EP2906900A1 - Firing practice method - Google Patents

Firing practice method

Info

Publication number
EP2906900A1
EP2906900A1 EP13773259.0A EP13773259A EP2906900A1 EP 2906900 A1 EP2906900 A1 EP 2906900A1 EP 13773259 A EP13773259 A EP 13773259A EP 2906900 A1 EP2906900 A1 EP 2906900A1
Authority
EP
European Patent Office
Prior art keywords
target
projectile
impact
chosen
materials
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP13773259.0A
Other languages
German (de)
French (fr)
Other versions
EP2906900B1 (en
Inventor
Jean-Michel Laporte
Jean-Marc Fouques
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.)
Laporte Holding SAS
Original Assignee
Laporte Holding SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Laporte Holding SAS filed Critical Laporte Holding SAS
Publication of EP2906900A1 publication Critical patent/EP2906900A1/en
Application granted granted Critical
Publication of EP2906900B1 publication Critical patent/EP2906900B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00Moving targets, i.e. moving when fired at
    • F41J9/16Clay-pigeon targets; Clay-disc targets
    • F41J9/165Clay-pigeon targets; Clay-disc targets with hit-marking or tracer means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J1/00Targets; Target stands; Target holders
    • F41J1/01Target discs characterised by their material, structure or surface, e.g. clay pigeon targets characterised by their material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J9/00Moving targets, i.e. moving when fired at
    • F41J9/16Clay-pigeon targets; Clay-disc targets
    • 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
    • F42B12/40Projectiles, 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 of target-marking, i.e. impact-indicating type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/12Projectiles or missiles

Definitions

  • the present invention relates in particular to a method and a system of exercise shooting. It also relates to a target and a device associating target and projectile for shooting.
  • a preferred application is the target launching industry and shooting industry, including the weapons and projectile industry.
  • the Bail Trap practice consists of a shot of a pigeon that the shooter tries to reach for the shots to dislocate. This dislocation provides a visual effect allowing the shooter and the eventual public to validate that the target has been hit. In some cases, the visual effect can be accentuated by the use of specific pigeons, containing a powdery material such as calcium carbonate. At the rupture of the target, the powdery material is dissipated into space surrounding the impact zone, producing a cloud, possibly colored according to the color of the powder material.
  • the document US-A1-20020125643 is part of such targets containing a marker material.
  • the invention solves all or part of the disadvantages of current techniques.
  • a method of firing practice comprising a step of launching a target in a portion of the space, a firing step of a projectile towards the target and a projectile impact step on the target.
  • this method is such that a projectile comprising a shell delimiting an interior volume containing a marker material and that it comprises a step of rupture of the shell during the impact of the projectile on the target, so that to release the marker material
  • This arrangement makes it possible to use reusable targets since the projectile is caused to break.
  • the visual effect is preserved because of the dynamic aspect of the operation of the invention: the movement of the target ensures, at the moment of impact, a distribution of the marker in space, and in particular over a large area of the target and / or around it. While current techniques focus on the destruction of the target, the invention adopts a reverse approach.
  • the launching step comprises a self-rotation of the target.
  • Another aspect of embodiments of the invention also relates to a system for firing practice, comprising a target and a projectile intended to impact the target, characterized in that the projectile comprises a shell delimiting an interior volume containing a target. marking material and thereby the impact of the projectile on the target is configured to cause the rupture of the hull, so as to release the marker material.
  • the system may also include a target launcher.
  • Another aspect of embodiments of the invention relates to a firing target.
  • the edge of the target has a lower density than the impact surface.
  • the targets of Bail Trap are of a single block of the same density, the invention stands out clearly, especially since it uses one or less dense materials at the level of the slice, area where we would place more naturally a high density material for reasons of mechanical strength.
  • the firing target comprises a peripheral surface comprising a slice joining a first face and a second face and an impact surface formed on at least one of the first face and the second face, capable of receiving the impact of a projectile, characterized in that the edge of the target and the impact surface are of different materials, the density of the material or materials of the wafer being less than the density of the material or materials of the impact surface.
  • Another aspect of embodiments of the invention is a device comprising a target and a projectile.
  • Figure 1 shows in perspective an example of a target used according to the present invention.
  • Figure 2 illustrates a possibility of mounting a portion of the target on the rest of the target.
  • Figure 3 shows an alternative to the embodiment of Figure 2 for mounting a portion of the target on the rest of the target.
  • FIG. 4 is a cross-sectional view along a diameter of the target according to the embodiment of FIG. 3.
  • Figure 6 shows in perspective another embodiment of the target and Figure 5 is a transverse view along a diameter of the target.
