- the transparent barrier is made of sapphire.
- a transparent barrier made of a material transparent to the wavelength of the beam used and of sealing means between this barrier and the body of the device makes it possible to protect the pyrotechnic charge from external aggressions while allowing passage the beam used to initiate this charge.
- this barrier allows it to resist the mechanical effects generated during the operation of the load, it remains intact after it has been ignited and any gas leaks are avoided through the passage for the laser beam.
- the device may further comprise a thin cover placed between the transparent barrier and the pyrotechnic charge, this cover having a face in contact with the pyrotechnic charge.
- this seal is especially useful in the case where the pyrotechnic charge is a substance which can explode under the action of a shock wave. It is used when the device includes means for focusing the laser beam. As we will see later, these are arranged so as to focus the beam on this operculum or to obtain on it the image of the exit face of the optical fiber: in this way the energy concentration is created in the mass of the operculum capable of creating a wave of shock. This shock wave is transmitted to the pyrotechnic substance which then explodes.
- sealing means are also provided between the body of the device and this support.
- the latter can be a device containing the main explosive charge which must be initiated by the photopyrotechnic device.
- the main load is itself protected from external aggressions.
- the initiating device conforms to what is described above and the laser source is preferably constituted by a pulsed pulsed laser.
- the expression "optical cable” it designates either an optical fiber alone, or a set of optical fibers.
- FIG. 1 schematically represents a photopyrotechnical functional chain comprising a laser source 10 and an optical fiber 12 transmitting the beam produced by the laser to a photopyrotechnical initiation device 14.
- a photopyrotechnical initiation device 14 This can be placed on a support 16 shown schematically in phantom in FIG. 1.
- the latter can be, for example, the wall of a container or of an apparatus containing the main charge which must be initiated by the device 14.
- This first consists of a body 18 fixed on the support 16 by any suitable means, for example by screwing.
- the body 18 has, at one of its ends, a cavity 20 for housing a pyrotechnic charge.
- this charge consists of an initiating charge 22 in contact with a reinforcing charge 24.
- the cavity 20 can be formed inside a load carrier constituted by a spacer 26 held against a shoulder provided inside the body 18 by a cap 28.
- the latter is fixed to the body 18 by any known means, for example by screwing as illustrated in Figure 2, the seal being provided by a seal 30.
- the cap 28 has a thinned part or cover 32 which is destroyed during the explosion of the charge 24.
- the charge 22 When the charge 22 is ignited under the effect of the laser beam emitted by the source 10, it is the seat of a shock wave. This wave propagates through the load 22, then through the load 24 where it is reinforced. The explosion of the charge 24 leads to the destruction of the cover 32 and the shock wave can thus ignite the main charge 34 contained inside the support 16 (the latter is shown diagrammatically in phantom on the figure 2).
- the body 18 of the device which is the subject of the invention also has a passage 36 allowing the laser beam 38 to penetrate inside the device.
- a transparent barrier 40 is mounted inside the passage 38, upstream of the cavity 20 relative to the direction of propagation of the beam. It should be noted that, in the example shown here, all the elements of the device have a symmetry of revolution about a common axis.
- the transparent barrier 40 has the shape of a truncated cone widening in the direction of the cavity 20 and limited at its two ends by circular faces. It is housed in a part of the passage 40 having the same seal between the barrier 40 and the body 18 being provided by sealing means 42, for example a rubber O-ring. As for the seal between the body 18 and the support 16, it can be ensured by an O-ring 46 or any other equivalent device.
- Sapphire which is a particular aluminum oxide crystal (Al2O3), is well suited for this use because it has a very high Young's modulus (3.7.105 MPa). In addition, its softening point is at 1800 ° C, which gives it good temperature resistance (for comparison, it can be noted that B1664 glass has a processing temperature of 559 ° C).
- this cover 44 is in the form of a thin coating deposited on the rear face of the barrier 40.
- the thickness of this coating is between a few hundred and a few thousand Angstroms and its constituent material can be a metal such as, for example, aluminum, gold, silver, niobium or indium.
- another material for example an organic material
- the coating being for example deposited on the initiating charge 22.
- This seal finds its usefulness when using a secondary explosive as the initiating charge. Indeed, to initiate such an explosive, you need a powerful shock wave. This can be obtained by the breakdown of a thin metallic layer and the breakdown of the cover 44 can be obtained by focusing the beam 38 on the cover 44.
- the device illustrated in Figure 2 further comprises means for focusing the laser beam.
- the latter essentially consist of an optical connector in the form of a hollow housing which can be threaded over the end of the body 18 opposite the cavity 20.
- the optical fiber 12 transmitting the beam of the laser 10 to the device 14 passes through a wall of the connector 48 and its end is inside the latter.
- the laser beam leaving the fiber 12 passes through a lens 50 mounted inside the connector 48. This can be held on a shoulder or a support using a spacer 52 screwed inside the connector 48
- the shape of the lens 50 is determined so that the beam 38, which is divergent when it leaves the fiber 12, is parallel after passing through the lens 50, its optical axis being coincident with the axis of revolution of the device 14 .
- the front face 41 of the barrier 40 is convex in shape when viewed from the entrance to the device. So the face front of the barrier 40 behaves like a plano-convex lens making the parallel beam coming from the lens 50 converge.
- the shape of the face 41 and the length of the barrier 40 are determined, as a function of the wavelength of the beam , so that it is focused at a given point, for example to obtain the image of the exit face of the fiber 12 on the cover 44. It is therefore the front face 41 of the barrier 40 which constitutes a second lens of the device.
- the device which is the subject of the invention has particularly advantageous advantages, the main one of which is good confinement of the pyrotechnic charge before operation and of the products of the detonation after operation.
- This is obtained by the presence of the transparent barrier 40 which is fixed in leaktight manner inside the body 18, and is made of a material resistant to the effects of detonation.
- the mounting, adjustment and positioning operations are facilitated by the use of an optical system which makes the laser beam 38 parallel over part of its path.
- the distance between the barrier 40 and the lens no longer needs to be determined with precision since, even if this distance varies, the beam remains parallel when it arrives at the optical barrier.
- care must be taken to center the various elements, which is relatively easy insofar as the components of the device have a symmetry of revolution.
- the barrier 40 has the shape of a truncated cone widening towards the load 23 while, in the case of FIG. 3b, it narrows in the direction of this load.
- the barrier 40 has the shape of a cylinder.
- Figures 4 illustrate variants in which the device of the invention is associated with an optical system.
- the transparent barrier 40 is in the form of a truncated cone widening towards the pyrotechnic charge 23.
