EP0906556B1 - Non-lethal projectile - Google Patents

Non-lethal projectile Download PDF

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Publication number
EP0906556B1
EP0906556B1 EP97930562A EP97930562A EP0906556B1 EP 0906556 B1 EP0906556 B1 EP 0906556B1 EP 97930562 A EP97930562 A EP 97930562A EP 97930562 A EP97930562 A EP 97930562A EP 0906556 B1 EP0906556 B1 EP 0906556B1
Authority
EP
European Patent Office
Prior art keywords
container
wall
projectile
striker
face
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP97930562A
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German (de)
French (fr)
Other versions
EP0906556A1 (en
Inventor
Régis Riffet
Walter Simonella
Guy Valembois
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Etienne LaCroix Tous Artifices SA
Original Assignee
Etienne LaCroix Tous Artifices SA
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Publication of EP0906556A1 publication Critical patent/EP0906556A1/en
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Publication of EP0906556B1 publication Critical patent/EP0906556B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/46Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
    • F42B12/50Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances by dispersion

Definitions

  • the present invention relates to a non-lethal projectile, intended for be projected, in particular pulled from a tube in a longitudinal direction predetermined, and to diffuse a pressurized fluid in a controlled manner, in particular by the impact on a target in said direction, the projectile comprising for this purpose a longitudinal body having a nose towards front and rear tail, a perforable container for fluid under pressure, disposed in said body between the nose and the tail of the latter, a longitudinal striker for perforating said container, juxtaposed longitudinally thereto and carried by a transverse wall integral with the body, means for authorizing or provoking a mutual longitudinal reconciliation of the container and the striker and the perforation of the container by the latter in a controlled manner, in particular by the impact on a target in this direction, and means of distribution of the fluid, to allow the fluid to exit the body, in a distributed manner transversely, after perforation of the container by the striker.
  • tube as well a weapon tube, housing directly the projectile until its shooting, that a tubular case, for example a shell, enveloping at least locally the projectile inside the weapon barrel and remaining therein when the projectile is fired.
  • a tubular case for example a shell
  • Such a projectile assigned to the diffusion of a pressurized fluid chosen from a group comprising incapacitating fluids and marking, is described in European patent application No. 96400608.4, filed on March 22, 1996 by the Applicant, in one embodiment in which the means for distributing the fluid consist of a plurality of transverse orifices arranged in a part of the body housing the container, close to the transverse wall carrying the striker.
  • This known projectile is intended to be fired in a longitudinal direction determined from a gun barrel, and to release the container pressurized fluid upon impact on a target in this sense, under the effect of an inertial percussion during this impact.
  • a projectile comprising, inside a body, a container which, upon impact of the projectile on a target in a determined longitudinal direction, breaks on a striker so that its contents escape through arranged side vents in the wall of the projectile body, around the container, i.e. on the same side that this of a wall carrying the striker as in the case of the projectile described in the aforementioned European patent application.
  • the container described in British Patent No. 1,354,307 is not punctured, but breaks into many pieces when it hits the striker, which required on the one hand to provide a cushion behind this container, to protect it during the firing of the projectile in particular, and on the other hand a wire mesh to inside the vents to prevent pieces of the container from escaping at the same time as the content, which could injure people the surrounding.
  • the present invention is concerned with projectiles whose container is perforable and opens by perforation using the striker, as shown in aforementioned European patent application.
  • the capacity described in this document is no more than a perforable container than the container described in the aforementioned British patent, and this capacity does not does not contain a pressurized fluid, the release of which would be effected by perforation of such a container. Indeed, this release is effected by the telescoping effect of the capacity and release of plugs initially closing the T-shaped end of the tube which is opposite to the rigid wall in which the outlet channels are arranged.
  • the object of the present invention is to remedy this drawback projectiles described in European patent application No. 96400608.4 and, for this purpose, it proposes a projectile of the type indicated in the preamble, characterized in that the means for distributing the fluid comprise a blind longitudinal passage through the striker, open towards the container and closed inside said wall, and a plurality of channels transverse, arranged in said wall, radiating from said passage and opening to the outside of the body.
  • such an embodiment of the means of distribution of the fluid accommodates however of any mode of percussion the container, i.e. the use of any phenomenon specific to cause mutual longitudinal reconciliation of the container and the striker, in conditions suitable for causing perforation of the container by the striker, in particular during impact on a target and given the deliberately limited impact energy in order to preserve the non-lethal nature of the projectile.
  • the percussion can implement a longitudinal displacement of the striker with respect to the transverse wall which carries it but, preferably, the striker is integral with it. So, depending on the case, the percussion may result from a longitudinal crushing of the body, to which case it is expected that the means to authorize or cause a mutual longitudinal reconciliation of the container and the striker and the container perforation by it have an area longitudinally compressible from the body, longitudinally intermediate between the container and said transverse wall, or else this crushing is completed or replaced by a sliding of the container, by inertia, towards the striker inside the body, in which case provision is made that the means to authorize or cause a merger mutual longitudinal of the container and the striker and the perforation of the container by it include a mounting of the container to longitudinal sliding relative to the body, the striker and said wall being placed in front of the container.
  • Percussion by longitudinal crushing of the body is associated with a command of the percussion by the inertia of the body itself upon impact on a target in a determined longitudinal direction while the percussion by sliding from container to striker is compatible with any percussion control mode, in particular with a control by the inertia of the container upon impact on a target in one direction determined longitudinal, or by pyrotechnic or mechanical-pyrotechnic means generally acting without impact the energy of percussion.
  • applications of the present invention are not limited to the case of projectiles intended to be fired from a tube in one direction determined longitudinal and to release the fluid under pressure from the container during an impact on a target in this sense, and which can be achieved in accordance with the present invention projectiles intended to be projected by another means, including being launched by hand as this is the case with hand grenades.
  • the percussion highlights preferably installs the sliding container longitudinal to the body, towards the striker, but it is preferably controlled by means other than inertial, in particular by pyrotechnic or mechanical-pyrotechnic means, known in themselves, in particular operated voluntarily by a user before launching and causing the container to slide towards the striker and its perforation by it under the effect of a release gaseous, generally delayed compared to actuation aforementioned volunteer.
  • inertial in particular by pyrotechnic or mechanical-pyrotechnic means, known in themselves, in particular operated voluntarily by a user before launching and causing the container to slide towards the striker and its perforation by it under the effect of a release gaseous, generally delayed compared to actuation aforementioned volunteer.
  • the notions of longitudinality, of longitudinal sense determined, and the concepts derived from it such as the concepts of transversality, front and rear, nose and tail of the projectile are then understood by reference to the direction of movement of the container towards the striker inside the body.
  • the projectile according to the invention comprises means locking device to immobilize the container relative to the body that the projectile is placed inside the tube, and to release the container automatically with regard to longitudinal sliding relative to the body at the exit of the projectile out of the tube.
  • the body is made in the form of a wall of an elastically deformable material between the nose and the tail, has a smooth inner surface for guiding the container to the longitudinal sliding in the body and a smooth outer face of guiding the projectile to longitudinal sliding in the tube, said face exterior has a localized protrusion capable of retracting by forming a projection on said inner face when the projectile is engaged in the tube and protruding on the outer face in retracting the projection from the inner face when the projectile is out of the tube, and the container integrally has a localized depression, transversely opposite said protuberance when the container is juxtaposed with the striker.
  • Said localized depression of the container can advantageously have the shape of a transverse annular groove, which allows protruding from the wall of the body in the form of a bead transverse, continuously connected to this wall.
  • the projectile has at least one tab elastically flexible released from said wall, having one end free integral with it and offset with respect to said protuberance and a free end integrally carrying said protuberance; then, a plurality of such tabs, advantageously oriented longitudinally, is preferably provided evenly around of the body wall.
  • the aforementioned protuberance not only ensures the containment of the container to against a sliding, inside the body, which can lead to accidental percussion, but also helps to retain the projectile inside the tube insofar as it is elastically stressed towards the outside of the body, it comes to rest against the tube inside of it.
  • this protuberance also provides a seal between the projectile and the tube, which makes it possible to use a gas pressure for firing the projectile developed inside the tube, behind the projectile, for example the pressure of a gas such as compressed air introduced into the tube or the combustion gas pressure of a pyrotechnic charge.
  • the projectile according to the invention when it is intended to be fired from a weapon barrel, in a determined longitudinal direction, comprises advantageously stabilization fins integral with the body at the tail of it, likely to occupy a retracted position in which they are retained under elastic stress by the tube when the projectile is engaged in it and deploy by elasticity when the projectile came out of the tube.
  • These fins are advantageously made of a material elastically deformable and having an end secured to the body and a free end tending by elasticity to shift transversely outwardly relative to the integral end of the body, which is particularly simple, economical and safe, and can be advantageously shaped so as to produce a hissing sound during flight of the projectile, which indicates the shooting and announces the imminence of a impact.
  • the projectile according to the invention may include all provisions known in itself, such as a warhead attached to its nose and made of elastically compressible material, for example of shore A hardness of between 10 and 30 approximately, preferably between 12 and 15, and for example made of silicone.
  • FIGS. 1 to 4 and in FIGS. 5 to 8 presenting great similarities, we will first describe their parts municipalities, indicated by the same reference numbers on all of these figures which will be referred to in the first place.
  • This projectile 1 has a common longitudinal axis 2, before its shooting, to a tube, constituted for example by a weapon tube 3, in which it is initially engaged and from which it leaves in a longitudinal direction 4, predetermined, when fired.
  • Axis 2 will serve as a reference for the concepts of longitudinal and transverse while the firing direction 4 will serve as reference to the concepts of front and back.
  • the tubular wall 6 is made of an elastic material flexible, such as a plastic material in which one can also line up 12.
  • the tail 12 has a wall 13 delimited by faces peripherals respectively external 14 and internal 15 frustoconical of revolution around axis 2 and narrowing towards the rear.
  • each of these faces 14 and 15 is connected to a peripheral face respective cylindrical of revolution around axis 2, namely respectively an outer peripheral face 16 with a diameter identical to that of the outer peripheral face 8 of the wall 6 and a inner peripheral face 17 with a diameter smaller than that of the face inner peripheral 7 of the wall 6.
  • the peripheral face outer 16 is connected to an annular shoulder 18, plan, of revolution around axis 2, turned forwards and placed in abutment, towards the front, against the rear face 10 of the wall 6.
  • This shoulder 18 connects the outer peripheral face 16 to another peripheral face outer 19 of the tail 12, which outer peripheral face 19 is cylindrical of revolution around axis 2 with a diameter substantially identical to that of the inner peripheral face 7 of the wall 6 so to marry an area of this inner peripheral face 7 directly adjacent to the rear face 10 of the wall 6.
  • the peripheral faces inner 17 and outer 19 of the tail 12 thus define, with respect at the wall 13, a tubular rim 20 for nesting inside the wall 6.
  • Towards the front, inner 17 and outer peripheral faces 19 of the flange 20 are connected to each other by a shoulder 81 annular, plane, of revolution around axis 2, thus delimiting the rim 20 forward.
  • the longitudinal dimension separating the shoulders 18 and 81 is much smaller than the dimension longitudinal of the wall 6 between its front 9 and rear 10 faces.
  • the outer 14 and inner peripheral faces 15 of the wall 13 are connected to a respective peripheral face cylindrical of revolution around axis 2, namely respectively a outer peripheral face 22 and an inner peripheral face 21, mutually connected, towards the rear, by an annular shoulder, plane 23, of revolution around axis 2 and turned towards the rear, so as to define a tubular end piece 24.
  • This tubular endpiece 24 is used for integral attachment to the body 5, a tail unit 25 intended to cause a nutation movement of the projectile 1 around axis 2 after firing, to stabilize its trajectory.
  • each fin 31 has a first plane plane 32 in the shape of a rectangular trapezium, the side perpendicular to the bases coincides with one side of the periphery 29 of the base 26 to constitute the front end 82 of the fin 31 and the large base extends to the free end 83 thereof, so that this first panel 32 presents the oblique side of the trapezoid towards the rear, defining a rectilinear fold 33 in the fin 31, and a second plane plane 34 having the shape of a right triangle including the hypotenuse coincides with fold 33, whose long side of the right angle extends the small base of the rectangular trapezoid defined by the first panel 32, forming an angle with this small base so that the pan 34 is offset towards the outside relative to the pan 32, and the short
  • the nose 11 has a flat transverse wall 35 rigid, for example metallic, delimited, in the direction of a distance relative to axis 2, by an outer peripheral face 36 having a diameter substantially equal to that of the inner peripheral face 7 of the wall 6 inside which the wall 35 is thus fitted, with intimate mutual contact between faces 36 and 7, in the immediate vicinity of the front face 9 of wall 6.
  • the outer peripheral face 36 is connected to a annular shoulder, plane 37, of revolution about axis 2, this shoulder 37 being turned towards the rear and bearing flat on the front face 9 of wall 6 to limit the penetration of wall 35 to inside of it.
  • this shoulder 37 connects itself to a peripheral face outer 38, cylindrical of revolution around axis 2 with a diameter identical to that of the outer peripheral face 8 of the wall 6, that this face 38 extends forward, without apparent discontinuity.
  • This outer peripheral face 38 delimits, in the direction of a distance relative to axis 2, a rim 39, annular of revolution around this axis, which the wall 35 has projecting forward, in one piece.
  • this rim 39 is delimited by an inner peripheral face 40 also cylindrical of revolution around axis 2 while it is delimited forwards by a flat annular face 41, of revolution around axis 2, which connects to the outer peripheral face 38 by a softened edge not referenced and to the inner peripheral face 40 by a collar 42, annular of revolution around the axis 2 and placed projecting towards the latter relative to the inner peripheral face 40, in an extreme area before it.
  • this face inner device 40 of the rim 39 is connected to a front face 43 of the wall 35, which front face 43 is transverse flat, and more precisely has the shape of a disc perpendicular to axis 2 and centered on it; this face 43 is for example coplanar with shoulder 37.
  • the face 43, the face 40 and the flange 42 thus define, immediately in front of the wall 35, a receiving cavity 44 and immobilization, for example by crimping by means of the collar 42 and gluing, of a warhead 45, of general shape of revolution around the axis 2, intended to undergo impact with the target and produced for this purpose in a material with elasticity of rubber, for example silicone with shore A hardness between 10 and 30, preferably between 12 and 15, this example is in no way limiting.
  • the warhead 45 has, in projecting forward with respect to the front face 41 of the rim 39, a form hemispherical around an unreferenced center located at the intersection of axis 2 with a geometric plane defined by the rim 41 and, projecting towards the rear inside the cavity 44, a cylindrical tenon retained in compression preload inside the collar 42 so ensure a crimping effect and glued flat to the front face 43 of the wall 35, these fixing examples being in no way limiting.
  • the wall 35 is delimited by a transverse face, plane 46 parallel to face 43 and having a shape annular of revolution around the axis 2.
  • this face 46 is connected to face 36, the distance mutually separating the faces 43 and 46, also defining the longitudinal dimension of the face 36 and therefore the depth depression of the wall 35 inside the wall 6, being weak by relative to the longitudinal dimension of the latter between its faces front and rear 9 and 10 so that between the face 46 of the wall 35 and the shoulder 81 of the tail 12 remains a free longitudinal distance constituting most of the longitudinal dimension of the wall 6.
  • this container 47 can cooperate with the inner peripheral face 7 of the wall 6, for the purpose of guiding relative longitudinal sliding, via a slide integral with this container 47 but mounted for longitudinal sliding against the inner peripheral face 7 of the wall 6, so illustrated but easily conceivable by a skilled person, or cooperate directly for this purpose with the inner peripheral face 7 of the wall 6, as is the case in the illustrated example where the container 47 has the shape of an aerosol can with a side wall 48 tubular, of revolution around axis 2 and essentially delimited, in the direction of a distance from it, by a face external device 49 cylindrical of revolution around this axis with a diameter substantially identical to that of the peripheral face inside 7 of the wall 6 so that is established between the faces 49 and 7 a sliding guide contact with relative longitudinal sliding.
  • this wall 48 is connected, advantageously by making it a single piece, to a flat bottom wall 50, perpendicular to the axis 4 and in particular bounded towards the front by a flat front face 51, in disc shape centered on axis 2 and connected to face 49 by an edge softened, in the direction of a distance from axis 2.
  • the wall 48 is connected in a sealed manner, by a crimping, to a filling valve mechanism 52 arranged as follows axis 2 and turned to the rear, the crimp creating behind the face external device 49 a shoulder 53 annular of revolution around axis 2, plane and facing back.
  • the wall 48 is locally deformed towards the axis 2 in order to present inside the container 47 a rib limiting the penetration of the valve mechanism 52, as is well known from a A person skilled in the art, and this deformation creates, in the peripheral face outside 49 of the wall 48, a groove-shaped depression 54 annular, of revolution around axis 2, closer to shoulder 53 than from the front face 51.
  • the longitudinal dimension mutually separating the shoulder 53 and the front face 51 is less than the longitudinal distance separating mutually the shoulder 81 and the rear face 46 of the wall 35, so that the container 47 can occupy in particular inside the body 5 and the projectile 1 the position illustrated in Figures 1 and 2, in which it rests backwards, by the shoulder 53, on the shoulder 81 of the tail 12, the valve mechanism 52 being freely received coaxially inside of the latter, and in which its front face 51 is spaced longitudinally of the rear face 46 of the wall 35, which corresponds to the position that the container 47 occupies inside the body 5 of the projectile 1 before the firing of the latter, after its shooting during its flight and until impact.
  • the striker 55 is delimited in the direction of a distance from the axis 2 by an outer peripheral face 56 of cylindrical revolution around of this axis with a diameter substantially smaller than that of the face inner peripheral 7 of the wall 6.
  • This outer peripheral face 56 is connected forwards to the rear face 46 of the wall 35 and towards the rear to a flat annular face 57, inclined for example by 45 ° by relative to axis 2 and facing down, which defines for striker 55 a free rear end, at a bevel, and connects this peripheral face outer 56 to an inner peripheral face 58, cylindrical of revolution around axis 2 and delimiting inside the striker 55 a longitudinal passage 59 open towards the rear inside the face in bevel 57 and extending forward to the inside of the wall 35, in which it is closed forward.
  • this passage 59 opens into a plurality of channels 60, the number of eight in the illustrated example, which radiate from it, radially with reference to axis 2, up to the peripheral face outside 36 of the wall 35 into which they open.
  • Each of these channels 60 is for example defined by an inner peripheral face 61, cylindrical of revolution about a respective axis 62 perpendicular to axis 2, the different axes 62 being regularly distributed angularly around it and the respective diameters of the peripheral faces interior 61 being mutually equal but less than the diameter of the inner peripheral face 58 of striker 55.
  • each of the channels 60 is drilled right through a hole 63 delimited by a cylindrical inner peripheral face 64 of revolution around the respective axis 62 with a diameter identical to that of the inner peripheral face 61 of a channel 60, so that the passage 59, channels 60 and holes 63 establish communication between a cavity 65, otherwise sealed, which define the walls 6 and 35 as well as the tail 12, and in which is housed the container 47, and the outside of the body 5.
  • a cavity 65 otherwise sealed, which define the walls 6 and 35 as well as the tail 12, and in which is housed the container 47, and the outside of the body 5.
  • the pressurized fluid 68 initially enclosed in the container 57 escapes from it by successively traversing the longitudinal passage 59 of striker 55, towards the front, then each of channels 60 and the holes 63, centrifugally with reference to axis 2, until it leaves the body 5 of the projectile 1, in a distributed manner transversely around it, and spreading over target 66.
  • the left half of it illustrates an alternative embodiment of the projectile, according to which this effect is completed or replaced by an effect longitudinal crushing of the wall 6 on impact.
  • compression can be promoted longitudinal of the wall 6 at least in a longitudinally zone intermediate between the container 47 and the transverse wall 35, by example as illustrated in the left half of Figure 1, in digging into the outer peripheral face 8 of the wall 6, so located immediately behind the rear face 46 of the wall 35, non-traversing longitudinal cuts 69 of one dimension longitudinal preferably corresponding approximately to double of the longitudinal distance mutually separating the front face 51 of the container 47 and the rear face 46 of the wall 35 when, as it is illustrated in the right half of FIG. 1, the front face 51 is in abutment without constraint and without perforation, forward, against the striker 55.
  • the notches 69 open and allow the formation, in the wall 6, of folds 70 projecting, in the direction of a distance from axis 2, on the face external device 8 of the wall 6, this formation translating itself by an apparent shortening of the wall 6 between the shoulder 81 and the rear face 46 of the wall 35, thus forcing the bottom 50 of the container 47 to press forcibly against the striker 55 which pierces it.
  • the formation of the folds 70 outwards makes it possible to prevent the presence of the container 47 inside the wall 6 does not prevent shortening apparent from the wall 6 and also makes it possible to avoid constituting a obstructs the longitudinal sliding of the container 47 inside the wall 6 when the two apparent shortening effects of this and sliding the container 47 forward inside the latter to cause perforation of the bottom 50 by the striker 55.
  • the arrangement of the passage 59 through the striker 55, channels 60 inside the wall 35 and holes 63 opposite these channels 8 prevents any obstacle to the exit of the fluid initially contained in container 47.
  • the orifice 85 is arranged according to an axis 88 located in this plane and perpendicularly cuts axis 2 to the intersection of this one with the geometrical plane, not referenced, of the face 57; the orifices 86 and 87 have the same axis 89 perpendicular to the plane of Figures 9 and 13 and cutting perpendicular to axis 2 between the intersection of axis 88 with it and the rear face 46 of the wall 35, and they have the same diameter which is less than that of the orifice.
  • the striker 55 does not differs from that which has been described with reference to FIGS. 1 to 8 than by the it is hollowed out, at its free rear end, with a step 90 which forms a step forward with respect to its annular face 57, in the area thereof closest to the wall 35, and opens out longitudinally backwards in this area and transversely in the inner 58 and outer 56 peripheral faces.
  • the annular face 57 has an interruption 91 located in its area closest to the wall 35, symmetrically with respect to a plane perpendicular to the annular face 57 and including axis 2, namely the plane of FIG. 11, and the step 90 is delimited by two flat longitudinal faces 92, 93, mutually symmetrical with respect to this plane and connecting towards the rear to the annular face 57, respectively on either side of the interruption 91 of the latter, and by a flat transverse face 94, facing backwards and mutually connecting these two faces longitudinal 92, 93 in front of the annular face 57.
  • the face transverse 94 is preferably placed at a longitudinal distance from the face 46 of the partition 35, behind the latter, greater than the thickness of the bottom wall 50 of the container 47.
  • the two longitudinal faces 92, 93 are for example located in the same plane not referenced parallel to axis 2 and perpendicular to plane of Figure 11.
  • the plane of the faces 92, 93 is located on the same side of axis 2 as the zone of the annular face 57 closest to the wall 35, so that the break 91 of the face annular 57, and with it the step 90, extend over less than half of the periphery of this annular face 57, and for example over 120 ° in reference to axis 2, this value being indicated only as an example not limiting.
  • step 90 can be adopted without leaving the part of the present invention.
  • the bottom 50 of the container 47 advances towards the wall 35, it first comes into contact with the striker 55 by the area of the bevel face 57 farthest from this wall 35, which causes it to perforate and can cause release progressive of a tongue 84, as the bottom 50 comes to contact of areas of face 57 respectively closer and closer to the wall 35; this tongue 84 tends to remain applied against the face 57, in an oblique orientation relative to the axis 2.
  • the bottom 50 When the bottom 50 reaches at the level of the interruption 91 of the face 57, it crosses the step 90 of which the longitudinal faces 92, 93 then the transverse face 94 straighten the tongue 84 to tend to orient it parallel to axis 2 before the bottom 50 does not come up against the front against the face 46 of the wall 35, as illustrated in Figure 14; so when container 47 comes stop against the face 46 of the wall 35, the tongue 84 possibly formed in its bottom 50 is oriented so that it does not risk to close the mouth of the passage 59 of the striker 55 in the face annular 57, that is to say that it does not constitute any obstacle to the exit, towards the passage 59, the channels 60 and the holes 63, of the fluid initially contained in container 47.
  • this is preferably provided with locking means for immobilize the container 47 relative to the body 5 as long as the projectile 1 is placed inside the weapon tube 3, and to automatically release the container 47 vis-à-vis a longitudinal sliding relative to the body 3 when the projectile 1 leaves the weapon barrel 3.
  • locking means for immobilize the container 47 relative to the body 5 as long as the projectile 1 is placed inside the weapon tube 3, and to automatically release the container 47 vis-à-vis a longitudinal sliding relative to the body 3 when the projectile 1 leaves the weapon barrel 3.
  • the bead 71 is continuous, connected without discontinuity to the wall 6 and advantageously made in one piece with it.
  • the projectile 1 is engaged in the weapon barrel 3, having a cylindrical inner peripheral face 72 of revolution around an axis then coinciding with axis 2 with a diameter substantially identical to that of the outer peripheral face 8 of the wall 6, in order to cooperate with this outer peripheral face 8 for guide the body 5 to longitudinal sliding in the weapon tube 3 during of the shot
  • the bead 71 bearing on this peripheral face interior 72 which applies compression to axis 2 causes it to at least partially elastic deformation, and where appropriate slightly plastic, from wall 6 in the direction of approximation opposite of axis 2, which gives birth, on the inner peripheral face 7 of the wall 6, to a bead 73 also annular of revolution around of axis 2 and forming a projection towards it relative to the face inner peripheral 7 of the wall 6, that is to say penetrating inside the groove 54 so as to immobilize the container 47 by relative to the wall 6, in the support position of the shoulder
  • the bead 71 resting under stress on the face inner device 72 of the weapon tube 3 due to the elasticity of the material constituting the wall 6, ensures retention of the projectile 1 by friction between this inner peripheral face 72, on the one hand, and a sealing between the projectile 1 and this face 72, on the other hand, so particularly advantageous when, as is frequently the case, the shot 1 is carried out by accumulation of gas under pressure between it and a cylinder head not shown closing the tube 3 backwards, either by introduction of a gas under pressure or direct generation of such a gas under pressure, for example by combustion of a pyrotechnic composition adapted.
  • the elasticity of the wall 6 brings back the bead 71, released from the compression applied to it by the inner peripheral face 72, in its original conformation, i.e. protruding on the peripheral face exterior 8 of the wall 6, which causes the protruding bead 73 to disappear on its inner peripheral face 7 and consequently frees the passage for sliding the container 47 forwards inside the wall 6.
  • Each tongue 74 thus integrally formed with the wall 6, has one end 75, here before, connected integrally to the rest of this wall 6, and a free end 76, here rear, bearing integrally, for example by making a single piece, a protrusion 77 in protruding in the direction of a distance from axis 2, on the face outer device 8 of the wall 6 when, as shown by Figures 5, 6, 8, the projectile 1 came out of the weapon barrel 3.
  • this tongue 74 tends elastically to maintain a conformation in which part of the inner 7 and outer 8 peripheral faces which corresponds to it remains arranged according to the same geometric cylinder respective that the rest of the respectively inner peripheral wall or outside of the wall 6.
  • the projectile 1 When, on the other hand, the projectile 1 is housed inside the tube weapon 3, as shown in Figure 7, the inner peripheral face 72 of it based on the respective protuberance 77 made disappear the projection that it forms relative to the peripheral face outside 8 of the wall 6, that is to say causes a bending of each tongue 74 towards axis 2 at the level of the protrusion 77, so that the free end 76 of each tongue 74 forms a projection towards axis 2 on the inner peripheral face 7 of the wall 6.
  • the container 47 instead of being mounted directly to the sliding inside the body 5, the container 47 would be mounted at sliding inside the body 5 by means of a slide, the bead 71 or the tabs 74 could cooperate, in a way identical to that which has been described with reference to groove 54, with a similar groove in the slide.
  • the bead 71 or the tabs 74 could cooperate, in a way identical to that which has been described with reference to groove 54, with a similar groove in the slide.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Dispersion Chemistry (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Earth Drilling (AREA)