  • FIGS 7 to 9 show in perspective an embodiment of launcher can be part of the present invention, Figures 7 to 9 showing different phases of operation of said machine. DETAILED DESCRIPTION
  • the own rotation speed of the target 1 is at least 300 revolutions per minute at the time of the launch and / or at the moment of the impact;
  • a target (1) whose peripheral surface comprises a wafer (2) joining a first face (3) and a second face (4) and the impact step is performed by contacting the projectile on a surface of impact (8) formed on at least one of the first face (3) and the second face (4);
  • the slice (2) of the target (1) and the impact surface (8) are chosen from different materials;
  • the material or materials of the wafer (2) is chosen with a density lower than the density of the material or materials of the impact surface (8);
  • the density of the material or materials of the impact surface (8) is chosen to be greater than 500 kg / m 3 ;
  • the density of the material or materials of the wafer (2) is less than 275 kg / m 3 ;
  • a target (1) comprising a target body (12) of cylindrical shape whose surface of revolution forms the wafer (2) and the impact surface (8) comprises, on at least one of the first face (3) and the second face (4), a disk-shaped area;
  • the diameter of the disk-shaped area is smaller than the diameter of the target body (12);
  • a target (1) is used whose body (12) is made of polymeric foam and at least a portion of the impact surface (8) is made by cross-linking said foam;
  • the fixing is carried out with at least one fixing member (1 1) situated on one face of the coating (10) opposite to the face of the coating (10) forming at least partly the impact surface (8), and with at least one complementary fastening member (13) formed on the target body (12);
  • the target comprises two coatings each fixed on a different face and each associated with at least one fastener, the fasteners of the two coatings being configured to be secured in a space within the thickness of the target body.
  • the coating (10) is a plate of polymeric material; a target (1) is used comprising a belt of which a peripheral part forms the wafer (2) of the target (1) and surrounding a target core (15), and the outer wall of the target core (15) forms at least in part the impact surface (8).
  • the target core (15) has a portion for fixing a zone of the belt (14) opposite to the peripheral part;
  • the target core (15) comprises a central core (16) chosen with a thickness less than that of the fixing portion;
  • the Young's modulus of the material or materials of the wafer (2) is chosen to be smaller than that of the material or materials of the impact surface (8);
  • the Young's modulus of the material or materials of the slice is less than 0.1 giga
  • the coating is a sheet of elastomeric material
  • the Young's modulus of the material or materials of the impact surface (8) is chosen greater than 0.8 giga Pascal
  • the marker of the projectile is chosen from a liquid dye and a powder
  • the shell of the projectile is made in the form of a rigid shell made of polymeric material or in the form of a flexible shell, preferably of gelatin;
  • the shell is formed as a smooth spherical envelope.
  • the device comprises a target and a projectile comprising a shell delimiting an interior volume containing a marker material.
  • the target preferably has a peripheral surface having a slice joining a first face and a second face and an impact surface formed on at least one of the first face and the second face, adapted to receive the impact of a projectile, the edge of the target and the impact surface being of different materials, the density of the material or materials of the slice being less than the density of the material or materials of the impact surface.
  • the slice of the target is configured to absorb the energy of a projectile impact in a greater proportion than the impact surface.
  • the target and the projectile are configured so that the projectile absorbs more than 60% of the energy generated by an impact of the projectile on the impact surface.
  • One aspect of the invention is related to launching a target in a portion of the space.
  • a launching machine is provided and a non-limiting example of embodiment is given in FIGS. 7 to 9.
  • the machine 19 has a launching surface advantageously in the form of a plane 20 for receiving at least one target 1 in contact with one of the faces 3, 4 of the target 1.
  • the launching plane 20 can be horizontal or inclined, in particular to vary the projection effects of the target and the area of the space in which the target is projected.
  • the machine 19 may be provided with means for tilting it.
  • a target 1 is on the launch plane 20
  • its launch is achieved by means of an ejection device here in the form of an arm 21 rotatably mounted about an axis x2.
  • the arm 21 is configured to be applied on a portion of wafer 2 of the target 1 to give it a kinetic energy to send it.
  • the machine 19 further comprises a peripheral application surface 22 of the target 1 and adapted to cooperate with the slice 2 of the target 1.
  • the target 1 can be guided during its movement on the launch plan 20 until ejection.
  • the surface 22 may constitute an adhesion zone which allows in a preferred embodiment to effectively put the target 1 in clean rotation. We will see later the interest of this own rotation to produce an increased visual technical effect.
  • the shape of the application surface 22 is not limited but is preferably curvilinear with a comma profile.
  • the components previously described for the machine 19 are, in the case of Figures 7 to 9, mounted on a frame 23.
  • the frame 23 can be articulated so as to produce the aforementioned inclination means and in particular to have an articulation capacity in rotation along at least one axis.
  • the machine 19 advantageously comprises a plurality of targets stored in a charger 24.
  • the charger 24 is substantially equivalent to those used to launch targets of the "pigeon dart" type.
  • “clay” and comprises for this purpose at least one column 25 for the superposition of the targets 1 during storage and has a delivery zone 26 in the lower part of the or columns 25, so that, on command, a target 1 can be evacuated from the column 25 which stored it to be directed towards the launching plane 20.
  • This target path 1 can be operated by gravity and / or thrust system.
  • the target 1 used in the invention may have different shapes and configurations. However, in view of the above with reference to the launching machine 19, it is advantageous for the target 1 to have an outer periphery in the form of a slice 2 of substantially circular shape. In addition, it is advantageous for the target 1 to have an axial symmetry along the axis through which it is brought to be setting in own rotation. The symmetry can be otherwise central, so that the target 1 is completely balanced around its center.