- the transparent barrier it would not go beyond the scope of the invention to give other forms to the transparent barrier, by example the shape of a truncated cone tapering towards the load 23 or of a cylindrical bar as illustrated in FIGS. 3.
- FIG. 5 represents a preferred embodiment of a laser which can be used in the invention.
- the laser 10 comprises an amplifier bar 62, a straight flash tube 64, two mirrors 66 and 68, a trigger 70 (with dye or Pockels cell) and electronics 72.
- the bar 62 is composed of a neodymium doped glass working at a wavelength 1.06 ⁇ m corresponding to an optical window of the optical figure 12.
- the operation in triggered mode is ensured by the interposition between the two mirrors.
- the optical cavity of the saturable absorbent 70 (triggering of the passive type) or of a Pockels cell (triggering of the active type).
- the laser pulse approximately Gaussian in shape, has a pulse duration of the order of 10 ns at mid-height.
- the optical energy is of the order of 75 mJ with a saturable absorbent as a trigger system and of the order of 150 mJ with a Pockels cell.
Landscapes
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Optical Couplings Of Light Guides (AREA)
- Headphones And Earphones (AREA)
- Lasers (AREA)
- Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
- Electron Tubes For Measurement (AREA)
- Addition Polymer Or Copolymer, Post-Treatments, Or Chemical Modifications (AREA)
- Air Bags (AREA)
- Manufacture Of Electron Tubes, Discharge Lamp Vessels, Lead-In Wires, And The Like (AREA)
- Micromachines (AREA)
- Semiconductor Lasers (AREA)
- Fuel-Injection Apparatus (AREA)
- Dental Preparations (AREA)
- Materials For Medical Uses (AREA)
Abstract
Description
La présente invention se rapporte au domaine de l'initiation de substances pyrotechniques par faisceaux lumineux produits par laser et transportés par des fibres ou des câbles optiques.The present invention relates to the field of initiation of pyrotechnic substances by light beams produced by laser and transported by fibers or optical cables.
On rappelle que, par l'expression "substances pyrotechniques", on entend les explosifs primaires (tels que les azotures, les fulminates, le tétrazène, etc...) les explosifs secondaires (tels que : PETN, RDX, HNS, etc...) et les compositions pyrotechniques comme les compositions d'allumage, les compositions éclairantes, traçantes, fumigènes, etc. Les différents éléments mis en oeuvre forment ce que l'on appelle une chaîne fonctionnelle photopyrotechnique. Cette chaîne se compose généralement de trois éléments :
- un laser comme source d'énergie,
- une fibre ou un câble optique pour transporter l'énergie, et
- une amorce détonateur ou un inflammateur pyrotechnique.
- a laser as an energy source,
- an optical fiber or cable to transport energy, and
- a detonator primer or a pyrotechnic igniter.
Comme source laser, on peut utiliser de préférence un laser pulsé déclenché. Un tel laser est décrit dans l'article de MM. C. CAREL et A.P. JOSSE de l'Aérospatiale et MM. M. MORISSON, P. BALDY et J. REFOUVELET des Ateliers de Construction de Tarbes intitulé " Initiation d'Explosifs par Laser" (communication faite au "colloque international de pyrotechnie fondamentale et appliquée : substances et systèmes" qui s'est tenu du 5 au 7 octobre 1982 à Arcachon (France)).As the laser source, it is preferably possible to use a triggered pulsed laser. Such a laser is described in the article by MM. C. CAREL and A.P. JOSSE of Aerospace and MM. M. MORISSON, P. BALDY and J. REFOUVELET from the Tarbes Construction Workshops entitled "Initiation of Explosives by Laser" (communication made at the "international symposium on fundamental and applied pyrotechnics: substances and systems" held on 5 on October 7, 1982 in Arcachon (France)).
Une amorce détonateur photopyrotechnique est un dispositif chargé d'explosifs primaires ou secondaires qui peuvent être initiés sous l'action d'un faisceau énergétique tel qu'un faisceau laser et permettent d'obtenir une onde de choc suffisante pour initier un autre composant pyrotechnique chargé d'explosif. Quant aux inflammateurs pyrotechniques, ce sont des dispositifs contenant une substance pyrotechnique capable de s'enflammer lorsqu'elle reçoit un apport calorifique, par exemple sous la forme d'un faisceau laser, cette flamme pouvant entraîner la mise à feu d'une autre composition pyrotechnique.A photopyrotechnic detonator primer is a device charged with primary or secondary explosives which can be initiated under the action of an energy beam such as a laser beam and make it possible to obtain a shock wave. sufficient to initiate another pyrotechnic component charged with explosive. As for pyrotechnic igniters, these are devices containing a pyrotechnic substance capable of igniting when it receives a calorific contribution, for example in the form of a laser beam, this flame possibly causing the ignition of another composition. pyrotechnic.
Le document US-A-4 391 195 décrit un système d'initiation d'explosifs avec une source laser et des fibres optiques pour transporter l;énergie depuis le laser jusqu'à des dispositifs d'amorçage photopyrotechniques. Dans ce document, l'extrémité de la fibre optique opposée au laser est en contact direct avec une substance capable de s'enflammer, l'énergie de la flamme servant à amorcer des charges d'explosifs. Cependant, dans la plupart des dispositifs d'amorçage photopyrotechniques actuels, ceux-ci présentent une mauvaise étanchéité vis-à-vis de l'extérieur, ce qui a deux inconvénients : tout d'abord, la substance pyrotechnique d'amorçage est mal protégée des influences extérieures (humidité ou atmosphères plus ou moins corrosives), ce qui peut nuire à son fonctionnement. D'autre part, lors de la mise à feu de la charge, on risque d'avoir des pertes de rendement à cause des fuites du gaz dégagé lors de la détonation ainsi que des risques de pollution des équipements environnants.Document US-A-4 391 195 describes an explosive initiation system with a laser source and optical fibers for transporting energy from the laser to photopyrotechnic initiators. In this document, the end of the optical fiber opposite the laser is in direct contact with a substance capable of igniting, the energy of the flame being used to ignite charges of explosives. However, in most of the current photopyrotechnical initiation devices, these have a poor seal vis-à-vis the outside, which has two drawbacks: first, the pyrotechnic initiation substance is poorly protected external influences (humidity or more or less corrosive atmospheres), which can affect its functioning. On the other hand, when the charge is ignited, there is a risk of yield losses due to the leakage of the gas released during the detonation as well as the risks of pollution of the surrounding equipment.
