EP2239535A1 - Ignition device of a munition by percussion - Google Patents

Ignition device of a munition by percussion Download PDF

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Publication number
EP2239535A1
EP2239535A1 EP10290186A EP10290186A EP2239535A1 EP 2239535 A1 EP2239535 A1 EP 2239535A1 EP 10290186 A EP10290186 A EP 10290186A EP 10290186 A EP10290186 A EP 10290186A EP 2239535 A1 EP2239535 A1 EP 2239535A1
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EP
European Patent Office
Prior art keywords
firing
rod
hammer
ammunition
tip
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP10290186A
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German (de)
French (fr)
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EP2239535B1 (en
Inventor
Renaud Lafont
Pierre Magnan
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Nexter Munitions SA
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Nexter Munitions SA
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Publication date
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Publication of EP2239535A1 publication Critical patent/EP2239535A1/en
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Publication of EP2239535B1 publication Critical patent/EP2239535B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • F42C1/04Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze operating by inertia of members on impact
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/24Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means

Definitions

  • the technical field of the invention is that of ammunition firing devices using a mechanical striker impelling a pyrotechnic composition.
  • the firing devices comprise a firing pin which is projected by inertia on the pyrotechnic composition after the lifting of a certain number of safety barriers.
  • This striker is also often projected by a spring, so as to ensure a self-destruct function (when for example there is no impact on a target).
  • the patent FR-2689972 thus describes a firing device for a projectile medium caliber (caliber between 20 mm and 50 mm).
  • This device comprises a striker which can be pushed to a primer by a spring.
  • the primer is secured to an arming rotor that keeps it away from the striker before firing.
  • the self-destruct spring is maintained in the bandaged state during all the storage and transport phases. Even if this spring compresses slightly more during the firing to allow more often the withdrawal of the locks of the gate rotor, sufficient energy for self destruction requires storage of the spring in the bandaged state.
  • the purpose of the invention is to simplify such a device by proposing an architecture in which the percussive primer is always aligned with the striker, but the shocks undergone during the storage and transport phases can not, however, provoke percussion of the primer.
  • the device according to the invention With the device according to the invention, only the constraints related to shooting can make the device bootable.
  • the invention thus makes it possible to completely secure the percussion function during the storage and transport phases.
  • the invention also allows the implementation of a self-destruction mechanism in which the spring means do not have to be compressed during assembly.
  • This device therefore comprises a firing pin which is permanently aligned with the primer but which is locked by security means which are erased during firing.
  • These safety means comprise two flyweights inertia, the first flyweight releasing the balls locking the striker.
  • This device is of complex structure. It is indeed necessary that the two weights slide in a well-defined order so that the firing pin is released. Indeed the balls are pushed by one of the weights against the second weight. It is therefore necessary for the latter to deviate rapidly during firing to avoid jamming the balls.
  • the second weight remains locked (at least temporarily) to allow the ejection of the striker locking balls.
  • This locking is provided by other balls housed in a groove of the second weight, groove whose bottom is tapered. These locking balls therefore deviate during firing by their axial inertia to engage against a ramp of the firing pin.
  • the energy available to the impact on a target is proportional to the mass of the firing pin and the distance traveled by the latter to initiate the primer.
  • This energy E is equal to myD, where m is the mass of the striker, D is the distance traveled by the striker, and y is the deceleration experienced at impact on a target.
  • the object of the invention is to propose a device of simple design in which only the constraints linked to the firing can make the device startable, and in which the percussion function of the energy supply function for the percussion is completely dissociated.
  • the invention is more particularly applicable in the field of rockets and firing devices comprising micro-machined or micro-engraved elements (MEMS technology such as Micro Electro Mechanical System).
  • MEMS technology such as Micro Electro Mechanical System
  • the device according to the invention is easily transposable to the realization of a device of very small dimensions and in particular a device made according to MEMS technologies.
  • the invention therefore relates to an ammunition firing device, comprising a firing pin intended to impact a pyrotechnic composition to control the initiation of the latter, characterized in that the firing pin comprises a sliding rod during firing.
  • the ammunition by the effect of the firing acceleration from a rest position to an extended position, and lockable in the deployed position, rod secured to a percussion tip occupying a fixed position in contact with the pyrotechnic composition, the rod being completely inside the tip in the rest position and being projecting relative to the tip in the deployed position, the device further comprising a hammer capable of striking the rod during the impact of the ammunition on a target for initiating the composition.
  • the sliding rod can be locked in the deployed position by at least one centrifugal latch.
  • the sliding rod is advantageously connected to the tip by a tension spring.
  • the percussion tip may be secured to a partition which will delimit a cavity receiving the pyrotechnic composition, embrittlement means being provided to separate the tip of the partition during the impact of the hammer.
  • the hammer can be projected against the extensible rod by a spring means.
  • the hammer can thus be in the rest position before firing in the vicinity of the undeployed rod, the spring means being in the uncompressed state and the firing acceleration will cause the movement of the hammer and the compression of the spring means.
  • the hammer may be kept away from the firing pin by holding means comprising at least one centrifugal flyweight cooperating with a fixed ramp.
  • the entire device may be made in the form of micromachined planar elements or micro etched on a wafer.
  • the device may include a riser for setting up the pyrotechnic composition above the tip.
  • the figure 1 schematically shows in section a body 2 of a munition 1 which contains an explosive charge 3. This explosive is initiated by a firing device 4 and a safety and arming device 5 is interposed between the firing device and the explosive charge 3.
  • the safety and arming device 5 is shown here very schematically. It essentially comprises a screen 6 which makes it possible to interrupt the transmission channel 9 between a pyrotechnic composition 8 (integral with the firing device 4) and the explosive charge 3.
  • the screen 6 is movable in translation by the action of motor means which are represented here schematically by a spring 7.
  • locking means (not shown) will release the flap 6 as a result of the detection of different events associated with ammunition firing (eg inertial locks).
  • the safety and arming device 5, the firing device 4 and the body 2 of the ammunition are connected to each other by means not shown, for example by threaded rings.
  • FIGS. 2a to 2c show a first embodiment of a firing device 4 according to the invention.
  • This device comprises a pyrotechnic composition 8 sensitive to percussion which is disposed in a cup 10 positioned in a cavity 31 of a front portion 11a of a body of the device 4.
  • a percussion tip 12 is positioned in the bucket 10 and in contact with the pyrotechnic composition 8. This point is secured to a partition 13 which is interposed between the rear portion 11b and 11a before the body of the device.
  • the partition 13 also makes it possible to close the cavity 31 and the bucket 10 enclosing the composition 8.
  • the front portions 11a and 11b of the rear body are connected to each other by means not shown, for example by a threaded ring.
  • a washer 23 is interposed between these two parts.
  • the tip 12 is secured to the partition 13 by a shearable connection means 14, for example a thread.
  • the tip 12 has an internal housing inside which is slidably mounted a rod 15.
  • the rod 15 can slide between a folded position ( figure 2a ) and an extended position ( figure 2b ) by the effect of the acceleration force F related to the firing of the ammunition.
