EP1530020B1 - Ignition device of at least two pyrotechnical compositions or propulsive charges of a projectile - Google Patents
Ignition device of at least two pyrotechnical compositions or propulsive charges of a projectile Download PDFInfo
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- EP1530020B1 EP1530020B1 EP04292290A EP04292290A EP1530020B1 EP 1530020 B1 EP1530020 B1 EP 1530020B1 EP 04292290 A EP04292290 A EP 04292290A EP 04292290 A EP04292290 A EP 04292290A EP 1530020 B1 EP1530020 B1 EP 1530020B1
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- EP
- European Patent Office
- Prior art keywords
- pyrotechnic
- piston
- sheath
- safety device
- ignition safety
- Prior art date
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- 239000000203 mixture Substances 0.000 title claims description 28
- 230000001141 propulsive effect Effects 0.000 title description 3
- 238000002485 combustion reaction Methods 0.000 claims abstract description 16
- 239000003380 propellant Substances 0.000 claims description 22
- 239000007789 gas Substances 0.000 claims description 8
- 239000007787 solid Substances 0.000 claims description 5
- 239000000567 combustion gas Substances 0.000 claims description 3
- 230000000977 initiatory effect Effects 0.000 description 5
- 238000010304 firing Methods 0.000 description 4
- 230000003111 delayed effect Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- RZVAJINKPMORJF-UHFFFAOYSA-N Acetaminophen Chemical compound CC(=O)NC1=CC=C(O)C=C1 RZVAJINKPMORJF-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 229920002379 silicone rubber Polymers 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/10—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by combustion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/18—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved
- F42C15/184—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a slidable carrier
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/28—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
- F42C15/31—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids generated by the combustion of a pyrotechnic or explosive charge within the fuze
Definitions
- the technical field of the invention is that of ignition safety devices of a pyrotechnic composition or a propellant charge of ammunition.
- Known igniters include a pyrotechnic component capable of generating a flame whose temperature is sufficient to ignite a propellant charge or a useful pyrotechnic composition (smoke composition, illuminant or gas generator for example).
- Such a pyrotechnic component is initiated by an electric current. It may be a component with hot wire, exploded wire or semiconductor bridge.
- the components usually used are safety components type 1Ampere / 1Watt, that is components that do not operate powered by a current of an ampere and under a power of one watt for a predefined period. These components consume a lot of electrical energy.
- One solution for igniting these different propellant charges or compositions is to use as many ignition devices as there are propellant charges or compositions to be ignited, the time delay between the ignition of the different charges being managed by an electronic module .
- Patent DE325292 which forms a basis for the preamble of claim 1, discloses a pyrotechnic double-chain starting device.
- the two pyrotechnic chains allow to initiate a single charge.
- the second chain to overcome a possible malfunction of the first pyrotechnic chain.
- the object of the present invention is to provide a pyrotechnic device initiating several pyrotechnic chains simultaneously from a single initiator and thus making it possible to switch on successively different pyrotechnic compositions or different propellant charges of ammunition.
- the subject of the invention is therefore a safety device for igniting at least two pyrotechnic compositions or propellant charges of a projectile, characterized in that it comprises at least two distinct pyrotechnic chains integrated into a mechanical device and initiated by a single igniter, each pyrotechnic chain allowing via at least one relay to initiate the pyrotechnic composition or corresponding propellant charge, at least a first pyrotechnic chain being slower combustion than a second pyrotechnic chain combustion or action rapid, the mechanical device consisting of movable elements relative to each other, to ensure an interruption of the slow pyrotechnic chain or chains if the combustion chain or rapid action did not work properly.
- the mechanical device consists of a piston sliding in an inner sheath itself slidably mounted in a bore of a body, the sheath carrying at least one opening allowing, when the sheath is in an armed position to connect the or slow pyrotechnic strings to at least one of the relays.
- the piston is movable under the action of the combustion gases of a pyrotechnic composition or a propellant charge initiated by the rapid pyrotechnic chain, against the action of a spring bearing on a support integral with the body.
- the piston consists of a massive portion extended by a skirt provided with a radial bore and enclosing the pyrotechnic relay.
- the device comprises means ensuring the locking of the piston and the sheath after displacement of the piston under the action of the combustion gases of the composition or propellant charge initiated by the rapid pyrotechnic chain.
- the means ensuring the locking of the piston and the sheath may be constituted by a finger disposed in a radial hole of the piston and subjected to the action of a spring, finger for cooperating with a first opening carried by the sheath.
- the body may comprise two longitudinal channels, at least one of the channels containing a delay pyrotechnic composition, a radial opening of the body making the body communicate with one another. channel enclosing the slow pyrotechnic chain with radial drilling of the piston skirt.
- one of the channels of the body may be empty and will thus directly connect the igniter to one of the relays.
- the body may have a radial opening disposed at the level of the pyrotechnic composition or propellant charge P2, opening closed by the sheath when it is in the safety position.
- a first advantage of the device according to the invention lies in the fact that it allows to initiate several pyrotechnic compositions or propellant charges with a single igniter.
- Another advantage lies in the fact that such a device requires very little electrical energy, which avoids the use of particularly bulky electrical capacity.
- Another advantage lies in the fact that the electrical energy can be supplied to the device at the last moment (for example during its ejection), which avoids any risk of accidental ignition during the handling of the projectile.