Le brevet américain US-A-4 600 472 décrit un détonateur pyrotechnique qui utilise une lentille focalisant un rayonnement parallèle sur un booster. Mais, aucune barrière mécanique n'est introduite à ce niveau et encore moins de moyens d'étanchéité de cette barrière.American patent US-A-4 600 472 describes a pyrotechnic detonator which uses a lens focusing parallel radiation on a booster. However, no mechanical barrier is introduced at this level and even less means for sealing this barrier.
Quant au brevet américain US-A-3 911 823, il ne décrit pas un dispositif d'amorçage pyrotechnique, mais une méthode d'attache de fibres optiques à un élément pyrotechnique fonctionnant à l'aide d'un rayonnement laser. Dans ce document, l'élément n'a pas de fonction focalisante du rayonnement utilisé. Le joint d'étanchéité n'est pas utilisé pour l'étanchéité de cet élément.As for the US patent US-A-3 911 823, it does not describe a pyrotechnic ignition device, but a method of attaching optical fibers to a pyrotechnic element operating using laser radiation. In this document, the element has no focusing function on the radiation used. The seal is not used for sealing this element.
La présente invention a pour but de remédier à ces inconvénients en proposant un dispositif d'amorçage photopyrotechnique dans lequel la substance pyrotechnique d'amorçage est protégée des agressions extérieures avant et pendant le fonctionnement.The object of the present invention is to remedy these drawbacks by proposing a photopyrotechnical initiation device in which the pyrotechnic initiation substance is protected from external aggressions before and during operation.
Plus précisément, l'invention a pour objet un dispositif photopyrotechnique comprenant un corps présentant, de manière connue dans le document US-A-4 391 195 :
- une cavité pour loger une charge pyrotechnique ;
- une entrée pour un faisceau énergétique de longueur d'onde donnée servant à initier cette charge ; et
- un passage pour le faisceau énergétique entre ladite entrée et la cavité.
- a cavity for housing a pyrotechnic charge;
- an input for an energy beam of given wavelength used to initiate this charge; and
- a passage for the energy beam between said entrance and cavity.
Selon l'invention, ce dispositif comporte en outre :
- une barrière transparente placée dans le passage sur le trajet du faisceau, cette barrière résistant aux effets mécaniques engendrés lors du fonctionnement de la charge et étant réalisée en un matériau transparent à la longueur d'onde de ce faisceau et ayant une première face du côté de l'entrée et une deuxième face du côté de la charge pyrotechnique, son emplacement et la forme de ses deux faces sont déterminés de manière à focaliser en un point donné un faisceau énergétique parallèle ayant ladite longueur d'onde donnée et pénétrant dans cette barrière transparente par sa première face ; et
des moyens d'étanchéité entre cette barrière et le corps du dispositif.
- a transparent barrier placed in the passage on the path of the beam, this barrier resistant to the mechanical effects generated during the operation of the load and being made of a material transparent to the wavelength of this beam and having a first face on the side of the entry and a second face on the side of the pyrotechnic charge, its location and the shape of its two faces are determined so as to focus at a given point a parallel energy beam having said given wavelength and penetrating this transparent barrier by its first face; and
sealing means between this barrier and the body of the device.
De préférence, la barrière transparente est en saphir.Preferably, the transparent barrier is made of sapphire.
Ainsi, la présence d'une barrière transparente réalisée en un matériau transparent à la longueur d'onde du faisceau utilisé et des moyens d'étanchéité entre cette barrière et le corps du dispositif permet de protéger la charge pyrotechnique des agressions extérieures tout en laissant passer le faisceau utilisé pour amorcer cette charge. De plus, comme la constitution de cette barrière lui permet de résister aux effets mécaniques engendrés lors du fonctionnement de la charge, elle reste intacte après la mise à feu de celle-ci et on évite d'éventuelles fuites de gaz à travers le passage ménagé pour le faisceau laser.Thus, the presence of a transparent barrier made of a material transparent to the wavelength of the beam used and of sealing means between this barrier and the body of the device makes it possible to protect the pyrotechnic charge from external aggressions while allowing passage the beam used to initiate this charge. In addition, as the constitution of this barrier allows it to resist the mechanical effects generated during the operation of the load, it remains intact after it has been ignited and any gas leaks are avoided through the passage for the laser beam.
Eventuellement, le dispositif peut comporter en outre un opercule mince placé entre la barrière transparente et la charge pyrotechnique, cet opercule ayant une face en contact avec la charge pyrotechnique.Optionally, the device may further comprise a thin cover placed between the transparent barrier and the pyrotechnic charge, this cover having a face in contact with the pyrotechnic charge.
La présence de cet opercule est surtout utile dans le cas où la charge pyrotechnique est une substance pouvant exploser sous l'action d'une onde de choc. Il est utilisé lorsque le dispositif comporte des moyens de focalisation du faisceau laser. Comme on le verra plus loin, ces derniers sont agencés de manière à focaliser le faisceau sur cet opercule ou à obtenir sur celui-ci l'image de la face de sortie de la fibre optique : on crée ainsi dans la masse de l'opercule une concentration d'énergie apte à créer une onde de choc. Cette onde de choc est transmise à la substance pyrotechnique qui explose alors.The presence of this seal is especially useful in the case where the pyrotechnic charge is a substance which can explode under the action of a shock wave. It is used when the device includes means for focusing the laser beam. As we will see later, these are arranged so as to focus the beam on this operculum or to obtain on it the image of the exit face of the optical fiber: in this way the energy concentration is created in the mass of the operculum capable of creating a wave of shock. This shock wave is transmitted to the pyrotechnic substance which then explodes.
Selon un autre aspect de l'invention, lorsque le corps du dispositif pyrotechnique est monté sur un support, on prévoit en outre des moyens d'étanchéité entre le corps du dispositif et ce support.According to another aspect of the invention, when the body of the pyrotechnic device is mounted on a support, sealing means are also provided between the body of the device and this support.
Ce dernier peut être un appareil contenant la charge d'explosif principale qui doit être amorcée par le dispositif photopyrotechnique. Ainsi, la charge principale est elle-même protégée des agressions extérieures.The latter can be a device containing the main explosive charge which must be initiated by the photopyrotechnic device. Thus, the main load is itself protected from external aggressions.
Enfin, l'invention a encore pour objet une chaîne fonctionnelle photopyrotechnique comprenant, de manière connue :
- une source laser émettant un faisceau de longueur d'onde donnée ;
- un dispositif d'amorçage photopyrotechnique ; et
- un câble optique transportant le faisceau de la source laser au dispositif d'amorçage.
- a laser source emitting a beam of given wavelength;
- a photopyrotechnical initiation device; and
- an optical cable transporting the beam from the laser source to the ignition device.