  • the rod 15 is lockable in the extended position by two centrifugal latches 16. These latches are cylindrical parts held in their folded position ( figure 2a ) by the internal cylindrical surface of the bore of the tip 12. They slide by the effect of the rotational acceleration developed during firing.
  • the figure 2d shows more precisely a latch 16 in the deployed position. It is seen that this lock is secured to the rod 15 by a tension spring 17.
  • Two resilient tongues 18 are held folded in housings 19 when the latch 16 is in the folded position. These tabs 18 unfold when the latch 16 is deployed and they maintain the latch in its extended position.
  • the spring 17 has the effect of maintaining the latch 16 in abutment against the tabs 18 and prevents inadvertent vibration or unlocking when the acceleration of rotation decreases.
  • a traction spring 20 is interposed between the point 12 and the rod 15. This spring ensures the maintenance of the rod in its deployed position ( figure 2b ) resting against the rear edge of the point 12. and also any movement of the rod 15 after deployment, even if the level of axial acceleration decreases.
  • the tip 12 and the rod 15 constitute a telescopic striker which is intended to initiate the pyrotechnic composition 8.
  • the device 4 further comprises a hammer 21 which is capable of striking the rod 15 during the impact of the munition on a target to cause the initiation of the composition 8.
  • the hammer 21 is constituted by a flyweight which is secured to the rear portion 11b of the body by a shearable ring 22.
  • the operation of the device is as follows.
  • the front (AV) and the rear (AR) of the ammunition have been marked by the letters AV and AR, respectively.
  • the device 4 is in the storage security state in the position shown in FIG. figure 2a . Note that in this position of the device, the rod 15 is completely inside the tip 12. No part of the tip 12 is also projecting relative to the partition 13 to the hammer 21.
  • the device 4 ( figure 2b ) is subjected to axial acceleration forces F as well as a rotation ⁇ which generates a centrifugal force of inertia.
  • the rod 15 then slides and is locked in the deployed position ( figure 2b ) in centrifugal locks 16. In this armed configuration, the rod 15 is projecting relative to the partition 13 and the striker 12-15 is deployed.
  • the hammer 21 then violently impacts the rod 15 which pushes the tip 12 against the pyrotechnic composition 8 by shearing the threading 14.
  • the pyrotechnic composition 8 is initiated by the shock and the explosive charge 3 is detonated.
  • the percussion function (which is ensured by the percussion tip 12, directly in contact with the pyrotechnic composition 8 and comprising a sliding rod 15) is completely dissociated from the energy supply function. for this percussion (which is ensured by the weight 21), flyweight which is then completely distinct from the tip 12 and its rod 5.
  • the masses of the tip 12 and its rod 5 then have no importance and can be greatly reduced.
  • the percussion energy will be given by the weight 21 which may have any shape and be particularly adapted to the housing available in the ammunition.
  • the percussion energy being proportional to the mass of the weight 21 and the distance traveled by the latter to impact the rod 5, we see that if the mass of the weight is large enough, it becomes possible to reduce the distance to be traveled by the latter quite
  • the percussion device according to the invention can therefore be very compact (it is thus possible to easily reduce by one third the axial size of the device).
  • the hammer 21 comprises radial bores 24 in which are positioned balls 25.
  • the hammer 21 is guided in its housing 26 by a front seat 21a. Guiding is completed by the sliding of a rear extension 21b of smaller diameter in a hole 27 of the rear portion 11b of the body of the device.
  • a compression spring 28 is mounted around the rear extension 21b. This spring is interposed between the bottom of the housing 26 and the hammer 21.
  • the rear portion of the housing 26 has a conical profile 26a whose conicity is oriented with the apex of the cone towards the front AV of the munition.
  • the axial acceleration F of the projectile during firing causes the recoil of the hammer 21 and the compression of the spring 28.
  • the balls 25 are spaced radially by the action of the centrifugal force of inertia. These balls then cooperate with the conical profile 26a which ensures a locking of the hammer 21 in the armed position shown in FIG. figure 3b .
  • the axial acceleration F decreases after the exit of the projectile from the tube of the weapon while the rotation is maintained.
  • the balls 25 applied on the conical profile 26a provide a locking hammer 21 in the armed position with the spring 28 compressed.
  • Such an embodiment makes it possible to ensure a self-destruction function of the munition. Indeed during the impact on a target the shock is sufficient to cause the projection of the hammer 21 on the rod 15 ( figure 3c ). When the ammunition does not impact a target but is stopped (fall on the ground for example), stopping the rotation puts an end to the centrifugal force which applied the balls 25 to the profile 26a. The spring 28 then relaxes by projecting the hammer 21 on the rod 15 which ensures the initiation of the composition 8.
  • centrifugal latches of a different structure from that of the balls 25.
  • the invention may advantageously be implemented to produce a miniaturized firing device in the form of micro-machined or micro-plane planar elements on a substrate.
  • the Figures 4a, 4b and 5 show such an embodiment in which the body is made in the form of a micro-machined or micro-etched plate 30 disposed on a substrate 29.
  • MEMS technology makes it possible to produce mobile mechanical elements having very large dimensions. reduced.
  • the substrate 29 shown here has a rectangular shape having dimensions of the order of 8 mm for the length and 4 mm for the width.
  • the machining carried out on the wafer 30 made it possible to produce a rectangular cavity 31 intended to receive the pyrotechnic composition (not shown).
  • the cavity 31 is delimited on one side by the partition 13 which is made in one piece with the wafer 30 and the tip 12.
  • the partition 13 will have a sufficiently small thickness for the bulkhead connection 13 / tip 12 can break at the impact by the hammer 21. It will be possible to develop during the etching of the rupture primers between the tip 12 and the partition 13.
  • the hammer 21 is also obtained by etching. It carries two centrifugal weights 32 which are connected to the hammer 21 by flexible lamellae 33. The hammer is guided in its housing by its front reach 21a and its rear reach 21b which is in the form of a sliding tongue in the hole 27.
  • Each weight 32 comprises a semicircular profile which is intended to cooperate with a ramp 34 integral with the plate 30.
  • the ramps 34 are oriented to be geometrically intersecting towards the front AV of the munition.
  • the springs 28 will be compressed by the axial acceleration forces (the axis 35 represents the firing direction of the ammunition and the letters AV and AR symbolize the front and the rear respectively. rear of the ammunition.
  • the figure 5 shows this set more precisely.
  • the rod 15 carries two centrifugal latches 16 which are connected to it by engraved springs 17.
  • the etching technology makes it possible to produce the springs 17 integral with the rod 15 as well as the bolts 16, their flanges 36a cooperating with the abutments 36b and locking tabs 18 (locking means similar to that described with reference to FIG. figure 2d ).
  • the springs 17 are obtained in the state of rest. They are stretched during the deployment of the latches 16 by the action of centrifugal forces.
  • the spring 20 is secured to the rod 15 and the tip 12. This spring is in the state of rest. It is stretched during firing by the action of axial acceleration efforts.
  • composition is placed in the form of, for example, a drop of pyrotechnic composition containing a primary explosive associated with a polymerizable binder and it covers the tip 12.
  • a method of setting up such a composition is described for example by the patent EP1101076 .
  • a flap 39 ensures the closure of the riser 37.
  • Another flap 40 closes an orifice 41 connecting the composition 8 to the pyrotechnic chain of the munition (not shown).
  • the firing acceleration causes both the recoil of the hammer 21 and the exit of the rod 15 from its housing in the tip 12. These movements have the effect of compressing the springs 28 and stretching the spring 20.
  • the force Centrifugal also has the effect of removing the locks 16 of their housing which blocks the rod 15 in the deployed position.
  • This centrifugal force also removes the weights 32 which apply to the ramps 34 which ensures the maintenance of the hammer 21 in the armed position against the action of the springs 28.
  • the hammer 21 At impact on a target the hammer 21 will be projected against the rod 15 which will push the tip 12 on the pyrotechnic composition. In case of stopping of the rotation it is the springs 28 which will push the hammer 21 thus causing the self-destruction.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Percussive Tools And Related Accessories (AREA)
  • Automotive Seat Belt Assembly (AREA)