Description

La présente invention concerne un projectile non létal, destiné à être projeté, notamment tiré à partir d'un tube dans un sens longitudinal prédéterminé, et à diffuser un fluide sous pression de façon commandée, notamment par l'impact sur une cible dans ledit sens, le projectile comportant à cet effet un corps longitudinal présentant un nez vers l'avant et une queue vers l'arrière, un conteneur perforable pour le fluide sous pression, disposé dans ledit corps entre le nez et la queue de celui-ci, un percuteur longitudinal de perforation dudit conteneur, juxtaposé longitudinalement à celui-ci et porté par une paroi transversale solidaire du corps, des moyens pour autoriser ou provoquer un rapprochement longitudinal mutuel du conteneur et du percuteur et la perforation du conteneur par celui-ci de façon commandée, notamment par l'impact sur une cible dans ledit sens, et des moyens de distribution du fluide, pour autoriser la sortie du fluide hors du corps, de façon répartie transversalement, après perforation du conteneur par le percuteur.The present invention relates to a non-lethal projectile, intended for be projected, in particular pulled from a tube in a longitudinal direction predetermined, and to diffuse a pressurized fluid in a controlled manner, in particular by the impact on a target in said direction, the projectile comprising for this purpose a longitudinal body having a nose towards front and rear tail, a perforable container for fluid under pressure, disposed in said body between the nose and the tail of the latter, a longitudinal striker for perforating said container, juxtaposed longitudinally thereto and carried by a transverse wall integral with the body, means for authorizing or provoking a mutual longitudinal reconciliation of the container and the striker and the perforation of the container by the latter in a controlled manner, in particular by the impact on a target in this direction, and means of distribution of the fluid, to allow the fluid to exit the body, in a distributed manner transversely, after perforation of the container by the striker.

On entendra ici par "tube" aussi bien un tube d'arme, logeant directement le projectile jusqu'à son tir, qu'un étui tubulaire, par exemple une douille, enveloppant au moins localement le projectile à l'intérieur du tube d'arme et restant dans celui-ci lors du tir du projectile.We will hear here by "tube" as well a weapon tube, housing directly the projectile until its shooting, that a tubular case, for example a shell, enveloping at least locally the projectile inside the weapon barrel and remaining therein when the projectile is fired.

Un tel projectile, affecté à la diffusion d'un fluide sous pression choisi dans un groupe comportant les fluides incapacitants et les fluides de marquage, est décrit dans la demande de brevet européen N° 96400608.4, déposée le 22 Mars 1996 par la Demanderesse, dans un mode de réalisation dans lequel les moyens de distribution du fluide sont constitués par une pluralité d'orifices transversaux aménagés dans une partie du corps logeant le conteneur, à proximité immédiate de la paroi transversale portant le percuteur. Ce projectile connu est destiné à être tiré dans un sens longitudinal déterminé à partir d'un tube d'arme, et à libérer le fluide sous pression du conteneur lors de l'impact sur une cible dans ce sens, sous l'effet d'une percussion inertielle lors de cet impact.Such a projectile, assigned to the diffusion of a pressurized fluid chosen from a group comprising incapacitating fluids and marking, is described in European patent application No. 96400608.4, filed on March 22, 1996 by the Applicant, in one embodiment in which the means for distributing the fluid consist of a plurality of transverse orifices arranged in a part of the body housing the container, close to the transverse wall carrying the striker. This known projectile is intended to be fired in a longitudinal direction determined from a gun barrel, and to release the container pressurized fluid upon impact on a target in this sense, under the effect of an inertial percussion during this impact.

Cette solution ne donne pas totalement satisfaction dans la mesure où l'énergie d'impact peut être suffisante pour provoquer non seulement la percussion, c'est-à-dire la perforation du conteneur par le percuteur, mais également un écrasement du conteneur sur la paroi transversale portant le percuteur, avec un effet de sertissage du conteneur à l'intérieur du corps et/ou sur le percuteur, à proximité immédiate de la paroi transversale précitée, c'est-à-dire dans la zone dans laquelle se situent les orifices.This solution is not entirely satisfactory to the extent where the impact energy can be sufficient to cause not only percussion, that is to say the perforation of the container by the striker, but also a crushing of the container on the transverse wall carrying the striker, with a crimping effect of the container to inside the body and / or on the striker, in the immediate vicinity of the the aforementioned transverse wall, that is to say in the area in which locate the holes.

Il en résulte un bouchage au moins partiel de ces derniers, affectant l'efficacité du projectile. En effet, il est important que non seulement le fluide en sorte, mais également que cette sortie s'effectue dans un temps extrêmement court, c'est-à-dire avant que le projectile ne tombe au sol après avoir heurté sa cible.This results in at least partial blockage of the latter, affecting the effectiveness of the projectile. Indeed, it is important that not only the fluid so, but also that this exit takes place in an extremely short time, that is to say before the projectile falls to the ground after hitting its target.

On connaít également, par la figure 7 du brevet britannique N° 1 354 307, un projectile comportant, à l'intérieur d'un corps, un conteneur qui, lors de l'impact du projectile sur une cible dans un sens longitudinal déterminé, vient se rompre sur un percuteur de telle sorte que son contenu s'échappe par des évents latéraux aménagés dans la paroi du corps du projectile, autour du conteneur, c'est-à-dire du même côté que celui-ci d'une paroi portant le percuteur comme dans le cas du projectile décrit dans la demande de brevet européen précitée.Also known, by Figure 7 of British Patent No. 1,354,307, a projectile comprising, inside a body, a container which, upon impact of the projectile on a target in a determined longitudinal direction, breaks on a striker so that its contents escape through arranged side vents in the wall of the projectile body, around the container, i.e. on the same side that this of a wall carrying the striker as in the case of the projectile described in the aforementioned European patent application.