  • the target 1 is preferably reusable and the impact of the projectile does not affect it fundamentally. This does not exclude that impact points persist after the shots, but these alterations are advantageously minor so that the target can operate multiple times.
  • the target 1 comprises a peripheral wall constituting its outer surface and advantageously having a wafer 2 and a first face 3 and a second face 4.
  • FIG. 1 shows an exemplary embodiment of this invention.
  • target typology 1 In the case illustrated, the first and second faces 3, 4 are substantially planar but this case is not limiting as will be seen later with reference to Figures 5 and 6 in particular.
  • the slice 2 is advantageously in the form of the outer surface of a cylinder of revolution.
  • the target 1 has essentially the shape of a relatively flattened cylinder portion, namely that the height is less than its diameter.
  • a target 1 of circular section having a diameter of between 25 and 33 centimeters and a height (dimension in thickness) between 25 and 50 millimeters.
  • the target 1 carries a body 12 preferably based on high or low density polymer foam.
  • a body 12 of target 1 giving a resistance to the target 1 without forming too much rigidity so as to limit the danger of the launch of the target 1.
  • the crushing capacity of the target 1 under the elastic deformation form at its edge 2 may make it possible to accentuate the effect of self-rotation by means of the launching machine 19.
  • the target body can be in one piece and in one material or have multiple materials.
  • the latter advantageously comprises an impact surface whose design is defined to ensure rupture.
  • the impact surface 8 is advantageously configured to limit the absorption of the energy of the impact so that this energy is sufficiently reflected towards the projectile to cause its rupture, that is to say to exceed its limit of resistance to rupture.
  • the impact surface 8 is in the case of Figures 1 and 2 made from at least one coating 10, each coating 10 can cooperate with one of the first and second faces 3, 4.
  • FIG. 1 shows that the coating 10 may have the shape of a disc that can be applied on a face 3, 4 in a centered manner and delimits an edge 9 on the face 3, 4 equipped so as to preserve a periphery which may be in a less dense material and / or less rigid.
  • FIG. 2 shows an example of a coating 10 in the form of a sheet of material that is sufficiently flexible to be easily positioned on the face 3.
  • the sheet is made of elastomer material which comprises both the elastomeric polymer materials. and natural materials especially rubber. Fixing the web can be done by any mechanical means or by gluing.
  • the outer surface of the sheet thus formed constitutes or participates in constituting the impact surface 8.
  • the material of the sheet is chosen to ensure good cooperation with the projectile.
  • the projectile is in the form of a ball or ball having a shell of flexible material and for example gelatin.
  • the use of an elastomeric coating provides increased frictional capability between the shell of the projectile and the impact surface 8 to facilitate rupture of the shell.
  • a coating 10 can be used so as to facilitate cleaning when the shell of flexible material contains a liquid dye product such as paint.
  • the surface of the impact surface 8 is advantageously smooth for this purpose. In this example, it suffices to rub the coating 10 with a cloth to easily remove the paint deposited by the projectile.
  • the coating 10 may be in the form of a rigid polymer material plate attached to one or other of the faces 3, 4.
  • the assembly is effected by fixing members cooperating with fastening members 1 1 on the internal face of the coating 10 and complementary members 13 in the target body 12 or another part of target.
  • the complementary members 13 advantageously comprise female housings formed in the target body 12 while the members 1 1 are male parts capable of being inserted into the housings.
  • At least one fastener 1 1 may be formed or more. In the illustrated case, at least four members are located at four cardinal points, so as to distribute the fixing force on the target 1.
  • the fasteners are inserted in the housing and can hang on the wall of the latter.
  • at least one fastening member January 1 can have a relief on its surface so as to increase the effect of hanging in the complementary fastening member 13.
  • This mounting example can be completed or replaced by any other form fixing and in particular by a collage.
  • FIG. 4 shows in section the result obtained in the embodiment of FIG. 3 with the passage of the fastening members 11 through the thickness of the target body 12.
  • This figure also shows that one can equip each face 3, 4 of the target 1 with a coating 10 so that the impact of the projectile can occur by both sides of the target 1.
  • each coating 10 carries fasteners, on the one hand in the form of male rods on the other hand in the form of rods having an inner conduit. It is arranged that the rods of the fasteners 1 1 of one of the coatings 10 can be inserted into the inner conduits of the fasteners of the other coating 10 on the opposite side.
  • coating 10 is made of polymeric material, it is advantageously a thermosetting polymer material.
  • the coating 10 may be in the following materials: polycarbonate, polyamide or ABS.
  • the thickness of the coating 10 may be in all cases between 0.5 and 3 millimeters and preferably 1 millimeter.
  • a coating 10 having an outer surface of dark color and preferentially black, this makes it possible to accentuate the visual effect by contrast. when the marker is released.
  • the embodiment shown in FIGS. 1 to 4 includes a border 9 around the covering 10.
  • the edge 9 can participate in the safety of the exercise of the shot by avoiding making the target too dangerous especially in the case where the coatings are rigid and have a density greater than the density of the target body 12.