Abstract

The device (4) has a firing pin intended to impact a pyrotechnic composition (8) to activate ignition, where the firing pin has a rod (15) that slides when ammunition is fired through effect of firing acceleration from a starting position to a deployed position. The rod is integrated with a percussion tip (12) occupying a fixed position in contact with the pyrotechnic composition. A hammer (21) strikes the rod during impact of the ammunition on a target to cause ignition of the composition.

Description

Le domaine technique de l'invention est celui des dispositifs de mise à feu de munition à l'aide d'un percuteur mécanique venant impacter une composition pyrotechnique.The technical field of the invention is that of ammunition firing devices using a mechanical striker impelling a pyrotechnic composition.

D'une façon classique les dispositifs de mise à feu comportent un percuteur qui est projeté par inertie sur la composition pyrotechnique après la levée d'un certain nombre de barrières de sécurité. Ce percuteur est également très souvent projetable par un ressort, cela de façon à assurer une fonction d'autodestruction (lorsque par exemple il n'y a pas d'impact sur une cible).In a conventional manner the firing devices comprise a firing pin which is projected by inertia on the pyrotechnic composition after the lifting of a certain number of safety barriers. This striker is also often projected by a spring, so as to ensure a self-destruct function (when for example there is no impact on a target).

Le brevet FR-2689972 décrit ainsi un dispositif de mise à feu pour un projectile de moyen calibre (calibre compris entre 20 mm et 50 mm). Ce dispositif comprend un percuteur qui peut être poussé vers une amorce par un ressort.The patent FR-2689972 thus describes a firing device for a projectile medium caliber (caliber between 20 mm and 50 mm). This device comprises a striker which can be pushed to a primer by a spring.

Afin d'éviter tout risque de percussion intempestive lors des phases de stockage ou de transport, l'amorce est solidaire d'un rotor d'armement qui permet de la maintenir écartée du percuteur avant le tir.In order to avoid any risk of inadvertent percussion during the storage or transport phases, the primer is secured to an arming rotor that keeps it away from the striker before firing.

Une telle architecture est cependant complexe et impose la réalisation de nombreuses pièces mécaniques comportant des usinages précis.Such an architecture is however complex and requires the realization of many mechanical parts with precise machining.

D'une façon classique, le ressort d'autodestruction est maintenu à l'état bandé pendant toutes les phases de stockage et de transport. Même si ce ressort se comprime légèrement plus lors du tir pour permettre le plus souvent le retrait des verrous du rotor porte amorce, une énergie suffisante pour l'autodestruction nécessite un stockage du ressort à l'état bandé.In a conventional manner, the self-destruct spring is maintained in the bandaged state during all the storage and transport phases. Even if this spring compresses slightly more during the firing to allow more often the withdrawal of the locks of the gate rotor, sufficient energy for self destruction requires storage of the spring in the bandaged state.

L'invention a pour but de simplifier un tel dispositif en proposant une architecture dans laquelle l'amorce percutante est toujours alignée avec le percuteur mais les chocs subis lors des phases de stockage et transport ne peuvent toutefois pas provoquer la percussion de l'amorce.The purpose of the invention is to simplify such a device by proposing an architecture in which the percussive primer is always aligned with the striker, but the shocks undergone during the storage and transport phases can not, however, provoke percussion of the primer.

Avec le dispositif selon l'invention, seules les contraintes liées au tir peuvent rendre le dispositif amorçable. L'invention permet donc de sécuriser complètement la fonction percussion lors des phases de stockage et transport.With the device according to the invention, only the constraints related to shooting can make the device bootable. The invention thus makes it possible to completely secure the percussion function during the storage and transport phases.

L'invention permet également la mise en oeuvre d'un mécanisme d'autodestruction dans lequel les moyens ressorts n'ont pas à être comprimés lors du montage.The invention also allows the implementation of a self-destruction mechanism in which the spring means do not have to be compressed during assembly.

Il n'y a donc pas, grâce à l'invention, de stockage de ressorts à l'état bandé ce qui assure un maintien des performances du dispositif malgré des phases de stockage de longues durées et avec des intervalles de températures importants.There is therefore not, thanks to the invention, storage of springs in the banded state which ensures a maintenance of the performance of the device despite storage phases of long durations and with significant temperature intervals.

On connaît aussi par le brevet FR-1300100 un dispositif de mise à feu de munition comportant un percuteur solidaire d'un corps de percussion qui est verrouillé en position de sécurité par des billes.Also known by the patent FR-1300100 an ammunition firing device comprising a striker integral with a percussion body which is locked in the safety position by balls.

Ce dispositif comporte donc un percuteur qui est en permanence aligné avec l'amorce mais qui se trouve verrouillé par des moyens de sécurité qui sont effacés lors du tir.This device therefore comprises a firing pin which is permanently aligned with the primer but which is locked by security means which are erased during firing.

Ces moyens de sécurité comprennent deux masselottes coulissantes par inertie, la première masselotte libérant les billes verrouillant le percuteur.These safety means comprise two flyweights inertia, the first flyweight releasing the balls locking the striker.

Ce dispositif est de structure complexe. Il est en effet nécessaire que les deux masselottes coulissent dans un ordre bien défini pour que le percuteur soit libéré. En effet les billes sont poussées par une des masselottes contre la deuxième masselotte. Il est donc nécessaire que cette dernière s'écarte rapidement lors du tir pour éviter un coincement des billes.This device is of complex structure. It is indeed necessary that the two weights slide in a well-defined order so that the firing pin is released. Indeed the balls are pushed by one of the weights against the second weight. It is therefore necessary for the latter to deviate rapidly during firing to avoid jamming the balls.

Il est nécessaire en outre que la deuxième masselotte reste verrouillée (au moins temporairement) pour permettre l'éjection des billes de verrouillage du percuteur. Ce verrouillage est assuré par d'autres billes logées dans une gorge de la deuxième masselotte, gorge dont le fond est conique. Ces billes de verrouillage s'écartent donc lors du tir par leur inertie axiale pour s'engager contre une rampe du percuteur.It is also necessary that the second weight remains locked (at least temporarily) to allow the ejection of the striker locking balls. This locking is provided by other balls housed in a groove of the second weight, groove whose bottom is tapered. These locking balls therefore deviate during firing by their axial inertia to engage against a ramp of the firing pin.

Cette solution particulièrement coûteuse du point de vue usinage et montage permet de s'affranchir de la vitesse de rotation du projectile. Elle est cependant peu fiable, les billes ne restant en position de verrouillage que par la seule action du ressort de rappel de la masselotte.This particularly expensive solution from the point of view of machining and mounting eliminates the rotational speed of the projectile. However, it is unreliable, the balls remaining in the locking position only by the sole action of the return spring of the weight.

Concrètement à l'impact sur la cible c'est, d'une façon classique, la seule inertie du percuteur (incluant celle de la deuxième masselotte) et agissant contre l'effet d'un ressort de rappel, qui assurera l'initiation de l'amorce.Specifically to the impact on the target is, in a conventional way, the only inertia of the striker (including that of the second weight) and acting against the effect of a spring, which will ensure the initiation of the primer.

Comme toutes les solutions connues mettant ainsi en oeuvre l'inertie d'un percuteur, l'énergie disponible à l'impact sur une cible est proportionnelle à la masse du percuteur et à la distance parcourue par ce dernier pour initier l'amorce. Cette énergie E est égale à myD, expression dans laquelle m est la masse du percuteur, D la distance parcourue par ce dernier et y la décélération subie à l'impact sur une cible.As all the known solutions thus implementing the inertia of a striker, the energy available to the impact on a target is proportional to the mass of the firing pin and the distance traveled by the latter to initiate the primer. This energy E is equal to myD, where m is the mass of the striker, D is the distance traveled by the striker, and y is the deceleration experienced at impact on a target.

Les géométries classiques dans lesquelles les percuteurs sont des tiges coulissantes non entraînées par des ressorts, conduisent à des courses relativement importantes (de l'ordre de la dizaine de millimètres).The conventional geometries in which the strikers are sliding rods not driven by springs, lead to relatively large strokes (of the order of tens of millimeters).

L'invention a pour but de proposer un dispositif de conception simple dans lequel seules les contraintes liées au tir peuvent rendre le dispositif amorçable, et dans lequel par ailleurs on dissocie complètement la fonction percussion de la fonction fourniture d'énergie pour 1a percussion.The object of the invention is to propose a device of simple design in which only the constraints linked to the firing can make the device startable, and in which the percussion function of the energy supply function for the percussion is completely dissociated.

Ceci autorise la définition de dispositifs de mise à feu par percussion plus compacts car il n'est plus alors nécessaire de prévoir une course importante pour le percuteur.This allows the definition of percussion firing devices more compact because it is no longer necessary to provide a significant stroke for the firing pin.

L'invention trouve plus particulièrement application dans le domaine des fusées et dispositifs de mise à feu comportant des éléments micro usinés ou micro gravés (technologie MEMS comme Micro Electro Mechanical System).The invention is more particularly applicable in the field of rockets and firing devices comprising micro-machined or micro-engraved elements (MEMS technology such as Micro Electro Mechanical System).