- FIG. 1 represents in partial section a projectile 100 equipped with an ignition safety device 1 according to the invention.
- the projectile 100 comprises two propulsive charges P1 and P2 that can be wish to initiate with some delay between them.
- the ignition safety device 1 is arranged to trigger the firing of the two propellant charges successively.
- a source not shown which may be a battery incorporated in the projectile or secured to a launch tube (not shown) and connected to the projectile by son broken during firing.
- FIG. 2a is a longitudinal sectional view of the ignition safety device 1 according to the invention in its safety position.
- the ignition safety device 1 consists of a casing 4 of substantially cylindrical tubular shape enclosing an electronic module 2 and a mechanical-pyrotechnic module 3 arranged in the present case in the extension of one another. Alternatively, these modules could be arranged side by side.
- the electronic module 2 is connected at one end to a connector 6, itself connected to a power source (not shown in this figure).
- the electronic module 2 consists of conventional electronic elements 34, such as energy accumulators, an electronic timer, as well as speed and / or acceleration sensors making it possible to know the ejection parameters of the projectile and that it is not necessary to describe for the understanding of the invention.
- the mechano-pyrotechnic module 3 comprises at one end an igniter support 30 extended by a body 15 within which an internal sheath 16 slides.
- Body and sheath may be made of metallic material or of a synthetic material that is sufficiently resistant to the stresses mechanical.
- the mechano-pyrotechnic module 3 comprises at its other end a tubular outlet 5 cooperating with the thruster P1
- FIG. 2b is a longitudinal sectional view of support 30 and body 15 alone
- FIG. 2c is a longitudinal sectional view of sheath 16 alone
- FIG. 2d is a longitudinal sectional view of piston 17.
- the body 15 is in abutment against one end of the tubular casing 4 which carries the tubular outlet 5. It has an internal bore 15b whose bottom constitutes an abutment surface 15a whose role will be explained below.
- the body 15 comprises at its lateral wall two longitudinal cylindrical channels 21 and 22 (the latter shown in dashed lines) intended to respectively contain the pyrotechnic chains 11 and 12.
- the channel 21 encloses a slow pyrotechnic chain 11 and the channel 22 is empty.
- the side wall of the body 15 is pierced with a radial opening 19 which is arranged opposite the propellant P2 (not shown).
- the channel 22 communicates with a chamber 45 connected to the tubular outlet 5 carrying a relay 13.
- the channel 21 also communicates with the internal bore 15b by a radial opening 40 whose role will be explained below.
- the inner sheath 16 is slidably mounted inside the body 15 and is provided with two radial openings 24 and 35 axially offset from one another and with respect to the opening 19 of the body 15.
- This sheath 16 is present in the form of a simple sheath. It contains a piston 17 slidably mounted against the action of a spring 20.
- This piston comprises a solid portion 41 extended by a skirt 42.
- the solid portion 41 is in abutment against the abutment surface 15a of the body 15 and the skirt 42 partially surrounds the spring 20 which bears against the igniter support 30.
- the solid portion 41 carries a shearable peripheral collar 46 which axially immobilizes the sheath 16 relative to the piston 17 and to the body 15 in the safety position of FIG. 2a.
- the solid portion 41 of the piston 17 is provided with a radial hole 43 intended to house a finger 18 subjected to the action of a spring 23.
- the finger assembly 18 and spring 23 constitutes a system for securing the piston 17 and of the sheath 16 in a configuration which will be explained below.
- the skirt 42 is provided with a radial bore 44.
- the support 30 carries an igniter 10 which is electrically connected to the electronic module 2 and which faces the two pyrotechnic chains 11 and 12 housed in the respective channels 21 and 22.
- a first pyrotechnic relay 13 is disposed in the tubular outlet 5. It receives directly the gases produced by the igniter 10 which are led through the channel 22 and the chamber 45. It ensures the ignition of the thruster P1.
- a second pyrotechnic relay 14 is disposed in a housing 25 of the skirt 42 of the piston 17, in the vicinity of the bore 44.
- the device 1 is in the safety position.
- the sheath 16 closes the openings 19 and 40 of the body 15.
- the sheath 16 thus isolates the relay 14 from both the slow pyrotechnic chain 11 and the propellant P2.
- Figure 2e is a cross-sectional view of the body alone, section taken along the plane AA. This sectional view shows the disposition of the cylindrical channels 21 and 22 placed side by side in the body 15, without communicating with each other, the channel 21 enclosing the pyrotechnic chain 11 the channel 22 being empty .
- FIGS. 3a to 3d illustrate the different operating phases of the device according to the invention.
- the electronic module 2 controls the initiation of the igniter 10 ( Figure 3a).
- the gases of the latter penetrate simultaneously into the two channels 21 and 22. They ensure the initiation of the slow pyrotechnic chain 11 while directly lighting the first relay 13 through the empty channel 22 and the chamber 45.
- the ignition of the first relay 13 causes the initiation of the thruster P1.
- the firing of the thruster P1 then creates an increase in pressure in the chamber 45 which causes the recoil of the piston 17 and causes the shearing of the flange 46.
- the piston 17 compresses the spring 20 as shown in Figure 3c.
- the finger 18 then comes opposite the opening 24 of the sheath 16 and is pushed by the spring 23 into this opening.
- the piston 17 and the sheath 16 are thus secured.