Selon l'invention, le dispositif d'amorçage est conforme à ce qui est décrit ci-dessus et la source laser est de préférence constituée par un laser pulsé déclenché. Quant à l'expression "câble optique", elle désigne soit une fibre optique seule, soit un ensemble de fibres optiques.According to the invention, the initiating device conforms to what is described above and the laser source is preferably constituted by a pulsed pulsed laser. As for the expression "optical cable", it designates either an optical fiber alone, or a set of optical fibers.
L'invention apparaîtra mieux à la lecture de la description qui va suivre, donnée à titre d'exemple purement illustratif et nullement limitatif, en référence aux dessins annexés dans lesquels :
- la figure 1 est un schéma de principe illustrant l'allure générale d'un système d'amorçage photopyrotechnique ;
- la figure 2 est une vue schématique en coupe d'un mode de réalisation du dispositif d'amorçage photopyrotechnique objet de l'invention ;
- les figures 3a à 3c et 4a à 4c sont des vues schématiques montrant divers modes de réalisation possibles du dispositif objet de l'invention lorsqu'il n'y a pas de système optique associé et lorsqu'il y a un système optique associé ; et
- la figure 5 est une vue schématique en coupe d'un laser utilisable dans une chaîne fonctionnelle photopyrotechnique selon l'invention.
- Figure 1 is a block diagram illustrating the general appearance of a photopyrotechnic initiation system;
- Figure 2 is a schematic sectional view of an embodiment of the photopyrotechnical initiation device of the invention;
- Figures 3a to 3c and 4a to 4c are schematic views showing various possible embodiments of the device object of the invention when there is no associated optical system and when there is an associated optical system; and
- Figure 5 is a schematic sectional view of a laser usable in a photopyrotechnical functional chain according to the invention.
La figure 1 représente schématiquement une chaîne fonctionnelle photopyrotechnique comprenant une source laser 10 et une fibre optique 12 transmettant le faisceau produit par le laser à un dispositif d'amorçage photopyrotechnique 14. Celui-ci peut être placé sur un support 16 représenté schématiquement en traits mixtes sur la figure 1. Ce dernier peut être, par exemple, la paroi d'un conteneur ou d'un appareil contenant la charge principale qui doit être initiée par le dispositif 14.FIG. 1 schematically represents a photopyrotechnical functional chain comprising a
Celui-ci se compose d'abord d'un corps 18 fixé sur le support 16 par tout moyen approprié, par exemple par vissage. Le corps 18 présente, à l'une de ses extrémités, une cavité 20 pour loger une charge pyrotechnique. Dans l'exemple illustré ici, cette charge se compose d'une charge initiatrice 22 en contact avec une charge renforçatrice 24. La cavité 20 peut être ménagée à l'intérieur d'un porte-charge constitué par une entretoise 26 maintenue contre un épaulement prévu à l'intérieur du corps 18 par un capuchon 28. Ce dernier est fixé sur le corps 18 par tout moyen connu, par exemple par vissage comme cela est illustré sur la figure 2, l'étanchéité étant assurée par un joint 30. Cependant, on peut envisager d'autres modes de fixation, par exemple par soudure laser.This first consists of a
Le capuchon 28 présente une partie amincie ou opercule 32 qui est détruit lors de l'explosion de la charge 24. Lorsque la charge 22 est mise à feu sous l'effet du faisceau laser émis par la source 10, elle est le siège d'une onde de choc. Cette onde se propage à travers la charge 22, puis à travers la charge 24 où elle est renforcée. L'explosion de la charge 24 entraîne la destruction de l'opercule 32 et l'onde de choc peut ainsi mettre à feu la charge principale 34 contenue à l'intérieur du support 16 (celui-ci est représenté schématiquement en traits mixtes sur la figure 2).The
Le corps 18 du dispositif objet de l'invention présente encore un passage 36 permettant au faisceau laser 38 de pénétrer à l'intérieur du dispositif. Une barrière transparente 40 est montée à l'intérieur du passage 38, en amont de la cavité 20 par rapport au sens de propagation du faisceau. Il est à noter que, dans l'exemple représenté ici, tous les éléments du dispositif présentent une symétrie de révolution autour d'un axe commun. La barrière transparente 40 a la forme d'un tronc de cône s'élargissant en direction de la cavité 20 et limité à ses deux extrémités par des faces circulaires. Elle est logée dans une partie du passage 40 ayant la même l'étanchéité entre la barrière 40 et le corps 18 étant assurée par des moyens d'étanchéité 42, par exemple un joint torique en caoutchouc. Quant à l'étanchéité entre le corps 18 et le support 16, elle peut être assurée par un joint torique 46 ou tout autre dispositif équivalent.The
Des essais ont montré que les meilleurs résultats ont été obtenus avec une barrière transparente en saphir ayant la forme d'un tronc de cône limité par deux faces circulaires de diamètre 4 mm et 6 mm respectivement et dont la longueur était de 10 mm. On a aussi obtenu de bons résultats avec un tronc de cône en saphir de 8 mm de longueur et dont les faces d'extrémité avaient des diamètres de 4 et 6 mm respectivement.Tests have shown that the best results have been obtained with a transparent sapphire barrier having the shape of a truncated cone limited by two circular faces of diameter 4 mm and 6 mm respectively and the length of which was 10 mm. Good results have also been obtained with a sapphire truncated cone 8 mm in length and the end faces of which had diameters of 4 and 6 mm respectively.
Le saphir, qui est un cristal d'oxyde d'aluminium (Al₂O₃) particulier, est bien adapté pour cet usage car il possède un module d'Young très élevé (3,7.10⁵ MPa). De plus, son point de ramollissement se situe à 1800°C, ce qui lui confère une bonne résistance à la température (à titre de comparaison, on peut noter que le verre B1664 a une température de transformation de 559°C).Sapphire, which is a particular aluminum oxide crystal (Al₂O₃), is well suited for this use because it has a very high Young's modulus (3.7.10⁵ MPa). In addition, its softening point is at 1800 ° C, which gives it good temperature resistance (for comparison, it can be noted that B1664 glass has a processing temperature of 559 ° C).