Depuis quelques années il a été proposé en effet de réaliser tout ou partie des dispositifs de sécurité de munitions à l'aide de puces incorporant des éléments électro mécaniques micro usinés ou micro gravés soit dans un élément déposé sur un substrat soit directement sur le substrat lui-même. Cette technologie connue sous le nom de MEMS (Micro Electro Mechanical System) permet en effet aujourd'hui de réaliser des micro-mécanismes en mettant en oeuvre une technique proche de celle permettant de réaliser les circuits intégrés électroniques.For some years now it has been proposed to carry out all or part of the ammunition safety devices using chips incorporating electromechanical micro-machined or micro-etched elements either in an element deposited on a substrate or directly on the substrate itself. -even. This technology known as the MEMS (Micro Electro Mechanical System) makes it possible today to achieve micro-mechanisms by implementing a technique similar to that for the realization of electronic integrated circuits.

On connaît notamment par les brevets EP-1780495 et EP1780496 des dispositifs de sécurité et armement mettant en oeuvre un volet d'interruption de chaîne pyrotechnique micro-usiné ou micro-gravé.We know in particular by patents EP-1780495 and EP1780496 safety and arming devices implementing a micro-machined or micro-etched pyrotechnic chain interruption flap.

On ne connaît cependant pas à ce jour de dispositif de mise à feu de munition par percuteur mécanique mettant en oeuvre la technologie MEMS.However, a firing device for mechanical firing using MEMS technology is not known to date.

Une des raisons de cette absence de solution est l'impossibilité qu'il y a à réaliser en technologie MEMS des ressorts à l'état bandé. Il est alors nécessaire de comprimer ces ressorts dans une position de stockage avec toutes les difficultés qu'il y a à conduire une telle opération avec un dispositif de dimensions très réduites (une puce MEMS a généralement des dimensions inférieures ou égales à 10 mm).One of the reasons for this lack of solution is the impossibility of making MEMS springs in the bandaged state. It is then necessary to compress these springs in a storage position with all the difficulties of conducting such an operation with a device of very small dimensions (a MEMS chip generally has dimensions less than or equal to 10 mm).

Le dispositif selon l'invention est aisément transposable à la réalisation d'un dispositif de dimensions très réduites et en particulier un dispositif réalisé suivant les technologies MEMS.The device according to the invention is easily transposable to the realization of a device of very small dimensions and in particular a device made according to MEMS technologies.

L'invention a donc pour objet un dispositif de mise à feu de munition, comportant un percuteur destiné à venir impacter une composition pyrotechnique pour commander l'initiation de celle ci, dispositif caractérisé en ce que le percuteur comporte une tige coulissante lors du tir de la munition par l'effet de l'accélération de tir d'une position de repos à une position déployée, et verrouillable en position déployée, tige solidaire d'une pointe de percussion occupant une position fixe en contact avec la composition pyrotechnique, la tige se situant complètement à l'intérieur de la pointe en position de repos et se trouvant en saillie par rapport à la pointe en position déployée, le dispositif comportant par ailleurs un marteau susceptible de venir frapper la tige lors de l'impact de la munition sur une cible pour provoquer l'initiation de la composition.The invention therefore relates to an ammunition firing device, comprising a firing pin intended to impact a pyrotechnic composition to control the initiation of the latter, characterized in that the firing pin comprises a sliding rod during firing. the ammunition by the effect of the firing acceleration from a rest position to an extended position, and lockable in the deployed position, rod secured to a percussion tip occupying a fixed position in contact with the pyrotechnic composition, the rod being completely inside the tip in the rest position and being projecting relative to the tip in the deployed position, the device further comprising a hammer capable of striking the rod during the impact of the ammunition on a target for initiating the composition.

La tige coulissante pourra être verrouillée en position déployée par au moins un verrou centrifuge.The sliding rod can be locked in the deployed position by at least one centrifugal latch.

La tige coulissante sera avantageusement reliée à la pointe par un ressort de traction.The sliding rod is advantageously connected to the tip by a tension spring.

La pointe de percussion pourra être solidaire d'une cloison qui délimitera une cavité recevant la composition pyrotechnique, des moyens de fragilisation étant prévus pour séparer la pointe de la cloison lors de l'impact du marteau.The percussion tip may be secured to a partition which will delimit a cavity receiving the pyrotechnic composition, embrittlement means being provided to separate the tip of the partition during the impact of the hammer.

Selon un mode de réalisation, le marteau pourra être projeté contre la tige extensible par un moyen ressort.According to one embodiment, the hammer can be projected against the extensible rod by a spring means.

Le marteau pourra ainsi se trouver en position de repos avant tir au voisinage de la tige non déployée, le moyen ressort étant à l'état non comprimé et l'accélération de tir provoquera le déplacement du marteau et la compression du moyen ressort.The hammer can thus be in the rest position before firing in the vicinity of the undeployed rod, the spring means being in the uncompressed state and the firing acceleration will cause the movement of the hammer and the compression of the spring means.

Le marteau pourra être maintenu écarté du percuteur par des moyens de maintien comprenant au moins une masselotte centrifuge coopérant avec une rampe fixe.The hammer may be kept away from the firing pin by holding means comprising at least one centrifugal flyweight cooperating with a fixed ramp.

Selon un mode de réalisation particulier, l'ensemble du dispositif pourra être réalisé sous la forme d'éléments plans micro usinés ou micro gravés sur une plaquette.According to a particular embodiment, the entire device may be made in the form of micromachined planar elements or micro etched on a wafer.

Le dispositif pourra comporter une rehausse permettant la mise en place de la composition pyrotechnique au-dessus de la pointe.The device may include a riser for setting up the pyrotechnic composition above the tip.

L'invention sera mieux comprise à la lecture de la description qui va suivre de différents modes de réalisation, description faite en référence aux dessins annexés et dans lesquels :

  • la figure 1 montre la configuration générale d'une munition incorporant un dispositif selon l'invention,
  • les figures 2a, 2b et 2c sont des vues schématiques en coupe d'un premier mode de réalisation d'un dispositif selon l'invention, la figure 2a montrant le dispositif en position de stockage, la figure 2b en position armée à l'issue du tir et la figure 2c en position de percussion,
  • la figure 2d est une vue de détail montrant l'immobilisation d'un verrou en position déployée,
  • les figures 3a, 3b et 3c sont des vues schématiques en coupe d'un second mode de réalisation du dispositif selon l'invention, la figure 3a montrant le dispositif en position de stockage, la figure 3b en position armée à l'issue du tir et la figure 3c en position de percussion,
  • les figures 4a et 4b sont des vues schématiques en coupe d'un troisième mode de réalisation du dispositif selon l'invention (réalisation sous forme de MEMS), la figure 4a montrant le dispositif en position de stockage et la figure 4b en position armée à l'issue du tir,
  • la figure 5 est une vue de détail d'un verrou centrifuge, et
  • la figure 6 est une vue en coupe partielle de la plaquette micro usinée.
The invention will be better understood on reading the following description of various embodiments, a description given with reference to the appended drawings and in which:
  • the figure 1 shows the general configuration of a munition incorporating a device according to the invention,
  • the Figures 2a, 2b and 2c are schematic sectional views of a first embodiment of a device according to the invention, the figure 2a showing the device in storage position, the figure 2b in armed position at the end of the shot and the Figure 2c in percussion position,
  • the figure 2d is a detail view showing the immobilization of a lock in the deployed position,
  • the Figures 3a, 3b and 3c are schematic sectional views of a second embodiment of the device according to the invention, the figure 3a showing the device in storage position, the figure 3b in armed position at the end of the shot and the figure 3c in percussion position,
  • the Figures 4a and 4b are schematic sectional views of a third embodiment of the device according to the invention (embodiment in the form of MEMS), the figure 4a showing the device in storage position and the figure 4b in armed position at the end of the shot,
  • the figure 5 is a detail view of a centrifugal latch, and
  • the figure 6 is a partial sectional view of the micromachined plate.

La figure 1 montre schématiquement en coupe un corps 2 d'une munition 1 qui renferme un chargement explosif 3. Cet explosif est initié par un dispositif de mise à feu 4 et un dispositif de sécurité et d'armement 5 est interposé entre le dispositif de mise à feu et le chargement explosif 3.The figure 1 schematically shows in section a body 2 of a munition 1 which contains an explosive charge 3. This explosive is initiated by a firing device 4 and a safety and arming device 5 is interposed between the firing device and the explosive charge 3.