- the bore 44 of the piston 17 is positioned opposite the opening 35 of the sheath 16.
- This translation of the sheath 16 positions the bore 44 of the piston and the opening 35 of the sheath 16 opposite the opening 40 of the body 15.
- the end of the slow combustion pyrotechnic chain 11 is thus connected to the second pyrotechnic relay 14.
- the chain 11 with slow combustion through the opening 35 of the sheath 16 and the bore 44 of the piston 17, initiates, at the end of its combustion, the second relay 14 disposed in the housing 25, then the thruster P2 via the opening 19 of the body 15. It was thus made in a simple manner a device allowing from a single igniter to provide a successive and delayed initiation of two thrusters P1 and P2.
- the operation of the device according to the invention is of course identical when the charges to be initiated are pyrotechnic timed ignition compositions, for example smoke compositions.
- the thruster P1 is not initiated, for example as a result of a fault of the first relay 13, the piston 17 and the sheath 16 do not move and the second relay 14 can not be initiated by the slow pyrotechnic chain.
- the device according to the invention thus ensures ignition safety of the second thruster.
- the latter can be turned on only after the delay whose duration is determined by the pyrotechnic delay composition 11 and only if the first thruster has operated and completed its combustion.
- Relays 13 and 14 are pyrotechnic relays. They will be made and arranged so as to create a sufficient gas evolution and whose temperature will be high enough to ignite the pyrotechnic compositions of propellants P1 and P2.
- a non-return valve (not shown) may also be provided in the channel 22 of the fast-combustion chain 12 in order to prevent the gases from the combustion of the propellant P1 coming through this channel 22 to disturb the operation of the the chain 11 with slow combustion.
- Such an anti-return valve is conventional. It may include a ball applied on a conical seat by a return spring and closing a gas passage opening. The gases can then flow only in one direction in the channel 22.
- the sealing of the ignition device according to the invention can be improved by using sealing elements such as O-rings disposed between the concentric parts (body 15 / casing 4, sheath 16 / body 15, piston 17 / sheath 16). ).
- the invention has been described here with the association of a slow pyrotechnic chain, comprising a pyrotechnic delay housed in a channel, and a fast chain in which the channel 22 is free of any composition.
- each channel 21 and 22 contains a pyrotechnic delay composition.
- the combustion rates and / or the lengths of each pyrotechnic chain 11, 12 will be chosen different according to the needs.
- a device comprising more than two delayed pyrotechnic chains.
- another relay will be provided, arranged in a separate chamber of the piston, and which will communicate when the device is in its armed position, on the one hand with the third pyrotechnic chain and on the other hand with a third composition or propellant charge. to initiate.
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Abstract
Description
Le domaine technique de l'invention est celui des dispositifs de sécurité d'allumage d'une composition pyrotechnique ou bien d'une charge propulsive de munition.The technical field of the invention is that of ignition safety devices of a pyrotechnic composition or a propellant charge of ammunition.
Les allumeurs connus comprennent un composant pyrotechnique susceptible d'engendrer une flamme dont la température est suffisante pour allumer une charge propulsive ou bien une composition pyrotechnique utile (composition fumigène, éclairante ou génératrice de gaz par exemple).Known igniters include a pyrotechnic component capable of generating a flame whose temperature is sufficient to ignite a propellant charge or a useful pyrotechnic composition (smoke composition, illuminant or gas generator for example).
Un tel composant pyrotechnique est initié par un courant électrique. Il pourra être un composant à fil chaud, à fil explosé ou encore à pont semi-conducteur. Les composants utilisés habituellement sont des composants de sécurité de type 1Ampère / 1Watt, c'est à dire des composants qui ne fonctionnent pas alimentés par un courant d'un ampère et sous une puissance d'un watt pendant une durée prédéfinie. Ces composants consomment beaucoup d'énergie électrique.Such a pyrotechnic component is initiated by an electric current. It may be a component with hot wire, exploded wire or semiconductor bridge. The components usually used are safety components type 1Ampere / 1Watt, that is components that do not operate powered by a current of an ampere and under a power of one watt for a predefined period. These components consume a lot of electrical energy.
Dans le cas de certains projectiles, la propulsion est assurée par plusieurs charges propulsives initiées successivement. D'autres projectiles comportent plusieurs compositions pyrotechniques allumées successivement.In the case of certain projectiles, the propulsion is ensured by several propulsive charges initiated successively. Other projectiles include several pyrotechnic compositions lit successively.
Une solution pour allumer ces différentes charges propulsives ou compositions consiste à mettre en oeuvre autant de dispositifs d'allumage qu'il y a de charges propulsives ou de compositions à allumer, la temporisation entre l'allumage des différentes charges étant gérée par un module électronique.One solution for igniting these different propellant charges or compositions is to use as many ignition devices as there are propellant charges or compositions to be ignited, the time delay between the ignition of the different charges being managed by an electronic module .
Un inconvénient de ce type de solution réside dans le fait qu'il nécessite une importante énergie électrique, donc des moyens de stockage de cette énergie.A disadvantage of this type of solution lies in the fact that it requires a large electrical energy, so storage means of this energy.