On voit encore sur la figure 2 un opercule mince 44 interposé entre la barrière transparente 40 et la charge initiatrice 22. Dans l'exemple représenté ici, cet opercule se présente sous la forme d'un revêtement mince déposé sur la face arrière de la barrière 40. L'épaisseur de ce revêtement est comprise entre quelques centaines et quelques milliers d'Angström et son matériau constitutif peut être un métal tel que, par exemple, l'aluminium, l'or, l'argent, le niobium ou l'indium. Cependant, on ne sortirait pas du cadre de l'invention en utilisant un autre matériau (par exemple une matière organique) ou une autre disposition, le revêtement étant par exemple déposé sur la charge initiatrice 22. Cet opercule trouve son utilité lorsqu'on utilise un explosif secondaire comme charge initiatrice. En effet, pour initier un tel explosif, il faut une onde de choc puissante. Celle-ci peut être obtenue par le claquage d'une fine couche métallique et on peut obtenir le claquage de l'opercule 44 en focalisant le faisceau 38 sur l'opercule 44.We also see in Figure 2 a
Le dispositif illustré à la figure 2 comporte en outre des moyens de focalisation du faisceau laser. Ces derniers consistent essentiellement en un connecteur optique se présentant sous la forme d'un boîtier creux pouvant être enfilé par dessus l'extrémité du corps 18 opposée à la cavité 20. La fibre optique 12 transmettant le faisceau du laser 10 au dispositif 14 traverse une paroi du connecteur 48 et son extrémité se trouve à l'intérieur de celui-ci. Le faisceau laser sortant de la fibre 12 traverse une lentille 50 montée à l'intérieur du connecteur 48. Celle-ci peut être maintenue sur un épaulement ou un support à l'aide d'une entretoise 52 vissée à l'intérieur du connecteur 48. La forme de la lentille 50 est déterminée pour que le faisceau 38, qui est divergent lorsqu'il sort de la fibre 12, soit parallèle après avoir traversé la lentille 50, son axe optique étant confondu avec l'axe de révolution du dispositif 14.The device illustrated in Figure 2 further comprises means for focusing the laser beam. The latter essentially consist of an optical connector in the form of a hollow housing which can be threaded over the end of the
La face avant 41 de la barrière 40 est de forme convexe lorsqu'elle est vue depuis l'entrée du dispositif. Ainsi, la face avant de la barrière 40 se comporte comme une lentille plan-convexe faisant converger le faisceau parallèle issu de la lentille 50. La forme de la face 41 et la longueur de la barrière 40 sont déterminées, en fonction de la longueur d'onde du faisceau, pour que celui-ci soit focalisé en un point donné, par exemple pour obtenir l'image de la face de sortie de la fibre 12 sur l'opercule 44. C'est donc la face avant 41 de la barrière 40 qui constitue une deuxième lentille du dispositif.The
Ainsi, le dispositif objet de l'invention présente des avantages particulièrement intéressants dont le principal est un bon confinement de la charge pyrotechnique avant fonctionnement et des produits de la détonation après fonctionnement. Ceci est obtenu par la présence de la barrière transparente 40 qui est fixée de manière étanche à l'intérieur du corps 18, et est réalisée en un matériau résistant aux effets de la détonation. D'autre part, les opérations de montage, réglage et positionnement sont facilitées par l'utilisation d'un système optique qui rend le faisceau laser 38 parallèle sur une partie de son parcours. La distance entre la barrière 40 et la lentille n'a plus besoin d'être déterminée avec précision puisque, même si cette distance varie, le faisceau reste parallèle lorsqu'il arrive sur la barrière optique. Il faut cependant veiller au centrage des différents éléments, ce qui est relativement facile dans la mesure où les constituants du dispositif présentent une symétrie de révolution.Thus, the device which is the subject of the invention has particularly advantageous advantages, the main one of which is good confinement of the pyrotechnic charge before operation and of the products of the detonation after operation. This is obtained by the presence of the
Enfin, il est bien entendu que l'invention ne se limite pas au seul mode de réalisation qui vient d'être décrit, mais qu'on peut imaginer de nombreuses variantes sans sortir pour autant du cadre de l'invention. C'est ainsi qu'on peut utiliser ou non l'opercule 44 ou remplacer la charge initiatrice 22 par une substance qui s'enflamme sous l'effet de l'énergie apportée par le faisceau laser, cette flamme provoquant l'explosion d'une autre substance pyrotechnique. On peut ainsi remplacer les deux charges 22 et 24 par une charge unique.Finally, it is understood that the invention is not limited to the single embodiment which has just been described, but that one can imagine many variants without departing from the scope of the invention. Thus it is possible to use or not the
On peut encore modifier la forme de la barrière 40 et associer ou non au dispositif de l'invention un système optique, comme cela est illustré aux figures 3 à 4.It is also possible to modify the shape of the
Elles illustrent le cas où la face avant 41 de la barrière 40 est de forme convexe et taillée de manière à focaliser un faisceau parallèle arrivant sur cette face 41 en un point donné du dispositif. Sur la figure 3a, la barrière 40 a la forme d'un tronc de cône s'élargissant vers la charge 23 tandis que, dans le cas de la figure 3b, elle se rétrécit en direction de cette charge. Enfin, dans le cas de la figure 3c, la barrière 40 a la forme d'un cylindre.They illustrate the case where the
Les figures 4 illustrent des variantes dans lesquelles le dispositif de l'invention est associé à un système optique.Figures 4 illustrate variants in which the device of the invention is associated with an optical system.
Elles concernent le cas où la face avant 41 de la barrière 40 est convexe afin de constituer la deuxième lentille. Sur la figure 4a, la lentille 50 est montée sur un connecteur 48 indépendant, tandis que, dans le cas de la figure 4b, la lentille 50 est montée à demeure sur le corps 18. Enfin, il est à noter que, sur les figures 4, la barrière transparente 40 se présente sous la forme d'un tronc de cône s'élargissant vers la charge pyrotechnique 23. Cependant, on ne sortirait pas du cadre de l'invention en donnant d'autres formes à la barrière transparente, par exemple la forme d'un tronc de cône se rétrécissant vers la charge 23 ou d'un barreau cylindrique comme illustré aux figures 3.They relate to the case where the
La figure 5 représente un mode de réalisation préféré d'un laser pouvant être utilisé dans l'invention.FIG. 5 represents a preferred embodiment of a laser which can be used in the invention.
Le laser 10 comprend un barreau amplificateur 62, un tube éclair droit 64, deux miroirs 66 et 68, un déclencheur 70 (à colorant ou à cellule de Pockels) et une électronique 72.The
Le barreau 62 est composé d'un verre dopé au néodyme travaillant à une longueur d'onde 1,06 µm correspondant à une fenêtre optique de la figure optique 12. Le fonctionnement en mode déclenché est assuré par l'interposition entre les deux miroirs de la cavité optique de l'absorbant saturable 70 (déclenchement de type passif) ou d'une cellule de Pockels (déclenchement de type actif). L'impulsion laser, de forme approximativement gaussienne, a une durée d'impulsion de l'ordre de 10 ns à mi-hauteur.The
L'énergie optique est de l'ordre de 75 mJ avec un absorbant saturable comme système de déclenchement et de l'ordre de 150 mJ avec une cellule de Pockels.The optical energy is of the order of 75 mJ with a saturable absorbent as a trigger system and of the order of 150 mJ with a Pockels cell.