Toutefois, le conteneur décrit dans le brevet britannique N° 1 354 307 n'est pas perforable, mais se brise en de nombreux morceaux lorsqu'il vient heurter le percuteur, ce qui a obligé à prévoir d'une part un coussin en arrière de ce conteneur, pour le protéger lors du tir du projectile notamment, et d'autre part un grillage à l'intérieur des évents pour empêcher les morceaux du conteneur de s'échapper en même temps que le contenu de celui-ci, ce qui risquerait de blesser des personnes à l'entour.However, the container described in British Patent No. 1,354,307 is not not punctured, but breaks into many pieces when it hits the striker, which required on the one hand to provide a cushion behind this container, to protect it during the firing of the projectile in particular, and on the other hand a wire mesh to inside the vents to prevent pieces of the container from escaping at the same time as the content, which could injure people the surrounding.

Par contre, la présente invention s'intéresse à des projectiles dont le conteneur est perforable et s'ouvre par perforation au moyen du percuteur, comme l'enseigne la demande de brevet européen précitée.On the other hand, the present invention is concerned with projectiles whose container is perforable and opens by perforation using the striker, as shown in aforementioned European patent application.

On connaít également, de par le brevet américain N° 1 671 364, un projectile comportant un tube plongeant en permanence à l'intérieur d'une capacité contenant un fluide à expulser et communiquant avec des canaux aménagés dans une paroi rigide du projectile.We also know, from US Patent No. 1,671,364, a projectile comprising a tube permanently immersed inside a container a fluid to be expelled and communicating with channels arranged in a wall rigid projectile.

La capacité décrite dans ce document n'est pas plus un conteneur perforable que le conteneur décrit dans le brevet britannique précité, et cette capacité ne contient pas un fluide sous pression dont la libération s'effectuerait par perforation d'un tel conteneur. En effet, cette libération s'effectue par effet de télescopage de la capacité et dégagement de bouchons obturant initialement l'extrémité, en T, du tube qui est opposée à la paroi rigide dans laquelle sont aménagés les canaux de sortie.The capacity described in this document is no more than a perforable container than the container described in the aforementioned British patent, and this capacity does not does not contain a pressurized fluid, the release of which would be effected by perforation of such a container. Indeed, this release is effected by the telescoping effect of the capacity and release of plugs initially closing the T-shaped end of the tube which is opposite to the rigid wall in which the outlet channels are arranged.

Par conséquent, pas plus que le brevet britannique N° 1 354 307, ce brevet américain N° 1 671 364 ne concerne des projectiles menant en oeuvre un conteneur perforable par l'effet d'un percuteur, c'est-à-dire du type décrit dans le demande de brevet européen précité. En particulier, aucun de ces documents n'enseigne un moyen de remédier à l'inconvénient, précité, du projectile décrit dans cette demande de brevet européen.Therefore, no more than British Patent No. 1,354,307, this patent American No. 1 671 364 does not relate to projectiles carrying out a container perforable by the effect of a striker, i.e. of the type described in the application for European patent cited above. In particular, none of these documents teaches a means of remedying the aforementioned drawback of the projectile described in this application European patent.

La présente invention a pour but de remédier à cet inconvénient des projectiles décrits dans la demande de brevet européen N° 96400608.4 et, à cet effet, elle propose un projectile du type indiqué en préambule, caractérisé en ce que les moyens de distribution du fluide comportent un passage longitudinal borgne traversant le percuteur, ouvert vers le conteneur et fermé à l'intérieur de ladite paroi, et une pluralité de canaux transversaux, aménagés dans ladite paroi, rayonnant à partir dudit passage et débouchant à l'extérieur du corps.The object of the present invention is to remedy this drawback projectiles described in European patent application No. 96400608.4 and, for this purpose, it proposes a projectile of the type indicated in the preamble, characterized in that the means for distributing the fluid comprise a blind longitudinal passage through the striker, open towards the container and closed inside said wall, and a plurality of channels transverse, arranged in said wall, radiating from said passage and opening to the outside of the body.

Un Homme du métier comprendra aisément qu'un éventuel écrasement du conteneur sur la paroi transversale portant le percuteur n'a aucun effet, dans ces conditions, sur la sortie du fluide sous pression, si bien que l'on est assuré que le projectile selon l'invention libère le fluide qu'il contient, et ceci en un temps très court après l'impact sur sa cible si l'on choisit de commander la percussion par inertie, lors de cet impact.A skilled person will easily understand that a possible crushing of the container on the transverse wall carrying the striker has no effect, under these conditions, on the outlet of the pressurized fluid, if although it is ensured that the projectile according to the invention releases the fluid that it contains, and this in a very short time after impact on its target if one chooses to control the percussion by inertia, during this impact.

Naturellement, un tel mode de réalisation des moyens de distribution du fluide s'accommode cependant de tout mode de percussion du conteneur, c'est-à-dire de l'utilisation de tout phénomène propre à provoquer le rapprochement longitudinal mutuel du conteneur et du percuteur, dans des conditions propres à provoquer la perforation du conteneur par le percuteur, notamment lors de l'impact sur une cible et compte tenu de l'énergie d'impact volontairement limitée afin de préserver le caractère non létal du projectile.Naturally, such an embodiment of the means of distribution of the fluid accommodates however of any mode of percussion the container, i.e. the use of any phenomenon specific to cause mutual longitudinal reconciliation of the container and the striker, in conditions suitable for causing perforation of the container by the striker, in particular during impact on a target and given the deliberately limited impact energy in order to preserve the non-lethal nature of the projectile.

La percussion peut mettre en oeuvre un déplacement longitudinal du percuteur par rapport à la paroi transversale qui le porte mais, de préférence, le percuteur est solidaire de celle-ci. Alors, selon les cas, la percussion peut résulter d'un écrasement longitudinal du corps, auquel cas on prévoit que les moyens pour autoriser ou provoquer un rapprochement longitudinal mutuel du conteneur et du percuteur et la perforation du conteneur par celui-ci comportent une zone longitudinalement compressible du corps, longitudinalement intermédiaire entre le conteneur et ladite paroi transversale, ou bien cet écrasement est complété ou remplacé par un coulissement du conteneur, par inertie, vers le percuteur à l'intérieur du corps, auquel cas on prévoit que les moyens pour autoriser ou provoquer un rapprochement longitudinal mutuel du conteneur et du percuteur et la perforation du conteneur par celui-ci comportent un montage du conteneur à coulissement longitudinal par rapport au corps, le percuteur et ladite paroi étant placés en avant du conteneur.The percussion can implement a longitudinal displacement of the striker with respect to the transverse wall which carries it but, preferably, the striker is integral with it. So, depending on the case, the percussion may result from a longitudinal crushing of the body, to which case it is expected that the means to authorize or cause a mutual longitudinal reconciliation of the container and the striker and the container perforation by it have an area longitudinally compressible from the body, longitudinally intermediate between the container and said transverse wall, or else this crushing is completed or replaced by a sliding of the container, by inertia, towards the striker inside the body, in which case provision is made that the means to authorize or cause a merger mutual longitudinal of the container and the striker and the perforation of the container by it include a mounting of the container to longitudinal sliding relative to the body, the striker and said wall being placed in front of the container.

Ces deux conceptions des moyens pour autoriser ou provoquer un rapprochement longitudinal mutuel du conteneur et du percuteur et la perforation du conteneur par celui-ci peuvent être combinés, de même que d'autres moyens peuvent être choisis, tels que des moyens pyrotechniques initiés par l'impact ou, avec retard, par le tir du projectile, ces exemples n'étant nullement limitatifs. La percussion par écrasement longitudinal du corps est associée à une commande de la percussion par l'inertie du corps lui-même lors d'un impact sur une cible dans un sens longitudinal déterminé alors que la percussion par coulissement du conteneur vers le percuteur est compatible avec tout mode de commande de la percussion, notamment avec une commande par l'inertie du conteneur lors d'un impact sur une cible dans un sens longitudinal déterminé, ou par des moyens pyrotechniques ou mécano-pyrotechniques agissant généralement sans qu'un impact fournisse l'énergie de percussion.These two conceptions of the means to authorize or provoke a mutual longitudinal reconciliation of the container and the striker and the container perforation by it can be combined, similarly that other means can be chosen, such as means pyrotechnics initiated by the impact or, with delay, by the firing of the projectile, these examples being in no way limiting. Percussion by longitudinal crushing of the body is associated with a command of the percussion by the inertia of the body itself upon impact on a target in a determined longitudinal direction while the percussion by sliding from container to striker is compatible with any percussion control mode, in particular with a control by the inertia of the container upon impact on a target in one direction determined longitudinal, or by pyrotechnic or mechanical-pyrotechnic means generally acting without impact the energy of percussion.

Un Homme du métier comprendra en effet aisément que les applications de la présente invention ne se limitent pas au cas de projectiles destinés à être tirés à partir d'un tube dans un sens longitudinal déterminé et à libérer le fluide sous pression du conteneur lors d'un impact sur une cible dans ce sens, et que l'on peut réaliser conformément à la présente invention des projectiles destinés à être projetés par un autre moyen, notamment à être lancés à la main comme c'est le cas des grenades à main. Dans un tel cas, la percussion met en oeuvre de préférence un montage du conteneur à coulissement longitudinal par rapport au corps, vers le percuteur, mais elle est de préférence commandée par des moyens autres qu'inertiels, notamment par des moyens pyrotechniques ou mécano-pyrotechniques, connus en eux-mêmes, notamment actionnés volontairement par un utilisateur préalablement au lancer et provoquant le coulissement du conteneur vers le percuteur et sa perforation par celui-ci sous l'effet d'un dégagement gazeux, de façon généralement retardée par rapport à l'actionnement volontaire précité. Les notions de longitudinalité, de sens longitudinal déterminé, et les notions qui en sont dérivées telles que les notions de transversalité, d'avant et d'arrière, de nez et de queue du projectile s'entendent alors par référence au sens de déplacement du conteneur vers le percuteur à l'intérieur du corps.A skilled person will easily understand that applications of the present invention are not limited to the case of projectiles intended to be fired from a tube in one direction determined longitudinal and to release the fluid under pressure from the container during an impact on a target in this sense, and which can be achieved in accordance with the present invention projectiles intended to be projected by another means, including being launched by hand as this is the case with hand grenades. In such a case, the percussion highlights preferably installs the sliding container longitudinal to the body, towards the striker, but it is preferably controlled by means other than inertial, in particular by pyrotechnic or mechanical-pyrotechnic means, known in themselves, in particular operated voluntarily by a user before launching and causing the container to slide towards the striker and its perforation by it under the effect of a release gaseous, generally delayed compared to actuation aforementioned volunteer. The notions of longitudinality, of longitudinal sense determined, and the concepts derived from it such as the concepts of transversality, front and rear, nose and tail of the projectile are then understood by reference to the direction of movement of the container towards the striker inside the body.

Lorsque la percussion met en oeuvre un montage du conteneur à coulissement longitudinal par rapport au corps et dans le cas d'un projectile destiné à être tiré à partir d'un tube d'arme, on prévoit avantageusement que le projectile selon l'invention comporte des moyens de verrouillage pour immobiliser le conteneur par rapport au corps tant que le projectile est placé à l'intérieur du tube, et pour libérer automatiquement le conteneur vis-à-vis d'un coulissement longitudinal par rapport au corps à la sortie du projectile hors du tube.When the percussion involves mounting the container to longitudinal sliding relative to the body and in the case of a projectile intended to be fired from a weapon tube, provision is made advantageously that the projectile according to the invention comprises means locking device to immobilize the container relative to the body that the projectile is placed inside the tube, and to release the container automatically with regard to longitudinal sliding relative to the body at the exit of the projectile out of the tube.

Selon un mode de réalisation particulièrement simple, tout en étant efficace, de ces moyens de verrouillage, le corps est réalisé sous forme d'une paroi en une matière élastiquement déformable entre le nez et la queue, présente une face intérieure lisse de guidage du conteneur au coulissement longitudinal dans le corps et une face extérieure lisse de guidage du projectile au coulissement longitudinal dans le tube, ladite face extérieure présente une protubérance localisée susceptible de s'escamoter en formant une saillie sur ladite face intérieure lorsque le projectile est engagé dans le tube et de revenir en saillie sur la face extérieure en escamotant la saillie de la face intérieure lorsque le projectile est sorti du tube, et le conteneur présente solidairement une dépression localisée, transversalement en regard de ladite protubérance lorsque le conteneur est juxtaposé au percuteur.According to a particularly simple embodiment, while being effective, of these locking means, the body is made in the form of a wall of an elastically deformable material between the nose and the tail, has a smooth inner surface for guiding the container to the longitudinal sliding in the body and a smooth outer face of guiding the projectile to longitudinal sliding in the tube, said face exterior has a localized protrusion capable of retracting by forming a projection on said inner face when the projectile is engaged in the tube and protruding on the outer face in retracting the projection from the inner face when the projectile is out of the tube, and the container integrally has a localized depression, transversely opposite said protuberance when the container is juxtaposed with the striker.

Ladite dépression localisée du conteneur peut avantageusement présenter la forme d'une gorge annulaire transversale, ce qui permet de réaliser la protubérance de la paroi du corps sous la forme d'un bourrelet transversal, raccordé sans discontinuité à cette paroi. On peut cependant également prévoir que le projectile comporte au moins une languette élastiquement flexible dégagée de ladite paroi, présentant une extrémité libre solidaire de celle-ci et décalée par rapport à ladite protubérance et une extrémité libre portant solidairement ladite protubérance ; alors, une pluralité de telles languettes, avantageusement orientées longitudinalement, est de préférence prévue de façon équirépartie autour de la paroi du corps.Said localized depression of the container can advantageously have the shape of a transverse annular groove, which allows protruding from the wall of the body in the form of a bead transverse, continuously connected to this wall. We can however also provide that the projectile has at least one tab elastically flexible released from said wall, having one end free integral with it and offset with respect to said protuberance and a free end integrally carrying said protuberance; then, a plurality of such tabs, advantageously oriented longitudinally, is preferably provided evenly around of the body wall.

On observera que, quel que soit son mode de réalisation, la protubérance précitée assure non seulement la retenue du conteneur à l'encontre d'un coulissement, à l'intérieur du corps, pouvant aboutir à une percussion accidentelle, mais contribue en outre à retenir le projectile à l'intérieur du tube dans la mesure où, sollicitée élastiquement vers l'extérieur du corps, elle vient s'appuyer contre le tube à l'intérieur de celui-ci. Dans le cas particulier où cette protubérance présente la forme d'un bourrelet transversal, raccordé sans discontinuité à la paroi du corps, cette protubérance assure en outre une étanchéité entre le projectile et le tube, ce qui permet d'utiliser pour le tir du projectile une pression gazeuse développée à l'intérieur du tube, en arrière du projectile, par exemple la pression d'un gaz tel que de l'air comprimé introduit dans le tube ou la pression de gaz de combustion d'une charge pyrotechnique.It will be observed that, whatever its embodiment, the the aforementioned protuberance not only ensures the containment of the container to against a sliding, inside the body, which can lead to accidental percussion, but also helps to retain the projectile inside the tube insofar as it is elastically stressed towards the outside of the body, it comes to rest against the tube inside of it. In the particular case where this protuberance has the form a transverse bead, connected without discontinuity to the wall of the body, this protuberance also provides a seal between the projectile and the tube, which makes it possible to use a gas pressure for firing the projectile developed inside the tube, behind the projectile, for example the pressure of a gas such as compressed air introduced into the tube or the combustion gas pressure of a pyrotechnic charge.

D'une façon connue généralement dans le domaine des projectiles, le projectile selon l'invention, lorsqu'il est destiné à être tiré à partir d'un tube d'arme, dans un sens longitudinal déterminé, comporte avantageusement des ailettes de stabilisation solidaires du corps à la queue de celui-ci, susceptibles d'occuper une position escamotée dans laquelle elles sont retenues sous contrainte élastique par le tube lorsque le projectile est engagé dans celui-ci et de se déployer par élasticité lorsque le projectile est sorti du tube.In a manner generally known in the field of projectiles, the projectile according to the invention, when it is intended to be fired from a weapon barrel, in a determined longitudinal direction, comprises advantageously stabilization fins integral with the body at the tail of it, likely to occupy a retracted position in which they are retained under elastic stress by the tube when the projectile is engaged in it and deploy by elasticity when the projectile came out of the tube.