On connaît par le brevet DE325292, qui forme une base pour le préambule de la revendication 1, un dispositif d'amorçage à double chaîne pyrotechnique. Les deux chaînes pyrotechniques permettent d'initier une seule et unique charge. La seconde chaîne permettant de pallier un éventuel dysfonctionnement de la première chaîne pyrotechnique.Patent DE325292, which forms a basis for the preamble of
Le but de la présente invention est de fournir un dispositif pyrotechnique initiant plusieurs chaînes pyrotechniques simultanément à partir d'un initiateur unique et permettant ainsi d'allumer successivement différentes compositions pyrotechniques ou bien différentes charges propulsives de munition.The object of the present invention is to provide a pyrotechnic device initiating several pyrotechnic chains simultaneously from a single initiator and thus making it possible to switch on successively different pyrotechnic compositions or different propellant charges of ammunition.
L'invention a donc pour objet un dispositif de sécurité d'allumage d'au moins deux compositions pyrotechniques ou charges propulsives d'un projectile, caractérisé en ce qu'il comprend au moins deux chaînes pyrotechniques distinctes intégrées dans un dispositif mécanique et initiées par un inflammateur unique, chaque chaîne pyrotechnique permettant par l'intermédiaire d'au moins un relais d'initier la composition pyrotechnique ou charge propulsive correspondante, au moins une première chaîne pyrotechnique étant à combustion plus lente qu' une deuxième chaîne pyrotechnique à combustion ou action rapide, le dispositif mécanique étant constitué d'éléments mobiles les uns par rapport aux autres, permettant d'assurer une interruption de la ou des chaînes pyrotechniques lentes si la chaîne à combustion ou action rapide n'a pas fonctionné correctement.The subject of the invention is therefore a safety device for igniting at least two pyrotechnic compositions or propellant charges of a projectile, characterized in that it comprises at least two distinct pyrotechnic chains integrated into a mechanical device and initiated by a single igniter, each pyrotechnic chain allowing via at least one relay to initiate the pyrotechnic composition or corresponding propellant charge, at least a first pyrotechnic chain being slower combustion than a second pyrotechnic chain combustion or action rapid, the mechanical device consisting of movable elements relative to each other, to ensure an interruption of the slow pyrotechnic chain or chains if the combustion chain or rapid action did not work properly.
Avantageusement, le dispositif mécanique est constitué d'un piston coulissant dans une gaine interne elle-même montée glissante dans un alésage d'un corps, la gaine portant au moins une ouverture permettant, lorsque la gaine se trouve dans une position armée de relier la ou les chaînes pyrotechniques lentes à au moins un des relais.Advantageously, the mechanical device consists of a piston sliding in an inner sheath itself slidably mounted in a bore of a body, the sheath carrying at least one opening allowing, when the sheath is in an armed position to connect the or slow pyrotechnic strings to at least one of the relays.
Avantageusement encore, le piston est mobile sous l'action des gaz de combustion d'une composition pyrotechnique ou d'une charge propulsive initiée par la chaîne pyrotechnique rapide, contre l'action d'un ressort en appui sur un support solidaire du corps.Advantageously, the piston is movable under the action of the combustion gases of a pyrotechnic composition or a propellant charge initiated by the rapid pyrotechnic chain, against the action of a spring bearing on a support integral with the body.
Avantageusement encore, le piston est constitué d'une partie massive prolongée par une jupe munie d'un perçage radial et renfermant le relais pyrotechnique.Advantageously, the piston consists of a massive portion extended by a skirt provided with a radial bore and enclosing the pyrotechnic relay.
Avantageusement encore, le dispositif comporte des moyens assurant le verrouillage du piston et de la gaine après déplacement du piston sous l'action des gaz de combustion de la composition ou charge propulsive initiée par la chaîne pyrotechnique rapide.Advantageously, the device comprises means ensuring the locking of the piston and the sheath after displacement of the piston under the action of the combustion gases of the composition or propellant charge initiated by the rapid pyrotechnic chain.
Les moyens assurant le verrouillage du piston et de la gaine pourront être constitués par un doigt disposé dans un trou radial du piston et soumis à l'action d'un ressort, doigt destiné à coopérer avec une première ouverture portée par la gaine.The means ensuring the locking of the piston and the sheath may be constituted by a finger disposed in a radial hole of the piston and subjected to the action of a spring, finger for cooperating with a first opening carried by the sheath.
Le corps pourra comprendre deux canaux longitudinaux, un au moins des canaux renfermant une composition pyrotechnique retard, une ouverture radiale du corps faisant communiquer le canal renfermant la chaîne pyrotechnique lente avec le perçage radial de la jupe du piston.The body may comprise two longitudinal channels, at least one of the channels containing a delay pyrotechnic composition, a radial opening of the body making the body communicate with one another. channel enclosing the slow pyrotechnic chain with radial drilling of the piston skirt.
Selon un mode de réalisation, un des canaux du corps pourra être vide et permettra ainsi de relier directement l'inflammateur à un des relais.According to one embodiment, one of the channels of the body may be empty and will thus directly connect the igniter to one of the relays.
Le corps pourra présenter une ouverture radiale disposée au niveau de la composition pyrotechnique ou charge propulsive P2, ouverture obturée par la gaine quand elle est en position de sécurité.The body may have a radial opening disposed at the level of the pyrotechnic composition or propellant charge P2, opening closed by the sheath when it is in the safety position.
Un tout premier avantage du dispositif selon l'invention réside dans le fait qu'il permet d'initier plusieurs compositions pyrotechniques ou charges propulsives avec un unique inflammateur.A first advantage of the device according to the invention lies in the fact that it allows to initiate several pyrotechnic compositions or propellant charges with a single igniter.