Claims (9)
- Photopyrotechnic detonating device comprising a body (18) with:
a cavity (30) to house a pyrotechnic charge (22, 24),
an output for an energy beam of a given wavelength, used to actuate this charge (22, 24) and
a passage (36) for the energy beam between said input and the cavity,
characterized in that it also comprises:
a transparent barrier (40) placed in the passage (36), said barrier withstanding the mechanical effects generated during the operation of the charge and made from a material which is transparent to the wavelength of the beam used and having a first surface (41) on the input side and a second surface on the side of the pyrotechnic charge (22, 24), its position and the shape of its two surfaces being defined so as to focus, on a given point, a parallel energy beam, having said given wavelength and penetrating this transparent barrier (40) through its first surface (41), and
sealing means (42) between this barrier (40) and the body of the device. - Device according to claim 1, characterized in that the transparent barrier (40) is made of sapphire.
- Device according to claim 2, characterized in that the transparent barrier (40) has the shape of a truncated cone that widens towards the cavity (20), and in that the sealing means (42) are formed by an O-ring.
- Device according to claim 1, characterized in that it comprises a thin percussion cap (44) placed between the transparent barrier (40) and the pyrotechnic charge and has one side in contact with the latter.
- Device according to claim 1, characterized in that the body (18) being mounted on a support (16), said device comprises sealing means (46) between the body (18) and said support (16).
- Device according to claim 1, characterized in that it comprises a lens (50) cut so as to make the high energy beam entering the device parallel, so that the high energy beam (38) successively passes through the lens (50) and the transparent barrier (40), the position and shape of the transparent barrier (40) being determined so that the parallel energy beam passing out of the lens (50) is focused at a given point.
- Device according to claim 6, characterized in that the lens (50) is installed on an optical connector (48), which can be dismantlably fixed to the body (18) of the device.
- Photopyrotechnic functional chain comprising a laser source (10) emitting a beam having a given wavelength, a pyrotechnic detonating device (14) and an optical cable (12) carrying the beam from the laser source (10) to the detonating device (14), characterized in that the detonating device (14) is in accordance with claim 1.
- Functional chain according to claim 8, characterized in that the laser source (10) is a triggered, pulsed laser.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT88401203T ATE80453T1 (en) | 1987-05-20 | 1988-05-18 | DEVICE FOR PHOTOPYROTECHNIC IGNITION AND PHOTOPYROTECHNIC CHAIN WITH SUCH DEVICE. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8707069 | 1987-05-20 | ||
FR8707069A FR2615609B1 (en) | 1987-05-20 | 1987-05-20 | PHOTOPYROTECHNICAL PRIMING DEVICE AND PHOTOPYROTECHNICAL CHAIN USING THE SAME |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0292383A1 EP0292383A1 (en) | 1988-11-23 |
EP0292383B1 true EP0292383B1 (en) | 1992-09-09 |
Family
ID=9351263
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP88401203A Expired - Lifetime EP0292383B1 (en) | 1987-05-20 | 1988-05-18 | Photopyrotechnic priming device, and photopyrotechnic chain using such a device |
Country Status (11)
Country | Link |
---|---|
US (1) | US4870903A (en) |
EP (1) | EP0292383B1 (en) |
JP (1) | JPS63311097A (en) |
AT (1) | ATE80453T1 (en) |
CA (1) | CA1324733C (en) |
DE (1) | DE3874413T2 (en) |
DK (1) | DK165710C (en) |
ES (1) | ES2035333T3 (en) |
FR (1) | FR2615609B1 (en) |
IL (1) | IL86441A (en) |
NO (1) | NO170041C (en) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3838896C2 (en) * | 1988-11-17 | 1999-07-01 | Dynamit Nobel Ag | Laser-initiable ignition / ignition element provided with a storage layer |
FR2646901B1 (en) * | 1989-05-12 | 1994-04-29 | Aerospatiale | PHOTOPYROTECHNICAL PRIMING DEVICE COMPRISING A MICROLENTIL CRIMPED BY A MEMORY MATERIAL AND PYROTECHNIC CHAIN USING THE SAME |
US5022324A (en) * | 1989-06-06 | 1991-06-11 | Hercules Incorporated | Piezoelectric crystal powered ignition device |
US5010822A (en) * | 1990-02-02 | 1991-04-30 | Whittaker Ordnance, Inc. | Explosive initiator with angled fiber optic input |
AU7278991A (en) * | 1990-03-13 | 1991-09-19 | Johnson, Richard John | Electro-optical detonator |
US5046423A (en) * | 1990-04-02 | 1991-09-10 | The United States Of America As Represented By The Department Of Energy | Laser-driven flyer plate |
US5029528A (en) * | 1990-04-02 | 1991-07-09 | The United States Of America As Represented By The United States Department Of Energy | Fiber optic mounted laser driven flyer plates |
US5036767A (en) * | 1990-07-02 | 1991-08-06 | Whittaker Ordnance, Inc. | Optical window for laser-initiated explosive devices |
US5179246A (en) * | 1991-01-28 | 1993-01-12 | The United States Of America As Represented By The Secretary Of The Army | Laser actuated thru-bulkhead initiator for detonable explosive material, pyrotechnic material and remotely located pyrotechnic or propellant material |
US5099761A (en) * | 1991-01-28 | 1992-03-31 | The United States Of America As Represented By The Secretary Of The Army | Laser actuated thru-bulkhead initiator |
US5206455A (en) * | 1991-03-28 | 1993-04-27 | Quantic Industries, Inc. | Laser initiated ordnance systems |
US5406889A (en) * | 1993-09-03 | 1995-04-18 | Morton International, Inc. | Direct laser ignition of ignition products |
US5473885A (en) * | 1994-06-24 | 1995-12-12 | Lockheed Corporation | Pulse detonation engine |
US5546744A (en) * | 1994-06-24 | 1996-08-20 | Lockheed Martin | Pulse detonation apparatus with spherical seals |
US5542247A (en) * | 1994-06-24 | 1996-08-06 | Lockheed Corporation | Apparatus powered using laser supplied energy |
US5579633A (en) * | 1994-06-24 | 1996-12-03 | Lockheed Martin Corporation | Annular pulse detonation apparatus and method |