  • the thickness of the rim may correspond to between 10 and 30% of the diameter of the faces 3, 4 targets.
  • FIG. 6 reveals that at least one of the faces 3, 4 may not be flat and have, particularly in the example shown, a central cavity surrounded at its periphery by an impact surface portion 8 located at a higher level.
  • This configuration can make it possible to limit the weight of the target 1, but also to promote breakage by proposing surface elements having different orientations so as to avoid too much tangential application of the projectile on the face 3.4 considered.
  • the coating 10 is of polymeric material, it is advantageously a thermosetting polymer material.
  • the coating 10 may be in the following materials: polycarbonate, polyamide or ABS.
  • FIGS. 5 and 6 comprises a belt 14 capable of constituting a peripheral member for the remainder of the target 1.
  • the belt 14 is in annular form, the outer surface of the ring constituting the slice 2 while the inner surface of the ring allows cooperation with the rest of the target 1.
  • the remainder of the target 1 may comprise, as in the case illustrated, a heart 15 having a portion of cooperation with the belt 14 and a central portion called "soul" 16.
  • the core 16 has a lower thickness That the rest of the heart 15.
  • the peripheral part of the heart 15 comprises an enlargement 17 framing the core 16 and can serve as a basis for the reception of two wings 18 located on either side of the enlargement and appearing at each level. one of the first and second faces 3, 4.
  • the wings 18 are preferably substantially parallel and cooperate with the sidewalls 2 of the belt 14 so that the two elements interlock to form a unitary assembly.
  • the heart 15 consists of a single piece but this case is not limiting.
  • the belt 14 is here monobloc but could be made of several parts assembled.
  • the core 15 can be realized in a material that is denser than the material of the belt 14 and / or a material having a Young's modulus higher than that of the belt 14. This provides an impact surface 8 that promotes the reflection of the energy of the body. impact on the projectile to produce its break while the rest of the target 1 and in particular the material located at its slice 2 is less dense and / or more elastically deformable (less rigid) to limit the risk of accident and promote the rotation by adhesion.
  • unit 2 it is possible to select for unit 2 one or more materials whose Young's modulus is less than or equal to 0.1 Gpa (gigaPascal).
  • one or more materials may be selected for the impact surface 8, the Young's modulus of which is greater than 0.8 Gpa.
  • the impact surface (8) is made of a polymer material and particularly of polyurethane.
  • This material is advantageously chosen to have a Shore hardness of more than 90 and more preferably of at least 99; it may be in the form of a plate of at least 1 mm, and preferably of 1 mm plus or minus 10%.
  • Another embodiment of the target 1 which is not shown in the figures, consists of a target 1 having a target body 12 substantially as in the case of Figures 1 and 2, to perform a crosslinking of a part of the surface of at least one of the first and second faces 3, 4, so as to harden this portion and form an impact surface 8 absorbing less impact energy than the rest of the body of target 12. It is nevertheless possible to preserve a border 9 around the impact surface 8 during the crosslinking phase by affixing a cover on the surface to be protected during this crosslinking.
  • the impact surface 8 is then formed directly in the target body 12, and advantageously in a polymer foam, but with a transformed material which has mechanical properties different from the rest of the target 1 and which in particular absorbs less the energy of the target.
  • the crosslinking is preferably done at a depth corresponding to the thickness of the target body.
  • the target 1 thus described ensures both the efficiency and safety of its launch and the effectiveness of cooperation with the projectile.
  • the impact surface 8 is advantageously configured in the previous examples to less absorb the energy of the impact than the slice portion 2 of the target 1, so that the energy returned to the projectile is sufficient to cause break the shell and release the marker.
  • the target 1 is brought to cooperate with a projectile not shown.
  • the projectile comprises a marker in the form of a powdery material which may for example be based on colored calcium carbonate or not.
  • the shell enclosing the marker is advantageously a rigid shell and preferably a shell of spherical shape.
  • the surface of the shell is advantageously smooth so as to promote the accuracy of the shot even if it can penalize the range of the shot.
  • the present invention is advantageously aimed at a firing exercise in which the projectile is launched via a weapon that can be part of the present invention, the distance between the weapon and the target being launched being included between ten and twenty meters and advantageously less than fifteen meters.
  • the rigid shell may for example be of polymeric material with a thickness of less than one millimeter and advantageously between 0.5 and 1 millimeter and have a diameter of between one and two centimeters and advantageously 1, 5 centimeters.
  • the shell is for example obtained by the following method: a powder mixture of polyethylene glycol and calcium carbonate is placed in a mold in the shape of the desired projectile; the mold is heated to cause a peripheral melting of the mixture; heating is stopped after a delay configured to allow the formation of an envelope layer of the desired thickness after cooling (the cooling may be forced, for example by quenching).
  • the shell is of flexible material and for example gelatin. It constitutes a coating delimiting the storage volume of the marker.
  • This solution is particularly suitable, although not limiting, to a marker of the liquid dye type.
  • the projectile has a more flexible conformation and is made to deform more easily during the impact on the target 1.
  • the flexible shell may be gelatin with a thickness of the same order as the thicknesses given for the case of rigid shells.