Un autre avantage réside dans le fait qu'un tel dispositif ne nécessite que très peu d'énergie électrique, ce qui évite l'utilisation de capacités électriques particulièrement encombrantes.Another advantage lies in the fact that such a device requires very little electrical energy, which avoids the use of particularly bulky electrical capacity.
Un autre avantage réside dans le fait que l'énergie électrique peut n'être fournie au dispositif qu'au dernier moment (par exemple lors de son éjection), ce qui évite tout risque d'inflammation accidentelle lors de la manipulation du projectile.Another advantage lies in the fact that the electrical energy can be supplied to the device at the last moment (for example during its ejection), which avoids any risk of accidental ignition during the handling of the projectile.
D'autres caractéristiques, détails et avantages de l'invention ressortiront plus clairement de la description donnée ci-après à titre indicatif en relation avec des dessins dans lesquels :
- la figure 1 représente en coupe un projectile équipé d'un dispositif de sécurité d'allumage selon l'invention,
- le figure 2a représente en coupe longitudinale le dispositif de sécurité d'allumage selon l'invention,
- les figures 2b à 2e sont des vues en coupe des pièces constituant le module mécano-pyrotechnique, et
- les figures 3a à 3d illustrent le dispositif de sécurité d'allumage selon l'invention à différentes étapes de fonctionnement.
- FIG. 1 is a sectional view of a projectile equipped with an ignition safety device according to the invention,
- FIG. 2a is a longitudinal section of the ignition safety device according to the invention,
- FIGS. 2b to 2e are sectional views of the parts constituting the mechano-pyrotechnic module, and
- Figures 3a to 3d illustrate the ignition safety device according to the invention at different stages of operation.
La figure 1 représente en coupe partielle un projectile 100 équipé d'un dispositif de sécurité d'allumage 1 selon l'invention. Dans cet exemple de réalisation, le projectile 100 comporte deux charges propulsives P1 et P2 que l'on souhaite initier avec un certain retard entre elles. Le dispositif de sécurité d'allumage 1 est disposé de manière à déclencher la mise à feu des deux charges propulsives de manière successive.FIG. 1 represents in partial section a
Il est alimenté en énergie à partir d'une source non représentée qui pourra être une pile incorporée au projectile ou bien solidaire d'un tube de lancement (non représenté) et reliée au projectile par des fils rompus lors du tir.It is supplied with energy from a source not shown which may be a battery incorporated in the projectile or secured to a launch tube (not shown) and connected to the projectile by son broken during firing.
La figure 2a représente en vue en coupe longitudinale le dispositif de sécurité d'allumage 1 selon l'invention dans sa position de sécurité. Le dispositif de sécurité d'allumage 1 est constitué d'une enveloppe 4 de forme tubulaire sensiblement cylindrique renfermant un module électronique 2 et un module mécano-pyrotechnique 3 disposés dans le cas présent dans le prolongement l'un de l'autre. En variante, ces modules pourraient être disposés côte à côte. Le module électronique 2 est relié à une extrémité à un connecteur 6, lui-même relié à une source d'énergie (non représentée sur cette figure). Le module électronique 2 est constitué d'éléments électroniques 34 classiques, tels des accumulateurs d'énergie, un temporisateur électronique, ainsi que des capteurs de vitesse et/ou d'accélération permettant de connaître les paramètres d'éjection du projectile et qu'il n'est pas nécessaire de décrire pour la compréhension de l'invention.FIG. 2a is a longitudinal sectional view of the
Afin de protéger les éléments électroniques 34 des contraintes thermiques et mécaniques qui nuiraient au fonctionnement correct du module électronique 2, celui-ci pourrait être noyé dans un enrobage 9, par exemple de type élastomère silicone.In order to protect the
Le module mécano-pyrotechnique 3 comporte à une extrémité un support d'inflammateur 30 prolongé par un corps 15 à l'intérieur duquel coulisse une gaine interne 16. Corps et gaine peuvent être réalisés en matériau métallique ou en un matériau synthétique suffisamment résistant aux contraintes mécaniques. Le module mécano-pyrotechnique 3 comporte à son autre extrémité une sortie tubulaire 5 coopérant avec le propulseur P1The mechano-
Les figures 2b à 2e représentent isolément différents éléments du module mécano-pyrotechnique de manière à mieux mettre en évidence leurs caractéristiques techniques. La figure 2b est une vue en coupe longitudinale du support 30 et du corps 15 seuls, la figure 2c est une vue en coupe longitudinale de la gaine 16 seule et la figure 2d est une vue en coupe longitudinale du piston 17.Figures 2b to 2e represent separately different mechano-pyrotechnic module elements in order to better highlight their technical characteristics. FIG. 2b is a longitudinal sectional view of