Ces ailettes sont avantageusement réalisées en une matière élastiquement déformable et présentant une extrémité solidaire du corps et une extrémité libre tendant par élasticité à se décaler transversalement vers l'extérieur par rapport à l'extrémité solidaire du corps, ce qui est particulièrement simple, économique et sûr, et peuvent être avantageusement conformées de façon à produire un sifflement lors du vol du projectile, ce qui témoigne du tir et annonce l'imminence d'un impact.These fins are advantageously made of a material elastically deformable and having an end secured to the body and a free end tending by elasticity to shift transversely outwardly relative to the integral end of the body, which is particularly simple, economical and safe, and can be advantageously shaped so as to produce a hissing sound during flight of the projectile, which indicates the shooting and announces the imminence of a impact.

En outre, le projectile selon l'invention peut comporter toutes dispositions connues en elle-même, telles qu'une ogive rapportée sur son nez et réalisée en matériau élastiquement compressible, par exemple de dureté shore A comprise entre 10 et 30 environ, de préférence entre 12 et 15, et par exemple en silicone.In addition, the projectile according to the invention may include all provisions known in itself, such as a warhead attached to its nose and made of elastically compressible material, for example of shore A hardness of between 10 and 30 approximately, preferably between 12 and 15, and for example made of silicone.

D'autres caractéristiques et avantages d'un projectile selon l'invention ressortiront de la description ci-dessous, relative à un exemple non limitatif de réalisation, ainsi que des dessins annexés qui font partie intégrante de cette description.

  • La figure 1 montre une vue d'un projectile selon l'invention, sorti du tube mais avant l'impact sur une cible, pour moitié en élévation et pour moitié en coupe par un demi-plan défini par un axe longitudinal de ce projectile.
  • La figure 2 montre, à plus grande échelle, un détail repéré en II à la figure 1.
  • La figure 3 montre ce même détail alors que le projectile est encore engagé dans le tube.
  • La figure 4 montre, en une vue analogue à celle de la figure 1, le projectile après impact sur sa cible, selon deux modes de comportement du projectile lors de l'impact, illustrés respectivement dans l'une et l'autre moitiés de cette figure.
  • Les figures 5 à 8 illustrent, en des vues correspondant respectivement à celles des figures 1 à 4, une variante de réalisation du projectile, la figure 6 illustrant un détail repéré en VI à la figure 5.
  • Les figures 9 et 10 illustrent, en des vues en coupe analogues à celles des figures 1, 4, 5, 8, deux variantes préférées de réalisation d'une pièce groupant le percuteur et la paroi transversale qui le porte.
  • Les figures 11 et 12 montrent ces deux variantes en perspective, respectivement.
  • Les figures 13 et 14 illustrent, en des vues correspondant à celles des figures 4 et 8 mais localisées autour du percuteur et de la paroi transversale qui le porte, la coopération du conteneur, après sa perforation elle-même consécutive à l'impact du projectile sur sa cible, avec ces deux variantes, respectivement.
Other characteristics and advantages of a projectile according to the invention will emerge from the description below, relating to a nonlimiting exemplary embodiment, as well as from the appended drawings which form an integral part of this description.
  • Figure 1 shows a view of a projectile according to the invention, out of the tube but before impact on a target, half in elevation and half in section by a half-plane defined by a longitudinal axis of this projectile.
  • FIG. 2 shows, on a larger scale, a detail identified in II in FIG. 1.
  • Figure 3 shows this same detail while the projectile is still engaged in the tube.
  • FIG. 4 shows, in a view similar to that of FIG. 1, the projectile after impact on its target, according to two modes of behavior of the projectile during impact, illustrated respectively in one and the other halves of this figure.
  • FIGS. 5 to 8 illustrate, in views corresponding respectively to those of FIGS. 1 to 4, an alternative embodiment of the projectile, FIG. 6 illustrating a detail marked in VI in FIG. 5.
  • Figures 9 and 10 illustrate, in sectional views similar to those of Figures 1, 4, 5, 8, two preferred embodiments of a part grouping the striker and the transverse wall which carries it.
  • Figures 11 and 12 show these two variants in perspective, respectively.
  • Figures 13 and 14 illustrate, in views corresponding to those of Figures 4 and 8 but located around the striker and the transverse wall which carries it, the cooperation of the container, after its perforation itself following the impact of the projectile on its target, with these two variants, respectively.

Les deux modes de réalisation d'un projectile selon l'invention qui ont été illustrés respectivement aux figures 1 à 4 et aux figures 5 à 8 présentant de grandes similitudes, on décrira en premier lieu leurs parties communes, indiquées par les mêmes références numériques sur l'ensemble de ces figures auxquelles on se référera en premier lieu. The two embodiments of a projectile according to the invention which have been illustrated respectively in FIGS. 1 to 4 and in FIGS. 5 to 8 presenting great similarities, we will first describe their parts municipalities, indicated by the same reference numbers on all of these figures which will be referred to in the first place.

Ce projectile 1 présente un axe longitudinal 2 commun, avant son tir, à un tube, constitué par exemple par un tube d'arme 3, dans lequel il est initialement engagé et dont il sort dans un sens longitudinal 4, prédéterminé, lors du tir. L'axe 2 servira de référence aux notions de longitudinalité et de transversalité alors que le sens de tir 4 servira de référence aux notions d'avant et d'arrière.This projectile 1 has a common longitudinal axis 2, before its shooting, to a tube, constituted for example by a weapon tube 3, in which it is initially engaged and from which it leaves in a longitudinal direction 4, predetermined, when fired. Axis 2 will serve as a reference for the concepts of longitudinal and transverse while the firing direction 4 will serve as reference to the concepts of front and back.

Le projectile 1 comporte un corps 5 défini dans l'exemple illustré par :

  • une paroi tubulaire 6, longitudinale, définie par des faces périphériques respectivement intérieure 7 et extérieure 8 cylindriques de révolution autour de l'axe 2 et lisses, à une exception près qui sera décrite ultérieurement, et par deux faces annulaires planes, transversales, de révolution autour de l'axe 2, à raison d'une face avant 9 et d'une face arrière 10, raccordant mutuellement les faces 7 et 8 respectivement en avant et en arrière du corps 5 ;
  • un nez 11, définissant une extrémité avant du corps 5 et fixé à la paroi 6 par exemple par emboítement et collage dans une zone de sa face périphérique intérieure 7 jouxtant directement la face avant 9 et collage, le nez 11 présentant une forme générale de révolution autour de l'axe 2 à des exceptions près qui seront décrites ultérieurement ;
  • une queue 12 définissant une extrémité arrière du corps 5 et fixée sur la paroi 6 par exemple par emboítement et collage dans une zone de sa face périphérique intérieure 7 jouxtant directement sa face arrière 10 et collage, cette queue 12 présentant une forme générale tubulaire, de révolution autour de l'axe 2.
The projectile 1 comprises a body 5 defined in the example illustrated by:
  • a tubular wall 6, longitudinal, defined by respectively inner 7 and outer 8 cylindrical faces of revolution around the axis 2 and smooth, with one exception which will be described later, and by two annular planar, transverse faces of revolution around the axis 2, at the rate of a front face 9 and a rear face 10, mutually connecting the faces 7 and 8 respectively in front and behind the body 5;
  • a nose 11, defining a front end of the body 5 and fixed to the wall 6 for example by fitting and bonding in a zone of its inner peripheral face 7 directly adjoining the front face 9 and bonding, the nose 11 having a general shape of revolution around axis 2 with exceptions which will be described later;
  • a tail 12 defining a rear end of the body 5 and fixed to the wall 6 for example by fitting and bonding in a zone of its inner peripheral face 7 directly adjoining its rear face 10 and bonding, this tail 12 having a generally tubular shape, revolution around axis 2.

La paroi tubulaire 6 est réalisée en une matière élastiquement flexible, telle qu'une matière plastique dans laquelle on peut également réaliser la queue 12.The tubular wall 6 is made of an elastic material flexible, such as a plastic material in which one can also line up 12.

La queue 12 présente une paroi 13 délimitée par des faces périphériques respectivement extérieure 14 et intérieure 15 tronconiques de révolution autour de l'axe 2 et se rétrécissant vers l'arrière. Vers l'avant, chacune de ces faces 14 et 15 se raccorde à une face périphérique respective cylindrique de révolution autour de l'axe 2, à savoir respectivement une face périphérique extérieure 16 d'un diamètre identique à celui de la face périphérique extérieure 8 de la paroi 6 et une face périphérique intérieure 17 d'un diamètre inférieur à celui de la face périphérique intérieure 7 de la paroi 6. Vers l'avant, la face périphérique extérieure 16 se raccorde à un épaulement 18 annulaire, plan, de révolution autour de l'axe 2, tourné vers l'avant et placé en butée, vers l'avant, contre la face arrière 10 de la paroi 6. Cet épaulement 18 raccorde la face périphérique extérieure 16 à une autre face périphérique extérieure 19 de la queue 12, laquelle face périphérique extérieure 19 est cylindrique de révolution autour de l'axe 2 avec un diamètre sensiblement identique à celui de la face périphérique intérieure 7 de la paroi 6 afin d'épouser une zone de cette face périphérique intérieure 7 directement adjacente à la face arrière 10 de la paroi 6. Les faces périphériques intérieure 17 et extérieure 19 de la queue 12 définissent ainsi, par rapport à la paroi 13, un rebord tubulaire 20 d'emboítement à l'intérieur de la paroi 6. Vers l'avant, des faces périphériques intérieure 17 et extérieure 19 du rebord 20 sont raccordées mutuellement par un épaulement 81 annulaire, plan, de révolution autour de l'axe 2, délimitant ainsi le rebord 20 vers l'avant. La dimension longitudinale séparant mutuellement les épaulements 18 et 81 est largement inférieure à la dimension longitudinale de la paroi 6 entre ses faces avant 9 et arrière 10.The tail 12 has a wall 13 delimited by faces peripherals respectively external 14 and internal 15 frustoconical of revolution around axis 2 and narrowing towards the rear. Towards the front, each of these faces 14 and 15 is connected to a peripheral face respective cylindrical of revolution around axis 2, namely respectively an outer peripheral face 16 with a diameter identical to that of the outer peripheral face 8 of the wall 6 and a inner peripheral face 17 with a diameter smaller than that of the face inner peripheral 7 of the wall 6. Towards the front, the peripheral face outer 16 is connected to an annular shoulder 18, plan, of revolution around axis 2, turned forwards and placed in abutment, towards the front, against the rear face 10 of the wall 6. This shoulder 18 connects the outer peripheral face 16 to another peripheral face outer 19 of the tail 12, which outer peripheral face 19 is cylindrical of revolution around axis 2 with a diameter substantially identical to that of the inner peripheral face 7 of the wall 6 so to marry an area of this inner peripheral face 7 directly adjacent to the rear face 10 of the wall 6. The peripheral faces inner 17 and outer 19 of the tail 12 thus define, with respect at the wall 13, a tubular rim 20 for nesting inside the wall 6. Towards the front, inner 17 and outer peripheral faces 19 of the flange 20 are connected to each other by a shoulder 81 annular, plane, of revolution around axis 2, thus delimiting the rim 20 forward. The longitudinal dimension separating the shoulders 18 and 81 is much smaller than the dimension longitudinal of the wall 6 between its front 9 and rear 10 faces.

Vers l'arrière, les faces périphériques extérieure 14 et intérieure 15 de la paroi 13 se raccordent à une face périphérique respective cylindrique de révolution autour de l'axe 2, à savoir respectivement une face périphérique extérieure 22 et une face périphérique intérieure 21, raccordées mutuellement, vers l'arrière, par un épaulement annulaire, plan 23, de révolution autour de l'axe 2 et tourné vers l'arrière, de façon à délimiter un embout tubulaire 24.Towards the rear, the outer 14 and inner peripheral faces 15 of the wall 13 are connected to a respective peripheral face cylindrical of revolution around axis 2, namely respectively a outer peripheral face 22 and an inner peripheral face 21, mutually connected, towards the rear, by an annular shoulder, plane 23, of revolution around axis 2 and turned towards the rear, so as to define a tubular end piece 24.

Cet embout tubulaire 24 sert à la fixation solidaire, sur le corps 5, d'un empennage 25 destiné à provoquer un mouvement de nutation du projectile 1 autour de l'axe 2 après son tir, afin de stabiliser sa trajectoire.This tubular endpiece 24 is used for integral attachment to the body 5, a tail unit 25 intended to cause a nutation movement of the projectile 1 around axis 2 after firing, to stabilize its trajectory.

L'empennage 25 est avantageusement réalisé par estampage et thermoformage d'une plaque de matière plastique, élastiquement flexible, définissant ainsi :

  • une embase plate 26 de fixation, laquelle est orientée transversalement à l'axe 2, axée sur celui-ci et présente d'une part un trou central 27 la traversant longitudinalement de part en part et délimité par une face périphérique intérieure 28 cylindrique de révolution autour de l'axe 2 avec un diamètre sensiblement identique à celui de la face périphérique intérieure 21 de l'embout 24, et d'autre part une périphérie extérieure 29, en forme de polygone régulier, et plus précisément à quatre côtés dans l'exemple illustré, avec un diamètre de cercle exinscrit inférieur à celui de la face périphérique extérieure 8 de la paroi 6, en référence à l'axe 2 ; le trou central 27 et la face périphérique intérieure 21 de l'embout 24, convenablement taraudée, reçoivent coaxialement, par l'arrière, un boulon 30 de serrage de l'embase 26, à plat, contre l'épaulement 23 de l'embout 24 afin d'assurer la solidarisation de l'empennage 25 avec le corps 5 ;
  • autant d'ailettes élastiquement flexibles 31 que de côtés du polygone définis par la périphérie 29 de l'embase 26, à savoir quatre ailettes 31 dans l'exemple illustré, chacune de ces ailettes présentant une extrémité avant 82 solidaire de l'embase 26 le long d'un côté du polygone et une extrémité arrière libre 83 qui, par élasticité du matériau constituant l'empennage 25, tend à se décaler transversalement vers l'extérieur par rapport à l'extémité avant 82, c'est-à-dire à être plus éloignée de l'axe 2 que celle-ci, de telle sorte que l'empennage 25 présente une forme évasée vers l'arrière avec un diamètre supérieur à celui de la face périphérique extérieure 8 de la paroi 6 en référence à l'axe 2, toutefois avec possibilité de rabattement des ailettes 31 vers ce dernier, jusqu'à un diamètre correspondant à celui de la face périphérique extérieure 8 de la paroi 6, ce qui correspond à un état de l'empennage 25 lorsque le projectile 1 est engagé dans le tube d'arme 3 ; par élasticité, les ailettes 31 se déplacent automatiquement pour gagner leur position d'évasement de l'empennage 25 vers l'arrière dès que le projectile 1 a quitté le tube d'arme 3, après le tir.
The empennage 25 is advantageously produced by stamping and thermoforming a plastic plate, elastically flexible, thus defining:
  • a flat mounting base 26, which is oriented transverse to the axis 2, centered on the latter and has on the one hand a central hole 27 passing through it longitudinally right through and delimited by an inner peripheral face 28 cylindrical of revolution around the axis 2 with a diameter substantially identical to that of the inner peripheral face 21 of the endpiece 24, and on the other hand an outer periphery 29, in the shape of a regular polygon, and more precisely with four sides in the illustrated example, with an exinscribed circle diameter smaller than that of the outer peripheral face 8 of the wall 6, with reference to the axis 2; the central hole 27 and the inner peripheral face 21 of the end piece 24, suitably tapped, receive coaxially, from the rear, a bolt 30 for tightening the base 26, flat, against the shoulder 23 of the end piece 24 in order to secure the empennage 25 with the body 5;
  • as many elastically flexible fins 31 as there are sides of the polygon defined by the periphery 29 of the base 26, namely four fins 31 in the example illustrated, each of these fins having a front end 82 secured to the base 26 the along one side of the polygon and a free rear end 83 which, by elasticity of the material constituting the empennage 25, tends to shift transversely towards the outside with respect to the front end 82, that is to say to be further from the axis 2 than the latter, so that the tail 25 has a flared shape towards the rear with a diameter greater than that of the outer peripheral face 8 of the wall 6 with reference to the axis 2, however with the possibility of folding the fins 31 towards the latter, up to a diameter corresponding to that of the outer peripheral face 8 of the wall 6, which corresponds to a state of the tail 25 when the projectile 1 East engaged in the weapon tube 3; by elasticity, the fins 31 move automatically to gain their flaring position of the tail 25 towards the rear as soon as the projectile 1 has left the weapon tube 3, after firing.