Le dispositif de sécurité et d'armement 5 est représenté ici très schématiquement. Il comporte essentiellement un écran 6 qui permet d'interrompre le canal 9 de transmission entre une composition pyrotechnique 8 (solidaire du dispositif de mise à feu 4) et le chargement explosif 3.The safety and arming device 5 is shown here very schematically. It essentially comprises a screen 6 which makes it possible to interrupt the transmission channel 9 between a pyrotechnic composition 8 (integral with the firing device 4) and the explosive charge 3.

L'écran 6 est mobile en translation par l'action de moyens moteurs qui sont représentés ici schématiquement par un ressort 7. D'une façon classique, des moyens de verrouillage (non représentés) vont libérer le volet 6 comme suite à la détection de différents évènements associés au tir de la munition (par exemple des verrous inertiels).The screen 6 is movable in translation by the action of motor means which are represented here schematically by a spring 7. In a conventional manner, locking means (not shown) will release the flap 6 as a result of the detection of different events associated with ammunition firing (eg inertial locks).

Ce dispositif de sécurité ne fait pas partie de la présente invention et il n'est donc pas nécessaire de le décrire en détails. Le dispositif de sécurité et d'armement 5, le dispositif de mise à feu 4 et le corps 2 de la munition sont liés les uns aux autres par des moyens non représentés, par exemple par des bagues filetées.This safety device does not form part of the present invention and it is therefore not necessary to describe it in detail. The safety and arming device 5, the firing device 4 and the body 2 of the ammunition are connected to each other by means not shown, for example by threaded rings.

Les figures 2a à 2c montrent un premier mode de réalisation d'un dispositif de mise à feu 4 selon l'invention.The Figures 2a to 2c show a first embodiment of a firing device 4 according to the invention.

Ce dispositif comporte une composition pyrotechnique 8 sensible à la percussion qui est disposée dans un godet 10 positionné dans une cavité 31 d'une partie avant 11a d'un corps du dispositif 4. Une pointe de percussion 12 est positionnée d'une façon fixe dans le godet 10 et en contact avec la composition pyrotechnique 8. Cette pointe est solidaire d'une cloison 13 qui est interposée entre la partie arrière 11b et avant 11a du corps du dispositif. La cloison 13 permet également de fermer la cavité 31 et le godet 10 renfermant la composition 8.This device comprises a pyrotechnic composition 8 sensitive to percussion which is disposed in a cup 10 positioned in a cavity 31 of a front portion 11a of a body of the device 4. A percussion tip 12 is positioned in the bucket 10 and in contact with the pyrotechnic composition 8. This point is secured to a partition 13 which is interposed between the rear portion 11b and 11a before the body of the device. The partition 13 also makes it possible to close the cavity 31 and the bucket 10 enclosing the composition 8.

Les parties avant 11a et arrière 11b du corps sont liées l'une à l'autre par des moyens non représentés, par exemple par une bague filetée. Une rondelle 23 est interposée entre ces deux parties.The front portions 11a and 11b of the rear body are connected to each other by means not shown, for example by a threaded ring. A washer 23 is interposed between these two parts.

La pointe 12 est rendue solidaire de la cloison 13 par un moyen de liaison cisaillable 14, par exemple un filetage.The tip 12 is secured to the partition 13 by a shearable connection means 14, for example a thread.

La pointe 12 présente un logement interne à l'intérieur duquel est montée coulissante une tige 15.The tip 12 has an internal housing inside which is slidably mounted a rod 15.

La tige 15 peut coulisser entre une position repliée (figure 2a) et une position déployée (figure 2b) par l'effet de l'effort F d'accélération lié au tir de la munition.The rod 15 can slide between a folded position ( figure 2a ) and an extended position ( figure 2b ) by the effect of the acceleration force F related to the firing of the ammunition.

La tige 15 est verrouillable en position déployée par deux verrous centrifuges 16. Ces verrous sont des pièces cylindriques maintenues dans leur position repliée (figure 2a) par la surface cylindrique interne de l'alésage de la pointe 12. Ils coulissent par l'effet de l'accélération de rotation développée lors du tir.The rod 15 is lockable in the extended position by two centrifugal latches 16. These latches are cylindrical parts held in their folded position ( figure 2a ) by the internal cylindrical surface of the bore of the tip 12. They slide by the effect of the rotational acceleration developed during firing.

La figure 2d montre de façon plus précise un verrou 16 en position déployée. On voit que ce verrou est rendu solidaire de la tige 15 par un ressort de traction 17. Deux languettes élastiques 18 sont maintenues rabattues dans des logements 19 quand le verrou 16 est en position repliée. Ces languettes 18 se déplient lorsque le verrou 16 est déployé et elles assurent le maintien de ce verrou dans sa position déployée. Le ressort 17 a pour effet de maintenir le verrou 16 en appui contre les languettes 18 et évite les vibrations ou déverrouillages intempestifs lorsque l'accélération de rotation diminue.The figure 2d shows more precisely a latch 16 in the deployed position. It is seen that this lock is secured to the rod 15 by a tension spring 17. Two resilient tongues 18 are held folded in housings 19 when the latch 16 is in the folded position. These tabs 18 unfold when the latch 16 is deployed and they maintain the latch in its extended position. The spring 17 has the effect of maintaining the latch 16 in abutment against the tabs 18 and prevents inadvertent vibration or unlocking when the acceleration of rotation decreases.

On voit sur les figures qu'un ressort de traction 20 est interposé entre la pointe 12 et la tige 15. Ce ressort assure le maintien de la tige dans sa position déployée (figure 2b) en appui contre le rebord arrière de la pointe 12. On évite ainsi également tout déplacement de la tige 15 après son déploiement, même si le niveau d'accélération axiale diminue.It can be seen in the figures that a traction spring 20 is interposed between the point 12 and the rod 15. This spring ensures the maintenance of the rod in its deployed position ( figure 2b ) resting against the rear edge of the point 12. and also any movement of the rod 15 after deployment, even if the level of axial acceleration decreases.

La pointe 12 et la tige 15 constituent un percuteur télescopique qui est destiné à venir initier la composition pyrotechnique 8.The tip 12 and the rod 15 constitute a telescopic striker which is intended to initiate the pyrotechnic composition 8.

Le dispositif 4 comporte par ailleurs un marteau 21 qui est susceptible de venir frapper la tige 15 lors de l'impact de la munition sur une cible pour provoquer l'initiation de la composition 8.The device 4 further comprises a hammer 21 which is capable of striking the rod 15 during the impact of the munition on a target to cause the initiation of the composition 8.

Selon le premier mode de réalisation qui est décrit en référence aux figures 2a à 2c, le marteau 21 est constitué par une masselotte qui est rendue solidaire de la partie arrière 11b du corps par un anneau cisaillable 22.According to the first embodiment which is described with reference to Figures 2a to 2c , the hammer 21 is constituted by a flyweight which is secured to the rear portion 11b of the body by a shearable ring 22.

Le fonctionnement du dispositif est le suivant.The operation of the device is as follows.

On a repéré par les lettres AV et AR respectivement l'avant (AV) et l'arrière (AR) de la munition.The front (AV) and the rear (AR) of the ammunition have been marked by the letters AV and AR, respectively.

Le dispositif 4 se trouve à l'état de sécurité de stockage dans la position représentée à la figure 2a. On notera que, dans cette position du dispositif, la tige 15 se situe complètement à l'intérieur de la pointe 12. Aucune partie de la pointe 12 n'est par ailleurs en saillie par rapport à la cloison 13 vers le marteau 21.The device 4 is in the storage security state in the position shown in FIG. figure 2a . Note that in this position of the device, the rod 15 is completely inside the tip 12. No part of the tip 12 is also projecting relative to the partition 13 to the hammer 21.

On notera que si un choc violent provoquait alors le cisaillement de l'anneau 22, le marteau serait arrêté par la rondelle 23. Aucun choc ne serait reçu par la composition pyrotechnique 8. La sécurité du dispositif est donc totale.Note that if a violent shock then caused the shearing of the ring 22, the hammer would be stopped by the washer 23. No shock would be received by the pyrotechnic composition 8. The safety of the device is therefore total.