  • the projectile can be launched via a compressed gas weapon that can for example operate on the basis of C0 2 and using the C0 2 expansion to achieve the projection effort.
  • a compressed gas weapon that can for example operate on the basis of C0 2 and using the C0 2 expansion to achieve the projection effort. They may be pistols or rifles.
  • the practice of shooting practice is as follows:
  • the machine starts launching a target 1 in a portion of the space.
  • the throw can be configured to expose essentially one of the first or second face 3, 4 facing the shooter, but any other inclination is possible.
  • the shooter tries to reach it by means of the projectile. If it succeeds, thanks to the invention, a visual effect is immediately produced by means of the release of the marker. Indeed, during the impact, the projectile sees its hull break so as to release the marker material which spreads rapidly by the dynamics of the target 1.
  • the marker is released and spreads on the target 1 at the impact surface 8 and / or in a portion of the space.
  • a marker of the painting type it is essentially on the target 1 that the marking will be produced.
  • the marker tends to dissipate as a cloud in a three-dimensional portion of the space.
  • it is advantageous to rotate the target 1 about its axis so that during the impact, a tangential effect occurs promoting the distribution of the marker on a larger area.
  • the point of impact follows a pseudo-cycloid trajectory which makes it possible to produce this widening of the zone of the visual effect.
  • the invention can be used for a fire drill in which the shooter repeatedly tries to hit the target 1.
  • the target 1 is launched at a height sufficient to allow a repetitive shooting. Whenever the target is hit, the shooter scores a point.
  • the target 1 is not altered during the impacts and, advantageously, its trajectory is not substantially modified. Therefore, one can for example operate at least 5 shots on a target 1 launched.
  • a system comprising several preferably aligned launching machines is set up.
  • the machines can be coordinated with a sequencer capable of defining the order and the intervals (for example between 3 and 10 seconds) of firing of the machines.
  • a firing pattern is as follows: Each machine launches a target in a direction specific to it, the launches are chained in time to not start before the target of the previous throw is no longer accessible to the shooter. Throws allow up to 5 impact possibilities. The player has the ability to score up to 15 points. The number of fencers who can participate in a contest is in no way limited.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The subject of the present invention is a method for carrying out firing practice, comprising a step of launching a target (1) into a portion of space, a step of firing a projectile towards the target (1) and a step of impact of the projectile on the target (1), characterized in that use is made of a projectile comprising a shell delimiting an internal volume containing a marking material and in that it involves a step of rupturing the shell upon impact of the projectile with the target (1), thereby releasing the marking material.

Description

«Procédé d'exercice au tir»  "Shooting exercise method"
La présente invention est relative notamment à un procédé et un système d'exercice au tir. Elle se rapporte aussi à une cible et un dispositif associant cible et projectile pour le tir. The present invention relates in particular to a method and a system of exercise shooting. It also relates to a target and a device associating target and projectile for shooting.
Une application préférée concerne l'industrie des lanceurs de cibles et celle des techniques de tirs, incluant l'industrie des armes et des projectiles.  A preferred application is the target launching industry and shooting industry, including the weapons and projectile industry.
ARRIERE-PLAN TECHNOLOGIQUE BACKGROUND
La discipline typique d'exercice au tir est celle du Bail Trap.  The typical discipline of shooting exercise is the Bail Trap.
Dans ce dernier domaine, on connaît des appareils de lancement de cibles souvent dénommées pigeons d'argile. Le tireur est équipé d'un fusil associé à des cartouches renfermant des plombs de calibre adapté au tir souhaité. Tant à l'entraînement qu'en compétition, l'exercice de tir au Bail Trap consiste en un lancer d'un pigeon que le tireur tente d'atteindre pour que les plombs le disloquent. Cette dislocation assure un effet visuel permettant au tireur et au public éventuel de valider que la cible a été atteinte. Dans certains cas, on peut accentuer l'effet visuel par l'emploi de pigeons spécifiques, renfermant un matériau pulvérulent tel du carbonate de calcium. A la rupture de la cible, le matériau pulvérulent est dissipé dans l'espace environnant la zone d'impact, produisant un nuage, éventuellement coloré selon la couleur du matériau en poudre. Le document US-A1 -20020125643 s'inscrit dans le cadre de telles cibles renfermant un matériau marqueur. In the latter area, there are known target launching devices often referred to as clay pigeons. The shooter is equipped with a rifle associated with cartridges containing pellets of caliber adapted to the desired shot. In both training and competition, the Bail Trap practice consists of a shot of a pigeon that the shooter tries to reach for the shots to dislocate. This dislocation provides a visual effect allowing the shooter and the eventual public to validate that the target has been hit. In some cases, the visual effect can be accentuated by the use of specific pigeons, containing a powdery material such as calcium carbonate. At the rupture of the target, the powdery material is dissipated into space surrounding the impact zone, producing a cloud, possibly colored according to the color of the powder material. The document US-A1-20020125643 is part of such targets containing a marker material.