US5557926A (en) * | 1994-06-24 | 1996-09-24 | Lockheed-Martin | Pulse detonation apparatus with inner and outer Spherical valves |
US5615548A (en) * | 1995-07-26 | 1997-04-01 | Lockheed Martin Corporation | Dual rotor pulse detonation apparatus |
US5660413A (en) * | 1995-08-24 | 1997-08-26 | Trw Vehicle Safety Systems Inc. | Air bag inflator with laser diode initiator |
DE19616627A1 (en) * | 1996-04-26 | 1997-11-06 | Dynamit Nobel Ag | Kindling mixtures |
DE19719273A1 (en) * | 1996-08-02 | 1998-02-05 | Dynamit Nobel Ag | Laser initiated simultaneous ignition system |
US5914458A (en) * | 1997-03-14 | 1999-06-22 | Quantic Industries, Inc. | Dual fiber laser initiator and optical telescope |
US6047643A (en) * | 1997-12-12 | 2000-04-11 | Eg&G Star City, Inc. | Hermetically sealed laser actuator/detonator and method of manufacturing the same |
FR2773394B1 (en) | 1998-01-07 | 2000-02-11 | Cardem Demolition Sa | OPTOPYROTECHNICAL DEMOLITION SYSTEM |
US6178888B1 (en) | 1998-01-20 | 2001-01-30 | Eg&G Star City, Inc. | Detonator |
FR2796166B1 (en) * | 1999-07-06 | 2003-05-30 | Saint Louis Inst | GLASS BAR INDEX WITH GRADIENT INDEX |
US6276276B1 (en) * | 1999-08-19 | 2001-08-21 | The United States Of America As Represented By The United States Department Of Energy | Thin-film optical initiator |
DE19939502A1 (en) * | 1999-08-20 | 2001-03-15 | Siemens Ag | Device for triggering an airbag device accommodated in a steering wheel |
SE0100864L (en) * | 2001-03-14 | 2002-09-03 | Bofors Bepab Ab | Methods and apparatus for initiating explosive charge |
FR2831659B1 (en) * | 2001-10-26 | 2004-04-09 | Saint Louis Inst | LOW ENERGY OPTICAL DETONATOR |
US7201103B1 (en) | 2002-02-25 | 2007-04-10 | Bofors Bepab Ab | Method for initiation and ignition of explosive charges through self-destruction of a laser source |
PE20060926A1 (en) * | 2004-11-02 | 2006-09-04 | Orica Explosives Tech Pty Ltd | ASSEMBLIES OF WIRELESS DETONATORS, CORRESPONDING BLASTING APPLIANCES AND BLASTING METHODS |
DE102009006079A1 (en) | 2009-01-26 | 2010-07-29 | Oao Znjj "Burevestnik" | Shot load igniting device for use in projectile chamber of artillery system, has coaxial apparatus whose part is provided at sides of chamber, and transmission source provided in frequency region, where chamber forms vertical shaft |
US9021782B1 (en) | 2010-08-24 | 2015-05-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aerospace laser ignition/ablation variable high precision thruster |
JP2013057446A (en) * | 2011-09-08 | 2013-03-28 | Nof Corp | Laser ignition type ignition tool |
JP5862129B2 (en) * | 2011-09-08 | 2016-02-16 | 日油株式会社 | Laser ignition igniter |
FR3005500B1 (en) * | 2013-05-07 | 2017-12-22 | Commissariat Energie Atomique | OPTO-PYROTECHNIC INITIATOR ENHANCED |
CA3000236C (en) * | 2015-11-09 | 2020-03-24 | Detnet South Africa (Pty) Ltd | Wireless detonator |
JP6650830B2 (en) * | 2016-05-24 | 2020-02-19 | 株式会社Ihiエアロスペース | Laser ignition device |
DE102022000418A1 (en) | 2022-02-03 | 2023-08-03 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mit beschränkter Haftung | Arrangement for initiating an explosive, method for producing an arrangement for initiating an explosive, and method for initiating an explosive |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3362329A (en) * | 1963-12-10 | 1968-01-09 | Epstein Sidney | Electro-explosive devices |
US3296795A (en) * | 1964-08-04 | 1967-01-10 | Floyd B Nielsen | Laser initiated rocket type igniter |
US3528372A (en) * | 1967-09-08 | 1970-09-15 | Space Ordnance Systems Inc | Explosive detonating device |
FR2031889A5 (en) * | 1969-02-12 | 1970-11-20 | Asnieres Union Metallurg | Photon firing system for aircraft ejector - seats etc |
US3618526A (en) * | 1969-09-26 | 1971-11-09 | Us Navy | Pyrotechnic pumped laser for remote ordnance initiation system |
US3685392A (en) * | 1970-02-12 | 1972-08-22 | Remington Arms Co Inc | Laser ignition system |
US3757078A (en) * | 1971-08-19 | 1973-09-04 | Gen Dynamics Corp | Apparatus for refocusing reflected energy at a target focal point |
US3812783A (en) * | 1972-08-03 | 1974-05-28 | Nasa | Optically detonated explosive device |
FR2263064A1 (en) * | 1974-03-05 | 1975-10-03 | Us Energy | Laser welding system - seals weld spot by small inert gas pressure chamber against substrate and laser head |
US3911822A (en) * | 1974-05-22 | 1975-10-14 | Us Army | Method of attaching fiber optics bundle to laser squib |
IT1117550B (en) * | 1977-08-01 | 1986-02-17 | Righini Giancarlo | TRANSPORT AND FOCUS SYSTEM OF LASER RADIATION WITH OPTICAL FIBER PARTICULARLY FOR MEDICAL SURGICAL AND BIOLOGICAL APPLICATIONS |
US4391195A (en) * | 1979-08-21 | 1983-07-05 | Shann Peter C | Detonation of explosive charges and equipment therefor |
US4343242A (en) * | 1980-04-28 | 1982-08-10 | Gould Inc. | Laser-triggered chemical actuator for high voltage isolation |
DE3165351D1 (en) * | 1980-05-09 | 1984-09-13 | Emi Ltd | Arrangements for igniting a pyrotechnic charge |
US4563057A (en) * | 1982-08-31 | 1986-01-07 | The United States Of America As Represented By The Secretary Of The Air Force | Fiber optic cable connector |
US4506606A (en) * | 1983-01-27 | 1985-03-26 | Caruso Anthony M | Firing mechanism |
US4660472A (en) * | 1985-10-07 | 1987-04-28 | Morton Thiokol Inc. | Optical through bulkhead initiator and safe-arm device |
-
1987
- 1987-05-20 FR FR8707069A patent/FR2615609B1/en not_active Expired - Fee Related
-
1988
- 1988-05-17 US US07/194,854 patent/US4870903A/en not_active Expired - Fee Related
- 1988-05-18 AT AT88401203T patent/ATE80453T1/en not_active IP Right Cessation
- 1988-05-18 JP JP63121657A patent/JPS63311097A/en active Pending
- 1988-05-18 ES ES198888401203T patent/ES2035333T3/en not_active Expired - Lifetime
- 1988-05-18 DE DE8888401203T patent/DE3874413T2/en not_active Expired - Fee Related
- 1988-05-18 CA CA000567149A patent/CA1324733C/en not_active Expired - Fee Related
- 1988-05-18 EP EP88401203A patent/EP0292383B1/en not_active Expired - Lifetime
- 1988-05-19 IL IL86441A patent/IL86441A/en unknown