A titre de variante, il serait possible de ne pas prévoir de rondelle 23 pour assurer l'arrêt du marteau. Dans ce cas c'est la cloison 13 qui assurera l'arrêt du marteau. La sécurité peut être assurée en prévoyant une cloison 13 d'épaisseur suffisante. Il n'y a pas d'initiation de la composition car, à l'état de repos, la tige 15 n'est pas saillante par rapport à la cloison 13.Alternatively, it would be possible not to provide a washer 23 to ensure the hammer stop. In this case it is the partition 13 which will ensure the stop of the hammer. Security can be ensured by providing a partition 13 of sufficient thickness. There is no initiation of the composition because, in the state of rest, the rod 15 is not protruding with respect to the partition 13.

Lorsque la munition est tirée par un système d'arme, le dispositif 4 (figure 2b) se trouve soumis à des efforts d'accélération axiaux F ainsi qu'à une rotation Ω qui engendre une force d'inertie centrifuge.When the ammunition is fired by a weapon system, the device 4 ( figure 2b ) is subjected to axial acceleration forces F as well as a rotation Ω which generates a centrifugal force of inertia.

La tige 15 coulisse alors et se trouve verrouillée en position déployée (figure 2b) par les verrous centrifuges 16. Dans cette configuration armée, la tige 15 est en saillie par rapport à la cloison 13 et le percuteur 12-15 est donc déployé.The rod 15 then slides and is locked in the deployed position ( figure 2b ) in centrifugal locks 16. In this armed configuration, the rod 15 is projecting relative to the partition 13 and the striker 12-15 is deployed.

A l'impact sur une cible (figure 2c), le marteau 21 est soumis à une force d'inertie G très importante qui provoque le cisaillement de l'anneau de maintien 22 (qui est calibré en fonction des efforts mis en jeu).At impact on a target ( Figure 2c ), the hammer 21 is subjected to a very large inertia force G which causes shearing of the retaining ring 22 (which is calibrated according to the forces involved).

Le marteau 21 impacte alors violemment la tige 15 qui pousse la pointe 12 contre la composition pyrotechnique 8 en cisaillant le filetage 14.The hammer 21 then violently impacts the rod 15 which pushes the tip 12 against the pyrotechnic composition 8 by shearing the threading 14.

Bien sûr, il serait possible de prévoir un autre moyen cisaillable que le filetage 14, par exemple une amorce de rupture circulaire portée par la cloison 13.Of course, it would be possible to provide another shearable means that the threading 14, for example a circular rupture leader carried by the partition 13.

La composition pyrotechnique 8 est initiée par le choc et le chargement explosif 3 est mis en détonation.The pyrotechnic composition 8 is initiated by the shock and the explosive charge 3 is detonated.

Tous les éléments mécaniques décrits ont ici une symétrie de révolution autour de l'axe 38 du dispositif (sauf les verrous 16 et leurs logements). Il serait bien entendu possible de réaliser des éléments de structure plane comme cela sera décrit plus loin.All the mechanical elements described here have a symmetry of revolution around the axis 38 of the device (except the locks 16 and their housings). It would of course be possible to make planar structure elements as will be described later.

On voit que, grâce à l'invention, on dissocie complètement la fonction percussion (qui est assurée par la pointe de percussion 12, directement en contact avec la composition pyrotechnique 8 et comportant une tige coulissante 15), de la fonction fourniture d'énergie pour cette percussion (qui est assurée par la masselotte 21), masselotte qui est alors complètement distincte de la pointe 12 et de sa tige 5.It can be seen that, thanks to the invention, the percussion function (which is ensured by the percussion tip 12, directly in contact with the pyrotechnic composition 8 and comprising a sliding rod 15) is completely dissociated from the energy supply function. for this percussion (which is ensured by the weight 21), flyweight which is then completely distinct from the tip 12 and its rod 5.

Les masses de la pointe 12 et de sa tige 5 n'ont alors aucune importance et peuvent être fortement réduites. L'énergie de percussion sera donnée par la masselotte 21 qui pourra avoir des formes quelconques et être en particulier adaptée aux logements disponibles dans la munition.The masses of the tip 12 and its rod 5 then have no importance and can be greatly reduced. The percussion energy will be given by the weight 21 which may have any shape and be particularly adapted to the housing available in the ammunition.

L'énergie de percussion étant proportionnelle à la masse de la masselotte 21 et à la distance parcourue par cette dernière pour venir impacter la tige 5, on voit donc que si la masse de la masselotte est suffisamment importante, il devient possible de réduire assez fortement la distance à parcourir par cette dernière. Le dispositif de percussion selon l'invention peut donc être très compact (on peut ainsi aisément réduire d'un tiers l'encombrement axial du dispositif).The percussion energy being proportional to the mass of the weight 21 and the distance traveled by the latter to impact the rod 5, we see that if the mass of the weight is large enough, it becomes possible to reduce the distance to be traveled by the latter quite The percussion device according to the invention can therefore be very compact (it is thus possible to easily reduce by one third the axial size of the device).

Les figures 3a, 3b et 3c décrivent un deuxième mode de réalisation qui ne diffère du précédent que par la structure du marteau 21 qui est mis en oeuvre.The Figures 3a, 3b and 3c describe a second embodiment which differs from the preceding only in the structure of the hammer 21 which is implemented.

Suivant ce mode le marteau 21 comporte des perçages radiaux 24 dans lesquels sont positionnées des billes 25. Le marteau 21 est guidé dans son logement 26 par une portée avant 21a . Le guidage est complété par le coulissement d'un prolongement arrière 21b de moindre diamètre dans un trou 27 de la partie arrière 11b du corps du dispositif.According to this mode the hammer 21 comprises radial bores 24 in which are positioned balls 25. The hammer 21 is guided in its housing 26 by a front seat 21a. Guiding is completed by the sliding of a rear extension 21b of smaller diameter in a hole 27 of the rear portion 11b of the body of the device.

Un ressort de compression 28 est monté autour du prolongement arrière 21b. Ce ressort est interposé entre le fond du logement 26 et le marteau 21.A compression spring 28 is mounted around the rear extension 21b. This spring is interposed between the bottom of the housing 26 and the hammer 21.

On constate également sur les figures que la partie arrière du logement 26 a un profil conique 26a dont la conicité est orientée avec le sommet du cône vers l'avant AV de la munition. L'accélération axiale F du projectile lors du tir provoque le recul du marteau 21 et la compression du ressort 28. Les billes 25 sont écartées radialement par l'action de la force d'inertie centrifuge. Ces billes coopèrent alors avec le profil conique 26a ce qui assure un verrouillage du marteau 21 dans la position armée représentée à la figure 3b.It can also be seen from the figures that the rear portion of the housing 26 has a conical profile 26a whose conicity is oriented with the apex of the cone towards the front AV of the munition. The axial acceleration F of the projectile during firing causes the recoil of the hammer 21 and the compression of the spring 28. The balls 25 are spaced radially by the action of the centrifugal force of inertia. These balls then cooperate with the conical profile 26a which ensures a locking of the hammer 21 in the armed position shown in FIG. figure 3b .

En effet, d'une façon classique et mise en oeuvre dans les fusées de projectiles, l'accélération axiale F diminue après la sortie du projectile hors du tube de l'arme alors que la rotation se maintient. Les billes 25 appliquées sur le profil conique 26a assurent un verrouillage du marteau 21 en position armée avec le ressort 28 comprimé.Indeed, in a conventional manner and implemented in projectile rockets, the axial acceleration F decreases after the exit of the projectile from the tube of the weapon while the rotation is maintained. The balls 25 applied on the conical profile 26a provide a locking hammer 21 in the armed position with the spring 28 compressed.