L'effet visuel produit par cette technique est satisfaisant mais implique la consommation de nombreuses cibles, dont le coût est relativement élevé s'agissant de consommables, et dont l'impact environnemental, une fois les pigeons détruits et jonchant le sol, n'est pas toujours négligeable.  The visual effect produced by this technique is satisfactory but involves the consumption of many targets, the cost of which is relatively high for consumables, and whose environmental impact, once the pigeons are destroyed and strewn on the ground, is not not always negligible.
L'invention permet de résoudre tout ou partie des inconvénients des techniques actuelles.  The invention solves all or part of the disadvantages of current techniques.
RESUME DE L'INVENTION SUMMARY OF THE INVENTION
Suivant un premier aspect de modes de réalisation, elle concerne en particulier un procédé d'exercice au tir, comprenant une étape de lancement d'une cible dans une portion de l'espace, une étape de tir d'un projectile en direction de la cible et une étape d'impact du projectile sur la cible.  According to a first aspect of embodiments, it relates in particular to a method of firing practice, comprising a step of launching a target in a portion of the space, a firing step of a projectile towards the target and a projectile impact step on the target.
De façon avantageuse, ce procédé est tel qu'on utilise un projectile comprenant une coque délimitant un volume intérieur contenant un matériau marqueur et qu'il comporte une étape de rupture de la coque lors de l'impact du projectile sur la cible, de sorte à libérer le matériau marqueur  Advantageously, this method is such that a projectile comprising a shell delimiting an interior volume containing a marker material and that it comprises a step of rupture of the shell during the impact of the projectile on the target, so that to release the marker material
Cette disposition permet d'employer des cibles réutilisables puisque c'est le projectile qui est amené à se rompre. L'effet visuel est préservé du fait de l'aspect dynamique du fonctionnement de l'invention : le mouvement de la cible assure, au moment de l'impact, une répartition du marqueur dans l'espace, et notamment sur une large surface de la cible et/ou autour de celle-ci. Alors que les techniques actuelles se focalisent sur la destruction de la cible, l'invention adopte une démarche inverse.  This arrangement makes it possible to use reusable targets since the projectile is caused to break. The visual effect is preserved because of the dynamic aspect of the operation of the invention: the movement of the target ensures, at the moment of impact, a distribution of the marker in space, and in particular over a large area of the target and / or around it. While current techniques focus on the destruction of the target, the invention adopts a reverse approach.
Suivant une possibilité non limitative, l'étape de lancement comprend une mise en rotation propre de la cible. Un avantage produit par cet aspect de l'invention est que le point d'impact du projectile est alors le lieu d'un mouvement ayant une composante tangentielle sur la surface de la cible, outre le mouvement de la cible suivant sa trajectoire de lancement. Cela provoque un net accroissement de la zone de libération du marqueur.  According to a non-limiting possibility, the launching step comprises a self-rotation of the target. An advantage produced by this aspect of the invention is that the point of impact of the projectile is then the locus of a movement having a tangential component on the surface of the target, in addition to the movement of the target along its launch trajectory. This causes a marked increase in the marker release zone.
Un autre aspect de modes de réalisation de l'invention concerne aussi un système pour l'exercice au tir, comportant une cible et un projectile destiné à impacter la cible, caractérisé par le fait que le projectile comprend une coque délimitant un volume intérieur contenant un matériau marqueur et par le fait l'impact du projectile sur la cible est configuré pour provoquer la rupture de la coque, de sorte à libérer le matériau marqueur. Le système peut aussi comprendre une machine de lancement de cibles. Another aspect of embodiments of the invention also relates to a system for firing practice, comprising a target and a projectile intended to impact the target, characterized in that the projectile comprises a shell delimiting an interior volume containing a target. marking material and thereby the impact of the projectile on the target is configured to cause the rupture of the hull, so as to release the marker material. The system may also include a target launcher.
Un autre aspect de modes de réalisation de l'invention concerne une cible de tir. Suivant un cas préféré, la tranche de la cible a une densité moindre que la surface d'impact. Alors que les cibles de Bail Trap sont d'un seul bloc de même densité, l'invention s'en démarque nettement, d'autant plus qu'elle emploie un ou des matériaux moins denses au niveau de la tranche, zone où on placerait plus naturellement un matériau de forte densité pour des raisons de tenue mécanique. Avantageusement, la cible de tir comprend une surface périphérique comportant une tranche joignant une première face et une deuxième face et une surface d'impact formée sur au moins l'une parmi la première face et la deuxième face, apte à recevoir l'impact d'un projectile, caractérisé en ce que la tranche de la cible et la surface d'impact sont en des matériaux différents, la densité du ou des matériaux de la tranche étant inférieure à la densité du ou des matériaux de la surface d'impact.  Another aspect of embodiments of the invention relates to a firing target. In a preferred case, the edge of the target has a lower density than the impact surface. While the targets of Bail Trap are of a single block of the same density, the invention stands out clearly, especially since it uses one or less dense materials at the level of the slice, area where we would place more naturally a high density material for reasons of mechanical strength. Advantageously, the firing target comprises a peripheral surface comprising a slice joining a first face and a second face and an impact surface formed on at least one of the first face and the second face, capable of receiving the impact of a projectile, characterized in that the edge of the target and the impact surface are of different materials, the density of the material or materials of the wafer being less than the density of the material or materials of the impact surface.