Afin de provoquer un mouvement de nutation du projectile 1 autour de l'axe 2, pendant le vol entre le tube d'arme 3 et l'impact sur la cible, dans le but de stabiliser la trajectoire du projectile 1, les ailettes 31 présentent une forme en hélice. Par exemple, à cet effet, chaque ailette 31 comporte un premier pan plan 32 en forme de trapèze rectangle dont le côté perpendiculaire aux bases coïncide avec un côté de la périphérie 29 de l'embase 26 pour constituer l'extrémité avant 82 de l'ailette 31 et dont la grande base s'étend jusqu'à l'extrémité libre 83 de celle-ci, de telle sorte que ce premier pan 32 présente vers l'arrière le côté oblique du trapèze, définissant un pli rectiligne 33 dans l'ailette 31, et un deuxième pan plan 34 présentant la forme d'un triangle rectangle dont l'hypothénuse coïncide avec le pli 33, dont le grand côté de l'angle droit prolonge la petite base du trapèze rectangle défini par le premier pan 32, en formant un angle avec cette petite base de telle sorte que le pan 34 soit décalé vers l'extérieur par rapport au pan 32, et dont le petit côté de l'angle droit définit l'extrémité libre 83 de l'ailette 31.In order to cause a nutation movement of the projectile 1 around axis 2, during the flight between the weapon tube 3 and the impact on the target, in order to stabilize the trajectory of the projectile 1, the fins 31 have a helical shape. For example, for this purpose, each fin 31 has a first plane plane 32 in the shape of a rectangular trapezium, the side perpendicular to the bases coincides with one side of the periphery 29 of the base 26 to constitute the front end 82 of the fin 31 and the large base extends to the free end 83 thereof, so that this first panel 32 presents the oblique side of the trapezoid towards the rear, defining a rectilinear fold 33 in the fin 31, and a second plane plane 34 having the shape of a right triangle including the hypotenuse coincides with fold 33, whose long side of the right angle extends the small base of the rectangular trapezoid defined by the first panel 32, forming an angle with this small base so that the pan 34 is offset towards the outside relative to the pan 32, and the short side of the right angle defines the free end 83 of the fin 31.

Le choix du matériau constitutif de l'empennage 25 et la conformation des pales 31 sont avantageusement effectués, dans le domaine des aptitudes normales d'un Homme du métier, de telle sorte que le vol du projectile 1 s'accompagne d'un sifflement.The choice of the constituent material of the empennage 25 and the conformation of the blades 31 are advantageously carried out, in the area of normal skill of a person skilled in the art, so that the flight of projectile 1 is accompanied by a whistling sound.

Le nez 11 comporte quant à lui une paroi plate, transversale 35 rigide, par exemple métallique, délimitée, dans le sens d'un éloignement par rapport à l'axe 2, par une face périphérique extérieure 36 présentant un diamètre sensiblement égal à celui de la face périphérique intérieure 7 de la paroi 6 à l'intérieur de laquelle la paroi 35 est ainsi emboítée, avec contact mutuel intime entre les faces 36 et 7, à proximité immédiate de la face avant 9 de la paroi 6.The nose 11 has a flat transverse wall 35 rigid, for example metallic, delimited, in the direction of a distance relative to axis 2, by an outer peripheral face 36 having a diameter substantially equal to that of the inner peripheral face 7 of the wall 6 inside which the wall 35 is thus fitted, with intimate mutual contact between faces 36 and 7, in the immediate vicinity of the front face 9 of wall 6.

Vers l'avant, la face périphérique extérieure 36 se raccorde à un épaulement annulaire, plan 37, de révolution autour de l'axe 2, cet épaulement 37 étant tourné vers l'arrière et prenant appui à plat sur la face avant 9 de la paroi 6 pour limiter l'enfoncement de la paroi 35 à l'intérieur de celle-ci. Dans le sens d'un éloignement par rapport à l'axe 2, cet épaulement 37 se raccorde lui-même à une face périphérique extérieure 38, cylindrique de révolution autour de l'axe 2 avec un diamètre identique à celui de la face périphérique extérieure 8 de la paroi 6, que cette face 38 prolonge vers l'avant, sans discontinuité apparente. Cette face périphérique extérieure 38 délimite, dans le sens d'un éloignement par rapport à l'axe 2, un rebord 39, annulaire de révolution autour de cet axe, que la paroi 35 présente en saillie vers l'avant, d'une seule pièce. Vers l'axe 2, ce rebord 39 est délimité par une face périphérique intérieure 40 également cylindrique de révolution autour de l'axe 2 alors qu'il est délimité vers l'avant par une face annulaire plane 41, de révolution autour de l'axe 2, qui se raccorde à la face périphérique extérieure 38 par une arête adoucie non référencée et à la face périphérique intérieure 40 par une collerette 42, annulaire de révolution autour de l'axe 2 et placée en saillie vers ce dernier par rapport à la face périphérique intérieure 40, dans une zone extrême avant de celle-ci. Vers l'arrière, cette face périphérique intérieure 40 du rebord 39 se raccorde à une face avant 43 de la paroi 35, laquelle face avant 43 est plate transversale, et plus précisément présente la forme d'un disque perpendiculaire à l'axe 2 et centré sur celui-ci ; cette face 43 est par exemple coplanaire avec l'épaulement 37.Forward, the outer peripheral face 36 is connected to a annular shoulder, plane 37, of revolution about axis 2, this shoulder 37 being turned towards the rear and bearing flat on the front face 9 of wall 6 to limit the penetration of wall 35 to inside of it. In the direction of a distance from axis 2, this shoulder 37 connects itself to a peripheral face outer 38, cylindrical of revolution around axis 2 with a diameter identical to that of the outer peripheral face 8 of the wall 6, that this face 38 extends forward, without apparent discontinuity. This outer peripheral face 38 delimits, in the direction of a distance relative to axis 2, a rim 39, annular of revolution around this axis, which the wall 35 has projecting forward, in one piece. Towards axis 2, this rim 39 is delimited by an inner peripheral face 40 also cylindrical of revolution around axis 2 while it is delimited forwards by a flat annular face 41, of revolution around axis 2, which connects to the outer peripheral face 38 by a softened edge not referenced and to the inner peripheral face 40 by a collar 42, annular of revolution around the axis 2 and placed projecting towards the latter relative to the inner peripheral face 40, in an extreme area before it. Backwards, this face inner device 40 of the rim 39 is connected to a front face 43 of the wall 35, which front face 43 is transverse flat, and more precisely has the shape of a disc perpendicular to axis 2 and centered on it; this face 43 is for example coplanar with shoulder 37.

La face 43, la face 40 et la collerette 42 définissent ainsi, immédiatement en avant de la paroi 35, une cavité 44 de réception et d'immobilisation, par exemple par sertissage au moyen de la collerette 42 et collage, d'une ogive 45, de forme générale de révolution autour de l'axe 2, destinée à subir l'impact avec la cible et réalisée à cet effet dans un matériau présentant l'élasticité du caoutchouc, et par exemple en silicone d'une dureté shore A comprise entre 10 et 30, de préférence entre 12 et 15, cet exemple n'étant nullement limitatif. A cet effet, l'ogive 45 présente, en saillie vers l'avant par rapport à la face avant 41 du rebord 39, une forme hémisphérique autour d'un centre non référencé situé à l'intersection de l'axe 2 avec un plan géométrique défini par le rebord 41 et, en saillie vers l'arrière à l'intérieur de la cavité 44, un tenon cylindrique retenu en précontrainte de compression à l'intérieur de la collerette 42 afin d'assurer un effet de sertissage et collé à plat sur la face avant 43 de la paroi 35, ces exemples de fixation n'étant nullement limitatifs.The face 43, the face 40 and the flange 42 thus define, immediately in front of the wall 35, a receiving cavity 44 and immobilization, for example by crimping by means of the collar 42 and gluing, of a warhead 45, of general shape of revolution around the axis 2, intended to undergo impact with the target and produced for this purpose in a material with elasticity of rubber, for example silicone with shore A hardness between 10 and 30, preferably between 12 and 15, this example is in no way limiting. For this purpose, the warhead 45 has, in projecting forward with respect to the front face 41 of the rim 39, a form hemispherical around an unreferenced center located at the intersection of axis 2 with a geometric plane defined by the rim 41 and, projecting towards the rear inside the cavity 44, a cylindrical tenon retained in compression preload inside the collar 42 so ensure a crimping effect and glued flat to the front face 43 of the wall 35, these fixing examples being in no way limiting.

Vers l'arrière, la paroi 35 est délimitée par une face transversale, plane 46 parallèle à la face 43 et présentant quant à elle une forme annulaire de révolution autour de l'axe 2. Dans le sens d'un éloignement par rapport à celui-ci, cette face 46 se raccorde à la face 36, la distance séparant mutuellement les faces 43 et 46, définissant également la dimension longitudinale de la face 36 et par conséquent la profondeur d'enfoncement de la paroi 35 à l'intérieur de la paroi 6, étant faible par rapport à la dimension longitudinale de cette dernière entre ses faces avant et arrière 9 et 10 de telle sorte qu'entre la face 46 de la paroi 35 et l'épaulement 81 de la queue 12 subsiste une distance longitudinale libre constituant l'essentiel de la dimension longitudinale de la paroi 6.Towards the rear, the wall 35 is delimited by a transverse face, plane 46 parallel to face 43 and having a shape annular of revolution around the axis 2. In the direction of a distance relative to this, this face 46 is connected to face 36, the distance mutually separating the faces 43 and 46, also defining the longitudinal dimension of the face 36 and therefore the depth depression of the wall 35 inside the wall 6, being weak by relative to the longitudinal dimension of the latter between its faces front and rear 9 and 10 so that between the face 46 of the wall 35 and the shoulder 81 of the tail 12 remains a free longitudinal distance constituting most of the longitudinal dimension of the wall 6.

Sur cette distance longitudinale est monté, à coulissement longitudinal à l'intérieur de la paroi 6 avec guidage à cet effet par la face périphérique intérieure 7 de celle-ci, un conteneur étanche 47 pour un fluide sous pression, notamment un fluide incapacitant ou un fluide de marquage, destiné à être répandu par le projectile 1 après son impact contre une cible dans le sens 4.Sliding mounted on this longitudinal distance longitudinal inside the wall 6 with guide for this purpose by the face inner peripheral 7 thereof, a sealed container 47 for a pressurized fluid, especially an incapacitating fluid or a marking, intended to be spread by the projectile 1 after its impact against a target in direction 4.

Selon la conformation de ce conteneur 47, il peut coopérer avec la face périphérique intérieure 7 de la paroi 6, à l'effet d'un guidage à coulissement longitudinal relatif, par l'intermédiaire d'un coulisseau solidaire de ce conteneur 47 mais monté au coulissement longitudinal contre la face périphérique intérieure 7 de la paroi 6, de façon non illustrée mais aisément concevable par un Homme du métier, ou encore coopérer directement à cet effet avec la face périphérique intérieure 7 de la paroi 6, comme c'est le cas dans l'exemple illustré où le conteneur 47 présente la forme d'une bombe aérosol présentant une paroi latérale 48 tubulaire, de révolution autour de l'axe 2 et pour l'essentiel délimitée, dans le sens d'un éloignement par rapport à celui-ci, par une face périphérique extérieure 49 cylindrique de révolution autour de cet axe avec un diamètre sensiblement identique à celui de la face périphérique intérieure 7 de la paroi 6 de telle sorte que s'établisse entre les faces 49 et 7 un contact glissant de guidage au coulissement longitudinal relatif. Vers l'avant, cette paroi 48 se raccorde, avantageusement par réalisation en une seule pièce, à une paroi de fond 50 plate, perpendiculaire à l'axe 4 et notamment délimitée vers l'avant par une face frontale 51 plane, en forme de disque centré sur l'axe 2 et raccordée à la face 49 par une arête adoucie, dans le sens d'un éloignement par rapport à l'axe 2. Vers l'arrière, la paroi 48 se raccorde solidairement de façon étanche, par un sertissage, à un mécanisme de valve de remplissage 52 disposé suivant l'axe 2 et tourné vers l'arrière, le sertissage créant en arrière de la face périphérique extérieure 49 un épaulement 53 annulaire de révolution autour de l'axe 2, plan et tourné vers l'arrière. Plus près de cet épaulement 53 que de la face frontale 51, la paroi 48 est localement déformée vers l'axe 2 afin de présenter à l'intérieur du conteneur 47 une nervure limitant la pénétration du mécanisme de valve 52, comme il est bien connu d'un Homme du métier, et cette déformation crée, dans la face périphérique extérieure 49 de la paroi 48, une dépression en forme de gorge 54 annulaire, de révolution autour de l'axe 2, plus près de l'épaulement 53 que de la face frontale 51.According to the conformation of this container 47, it can cooperate with the inner peripheral face 7 of the wall 6, for the purpose of guiding relative longitudinal sliding, via a slide integral with this container 47 but mounted for longitudinal sliding against the inner peripheral face 7 of the wall 6, so illustrated but easily conceivable by a skilled person, or cooperate directly for this purpose with the inner peripheral face 7 of the wall 6, as is the case in the illustrated example where the container 47 has the shape of an aerosol can with a side wall 48 tubular, of revolution around axis 2 and essentially delimited, in the direction of a distance from it, by a face external device 49 cylindrical of revolution around this axis with a diameter substantially identical to that of the peripheral face inside 7 of the wall 6 so that is established between the faces 49 and 7 a sliding guide contact with relative longitudinal sliding. Towards the front, this wall 48 is connected, advantageously by making it a single piece, to a flat bottom wall 50, perpendicular to the axis 4 and in particular bounded towards the front by a flat front face 51, in disc shape centered on axis 2 and connected to face 49 by an edge softened, in the direction of a distance from axis 2. Towards the rear, the wall 48 is connected in a sealed manner, by a crimping, to a filling valve mechanism 52 arranged as follows axis 2 and turned to the rear, the crimp creating behind the face external device 49 a shoulder 53 annular of revolution around axis 2, plane and facing back. Closer to this shoulder 53 that of the front face 51, the wall 48 is locally deformed towards the axis 2 in order to present inside the container 47 a rib limiting the penetration of the valve mechanism 52, as is well known from a A person skilled in the art, and this deformation creates, in the peripheral face outside 49 of the wall 48, a groove-shaped depression 54 annular, of revolution around axis 2, closer to shoulder 53 than from the front face 51.

La dimension longitudinale séparant mutuellement l'épaulement 53 et la face frontale 51 est inférieure à la distance longitudinale séparant mutuellement l'épaulement 81 et la face arrière 46 de la paroi 35, si bien que le conteneur 47 peut notamment occuper à l'intérieur du corps 5 et du projectile 1 la position illustrée aux figures 1 et 2, dans laquelle il s'appuie vers l'arrière, par l'épaulement 53, sur l'épaulement 81 de la queue 12, le mécanisme de valve 52 étant librement reçu coaxialement à l'intérieur de cette dernière, et dans laquelle sa face frontale 51 est espacée longitudinalement de la face arrière 46 de la paroi 35, ce qui correspond à la position que le conteneur 47 occupe à l'intérieur du corps 5 du projectile 1 avant le tir de ce dernier, après son tir pendant son vol et jusqu'à l'impact.The longitudinal dimension mutually separating the shoulder 53 and the front face 51 is less than the longitudinal distance separating mutually the shoulder 81 and the rear face 46 of the wall 35, so that the container 47 can occupy in particular inside the body 5 and the projectile 1 the position illustrated in Figures 1 and 2, in which it rests backwards, by the shoulder 53, on the shoulder 81 of the tail 12, the valve mechanism 52 being freely received coaxially inside of the latter, and in which its front face 51 is spaced longitudinally of the rear face 46 of the wall 35, which corresponds to the position that the container 47 occupies inside the body 5 of the projectile 1 before the firing of the latter, after its shooting during its flight and until impact.

Afin que cet impact se traduise par une perforation du fond 50 du conteneur 47, c'est-à-dire par la libération du fluide qu'il contient, la paroi 35 présente en saillie vers l'arrière, suivant l'axe 2, sur sa face arrière 46 un percuteur 55 en forme d'aiguille longitudinale creuse, biseautée vers l'arrière, présentant perpendiculairement à la face 46 une dimension longitudinale correspondant sensiblement à la différence entre la dimension longitudinale séparant mutuellement l'épaulement 81 et la face 46 et la distance séparant mutuellement l'épaulement 53 et la face 51 de telle sorte que, dans la position illustrée aux figures 1 et 2, c'est-à-dire dans la position avant l'impact, le percuteur 35 soit placé en contact avec la face frontale 51 du conteneur 47 reposant par son épaulement 53 sur l'épaulement 81 de la queue 12, toutefois sans contrainte.So that this impact results in a perforation of the bottom 50 of the container 47, that is to say by the release of the fluid which it contains, the wall 35 projecting rearwards, along axis 2, on its face rear 46 a striker 55 in the form of a hollow longitudinal needle, bevelled towards the rear, presenting perpendicularly to the face 46 a longitudinal dimension corresponding substantially to the difference between the longitudinal dimension mutually separating the shoulder 81 and the face 46 and the distance mutually separating the shoulder 53 and the face 51 so that, in the position illustrated in FIGS. 1 and 2, that is to say in the position before impact, the striker 35 is placed in contact with the front face 51 of the container 47 resting by its shoulder 53 on the shoulder 81 of the tail 12, however without constraint.