Un tel mode de réalisation permet d'assurer une fonction d'autodestruction de la munition. En effet lors de l'impact sur une cible le choc suffit à provoquer la projection du marteau 21 sur la tige 15 (figure 3c). Lorsque la munition n'impacte pas de cible mais qu'elle se trouve arrêtée (chute sur le sol par exemple), l'arrêt de la rotation met fin à l'effort centrifuge qui appliquait les billes 25 sur le profil 26a. Le ressort 28 se détend alors en projetant le marteau 21 sur la tige 15 ce qui assure l'initiation de la composition 8.Such an embodiment makes it possible to ensure a self-destruction function of the munition. Indeed during the impact on a target the shock is sufficient to cause the projection of the hammer 21 on the rod 15 ( figure 3c ). When the ammunition does not impact a target but is stopped (fall on the ground for example), stopping the rotation puts an end to the centrifugal force which applied the balls 25 to the profile 26a. The spring 28 then relaxes by projecting the hammer 21 on the rod 15 which ensures the initiation of the composition 8.

Diverses variantes sont possibles sans sortir du cadre de l'invention. Il est notamment possible de définir des verrous centrifuges de structure différente de celle des billes 25.Various variants are possible without departing from the scope of the invention. It is in particular possible to define centrifugal latches of a different structure from that of the balls 25.

L'invention peut avantageusement être mise en oeuvre pour réaliser un dispositif de mise à feu miniaturisé sous la forme d'éléments plans micro usinés ou micro gravés sur un substrat.The invention may advantageously be implemented to produce a miniaturized firing device in the form of micro-machined or micro-plane planar elements on a substrate.

Les figures 4a, 4b et 5 montrent un tel mode de réalisation dans lequel le corps est réalisé sous la forme d'une plaquette 30 micro usinée ou micro gravée disposée sur un substrat 29. D'une façon classique la technologie MEMS permet de réaliser des éléments mécaniques mobiles ayant des dimensions très réduites. A titre d'exemple le substrat 29 représenté ici a une forme rectangulaire ayant des dimensions de l'ordre de 8 mm pour la longueur et 4 mm pour la largeur.The Figures 4a, 4b and 5 show such an embodiment in which the body is made in the form of a micro-machined or micro-etched plate 30 disposed on a substrate 29. In a conventional manner, MEMS technology makes it possible to produce mobile mechanical elements having very large dimensions. reduced. For example, the substrate 29 shown here has a rectangular shape having dimensions of the order of 8 mm for the length and 4 mm for the width.

Les usinages réalisés sur la plaquette 30 ont permis de réaliser une cavité rectangulaire 31 destinée à recevoir la composition pyrotechnique (non représentée).The machining carried out on the wafer 30 made it possible to produce a rectangular cavity 31 intended to receive the pyrotechnic composition (not shown).

La cavité 31 est délimitée d'un côté par la cloison 13 qui est réalisée d'une seule pièce avec la plaquette 30 et la pointe 12. La cloison 13 aura une épaisseur suffisamment réduite pour que la liaison cloison 13 / pointe 12 puisse se rompre à l'impact par le marteau 21. On pourra aménager lors de la gravure des amorces de rupture entre la pointe 12 et la cloison 13.The cavity 31 is delimited on one side by the partition 13 which is made in one piece with the wafer 30 and the tip 12. The partition 13 will have a sufficiently small thickness for the bulkhead connection 13 / tip 12 can break at the impact by the hammer 21. It will be possible to develop during the etching of the rupture primers between the tip 12 and the partition 13.

Le marteau 21 est également obtenu par gravure. Il porte deux masselottes centrifuge 32 qui sont reliées au marteau 21 par des lamelles flexibles 33. Le marteau est guidé dans son logement par sa portée avant 21a et sa portée arrière 21b qui est sous la forme d'une languette coulissante dans le trou 27.The hammer 21 is also obtained by etching. It carries two centrifugal weights 32 which are connected to the hammer 21 by flexible lamellae 33. The hammer is guided in its housing by its front reach 21a and its rear reach 21b which is in the form of a sliding tongue in the hole 27.

Chaque masselotte 32 comporte un profil hémicirculaire qui est destiné à coopérer avec une rampe 34 solidaire de la plaquette 30. Les rampes 34 sont orientées de façon à être géométriquement sécantes en direction de l'avant AV de la munition.Each weight 32 comprises a semicircular profile which is intended to cooperate with a ramp 34 integral with the plate 30. The ramps 34 are oriented to be geometrically intersecting towards the front AV of the munition.

On voit que deux ressorts de compression 28 sont fixés entre le marteau 21 et la plaquette 30. La technologie MEMS ne permet pas de réaliser des ressorts maintenus à l'état bandé. L'architecture du dispositif selon l'invention permet de mettre en oeuvre un ressort 28 qui est à l'état de repos dans la configuration gravée représentée à la figure 4a (et qui est aussi la configuration de stockage).It can be seen that two compression springs 28 are fixed between the hammer 21 and the wafer 30. The MEMS technology does not make it possible to produce springs maintained in the bandaged state. The architecture of the device according to the invention makes it possible to implement a spring 28 which is in the idle state in the engraved configuration shown in FIG. figure 4a (and that is also the storage configuration).

Ce n'est que lors du tir que les ressorts 28 seront comprimés par les efforts d'accélération axiale (on a représenté par l'axe 35 la direction de tir de la munition et les lettres AV et AR symbolisent respectivement l'avant et l'arrière de la munition.It is only during firing that the springs 28 will be compressed by the axial acceleration forces (the axis 35 represents the firing direction of the ammunition and the letters AV and AR symbolize the front and the rear respectively. rear of the ammunition.

On a également réalisé par gravure la tige 15 qui est reliée à la pointe 12 par un ressort 20 également obtenu par gravure. La figure 5 montre cet ensemble de façon plus précise. La tige 15 porte deux verrous centrifuges 16 qui lui sont reliés par des ressorts gravés 17.The rod 15, which is connected to the tip 12 by a spring 20 also obtained by etching, has also been etched. The figure 5 shows this set more precisely. The rod 15 carries two centrifugal latches 16 which are connected to it by engraved springs 17.

La technologie de gravure permet de réaliser les ressorts 17 solidaires de la tige 15 ainsi que les verrous 16, leurs ailes 36a coopérant avec les butées 36b et des languettes de verrouillage 18 (moyen de verrouillage analogue à celui décrit en référence à la figure 2d).The etching technology makes it possible to produce the springs 17 integral with the rod 15 as well as the bolts 16, their flanges 36a cooperating with the abutments 36b and locking tabs 18 (locking means similar to that described with reference to FIG. figure 2d ).

Les ressorts 17 sont obtenus à l'état de repos. Ils sont étirés lors du déploiement des verrous 16 par l'action des forces centrifuges. Le ressort 20 est solidaire de la tige 15 et de la pointe 12. Ce ressort est à l'état de repos. Il se trouve étiré lors du tir par l'action des efforts d'accélération axiale.The springs 17 are obtained in the state of rest. They are stretched during the deployment of the latches 16 by the action of centrifugal forces. The spring 20 is secured to the rod 15 and the tip 12. This spring is in the state of rest. It is stretched during firing by the action of axial acceleration efforts.

Bien entendu tous les éléments mobiles (marteau 21, masselottes 32, ressorts 28, 20, 17, tige 15) ont été réalisés de telle sorte qu'ils ne sont pas adhérents sur le substrat 29. Il en est de même pour la pointe 12 qui doit pouvoir être poussée par la tige 15. La plaquette 30 n'adhère donc au substrat 29 que par sa périphérie rectangulaire et éventuellement par une partie de la cloison 13.Of course, all the mobile elements (hammer 21, flyweights 32, springs 28, 20, 17, rod 15) have been made in such a way that they are not adherent on the substrate 29. The same is true for the tip 12 which must be able to be pushed by the rod 15. The wafer 30 therefore adheres to the substrate 29 only by its rectangular periphery and possibly by a part of the partition 13.

On a représenté sur la figure 6 une coupe partielle du dispositif au niveau de la cavité 31. On voit qu'il a été disposé au-dessus de celle ci une rehausse 37 qui permet la mise en place d'une masse de composition pyrotechnique 8 supérieure à ce qui pourrait être mis dans la seule cavité 31.We have shown on the figure 6 a partial section of the device at the level of the cavity 31. It is seen that it has been disposed above it a riser 37 which allows the establishment of a mass of pyrotechnic composition 8 greater than what could be put in the single cavity 31.