Le corps 15 est en butée contre une extrémité de l'enveloppe tubulaire 4 qui porte la sortie tubulaire 5. Il comporte un alésage interne 15b dont le fond constitue une surface de butée 15a dont le rôle sera expliqué ci-après. Le corps 15 comporte au niveau de sa paroi latérale deux canaux cylindriques longitudinaux 21 et 22 (ce dernier représenté en pointillés) destinés à contenir respectivement les chaînes pyrotechniques 11 et 12. Ici le canal 21 renferme une chaîne pyrotechnique lente 11 et le canal 22 est vide.The
La paroi latérale du corps 15 est percée d'une ouverture radiale 19 qui est disposée en regard du propulseur P2 (non représenté). Le canal 22 communique avec une chambre 45 raccordée à la sortie tubulaire 5 portant un relais 13. Le canal 21 communique également avec l'alésage interne 15b par une ouverture radiale 40 dont le rôle sera expliqué ci-après.The side wall of the
La gaine interne 16 est montée coulissante à l'intérieur du corps 15 et elle est munie de deux ouvertures radiales 24 et 35 décalées axialement l'une de l'autre et par rapport à l'ouverture 19 du corps 15. Cette gaine 16 se présente sous la forme d'un simple fourreau. Elle renferme un piston 17 monté coulissant contre l'action d'un ressort 20. Ce piston comprend une partie massive 41 prolongée par une jupe 42. La partie massive 41 est en butée contre la surface de butée 15a du corps 15 et la jupe 42 entoure partiellement le ressort 20 qui est en appui contre le support d'inflammateur 30. La partie massive 41 porte une collerette périphérique 46 cisaillable qui immobilise axialement la gaine 16 par rapport au piston 17 et au corps 15 dans la position de sécurité de la figure 2a.The
La partie massive 41 du piston 17 est munie d'un trou radial 43 destiné à loger un doigt 18 soumis à l'action d'un ressort 23. L'ensemble doigt 18 et ressort 23 constitue un système permettant la solidarisation du piston 17 et de la gaine 16 dans une configuration qui sera expliquée ci-après. La jupe 42 est munie d'un perçage radial 44.The
Cet ensemble mécanique qui vient d'être décrit renferme les éléments pyrotechniques nécessaires au fonctionnement du dispositif selon l'invention. Le support 30 porte un inflammateur 10 qui est relié électriquement au module électronique 2 et qui se trouve en regard des deux chaînes pyrotechniques 11 et 12 logées dans les canaux respectifs 21 et 22. Un premier relais pyrotechnique 13 est disposé dans la sortie tubulaire 5. Il reçoit directement les gaz produits par l'inflammateur 10 qui lui sont conduits par le canal 22 et la chambre 45. Il assure l'allumage du propulseur P1. Un deuxième relais pyrotechnique 14 est disposé dans un logement 25 de la jupe 42 du piston 17, au voisinage du perçage 44.This mechanical assembly which has just been described contains the pyrotechnic elements necessary for the operation of the device according to the invention. The
Sur la figure 2a, le dispositif 1 est en position de sécurité. Dans cette position la gaine 16 obture les ouvertures 19 et 40 du corps 15. La gaine 16 isole donc le relais 14 à la fois de la chaîne pyrotechnique lente 11 et du propulseur P2.In Figure 2a, the
La figure 2e est une vue en coupe transversale du corps 15 seul, coupe réalisée suivant le plan AA. Cette vue en coupe permet d'observer la disposition des canaux cylindriques 21 et 22 placés côte à côte dans le corps 15, sans pour autant communiquer l'un avec l'autre, le canal 21 renfermant la chaîne pyrotechnique 11 le canal 22 étant vide.Figure 2e is a cross-sectional view of the body alone, section taken along the plane AA. This sectional view shows the disposition of the
Les figures 3a à 3d illustrent les différentes phases de fonctionnement du dispositif selon l'invention.FIGS. 3a to 3d illustrate the different operating phases of the device according to the invention.
Lorsque les conditions de déclenchement sont réunies (le projectile a été éjecté de son tube de lancement, sa vitesse est vérifiée supérieure à un seuil prédéterminé et après une temporisation électronique assurant la distance de sécurité de tir), le module électronique 2 commande l'initiation de l'inflammateur 10 (figure 3a). Les gaz de ce dernier pénètrent simultanément dans les deux canaux 21 et 22. Ils assurent l'initiation de la chaîne pyrotechnique lente 11 tout en allumant directement le premier relais 13 au travers du canal vide 22 et de la chambre 45.When the trigger conditions are met (the projectile has been ejected from its launch tube, its speed is verified above a predetermined threshold and after an electronic delay ensuring the firing safety distance), the
L'allumage du premier relais 13 (figure 3b) entraîne l'initiation du propulseur P1.The ignition of the first relay 13 (Figure 3b) causes the initiation of the thruster P1.