- 1988-05-19 DK DK274988A patent/DK165710C/en not_active IP Right Cessation
- 1988-05-20 NO NO882230A patent/NO170041C/en unknown
Also Published As
Publication number | Publication date |
---|---|
DK165710C (en) | 1993-05-24 |
US4870903A (en) | 1989-10-03 |
DK274988D0 (en) | 1988-05-19 |
FR2615609A1 (en) | 1988-11-25 |
FR2615609B1 (en) | 1991-12-20 |
IL86441A (en) | 1993-01-31 |
JPS63311097A (en) | 1988-12-19 |
DE3874413T2 (en) | 1993-03-11 |
ES2035333T3 (en) | 1993-04-16 |
NO170041C (en) | 1992-09-02 |
DE3874413D1 (en) | 1992-10-15 |
DK165710B (en) | 1993-01-04 |
ATE80453T1 (en) | 1992-09-15 |
NO882230D0 (en) | 1988-05-20 |
EP0292383A1 (en) | 1988-11-23 |
CA1324733C (en) | 1993-11-30 |
DK274988A (en) | 1988-11-21 |
NO882230L (en) | 1988-11-21 |
NO170041B (en) | 1992-05-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0292383B1 (en) | Photopyrotechnic priming device, and photopyrotechnic chain using such a device | |
CA2056170A1 (en) | Coaxial connection pyrotechnic detonator | |
EP3102906B1 (en) | Hollow charge and use for separating two floors of an aeronautical vehicle or for the neutralization thereof | |
EP0397572B1 (en) | Photopyrotechnic priming device comprising a microlens crimped with a material having shape recollection power and a pyrotechnic line using such device | |
EP0030498A1 (en) | Self separating pyrotechnic connector having sealed parts | |
FR2760266A1 (en) | Fibre=optic system for multipoint explosive firing mechanism | |
FR2699659A1 (en) | Breakable join device between front and rear sections of munition | |
FR2692346A1 (en) | Optical detonator for low-energy pyrotechnical generator - has pyrotechnic charge set off by optical system, e.g. with optical fibre, aperture or lens and triggered by laser beam, etc. | |
EP0296962A1 (en) | Initiator for a pyrotechnic generator | |
FR2775770A1 (en) | Explosive mine clearance munition | |
FR2519784A1 (en) | Multichannel transmission assembly for pyrotechnic firing signal - uses shock generator to detonate explosive to force metal strips against multiple output relay elements | |
WO2023111463A1 (en) | Assembly that is separable by means of pyrotechnic cutting | |
FR2601763A1 (en) | SUB-CALIBER PROJECTILE OF ARRAY TYPE FOR ACTIVE SHIELDS | |
EP2554529B1 (en) | Security detonator | |
FR2469690A1 (en) | Distress flare providing visual and electromagnetic signal - has electromagnetic lures made from metallised glass fibres and dispersed by combustion of charge providing flame | |
EP2103896B1 (en) | Flyer disk and slapper detonator without primary explosive comprising such a flyer disk | |
FR2690239A1 (en) | Optical primer for plasma pyrotechnic generator - having readily vaporised metallic coating on end of fibre=optic | |
EP0443018A1 (en) | Security igniter for propulsor | |
EP3910280A1 (en) | Device for detecting absence of mechanical barrier for a missile and missile comprising such a device | |
CA2017495A1 (en) | Pyrotechnic igniter for weapon loads or thruster or gas generator | |
FR2572514A1 (en) | OPTO-ELECTRONIC IMPACT DETECTOR FOR MISSILES, ROCKETS AND THE LIKE | |
FR2775769A1 (en) | Submarine launched munition for mine clearance | |
FR2775134A1 (en) | Solid laser/optical pump construction | |
FR2846408A1 (en) | Aircraft/satellite structure separation pyrotechnic charge initiation mechanism having charge and luminous energy source initiator connected optical fibre with constant index fibre extension within charge area | |
FR2707751A1 (en) | Girl missile release device. |
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 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE CH DE ES GB IT LI NL SE |
|
17P | Request for examination filed |
Effective date: 19890426 |
|
17Q | First examination report despatched |
Effective date: 19900823 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH DE ES GB IT LI NL SE |
|
REF | Corresponds to: |
Ref document number: 80453 Country of ref document: AT Date of ref document: 19920915 Kind code of ref document: T |
|
REF | Corresponds to: |
Ref document number: 3874413 Country of ref document: DE Date of ref document: 19921015 |
|
ITF | It: translation for a ep patent filed |
Owner name: JACOBACCI & PERANI S.P.A. |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19921201 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 19930225 Year of fee payment: 6 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2035333 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: BE Payment date: 19930505 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19930507 Year of fee payment: 6 Ref country code: ES Payment date: 19930507 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 19930510 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 19930514 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 19930517 Year of fee payment: 6 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 19930531 Year of fee payment: 6 |
|
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 |
|
26N | No opposition filed | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Effective date: 19940518 Ref country code: AT Effective date: 19940518 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Effective date: 19940519 Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19940519 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Effective date: 19940531 Ref country code: CH Effective date: 19940531 Ref country code: BE Effective date: 19940531 |
|
BERE | Be: lapsed |
Owner name: AEROSPATIALE SOC. NATIONALE INDUSTRIELLE Effective date: 19940531 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Effective date: 19941201 |
|
NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee | ||
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19940518 |
|
EUG | Se: european patent has lapsed |
Ref document number: 88401203.0 Effective date: 19941210 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Effective date: 19950201 |
|
EUG | Se: european patent has lapsed |
Ref document number: 88401203.0 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 19990405 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20050518 |