Le percuteur 55, avantageusement réalisé en une seule pièce avec la paroi 35, est délimité dans le sens d'un éloignement par rapport à l'axe 2 par une face périphérique extérieure 56 cylindrique de révolution autour de cet axe avec un diamètre sensiblement inférieur à celui de la face périphérique intérieure 7 de la paroi 6. Cette face périphérique extérieure 56 se raccorde vers l'avant à la face arrière 46 de la paroi 35 et vers l'arrière à une face annulaire plane 57, inclinée par exemple de 45° par rapport à l'axe 2 et tournée vers le bas, qui définit pour le percuteur 55 une extrémité arrière libre, en biseau, et raccorde cette face périphérique extérieure 56 à une face périphérique intérieure 58, cylindrique de révolution autour de l'axe 2 et délimitant à l'intérieur du percuteur 55 un passage longitudinal 59 ouvert vers l'arrière à l'intérieur de la face en biseau 57 et se prolongeant vers l'avant jusqu'à l'intérieur de la paroi 35, dans laquelle il est fermé vers l'avant. Toutefois, à l'intérieur de la paroi 35, ce passage 59 débouche dans une pluralité de canaux 60, au nombre de huit dans l'exemple illustré, lesquels rayonnent à partir de lui, radialement en référence à l'axe 2, jusqu'à la face périphérique extérieure 36 de la paroi 35 dans laquelle ils débouchent. Chacun de ces canaux 60 est par exemple défini par une face périphérique intérieure 61, cylindrique de révolution autour d'un axe respectif 62 perpendiculaire à l'axe 2, les différents axes 62 étant régulièrement répartis angulairement autour de celui-ci et les diamètres respectifs des faces périphériques intérieures 61 étant mutuellement égaux mais inférieurs au diamètre de la face périphérique intérieure 58 du percuteur 55. En regard de chacun des canaux 60, coaxialement à celui-ci, la paroi 6 est percée de part en part d'un trou 63 délimité par une face périphérique intérieure 64 cylindrique de révolution autour de l'axe 62 respectif avec un diamètre identique à celui de la face périphérique intérieure 61 d'un canal 60, si bien que le passage 59, les canaux 60 et les trous 63 établissent une communication entre une cavité 65, par ailleurs fermée de façon étanche, que définissent les parois 6 et 35 ainsi que la queue 12, et dans laquelle est logé le conteneur 47, et l'extérieur du corps 5. Naturellement, d'autres modes d'aménagement, dans la paroi 35, des canaux 60 et d'autres nombres de ceux-ci pourraient être choisis sans que l'on sorte pour autant du cadre de la présente invention.The striker 55, advantageously made in one piece with the wall 35, is delimited in the direction of a distance from the axis 2 by an outer peripheral face 56 of cylindrical revolution around of this axis with a diameter substantially smaller than that of the face inner peripheral 7 of the wall 6. This outer peripheral face 56 is connected forwards to the rear face 46 of the wall 35 and towards the rear to a flat annular face 57, inclined for example by 45 ° by relative to axis 2 and facing down, which defines for striker 55 a free rear end, at a bevel, and connects this peripheral face outer 56 to an inner peripheral face 58, cylindrical of revolution around axis 2 and delimiting inside the striker 55 a longitudinal passage 59 open towards the rear inside the face in bevel 57 and extending forward to the inside of the wall 35, in which it is closed forward. However, inside the wall 35, this passage 59 opens into a plurality of channels 60, the number of eight in the illustrated example, which radiate from it, radially with reference to axis 2, up to the peripheral face outside 36 of the wall 35 into which they open. Each of these channels 60 is for example defined by an inner peripheral face 61, cylindrical of revolution about a respective axis 62 perpendicular to axis 2, the different axes 62 being regularly distributed angularly around it and the respective diameters of the peripheral faces interior 61 being mutually equal but less than the diameter of the inner peripheral face 58 of striker 55. Opposite each of the channels 60, coaxial to this, the wall 6 is drilled right through a hole 63 delimited by a cylindrical inner peripheral face 64 of revolution around the respective axis 62 with a diameter identical to that of the inner peripheral face 61 of a channel 60, so that the passage 59, channels 60 and holes 63 establish communication between a cavity 65, otherwise sealed, which define the walls 6 and 35 as well as the tail 12, and in which is housed the container 47, and the outside of the body 5. Naturally, other modes arrangement, in wall 35, of channels 60 and other numbers of these could be chosen without departing from the framework of the present invention.

Ainsi, lorsque le projectile 1, sorti du tube d'arme, heurte sa cible 66, dans le sens 4, comme le montre la figure 4, le conteneur 47 tendant à continuer à se déplacer par inertie, vers l'avant, à l'intérieur de la paroi 6 quant à elle immobilisée dans ce sens par la cible 66 vient s'appuyer avec un effort longitudinal conséquent, vers l'avant, sur le percuteur 55 qui perfore le fond 50, ce qui libère le conteneur 47 vis-à-vis d'un coulissement vers l'avant par rapport à la paroi 6, si bien que le conteneur 47 avance dans le corps 1 jusqu'à ce que son fond 50 vienne s'appliquer à plat, par sa face 51, contre la face arrière 46 de la paroi 35 comme on l'a illustré à la figure 4. Par la perforation 67 alors causée dans le fond 50, le fluide sous pression 68 initialement enfermé dans le conteneur 57 s'échappe de celui-ci en parcourant successivement le passage longitudinal 59 du percuteur 55, vers l'avant, puis chacun des canaux 60 et les trous 63, de façon centrifuge en référence à l'axe 2, jusqu'à sortir du corps 5 du projectile 1, de façon répartie transversalement autour de celui-ci, et à se répandre sur la cible 66.Thus, when projectile 1, taken out of the weapon barrel, strikes its target 66, in direction 4, as shown in FIG. 4, the container 47 tending to continue to move by inertia, forwards, inside the wall 6 meanwhile immobilized in this direction by target 66 comes to rest with a consequent longitudinal force, towards the front, on the striker 55 which perforates the bottom 50, which frees the container 47 from a sliding forward with respect to wall 6, so that the container 47 advances in body 1 until its bottom 50 comes apply flat, by its face 51, against the rear face 46 of the wall 35 as illustrated in Figure 4. By the perforation 67 then caused in the bottom 50, the pressurized fluid 68 initially enclosed in the container 57 escapes from it by successively traversing the longitudinal passage 59 of striker 55, towards the front, then each of channels 60 and the holes 63, centrifugally with reference to axis 2, until it leaves the body 5 of the projectile 1, in a distributed manner transversely around it, and spreading over target 66.

Ce processus, mettant en oeuvre exclusivement un coulissement du conteneur 47 vers l'avant à l'intérieur du corps 5, est illustré dans la moitié droite de la figure 4.This process, implementing exclusively a sliding of the container 47 forward inside the body 5, is illustrated in the right half of Figure 4.

La moitié gauche de celle-ci illustre une variante de réalisation du projectile, selon laquelle cet effet est complété ou remplacé par un effet d'écrasement longitudinal de la paroi 6 à l'impact. The left half of it illustrates an alternative embodiment of the projectile, according to which this effect is completed or replaced by an effect longitudinal crushing of the wall 6 on impact.

Pour faciliter un tel écrasement, on peut favoriser la compression longitudinale de la paroi 6 au moins dans une zone longitudinalement intermédiaire entre le conteneur 47 et la paroi transversale 35, par exemple comme on l'a illustré dans la moitié gauche de la figure 1, en creusant dans la face périphérique extérieure 8 de la paroi 6, de façon localisée immédiatement en arrière de la face arrière 46 de la paroi 35, des entailles longitudinales non traversantes 69 d'une dimension longitudinale correspondant de préférence approximativement au double de la distance longitudinale séparant mutuellement la face frontale 51 du conteneur 47 et la face arrière 46 de la paroi 35 lorsque, comme il est illustré dans la moitié droite de la figure 1, la face frontale 51 est en appui sans contrainte et sans perforation, vers l'avant, contre le percuteur 55. Lors de l'impact, et comme le montre la moitié gauche de la figure 4, les entailles 69 s'ouvrent et autorisent la formation, dans la paroi 6, de plis 70 en saillie, dans le sens d'un éloignement par rapport à l'axe 2, sur la face périphérique extérieure 8 de la paroi 6, cette formation se traduisant elle-même par un raccourcissement apparent de la paroi 6 entre l'épaulement 81 et la face arrière 46 de la paroi 35, obligeant ainsi le fond 50 du conteneur 47 à s'appuyer à force contre le percuteur 55 qui le perfore. La formation des plis 70 vers l'extérieur permet d'éviter que la présence du conteneur 47 à l'intérieur de la paroi 6 n'entrave le raccourcissement apparent de la paroi 6 et permet, en outre, d'éviter de constituer une entrave au coulissement longitudinal du conteneur 47 à l'intérieur de la paroi 6 lorsqu'on combine les deux effets de raccourcissement apparent de celle-ci et de coulissement du conteneur 47 vers l'avant à l'intérieur de celle-ci pour provoquer la perforation du fond 50 par le percuteur 55. Dans tous les cas, l'aménagement du passage 59 à travers le percuteur 55, des canaux 60 à l'intérieur de la paroi 35 et des trous 63 en regard de ces canaux 8 évite toute entrave à la sortie du fluide initialement contenu dans le conteneur 47.To facilitate such crushing, compression can be promoted longitudinal of the wall 6 at least in a longitudinally zone intermediate between the container 47 and the transverse wall 35, by example as illustrated in the left half of Figure 1, in digging into the outer peripheral face 8 of the wall 6, so located immediately behind the rear face 46 of the wall 35, non-traversing longitudinal cuts 69 of one dimension longitudinal preferably corresponding approximately to double of the longitudinal distance mutually separating the front face 51 of the container 47 and the rear face 46 of the wall 35 when, as it is illustrated in the right half of FIG. 1, the front face 51 is in abutment without constraint and without perforation, forward, against the striker 55. Upon impact, and as shown in the left half of Figure 4, the notches 69 open and allow the formation, in the wall 6, of folds 70 projecting, in the direction of a distance from axis 2, on the face external device 8 of the wall 6, this formation translating itself by an apparent shortening of the wall 6 between the shoulder 81 and the rear face 46 of the wall 35, thus forcing the bottom 50 of the container 47 to press forcibly against the striker 55 which pierces it. The formation of the folds 70 outwards makes it possible to prevent the presence of the container 47 inside the wall 6 does not prevent shortening apparent from the wall 6 and also makes it possible to avoid constituting a obstructs the longitudinal sliding of the container 47 inside the wall 6 when the two apparent shortening effects of this and sliding the container 47 forward inside the latter to cause perforation of the bottom 50 by the striker 55. In all cases, the arrangement of the passage 59 through the striker 55, channels 60 inside the wall 35 and holes 63 opposite these channels 8 prevents any obstacle to the exit of the fluid initially contained in container 47.

En raison de la forte ductilité que présentent généralement les matériaux, tels que de l'aluminium ou des alliages à base d'aluminium, constituant les parois des bombes aérosols que l'on utilise de préférence pour constituer le conteneur 47, il peut cependant se produire une déchirure imparfaite du fond 50 du conteneur 47 autour de la perforation 60, en ce sens que cette déchirure dégage dans ce fond 50 une languette qui reste rattachée au reste du fond et se plaque sur la face annulaire 57 à l'intérieur de laquelle le passage 59 débouche longitudinalement vers l'arrière, ce qui a pour effet d'obturer le passage 59 et d'empêcher par conséquent l'acheminement du fluide vers les canaux 60 et les trous 63.Due to the high ductility generally exhibited by materials, such as aluminum or aluminum-based alloys, constituting the walls of aerosol cans which are preferably used to constitute the container 47, however, there may be a imperfect tear in the bottom 50 of the container 47 around the perforation 60, in the sense that this tear releases in this bottom 50 a tongue which remains attached to the rest of the bottom and is plate on the annular face 57 to the interior of which the passage 59 opens longitudinally towards the rear, which has the effect of closing the passage 59 and preventing by Consequently the routing of the fluid towards the channels 60 and the holes 63.

On peut cependant pallier ou éliminer ce risque en conformant différemment le percuteur 55, par exemple selon une variante illustrée aux figures 9, 11, 13 ou selon une variante illustrée aux figures 10, 12, 14, respectivement, étant entendu que les autres composants du projectile peuvent rester conformes à l'un ou l'autre des modes de réalisation par ailleurs décrits. On retrouve par conséquent aux figures 9 à 14, sous les mêmes références numériques qu'aux figures 1 à 8, différents composants décrits en relation avec ces figures, à l'identique à l'exception de différences localisées qui vont être décrites à présent.However, this risk can be mitigated or eliminated by conforming differently the striker 55, for example according to an illustrated variant in FIGS. 9, 11, 13 or according to a variant illustrated in FIGS. 10, 12, 14, respectively, it being understood that the other components of the projectile may remain in accordance with one or other of the embodiments by elsewhere described. We therefore find in Figures 9 to 14, under the same reference numbers as in Figures 1 to 8, different components described in relation to these figures, identically except for localized differences which will now be described.

On se référera en premier lieu aux figures 9, 11, 13 où l'on a illustré une variante du percuteur 55 qui ne diffère du mode de réalisation de celui-ci précédemment décrit que par le fait qu'il est percé transversalement de part en part, de l'une à l'autre de ses faces périphériques intérieure 58 et extérieure 56, d'au moins un orifice débouchant ainsi d'une part dans le passage 59 et d'autre part à l'intérieur du corps 5, en arrière de la paroi 35 et plus précisément à une distance longitudinale de la face arrière 46 de celle-ci au moins égale et de préférence supérieure à l'épaisseur du fond 50.We will first refer to Figures 9, 11, 13 where we have illustrated a variant of striker 55 which does not differ from the embodiment of this one previously described only by the fact that it is pierced transversely right through, from one to the other of its faces interior 58 and exterior 56 peripherals, of at least one orifice thus opening on the one hand into passage 59 and on the other hand inside of the body 5, behind the wall 35 and more precisely at a distance longitudinal of the rear face 46 thereof at least equal and of preferably greater than the thickness of the bottom 50.

Dans l'exemple non limitatif illustré, on a prévu trois de ces orifices 85, 86, 87, dont chacun est orienté suivant un axe respectif perpendiculaire à l'axe 2 et présente une périphérie cylindrique de révolution autour de cet axe respectif, avec un diamètre respectif aussi grand que possible dans des limites compatibles avec un impératif de résistance mécanique du percuteur 55 de façon à offrir au fluide une section cumulée de passage aussi proche que possible de celle du passage 59.In the nonlimiting example illustrated, three of these orifices have been provided. 85, 86, 87, each of which is oriented along a respective axis perpendicular to axis 2 and has a cylindrical periphery of revolution around this respective axis, with a respective diameter also as large as possible within limits compatible with an imperative of mechanical resistance of striker 55 so as to provide the fluid with a cumulative section of passage as close as possible to that of passage 59.

Plus précisément, dans l'exemple illustré et si l'on se réfère aux figures 9 et 13 sur lesquelles la face annulaire 57 est orientée perpendiculairement au plan de coupe, l'orifice 85 est aménagé suivant un axe 88 situé dans ce plan et coupe perpendiculairement l'axe 2 à l'intersection de celui-ci avec le plan géométrique, non référencé, de la face 57 ; les orifices 86 et 87 présentent quant à eux un même axe 89 perpendiculaire au plan des figures 9 et 13 et coupant perpendiculairement l'axe 2 entre l'intersection de l'axe 88 avec celui-ci et la face arrière 46 de la paroi 35, et ils présentent un même diamètre qui est inférieur à celui de l'orifice.More specifically, in the example illustrated and if we refer to Figures 9 and 13 on which the annular face 57 is oriented perpendicular to the cutting plane, the orifice 85 is arranged according to an axis 88 located in this plane and perpendicularly cuts axis 2 to the intersection of this one with the geometrical plane, not referenced, of the face 57; the orifices 86 and 87 have the same axis 89 perpendicular to the plane of Figures 9 and 13 and cutting perpendicular to axis 2 between the intersection of axis 88 with it and the rear face 46 of the wall 35, and they have the same diameter which is less than that of the orifice.

Ainsi, même si la percussion du fond 50, lors de l'impact du projectile 1 sur sa cible, dégage de ce fond 50 une languette 84 qui vient se plaquer sur la face 57 et obture ainsi le passage 59 vers l'arrière, comme le montre la figure 13, celui-ci communique avec l'intérieur du conteneur 47 par les orifices 85, 86, 87 qui sont placés en arrière du fond 50 et, ainsi, permettent au fluide du conteneur 47 de s'échapper de celui-ci, vers l'extérieur du projectile 1, par le passage 50, les canaux 60 et les trous 63.Thus, even if the percussion of the bottom 50, during the impact of the projectile 1 on its target, releases from this bottom 50 a tongue 84 which comes press on face 57 and thus close passage 59 backwards, like the shows figure 13, this communicates with the interior of the container 47 by the orifices 85, 86, 87 which are placed behind the bottom 50 and, thus, allow the fluid of the container 47 to escape from it, towards outside the projectile 1, through the passage 50, the channels 60 and the holes 63.