La mise à feu du propulseur P1 crée alors une augmentation de pression dans la chambre 45 ce qui provoque le recul du piston 17 et entraîne le cisaillement de la collerette 46. Le piston 17 comprime le ressort 20 comme représenté sur la figure 3c. Le doigt 18 vient alors en regard de l'ouverture 24 de la gaine 16 et il est poussé par le ressort 23 dans cette ouverture. On réalise ainsi la solidarisation du piston 17 et de la gaine 16. Dans le même temps le perçage 44 du piston 17 se positionne en regard de l'ouverture 35 de la gaine 16.The firing of the thruster P1 then creates an increase in pressure in the
En fin de combustion du propulseur P1, la pression dans la chambre 45 diminue et sous l'effort prépondérant du ressort 20 le piston 17 revient dans sa position initiale, entraînant la gaine 16 dont il est solidaire jusqu'en butée contre la surface de butée 15a du corps 15 comme illustré sur la figure 3d. Le dispositif se trouve alors dans sa position armée.At the end of the combustion of the thruster P1, the pressure in the
Cette translation de la gaine 16 positionne le perçage 44 du piston ainsi que l'ouverture 35 de la gaine 16 en regard de l'ouverture 40 du corps 15.This translation of the
L'extrémité de la chaîne pyrotechnique à combustion lente 11 se trouve donc reliée au deuxième relais pyrotechnique 14.The end of the slow combustion
Par ailleurs le déplacement de la gaine 16 libère l'ouverture 19 du corps 15.Moreover, the displacement of the
Ainsi, la chaîne 11 à combustion lente, par l'intermédiaire de l'ouverture 35 de la gaine 16 et du perçage 44 du piston 17, initie, à l'issue de sa combustion, le deuxième relais 14 disposé dans le logement 25, puis le propulseur P2 par l'intermédiaire de l'ouverture 19 du corps 15. On a ainsi réalisé de manière simple un dispositif permettant à partir d'un seul inflammateur d'assurer une initiation successive et temporisée de deux propulseurs P1 et P2.Thus, the
Le fonctionnement du dispositif selon l'invention est bien entendu identique lorsque les charges à initier sont des compositions pyrotechniques à allumage temporisé, par exemple des compositions fumigènes.The operation of the device according to the invention is of course identical when the charges to be initiated are pyrotechnic timed ignition compositions, for example smoke compositions.
Si le propulseur P1 n'est pas initié, par exemple comme suite à un défaut du premier relais 13, le piston 17 et la gaine 16 ne bougent pas et le deuxième relais 14 ne peut être initié par la chaîne pyrotechnique lente. Le dispositif selon l'invention assure ainsi une sécurité d'allumage du deuxième propulseur. Ce dernier ne pouvant être allumé qu'à l'issue du retard dont la durée est déterminée par la composition pyrotechnique retard 11 et uniquement si le premier propulseur a fonctionné et achevé sa combustion.If the thruster P1 is not initiated, for example as a result of a fault of the
Les relais 13 et 14 sont des relais pyrotechniques. Ils seront réalisés et disposés de manière à créer un dégagement gazeux suffisant et dont la température sera suffisamment élevée pour enflammer les compositions pyrotechniques des propulseurs P1 et P2.Relays 13 and 14 are pyrotechnic relays. They will be made and arranged so as to create a sufficient gas evolution and whose temperature will be high enough to ignite the pyrotechnic compositions of propellants P1 and P2.
On pourra également prévoir un clapet anti-retour (non représenté) dans le canal 22 de la chaîne 12 à combustion rapide afin d'éviter que les gaz issus de la combustion du propulseur P1 ne vienne au travers de ce canal 22 perturber le fonctionnement de la chaîne 11 à combustion lente.A non-return valve (not shown) may also be provided in the
Un tel clapet anti retour est classique. Il pourra comporter une bille appliquée sur une portée conique par un ressort de rappel et venant obturer un orifice de passage des gaz. Les gaz ne pourront alors circuler que dans un seul sens dans le canal 22.Such an anti-return valve is conventional. It may include a ball applied on a conical seat by a return spring and closing a gas passage opening. The gases can then flow only in one direction in the
On pourra améliorer l'étanchéité du dispositif d'allumage selon l'invention en utilisant des éléments d'étanchéité, tels des joints toriques disposés entre les pièces concentrique (corps 15/enveloppe 4; gaine 16/ corps 15; piston 17/ gaine 16).The sealing of the ignition device according to the invention can be improved by using sealing elements such as O-rings disposed between the concentric parts (
L'invention a été ici décrite avec l'association d'une chaîne pyrotechnique lente, comprenant un retard pyrotechnique logé dans un canal, et d'une chaîne rapide dans laquelle le canal 22 est libre de toute composition.The invention has been described here with the association of a slow pyrotechnic chain, comprising a pyrotechnic delay housed in a channel, and a fast chain in which the
En fonction des besoins opérationnels, il est bien entendu possible de réaliser un dispositif de sécurité d'allumage selon l'invention dans lequel chaque canal 21 et 22 renferme une composition pyrotechnique à retard. Les vitesses de combustion et/ou les longueurs de chaque chaîne pyrotechnique 11, 12 seront choisies différentes en fonction des besoins.Depending on the operational requirements, it is of course possible to provide an ignition safety device according to the invention in which each
Il est également possible de définir un dispositif comprenant plus de deux chaînes pyrotechnique à retard. Dans ce cas on prévoira un autre relais, disposé dans un chambre distincte du piston, et qui communiquera lorsque le dispositif sera dans sa position armée, d'une part avec la troisième chaîne pyrotechnique et d'autre part avec une troisième composition ou charge propulsive à initier.It is also possible to define a device comprising more than two delayed pyrotechnic chains. In this case another relay will be provided, arranged in a separate chamber of the piston, and which will communicate when the device is in its armed position, on the one hand with the third pyrotechnic chain and on the other hand with a third composition or propellant charge. to initiate.
Claims (9)
- An ignition safety device (1) for at least two pyrotechnic compositions or propellant charges for a projectile (100), comprising at least two separate pyrotechnic trains (11, 12) integrated into a mechanical device (15, 16, 17) and ignited by a single squib (10), each pyrotechnic train enabling, by means of at least one relay (13, 14), the corresponding pyrotechnic composition or propellant charge (P1, P2) to be ignited, at least a first pyrotechnic train (11) being of slower combustion than a second pyrotechnic train (12) with faster action or combustion, characterised in that the mechanical device (15, 16, 17) is formed of elements able to move with respect to one another enabling the interruption of the slow pyrotechnic train(s) to be ensured should the pyrotechnic train with faster action or combustion not have functioned correctly.