Un autre aspect de modes de réalisation de l'invention concerne un dispositif comprenant une cible et un projectile. Another aspect of embodiments of the invention is a device comprising a target and a projectile.
BREVE INTRODUCTION DES FIGURES BRIEF INTRODUCTION OF FIGURES
D'autres caractéristiques, buts et avantages de la présente invention apparaîtront à la lecture de la description détaillée qui suit, et en regard des dessins annexés donnés à titre d'exemples non limitatifs et sur lesquels :  Other features, objects and advantages of the present invention will appear on reading the detailed description which follows, and with reference to the appended drawings given as non-limiting examples and in which:
la figure 1 présente en perspective un exemple de cible utilisable selon la présente invention.  Figure 1 shows in perspective an example of a target used according to the present invention.
La figure 2 illustre une possibilité de montage d'une partie de la cible sur le reste de la cible.  Figure 2 illustrates a possibility of mounting a portion of the target on the rest of the target.
La figure 3 présente une alternative au mode de réalisation de la figure 2 pour le montage d'une partie de la cible sur le reste de la cible.  Figure 3 shows an alternative to the embodiment of Figure 2 for mounting a portion of the target on the rest of the target.
La figure 4 est une vue en coupe transversale suivant un diamètre de la cible selon le mode de réalisation de la figure 3.  FIG. 4 is a cross-sectional view along a diameter of the target according to the embodiment of FIG. 3.
La figure 6 présente en perspective un autre mode de réalisation de la cible et la figure 5 en est une vue transversale suivant un diamètre de la cible.  Figure 6 shows in perspective another embodiment of the target and Figure 5 is a transverse view along a diameter of the target.
Les figures 7 à 9 présentent en perspective un mode de réalisation de machine de lancement pouvant faire partie de la présente invention, les figures 7 à 9 montrant différentes phases de fonctionnement de ladite machine. DESCRIPTION DETAILLEE Figures 7 to 9 show in perspective an embodiment of launcher can be part of the present invention, Figures 7 to 9 showing different phases of operation of said machine. DETAILED DESCRIPTION
Avant d'entrer dans le détail de modes de réalisation de l'invention en référence aux figures, on énonce ci-après des caractéristiques optionnelles qui peuvent être mises en œuvre de façon combinée ou alternative:  Before going into the details of embodiments of the invention with reference to the figures, the following are optional features that can be implemented in a combined or alternative way:
- la vitesse de rotation propre de la cible 1 est au moins de 300 tours par minute au moment du lancer et/ ou au moment de l'impact;  the own rotation speed of the target 1 is at least 300 revolutions per minute at the time of the launch and / or at the moment of the impact;
- on utilise une cible (1 ) dont la surface périphérique comporte une tranche (2) joignant une première face (3) et une deuxième face (4) et l'étape d'impact est réalisée par contact du projectile sur une surface d'impact (8) formée sur au moins l'une parmi la première face (3) et la deuxième face (4) ;  a target (1) is used whose peripheral surface comprises a wafer (2) joining a first face (3) and a second face (4) and the impact step is performed by contacting the projectile on a surface of impact (8) formed on at least one of the first face (3) and the second face (4);
- la tranche (2) de la cible (1 ) et la surface d'impact (8) sont choisies en des matériaux différents ;  the slice (2) of the target (1) and the impact surface (8) are chosen from different materials;
- le ou les matériaux de la tranche (2) est choisi avec une densité inférieure à la densité du ou des matériaux de la surface d'impact (8) ;  the material or materials of the wafer (2) is chosen with a density lower than the density of the material or materials of the impact surface (8);
- la densité du ou des matériaux de la surface d'impact (8) est choisie supérieure à 500 kg/m3 ; the density of the material or materials of the impact surface (8) is chosen to be greater than 500 kg / m 3 ;
- la densité du ou des matériaux de la tranche (2) est inférieure à 275 kg/m3 ;the density of the material or materials of the wafer (2) is less than 275 kg / m 3 ;
- on utilise une cible (1 ) comprenant un corps de cible (12) de forme cylindrique dont la surface de révolution forme la tranche (2) et la surface d'impact (8) comprend, sur au moins l'une parmi la première face (3) et la deuxième face (4), une zone en forme de disque ; a target (1) comprising a target body (12) of cylindrical shape whose surface of revolution forms the wafer (2) and the impact surface (8) comprises, on at least one of the first face (3) and the second face (4), a disk-shaped area;
- le diamètre de la zone en forme de disque est inférieur au diamètre du corps de cible (12) ;  the diameter of the disk-shaped area is smaller than the diameter of the target body (12);
- on utilise une cible (1 ) dont le corps (12) est en mousse polymère et au moins une partie de la surface d'impact (8) est réalisée par réticulation de ladite mousse ;  a target (1) is used whose body (12) is made of polymeric foam and at least a portion of the impact surface (8) is made by cross-linking said foam;
- on forme au moins une partie de la surface d'impact (8) par fixation d'un revêtement (10) sur le corps de cible (12) ;  forming at least a portion of the impact surface (8) by attaching a coating (10) to the target body (12);
- la fixation est opérée avec au moins un organe de fixation (1 1 ) situé sur une face du revêtement (10) opposée à la face du revêtement (10) formant au moins en partie la surface d'impact (8), et avec au moins un organe de fixation complémentaire (13) formé sur le corps de cible (12) ;  the fixing is carried out with at least one fixing member (1 1) situated on one face of the coating (10) opposite to the face of the coating (10) forming at least partly the impact surface (8), and with at least one complementary fastening member (13) formed on the target body (12);
- la cible comporte deux revêtements fixés chacun sur une face différente et chacun associés à au moins un organe de fixation, les organes de fixation des deux revêtements étant configurés pour se solidariser dans un espace situé dans l'épaisseur du corps de cible.  - The target comprises two coatings each fixed on a different face and each associated with at least one fastener, the fasteners of the two coatings being configured to be secured in a space within the thickness of the target body.