Naturellement, on ne sortirait pas du cadre de l'invention en choisissant d'autres dispositions à l'effet de préserver une communication entre l'intérieur du conteneur 47, après perforation de celui-ci, et le passage 59 même si une languette 84 de matière du fond 50 vient obturer celui-ci vers l'arrière.Naturally, it would not go beyond the scope of the invention to choosing other arrangements to preserve communication between the interior of the container 47, after perforation thereof, and the passage 59 even if a tongue 84 of bottom material 50 closes this one backwards.

On ne sortirait pas non plus du cadre de la présente invention en conformant le percuteur 55 de telle sorte qu'il évite la formation d'une telle languette 84 ou, du moins, l'obturation de passage 59 par celle-ci et une variante de réalisation du percuteur 55, à cet effet, va être décrite à présent en référence aux figures 10, 12, 14. Un Homme du métier comprendra aisément que, bien que cette autre variante soit décrite indépendamment de la variante illustrée aux figures 9, 11, 13, les deux variantes pourraient aisément se combiner.It would not go beyond the scope of the present invention in shaping the striker 55 so that it prevents the formation of a such tab 84 or, at least, the passage closure 59 by the latter and an alternative embodiment of the striker 55, for this purpose, will be described in present with reference to Figures 10, 12, 14. A skilled person will easily understand that, although this other variant is described regardless of the variant illustrated in Figures 9, 11, 13, both variants could easily be combined.

Dans la variante illustrée aux figures 10, 12, 14, le percuteur 55 ne diffère de celui qui a été décrit en référence aux figures 1 à 8 que par le fait qu'il est creusé, à son extrémité arrière libre, d'un gradin 90 qui forme un décrochement vers l'avant par rapport à sa face annulaire 57, dans la zone de celle-ci la plus proche de la paroi 35, et débouche longitudinalement vers l'arrière dans cette zone et transversalement dans les faces périphériques intérieure 58 et extérieure 56.In the variant illustrated in FIGS. 10, 12, 14, the striker 55 does not differs from that which has been described with reference to FIGS. 1 to 8 than by the it is hollowed out, at its free rear end, with a step 90 which forms a step forward with respect to its annular face 57, in the area thereof closest to the wall 35, and opens out longitudinally backwards in this area and transversely in the inner 58 and outer 56 peripheral faces.

Plus précisément, dans l'exemple illustré, la face annulaire 57 présente une interruption 91 localisée dans sa zone la plus proche de la paroi 35, de façon symétrique par rapport à un plan perpendiculaire à la face annulaire 57 et incluant l'axe 2, à savoir le plan de la figure 11, et le gradin 90 est délimité par deux faces longitudinales planes 92, 93, mutuellement symétriques par rapport à ce plan et se raccordant vers l'arrière à la face annulaire 57, respectivement de part et d'autre de l'interruption 91 de celle-ci, et par une face transversale plane 94, tournée vers l'arrière et raccordant mutuellement ces deux faces longitudinales 92, 93 en avant de la face annulaire 57. Cependant, la face transversale 94 est de préférence placée à une distance longitudinale de la face 46 de la cloison 35, en arrière de celle-ci, supérieure à l'épaisseur de la paroi de fond 50 du conteneur 47.More specifically, in the example illustrated, the annular face 57 has an interruption 91 located in its area closest to the wall 35, symmetrically with respect to a plane perpendicular to the annular face 57 and including axis 2, namely the plane of FIG. 11, and the step 90 is delimited by two flat longitudinal faces 92, 93, mutually symmetrical with respect to this plane and connecting towards the rear to the annular face 57, respectively on either side of the interruption 91 of the latter, and by a flat transverse face 94, facing backwards and mutually connecting these two faces longitudinal 92, 93 in front of the annular face 57. However, the face transverse 94 is preferably placed at a longitudinal distance from the face 46 of the partition 35, behind the latter, greater than the thickness of the bottom wall 50 of the container 47.

Les deux faces longitudinales 92, 93 sont par exemple situées dans un même plan non référencé parallèle à l'axe 2 et perpendiculaire au plan de la figure 11. De préférence, comme il est illustré, le plan des faces 92, 93 est situé du même côté de l'axe 2 que la zone de la face annulaire 57 la plus proche de la paroi 35, de telle sorte que l'interruption 91 de la face annulaire 57, et avec elle le gradin 90, s'étendent sur moins de la moitié de la périphérie de cette face annulaire 57, et par exemple sur 120° en référence à l'axe 2, cette valeur n'étant indiquée qu'à titre d'exemple non limitatif.The two longitudinal faces 92, 93 are for example located in the same plane not referenced parallel to axis 2 and perpendicular to plane of Figure 11. Preferably, as illustrated, the plane of the faces 92, 93 is located on the same side of axis 2 as the zone of the annular face 57 closest to the wall 35, so that the break 91 of the face annular 57, and with it the step 90, extend over less than half of the periphery of this annular face 57, and for example over 120 ° in reference to axis 2, this value being indicated only as an example not limiting.

Un Homme du métier comprendra aisément que d'autres conformations du gradin 90 puissent être adoptées sans que l'on sorte du cadre de la présente invention.A skilled person will easily understand that others conformations of step 90 can be adopted without leaving the part of the present invention.

Lorsque, lors de l'impact du projectile sur sa cible, le fond 50 du conteneur 47 avance vers la paroi 35, il vient d'abord au contact du percuteur 55 par la zone de la face en biseau 57 la plus éloignée de cette paroi 35, ce qui provoque sa perforation et peut provoquer le dégagement progressif d'une languette 84, au fur et à mesure que le fond 50 vient au contact de zones de la face 57 respectivement de plus en plus proches de la paroi 35 ; cette languette 84 tend à rester appliquée contre la face 57, dans une orientation oblique par rapport à l'axe 2. Lorsque le fond 50 parvient au niveau de l'interruption 91 de la face 57, il franchit le gradin 90 dont les faces longitudinales 92, 93 puis la face transversale 94 redressent la languette 84 pour tendre à l'orienter parallèlement à l'axe 2 avant que le fond 50 ne vienne buter vers l'avant contre la face 46 de la paroi 35, comme on l'a illustré à la figure 14 ; ainsi, lorsque le conteneur 47 vient s'arrêter contre la face 46 de la paroi 35, la languette 84 éventuellement formée dans son fond 50 est orientée de telle sorte qu'elle ne risque pas d'obturer l'embouchure du passage 59 du percuteur 55 dans la face annulaire 57, c'est-à-dire qu'elle ne constitue aucune entrave à la sortie, vers le passage 59, les canaux 60 et les trous 63, du fluide initialement contenu dans le conteneur 47. When, during the impact of the projectile on its target, the bottom 50 of the container 47 advances towards the wall 35, it first comes into contact with the striker 55 by the area of the bevel face 57 farthest from this wall 35, which causes it to perforate and can cause release progressive of a tongue 84, as the bottom 50 comes to contact of areas of face 57 respectively closer and closer to the wall 35; this tongue 84 tends to remain applied against the face 57, in an oblique orientation relative to the axis 2. When the bottom 50 reaches at the level of the interruption 91 of the face 57, it crosses the step 90 of which the longitudinal faces 92, 93 then the transverse face 94 straighten the tongue 84 to tend to orient it parallel to axis 2 before the bottom 50 does not come up against the front against the face 46 of the wall 35, as illustrated in Figure 14; so when container 47 comes stop against the face 46 of the wall 35, the tongue 84 possibly formed in its bottom 50 is oriented so that it does not risk to close the mouth of the passage 59 of the striker 55 in the face annular 57, that is to say that it does not constitute any obstacle to the exit, towards the passage 59, the channels 60 and the holes 63, of the fluid initially contained in container 47.

Afin d'éviter une perforation accidentelle de celui-ci avant l'impact sur une cible 66, et notamment lors du stockage du projectile, lors du chargement de l'arme non représentée et pendant les manutentions de celle-ci, on prévoit de préférence des moyens de verrouillage pour immobiliser le conteneur 47 par rapport au corps 5 tant que le projectile 1 est placé à l'intérieur du tube d'arme 3, et pour libérer automatiquement le conteneur 47 vis-à-vis d'un coulissement longitudinal par rapport au corps 3 lorsque le projectile 1 sort du tube d'arme 3. On a illustré un premier exemple de réalisation de ces moyens de verrouillage aux figures 1 à 4, et un deuxième exemple aux figures 5 à 7, étant entendu que ces exemples sont également compatibles avec les variantes de réalisation du percuteur illustrées aux figures 8 à 14.In order to avoid accidental perforation of it before the impact on a target 66, and in particular during storage of the projectile, during loading of the weapon not shown and during handling this is preferably provided with locking means for immobilize the container 47 relative to the body 5 as long as the projectile 1 is placed inside the weapon tube 3, and to automatically release the container 47 vis-à-vis a longitudinal sliding relative to the body 3 when the projectile 1 leaves the weapon barrel 3. A first embodiment of these locking means in the figures 1 to 4, and a second example in FIGS. 5 to 7, it being understood that these examples are also compatible with the variant embodiments of the striker illustrated in Figures 8 to 14.

On se référera en premier lieu aux figures 1 à 4, où l'on a illustré ces moyens de verrouillage sous la forme d'un bourrelet annulaire 71 transversal, annulaire de révolution autour de l'axe 2, aménagé en saillie sur la face périphérique extérieure 8 de la paroi 6 du corps 5 dans une zone placée transversalement en regard de la gorge 54 formant une dépression dans la face périphérique extérieure 49 de la paroi 48 du conteneur 47 lorsque ce dernier est en appui vers l'arrière, par l'épaulement 53, sur l'épaulement 81 de la queue 12 du corps 5.We will first refer to Figures 1 to 4, where we have illustrated these locking means in the form of an annular bead 71 transverse, annular of revolution around the axis 2, projecting on the outer peripheral face 8 of the wall 6 of the body 5 in a area placed transversely opposite the groove 54 forming a depression in the outer peripheral face 49 of the wall 48 of the container 47 when the latter is supported rearward, by the shoulder 53, on the shoulder 81 of the tail 12 of the body 5.

Le bourrelet 71 est continu, raccordé sans discontinuité à la paroi 6 et avantageusement réalisé en une seule pièce avec celle-ci. Lorsque, comme le montre la figure 3, le projectile 1 est engagé dans le tube d'arme 3, présentant une face périphérique intérieure 72 cylindrique de révolution autour d'un axe coïncidant alors avec l'axe 2 avec un diamètre sensiblement identique à celui de la face périphérique extérieure 8 de la paroi 6, afin de coopérer avec cette face périphérique extérieure 8 pour guider le corps 5 au coulissement longitudinal dans le tube d'arme 3 lors du tir, le bourrelet 71 prenant appui sur cette face périphérique intérieure 72 qui lui applique une compression vers l'axe 2 provoque une déformation au moins partiellement élastique, et le cas échéant légèrement plastique, de la paroi 6 dans le sens d'un rapprochement vis-à-vis de l'axe 2, ce qui donne naissance, sur la face périphérique intérieure 7 de la paroi 6, à un bourrelet 73 également annulaire de révolution autour de l'axe 2 et formant une saillie vers celui-ci par rapport à la face périphérique intérieure 7 de la paroi 6, c'est-à-dire pénétrant à l'intérieur de la gorge 54 de façon à immobiliser le conteneur 47 par rapport à la paroi 6, dans la position d'appui de l'épaulement 53 sur l'épaulement 21.The bead 71 is continuous, connected without discontinuity to the wall 6 and advantageously made in one piece with it. When, as shown in Figure 3, the projectile 1 is engaged in the weapon barrel 3, having a cylindrical inner peripheral face 72 of revolution around an axis then coinciding with axis 2 with a diameter substantially identical to that of the outer peripheral face 8 of the wall 6, in order to cooperate with this outer peripheral face 8 for guide the body 5 to longitudinal sliding in the weapon tube 3 during of the shot, the bead 71 bearing on this peripheral face interior 72 which applies compression to axis 2 causes it to at least partially elastic deformation, and where appropriate slightly plastic, from wall 6 in the direction of approximation opposite of axis 2, which gives birth, on the inner peripheral face 7 of the wall 6, to a bead 73 also annular of revolution around of axis 2 and forming a projection towards it relative to the face inner peripheral 7 of the wall 6, that is to say penetrating inside the groove 54 so as to immobilize the container 47 by relative to the wall 6, in the support position of the shoulder 53 on shoulder 21.

En outre, le bourrelet 71, s'appuyant en contrainte sur la face périphérique intérieure 72 du tube d'arme 3 du fait de l'élasticité du matériau constituant la paroi 6, assure une retenue du projectile 1 par friction entre cette face périphérique intérieure 72, d'une part, et une étanchéité entre le projectile 1 et cette face 72, d'autre part, de façon particulièrement avantageuse lorsque, comme c'est fréquemment le cas, le tir 1 s'effectue par accumulation de gaz sous pression entre lui et une culasse non représentée fermant le tube 3 vers l'arrière, que ce soit par introduction d'un gaz sous pression ou génération directe d'un tel gaz sous pression, par exemple par combustion d'une composition pyrotechnique adaptée.In addition, the bead 71, resting under stress on the face inner device 72 of the weapon tube 3 due to the elasticity of the material constituting the wall 6, ensures retention of the projectile 1 by friction between this inner peripheral face 72, on the one hand, and a sealing between the projectile 1 and this face 72, on the other hand, so particularly advantageous when, as is frequently the case, the shot 1 is carried out by accumulation of gas under pressure between it and a cylinder head not shown closing the tube 3 backwards, either by introduction of a gas under pressure or direct generation of such a gas under pressure, for example by combustion of a pyrotechnic composition adapted.

Une fois le projectile sorti du tube d'arme 3, comme le montrent les figures 1, 2, 4, l'élasticité de la paroi 6 ramène le bourrelet 71, libéré de la compression que lui appliquait la face périphérique intérieure 72, dans sa conformation d'origine, c'est-à-dire en saillie sur la face périphérique extérieure 8 de la paroi 6, ce qui fait disparaítre le bourrelet 73 en saillie sur sa face périphérique intérieure 7 et libère par conséquent le passage pour le coulissement du conteneur 47 vers l'avant à l'intérieur de la paroi 6.Once the projectile has left the weapon tube 3, as shown in the Figures 1, 2, 4, the elasticity of the wall 6 brings back the bead 71, released from the compression applied to it by the inner peripheral face 72, in its original conformation, i.e. protruding on the peripheral face exterior 8 of the wall 6, which causes the protruding bead 73 to disappear on its inner peripheral face 7 and consequently frees the passage for sliding the container 47 forwards inside the wall 6.

Si l'on se réfère à présent aux figures 5 à 8, le bourrelet 71 est supprimé, mais dans la paroi 6 sont dégagées, par des découpes appropriées, des languettes élastiquement flexibles 74, par exemple orientées longitudinalement et au nombre de huit, équiréparties angulairement autour de l'axe 2 bien que d'autres dispositions et d'autres nombres puissent être choisis sans que l'on sorte pour autant du cadre de la présente invention.Referring now to Figures 5 to 8, the bead 71 is removed, but in the wall 6 are cleared, by cutouts suitable, resiliently flexible tabs 74, for example longitudinally oriented and eight in number, equally divided angularly around axis 2 although other arrangements and other numbers can be chosen without leaving the framework of the present invention.

Chaque languette 74, ainsi venue de matière avec la paroi 6, comporte une extrémité 75, ici avant, raccordée solidairement au reste de cette paroi 6, et une extrémité libre 76, ici arrière, portant solidairement, par exemple par réalisation d'une seule pièce, une protubérance 77 en saillie dans le sens d'un éloignement par rapport à l'axe 2, sur la face périphérique extérieure 8 de la paroi 6 lorsque, comme le montrent les figures 5, 6, 8, le projectile 1 est sorti du tube d'arme 3. En effet, cette languette 74 tend élastiquement à conserver une conformation dans laquelle la partie des faces périphériques intérieure 7 et extérieure 8 qui lui correspond reste disposée suivant le même cylindre géométrique respectif que le reste de la paroi périphérique respectivement intérieure ou extérieure de la paroi 6.Each tongue 74, thus integrally formed with the wall 6, has one end 75, here before, connected integrally to the rest of this wall 6, and a free end 76, here rear, bearing integrally, for example by making a single piece, a protrusion 77 in protruding in the direction of a distance from axis 2, on the face outer device 8 of the wall 6 when, as shown by Figures 5, 6, 8, the projectile 1 came out of the weapon barrel 3. Indeed, this tongue 74 tends elastically to maintain a conformation in which part of the inner 7 and outer 8 peripheral faces which corresponds to it remains arranged according to the same geometric cylinder respective that the rest of the respectively inner peripheral wall or outside of the wall 6.