- An ignition safety device (1) according to Claim 1, characterised in that the mechanical device is constituted by a piston (17) sliding in an internal sheath (16) itself mounted able to slide in a bore hole (15b) in a body (15), the sheath having at least one opening (35) which, when the sheath (16) is in its armed position, enables the slow pyrotechnic train or trains to be connected to at least one of the relays (14).
- An ignition safety device (1) according to Claim 2, characterised in that the piston (17) can move under the action of the combustion gases of a pyrotechnic composition or a propellant charge ignited by the fast pyrotechnic train, against the action of a spring (20) pressing on a support (30) integral with the body.
- An ignition safety device (1) according to Claim 3, characterised in that the piston (17) is constituted by a solid part (41) extended by a skirt (42) provided with a radial drill hole (44) and enclosing the pyrotechnic relay (14).
- An ignition safety device (1) according to one of Claims 3 or 4, characterised in that it incorporates means to ensure the piston (17) and sheath (16) are locked in place after the piston (17) has moved under the action of the combustive gases from the composition or propellant charge ignited by the fast pyrotechnic train (12).
- An ignition safety device (1) according to Claim 5, characterised in that the means locking the piston (17) and sheath (16) in place are constituted by a finger (18) positioned in a radial hole (43) in the piston (17) and subject to a spring (23), such finger intended to cooperate with a first opening (24) in the sheath (16).
- An ignition safety device (1) according to one of Claims 4 to 6, characterised in that the body (15) incorporates two longitudinal canals (21, 22), at least one of which encloses a pyrotechnic delay composition (11), a radial opening (40) in the body (15) enabling the canal (21) enclosing the slow pyrotechnic train (11) to communicate with the radial drill hole (44) in the skirt (42) of the piston (17).
- An ignition safety device (1) according to Claim 7, characterised in that one of the canals (22) in the body (15) is empty enabling the squib (10) to be directly connected to one of the relays (13).
- An ignition safety device (1) according to Claim 7, characterised in that the body (15) has a radial opening (19) arranged near the pyrotechnic composition or propellant charge P2, such opening being blocked by the sheath (16) when this is in the safety position.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0312996A FR2861842B1 (en) | 2003-11-05 | 2003-11-05 | MECANO-PYROTECHNIC MODULE |
FR0312996 | 2003-11-05 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1530020A1 EP1530020A1 (en) | 2005-05-11 |
EP1530020B1 true EP1530020B1 (en) | 2006-12-06 |
Family
ID=34429928
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04292290A Active EP1530020B1 (en) | 2003-11-05 | 2004-09-23 | Ignition device of at least two pyrotechnical compositions or propulsive charges of a projectile |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1530020B1 (en) |
AT (1) | ATE347680T1 (en) |
DE (1) | DE602004003544T2 (en) |
FR (1) | FR2861842B1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012014150A1 (en) * | 2012-07-18 | 2014-01-23 | Rheinmetall Waffe Munition Gmbh | Pressure-controlled delay element and ammunition |
DE102013013705A1 (en) | 2013-08-20 | 2015-02-26 | Rheinmetall Waffe Munition Gmbh | Pyrotechnic deceleration device for an ammunition fuse and mortar shell with such a delay device |
FR3010784B1 (en) * | 2013-09-16 | 2017-05-19 | Nexter Munitions | DETONATOR WITH DELAY |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE325292C (en) * | 1918-06-11 | 1920-09-23 | Siemens Schuckertwerke G M B H | Double fuse for grenades |
NL176806B (en) * | 1952-03-18 | Zink Co John | FIRE SYSTEM FOR BOTH LIQUID AND GAS FUEL FOR USE IN HOT EXHAUST GAS TUBES. | |
FR2149000A5 (en) * | 1971-08-12 | 1973-03-23 | Ruggieri Ets | Electropyrotechnic igniter - for munitions such as illuminating flare bomb etc |
FR2280878A1 (en) * | 1974-08-01 | 1976-02-27 | France Etat | PYROTECHNICAL TIMED SAFETY RELAY |
FR2346676A1 (en) * | 1976-03-29 | 1977-10-28 | Luchaire Sa | DELAY INITIATION SYSTEM, WITH SAFETY, FOR MACHINERY, ESPECIALLY FOR SELF-PROPELLED MACHINERY |
-
2003
- 2003-11-05 FR FR0312996A patent/FR2861842B1/en not_active Expired - Fee Related
-
2004
- 2004-09-23 AT AT04292290T patent/ATE347680T1/en not_active IP Right Cessation
- 2004-09-23 DE DE602004003544T patent/DE602004003544T2/en not_active Expired - Fee Related
- 2004-09-23 EP EP04292290A patent/EP1530020B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
DE602004003544D1 (en) | 2007-01-18 |
FR2861842A1 (en) | 2005-05-06 |
ATE347680T1 (en) | 2006-12-15 |
DE602004003544T2 (en) | 2007-07-05 |
FR2861842B1 (en) | 2007-12-21 |
EP1530020A1 (en) | 2005-05-11 |
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