La composition est mise en place sous forme par exemple d'une goutte de composition pyrotechnique renfermant un explosif primaire associé à un liant polymérisable et elle recouvre la pointe 12. Un procédé de mise en place d'une telle composition est décrit par exemple par le brevet EP1101076 .The composition is placed in the form of, for example, a drop of pyrotechnic composition containing a primary explosive associated with a polymerizable binder and it covers the tip 12. A method of setting up such a composition is described for example by the patent EP1101076 .

La friction provoquée par le déplacement de la pointe 12 est suffisante pour provoquer l'initiation de toute la composition 8. Un paillet 39 assure la fermeture de la rehausse 37. Un autre paillet 40 permet d'obturer un orifice 41 reliant la composition 8 à la chaîne pyrotechnique de la munition (non représentée).The friction caused by the displacement of the tip 12 is sufficient to cause the initiation of the entire composition 8. A flap 39 ensures the closure of the riser 37. Another flap 40 closes an orifice 41 connecting the composition 8 to the pyrotechnic chain of the munition (not shown).

Le fonctionnement de ce mode de réalisation est identique à celui décrit précédemment en référence aux figures 3a à 3c.The operation of this embodiment is identical to that described above with reference to Figures 3a to 3c .

L'accélération de tir provoque à la fois le recul du marteau 21 et la sortie de la tige 15 hors de son logement dans la pointe 12. Ces mouvements ont pour effet de comprimer les ressorts 28 et d'étirer le ressort 20. La force centrifuge a par ailleurs pour effet de faire sortir les verrous 16 de leurs logements ce qui bloque la tige 15 en position déployée.The firing acceleration causes both the recoil of the hammer 21 and the exit of the rod 15 from its housing in the tip 12. These movements have the effect of compressing the springs 28 and stretching the spring 20. The force Centrifugal also has the effect of removing the locks 16 of their housing which blocks the rod 15 in the deployed position.

Cette force centrifuge écarte également les masselottes 32 qui s'appliquent sur les rampes 34 ce qui assure le maintien du marteau 21 en position armée contre l'action des ressorts 28.This centrifugal force also removes the weights 32 which apply to the ramps 34 which ensures the maintenance of the hammer 21 in the armed position against the action of the springs 28.

A l'impact sur une cible le marteau 21 sera projeté contre la tige 15 qui poussera la pointe 12 sur la composition pyrotechnique. En cas d'arrêt de la rotation c'est les ressorts 28 qui pousseront le marteau 21 provoquant ainsi l'autodestruction.At impact on a target the hammer 21 will be projected against the rod 15 which will push the tip 12 on the pyrotechnic composition. In case of stopping of the rotation it is the springs 28 which will push the hammer 21 thus causing the self-destruction.

Claims (9)

Dispositif (4) de mise à feu de munition, comportant un percuteur (12, 15) destiné à venir impacter une composition pyrotechnique (8) pour commander l'initiation de celle ci, dispositif caractérisé en ce que le percuteur comporte une tige (15) coulissante lors du tir de la munition par l'effet de l'accélération de tir d'une position de repos à une position déployée, et verrouillable en position déployée, tige (15) solidaire d'une pointe (12) de percussion occupant une position fixe en contact avec la composition pyrotechnique (8), la tige (15) se situant complètement à l'intérieur de la pointe (12) en position de repos et se trouvant en saillie par rapport à la pointe (12) en position déployée, le dispositif comportant par ailleurs un marteau (21) susceptible de venir frapper la tige (15) lors de l'impact de la munition sur une cible pour provoquer l'initiation de la composition (8).Device (4) for firing ammunition, comprising a striker (12, 15) intended to impact a pyrotechnic composition (8) to control the initiation thereof, characterized in that the firing pin comprises a rod (15) ) sliding when firing the munition by the effect of the firing acceleration from a rest position to an extended position, and lockable in the deployed position, rod (15) integral with a point (12) occupying percussion a fixed position in contact with the pyrotechnic composition (8), the rod (15) being completely inside the tip (12) in the rest position and projecting from the tip (12) in position deployed, the device further comprising a hammer (21) capable of striking the rod (15) during the impact of the munition on a target to cause the initiation of the composition (8). Dispositif de mise à feu de munition selon la revendication 1, caractérisé en ce que la tige coulissante (15) est verrouillée en position déployée par au moins un verrou centrifuge (16).Ammunition firing device according to claim 1, characterized in that the sliding rod (15) is locked in the deployed position by at least one centrifugal latch (16). Dispositif de mise à feu de munition selon une des revendications 1 ou 2, caractérisé en ce que la tige coulissante (15) est reliée à la pointe (12) par un ressort de traction (20).Ammunition firing device according to one of claims 1 or 2, characterized in that the sliding rod (15) is connected to the tip (12) by a tension spring (20). Dispositif de mise à feu de munition selon une des revendications 1 à 3, caractérisé en ce que la pointe de percussion (12) est solidaire d'une cloison (13) qui délimite une cavité (31) recevant la composition pyrotechnique (8), des moyens de fragilisation (14) étant prévus pour séparer la pointe (12) de la cloison (13) lors de l'impact du marteau (21).Ammunition firing device according to one of claims 1 to 3, characterized in that the percussion tip (12) is integral with a partition (13) defining a cavity (31) receiving the pyrotechnic composition (8), embrittlement means (14) being provided for separating the tip (12) from the partition (13) during the impact of the hammer (21). Dispositif de mise à feu de munition selon une des revendications 1 à 4, caractérisé en ce que le marteau (21) peut être projeté contre la tige extensible (15) par un moyen ressort (28).Ammunition firing device according to one of claims 1 to 4, characterized in that the hammer (21) can be thrown against the extendable rod (15) by spring means (28). Dispositif de mise à feu de munition selon la revendication 5, caractérisé en ce que le marteau (21) se trouve en position de repos avant tir au voisinage de la tige (15) non déployée, le moyen ressort (28) étant à l'état non comprimé et en ce que l'accélération de tir provoque le déplacement du marteau (21) et la compression du moyen ressort (28).Ammunition firing device according to Claim 5, characterized in that the hammer (21) is is in the position of rest before firing in the vicinity of the undeployed rod (15), the spring means (28) being in the uncompressed state and in that the firing acceleration causes the movement of the hammer (21) and the compression of the spring means (28). Dispositif de mise à feu de munition selon la revendication 6, caractérisé en ce que le marteau (21) est maintenu écarté du percuteur par des moyens de maintien comprenant au moins une masselotte centrifuge (25,32) coopérant avec une rampe fixe (26a,34).Ammunition firing device according to claim 6, characterized in that the hammer (21) is kept away from the firing pin by holding means comprising at least one centrifugal flyweight (25,32) cooperating with a fixed ramp (26a, 34). Dispositif de mise à feu de munition selon une des revendications 1 à 7, caractérisé en ce que l'ensemble du dispositif est réalisé sous la forme d'éléments plans micro usinés ou micro gravés sur une plaquette (30).Ammunition firing device according to one of Claims 1 to 7, characterized in that the entire device is designed as micromachined or micro-planar planar elements on a wafer (30). Dispositif de mise à feu de munition selon la revendication 8, caractérisé en ce qu'il comporte une rehausse (37) permettant la mise en place de la composition pyrotechnique (8) au-dessus de la pointe (12).Ammunition firing device according to claim 8, characterized in that it comprises a riser (37) allowing the setting up of the pyrotechnic composition (8) above the tip (12).
EP10290186A 2009-04-10 2010-04-07 Ignition device of a munition by percussion Active EP2239535B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0901797A FR2944348A1 (en) 2009-04-10 2009-04-10 PERCUSSION MUNITING DEVICE

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EP2239535A1 true EP2239535A1 (en) 2010-10-13
EP2239535B1 EP2239535B1 (en) 2012-01-18

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EP (1) EP2239535B1 (en)
AT (1) ATE542103T1 (en)
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Also Published As

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US8104405B2 (en) 2012-01-31
FR2944348A1 (en) 2010-10-15
ATE542103T1 (en) 2012-02-15
EP2239535B1 (en) 2012-01-18
US20100258021A1 (en) 2010-10-14

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