Lorsque, par contre, le projectile 1 est logé à l'intérieur du tube d'arme 3, comme le montre la figure 7, la face périphérique intérieure 72 de celui-ci prenant appui sur la protubérance respective 77 fait disparaítre la saillie que celle-ci forme par rapport à la face périphérique extérieure 8 de la paroi 6, c'est-à-dire provoque une flexion de chaque languette 74 vers l'axe 2 au niveau de la protubérance 77, si bien que l'extrémité libre 76 de chaque languette 74 vient former une saillie vers l'axe 2 sur la face périphérique intérieure 7 de la paroi 6. Compte tenu d'un positionnement des protubérances 77 identique à celui du bourrelet 71, c'est-à-dire en coïncidence avec la gorge 54 de la paroi 48 du conteneur 47 en appui par un épaulement 53 sur l'épaulement 81 de la queue 12 du corps 5 du projectile 1, les extrémités libres 76 des différentes languettes 74 pénètrent alors dans la gorge 54 et constituent une butée s'opposant à un mouvement du conteneur 47 vers l'avant à l'intérieur du corps 5.When, on the other hand, the projectile 1 is housed inside the tube weapon 3, as shown in Figure 7, the inner peripheral face 72 of it based on the respective protuberance 77 made disappear the projection that it forms relative to the peripheral face outside 8 of the wall 6, that is to say causes a bending of each tongue 74 towards axis 2 at the level of the protrusion 77, so that the free end 76 of each tongue 74 forms a projection towards axis 2 on the inner peripheral face 7 of the wall 6. Given of a positioning of the protrusions 77 identical to that of the bead 71, that is to say in coincidence with the groove 54 of the wall 48 of the container 47 supported by a shoulder 53 on the shoulder 81 of the tail 12 of body 5 of projectile 1, the free ends 76 of the different tabs 74 then penetrate into the groove 54 and constitute a stop opposing a movement of the container 47 forwards inside the body 5.

Une fois que le projectile 1 est sorti du tube d'arme 3, la contrainte exercée par la face 72 de celui-ci sur les protubérances 77 cesse et les languettes 74 reviennent par élasticité dans une position dans laquelle chaque protubérance 77 est placée en saillie sur la face périphérique extérieure 8, si bien que les extrémités libres 76 des languettes 74 s'escamotent vis-à-vis de la face périphérique intérieure 7 de la paroi 6 dans le sens d'un éloignement par rapport à l'axe 2, libérant ainsi le conteneur 47 vis-à-vis d'un coulissement vers l'avant à l'intérieur du corps 5.Once the projectile 1 is out of the weapon tube 3, the constraint exerted by the face 72 thereof on the protrusions 77 ceases and the tabs 74 spring back in a position in which each protrusion 77 is placed projecting from the peripheral face outer 8, so that the free ends 76 of the tabs 74 retract vis-à-vis the inner peripheral face 7 of the wall 6 in the direction of a distance from axis 2, thereby releasing the container 47 vis-à-vis a sliding forward inside the body 5.

Dans l'hypothèse où, au lieu d'être monté directement au coulissement à l'intérieur du corps 5, le conteneur 47 serait monté au coulissement à l'intérieur du corps 5 par l'intermédiaire d'un coulisseau, le bourrelet 71 ou les languettes 74 pourraient coopérer, d'une façon identique à celle qui a été décrite en référence à la gorge 54, avec une gorge similaire aménagée dans le coulisseau. Une telle solution n'a pas été représentée, et sa réalisation relève des aptitudes normales d'un Homme du métier.In the event that, instead of being mounted directly to the sliding inside the body 5, the container 47 would be mounted at sliding inside the body 5 by means of a slide, the bead 71 or the tabs 74 could cooperate, in a way identical to that which has been described with reference to groove 54, with a similar groove in the slide. Such a solution was not represented, and its realization falls within the normal aptitudes of a Man of career.

Naturellement, d'autres modes de verrouillage du conteneur 47, ou du coulisseau le portant solidairement, à l'intérieur du corps 5 pourraient être choisis sans que l'on sorte pour autant du cadre de la présente invention, notamment si l'on choisissait de provoquer le mouvement du conteneur 47 aboutissant à la perforation de son fond 50 par le percuteur 55 non pas par déplacement inertiel du conteneur 47 ou par raccourcissement apparent de la paroi 6, comme on l'a illustré, mais par d'autres moyens tels que des moyens pyrotechniques à retard initiés lors du tir du projectile. Dans un tel cas, par exemple, on pourrait assurer une retenue provisoire du conteneur 47 à l'encontre d'un coulissement à l'intérieur du corps 5 par des goupilles travaillant au cisaillement et se rompant lorsque la pression de gaz généré par les moyens pyrotechniques précités serait suffisante pour dépasser un seuil prédéterminé, ou encore lorsque la combinaison de cet effet et d'un effet inertiel exercé sur le conteneur 47 lors de l'impact devenait suffisante pour dépasser ce seuil prédéterminé de rupture des goupilles. La réalisation du projectile 1 selon cette variante, de même que selon d'autres variantes, relève des aptitudes normales d'un Homme du métier et ne sortirait pas du cadre de la présente invention.Naturally, other methods of locking the container 47, or of the slide carrying it integrally, inside the body 5 could be chosen without departing from the scope of this invention, especially if one chose to cause the movement of the container 47 leading to the perforation of its bottom 50 by the striker 55 not by inertial movement of the container 47 or by apparent shortening of the wall 6, as illustrated, but by other means such as delay pyrotechnic means initiated during of the projectile. In such a case, for example, one could ensure temporary containment of container 47 against sliding at inside the body 5 by pins working in shear and breaking when the gas pressure generated by the pyrotechnic means above would be sufficient to exceed a predetermined threshold, or when the combination of this effect and an inertial effect exerted on the container 47 on impact became sufficient to exceed this threshold predetermined breakage of the pins. The realization of projectile 1 according to this variant, as well as other variants, is a skill normal of a skilled person and would not depart from the framework of the present invention.

De même, bien que l'on ait décrit en référence aux figures 1 à 14 des modalités d'application de la présente invention au cas d'un projetile 1 destiné à être tiré dans un sens longitudinal déterminé 4 à partir d'un tube d'arme 3 et à libérer le fluide sous pression 68 du conteneur 47 lors d'un impact dans ce sens 4 sur une cible 66, il relève des aptitudes normales d'un Homme du métier d'adapter ces modalités au cas d'un projectile 1 destiné à être projeté par un autre moyen, notamment lancé à la main, et/ou à libérer le fluide sous pression du conteneur de façon commandée autrement que par l'impact sur une cible dans le sens longitudinal déterminé, notamment par percussion du conteneur 47 en conséquence d'un coulissement longitudinal de celui-ci à l'intérieur du corps 5 du projectile 1, vers le percuteur 55 et vers la cloison transversale 35 qui porte ce dernier, par action de moyens pyrotechniques ou mécano-pyrotechniques connus en eux-mêmes, notamment mis en service volontairement par un utilisateur préalablement au lancer du projectile 1.Similarly, although we have described with reference to Figures 1 to 14 of the modalities of application of the present invention in the case of a projectile 1 intended to be pulled in a specified longitudinal direction 4 from a tube weapon 3 and to release the pressurized fluid 68 from the container 47 during a impact in this direction 4 on a target 66, it comes under normal skills of a person skilled in the art of adapting these methods to the case of a projectile 1 intended to be projected by another means, in particular launched by hand, and / or releasing the pressurized fluid from the container in a controlled manner other than by impact on a target in the longitudinal direction determined, in particular by percussion of the container 47 accordingly a longitudinal sliding thereof inside the body 5 of the projectile 1, towards the striker 55 and towards the transverse partition 35 which carries the latter, by action of pyrotechnic or mechanical-pyrotechnic means known in themselves, in particular put into service voluntarily by a user before launching projectile 1.

Claims (17)

  1. A non-lethal projectile adapted to be projected, in particular fired, from a tube (3) in a given longitudinal direction (4), and to disperse a pressurized fluid (68) in a controlled manner, in particular by impact on a target (66) in said direction (4), the projectile (1) including to this end a longitudinal body (5) having a nose (11) at the front and a tail (12) at the rear, a container (47) for the pressurized fluid (68) adapted to be perforated and disposed in said body (5) between its nose (11) and its tail (12), a longitudinal striker (55) for perforating said container (47) juxtaposed longitudinally thereto and carried by a transverse wall (35) attached to the body (5), means (7, 49, 69) for enabling or causing longitudinal movement towards each other of the container (47) and the striker (55) and controlled perforation of the container by the striker, in particular by impact on the target (66) in said direction (4), and means (59, 60, 63) for dispersing the fluid (68) to enable the fluid (68) to exit the body (5) in a transversely-distributed manner on perforation of the container (47) by the striker (55),
       characterized in that the means (59, 60, 63) for dispersing the fluid (68) include a blind longitudinal passage (59) through the striker (55) open at the end towards the container (47) and closed inside said wall (35), and a plurality of transverse passages (60) in said wall (35) radiating from said passage (59) and opening to the exterior of the body (5) (holes 63).
  2. A projectile according to claim 1, characterized in that the striker (55) has longitudinally opposite said wall (35) a free end (59) in the form of a bevel onto which said blind passage (59) opens longitudinally.
  3. A projectile according to claim 1 or claim 2, characterized in that the striker (55) has longitudinally opposite said wall (35) a free end (face 57) that includes a step (29) set back longitudinally towards said wall (35) and onto which said blind passage (59) opens longitudinally.
  4. A projectile according to claim 2 in combination with claim 3, characterized in that the step (90) is formed in the area of the bevel (face 57) closest to said wall (35) in the longitudinal direction.
  5. A projectile according to claim 4, characterized in that the step (90) extends over at least half the periphery of the bevel (face 57).
  6. A projectile according to any one of claims 1 to 5, characterized in that the striker (55) has, longitudinally on the same side of said wall (35) as the container (47), at least one transverse orifice (85, 86, 87) that opens into said blind longitudinal passage (59).
  7. A projectile according to any one of claims 1 to 6, characterized in that the striker (55) is attached to said transverse wall (35) and the means (7, 49, 69) for enabling or causing longitudinal movement of the container (47) and the striker (55) towards each other and perforation of the container (47) by the striker include a longitudinally compressible area of the body (5) longitudinally between the container (47) and said transverse wall (55).
  8. A projectile according to any one of claims 1 to 7, characterized in that the striker (55) is attached to said transverse wall (35) and the means (7, 49, 69) for enabling or causing longitudinal movement of the container (47) and the striker (55) towards each other and perforation of the container (47) by the striker include mounting the container (47) to slide longitudinally relative to the body (5), the striker (55) and said wall (35) being disposed in front of the container (47).
  9. A projectile according to claim 8, characterized in that it includes locking means (71, 74 through 77) for immobilizing the container (47) relative to the body (5) when the projectile (1) is inside the tube (3) and to release the container (47) automatically to slide longitudinally relative to the body (5) when the projectile (1) exits the tube (3).
  10. A projectile according to claim 9, characterized in that the body (5) is in the form of an elastically deformable material wall (6) between the nose (11) and the tail (12) and has a smooth inside face (7) for guiding the container (47) when it slides longitudinally in the body (5) and a smooth outside face (8) for guiding the projectile (1) when it slides longitudinally in the tube (3), in that said outside face (8) has a localized protuberance (71, 77) adapted to be depressed and form a projection on said inside face (7) when the projectile (1) is engaged in the tube (3) and to project on the outside face (8) and eliminate the projection on the inside face (7) when the projectile (1) has left the tube (3), and in that the container (47) has a localized depression (groove 54) in it transversely facing said protuberance (71, 77) when the container (47) is juxtaposed to the striker (55).
  11. A projectile according to claim 10, characterized in that said localized depression (54) is in the form of a transverse annular groove (54).
  12. A projectile according to claim 11, characterized in that the protuberance (71, 77) is in the form of a transverse bead (71) connected without discontinuity to the wall (6) of the body (5).
  13. A projectile according to claim 10 or claim 11, characterized in that said wall (6) includes at least one elastically flexible tongue (74) having one end (75) attached to the wall and offset relative to said protuberance (77) and a free end (76) carrying said protuberance (77) which is attached to it.
  14. A projectile according to any one of claims 8 through 13, characterized in that means (7, 49, 69) for enabling or causing longitudinal movement towards each other of the container (47) and the striker (55) and perforation of the container (47) by the striker are controlled by means chosen from a group including inertial means, pyrotechnic means and mechanical-pyrotechnic means.
  15. A projectile according to any one of claims 1 through 14, characterized in that it includes stabilizing fins (3) attached to the tail (12) of the body (5) and adapted to occupy a retracted position in which they are retained and elastically stressed by the tube (3) when the projectile (1) is engaged therein and to be deployed by virtue of their elasticity when the projectile (1) has left the tube (3).
  16. A projectile according to claim 15, characterized in that the fins (31) are made from an elastically deformable material and have one end (82) attached to the body (5) and a free end (83) tending by virtue of its elasticity to spread transversely outwards relative to the end (81) attached to the body (5).
  17. A projectile according to claim 15 or claim 16, characterized in that the fins (31) are shaped to cause a whistling sound when the projectile (1) is in flight.
EP97930562A 1996-06-21 1997-06-20 Non-lethal projectile Expired - Lifetime EP0906556B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9607780 1996-06-21
FR9607780A FR2750206B1 (en) 1996-06-21 1996-06-21 NON-LETHAL PROJECTILE
PCT/FR1997/001109 WO1997049969A1 (en) 1996-06-21 1997-06-20 Non-lethal projectile

Publications (2)

Publication Number Publication Date
EP0906556A1 EP0906556A1 (en) 1999-04-07
EP0906556B1 true EP0906556B1 (en) 2000-09-06

Family

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Application Number Title Priority Date Filing Date
EP97930562A Expired - Lifetime EP0906556B1 (en) 1996-06-21 1997-06-20 Non-lethal projectile

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US (1) US6209461B1 (en)
EP (1) EP0906556B1 (en)
AU (1) AU3447197A (en)
CA (1) CA2259452C (en)
DE (1) DE69703042T2 (en)
ES (1) ES2150265T3 (en)
FR (1) FR2750206B1 (en)
WO (1) WO1997049969A1 (en)

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DE102010047966A1 (en) 2010-10-08 2012-04-12 Rheinmetall Waffe Munition Gmbh Non-lethal ammunition for neutralizing targets

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US6955125B1 (en) * 2002-02-26 2005-10-18 The United States Of America As Represented By The Secretary Of The Army Practice projectile with smoke signature
US6779459B2 (en) * 2002-07-02 2004-08-24 Hunter Pacific Limited Pyrotechnic projectile launcher
US6968982B1 (en) 2002-09-18 2005-11-29 Burns Caleb E S Multiple-mist dispenser
US7526998B2 (en) * 2003-02-10 2009-05-05 Pepperball Technologies, Inc. Stabilized non-lethal projectile systems
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US7261041B2 (en) * 2003-10-27 2007-08-28 Nathan Randall Brock Non-pyrotechnic explosion device
US7225741B2 (en) * 2004-01-22 2007-06-05 Pdt Tech, Llc Reduced energy training cartridge for self-loading firearms
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US20080017179A1 (en) * 2004-05-12 2008-01-24 Pepperball Technologies, Inc. Compressed Gas Cartridge Puncture Apparatus
US7571680B1 (en) * 2006-09-05 2009-08-11 Samuel Barran Tafoya Ordnance canister with collapsible fuel-storing structure that after descent and impact atomizes and forcefully disperses fuel
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CN115127404B (en) * 2022-07-19 2024-01-09 中国人民武装警察部队工程大学 Impact blasting type composite kinetic energy bullet with rear buried tail wing

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Cited By (2)

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Publication number Priority date Publication date Assignee Title
DE102010047966A1 (en) 2010-10-08 2012-04-12 Rheinmetall Waffe Munition Gmbh Non-lethal ammunition for neutralizing targets
WO2012045389A1 (en) 2010-10-08 2012-04-12 Rheinmetall Waffe Munition Gmbh Deployable ammunition for rendering engines harmless

Also Published As

Publication number Publication date
CA2259452C (en) 2004-10-19
FR2750206B1 (en) 1998-09-11
AU3447197A (en) 1998-01-14
US6209461B1 (en) 2001-04-03
EP0906556A1 (en) 1999-04-07
FR2750206A1 (en) 1997-12-26
CA2259452A1 (en) 1997-12-31
WO1997049969A1 (en) 1997-12-31
ES2150265T3 (en) 2000-11-16
DE69703042D1 (en) 2000-10-12
DE69703042T2 (en) 2001-07-19

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