- le revêtement (10) est une plaque de matériau polymère ; - on utilise une cible (1 ) comprenant une ceinture dont une partie de pourtour forme la tranche (2) de la cible (1 ) et entourant un cœur (15) de cible, et la paroi externe du cœur (15) de cible forme au moins en partie la surface d'impact (8). the coating (10) is a plate of polymeric material; a target (1) is used comprising a belt of which a peripheral part forms the wafer (2) of the target (1) and surrounding a target core (15), and the outer wall of the target core (15) forms at least in part the impact surface (8).
- le cœur (15) de cible comporte une partie de fixation d'une zone de la ceinture (14) opposée à la partie de pourtour ;  the target core (15) has a portion for fixing a zone of the belt (14) opposite to the peripheral part;
- le cœur (15) de cible comporte une âme (16) centrale choisie avec une épaisseur inférieure à celle de la partie de fixation ;  the target core (15) comprises a central core (16) chosen with a thickness less than that of the fixing portion;
- le module de Young du ou des matériaux de la tranche (2) est choisi inférieur à celui du ou des matériaux de la surface d'impact (8) ;  the Young's modulus of the material or materials of the wafer (2) is chosen to be smaller than that of the material or materials of the impact surface (8);
- le module de Young du ou des matériaux de la tranche est inférieur à 0,1 giga the Young's modulus of the material or materials of the slice is less than 0.1 giga
Pascal ; Pascal;
- le revêtement est une nappe de matériau élastomère ;  the coating is a sheet of elastomeric material;
- le module de Young du ou des matériaux de la surface d'impact (8) est choisi supérieur à 0,8 giga Pascal ;  the Young's modulus of the material or materials of the impact surface (8) is chosen greater than 0.8 giga Pascal;
- le marqueur du projectile est choisi parmi un colorant liquide et une poudre ; the marker of the projectile is chosen from a liquid dye and a powder;
- la coque du projectile est réalisée sous forme d'une coque rigide en matériau polymère ou sous forme d'une coque souple, de préférence en gélatine ; the shell of the projectile is made in the form of a rigid shell made of polymeric material or in the form of a flexible shell, preferably of gelatin;
- la coque est réalisée sous forme d'enveloppe sphérique lisse.  - The shell is formed as a smooth spherical envelope.
- le dispositif comporte une cible et un projectile comprenant une coque délimitant un volume intérieur contenant un matériau marqueur.  the device comprises a target and a projectile comprising a shell delimiting an interior volume containing a marker material.
- La cible présente préférentiellement une surface périphérique comportant une tranche joignant une première face et une deuxième face et une surface d'impact formée sur au moins l'une parmi la première face et la deuxième face, apte à recevoir l'impact d'un projectile, la tranche de la cible et la surface d'impact étant en des matériaux différents, la densité du ou des matériaux de la tranche étant inférieure à la densité du ou des matériaux de la surface d'impact.  - The target preferably has a peripheral surface having a slice joining a first face and a second face and an impact surface formed on at least one of the first face and the second face, adapted to receive the impact of a projectile, the edge of the target and the impact surface being of different materials, the density of the material or materials of the slice being less than the density of the material or materials of the impact surface.
- la tranche de la cible est configurée pour absorber l'énergie d'un impact du projectile dans une plus large proportion que la surface d'impact.  the slice of the target is configured to absorb the energy of a projectile impact in a greater proportion than the impact surface.
- la cible et le projectile sont configurés pour que le projectile absorbe plus de 60% de l'énergie généré par un impact du projectile sur la surface d'impact.  the target and the projectile are configured so that the projectile absorbs more than 60% of the energy generated by an impact of the projectile on the impact surface.
Un aspect de l'invention est lié au lancement d'une cible dans une portion de l'espace. Une machine de lancement est prévue et un exemple de réalisation non limitatif est donné aux figures 7 à 9.  One aspect of the invention is related to launching a target in a portion of the space. A launching machine is provided and a non-limiting example of embodiment is given in FIGS. 7 to 9.
A ces figures, la machine 19 présente une surface de lancement avantageusement sous forme d'un plan 20 permettant de recevoir au moins une cible 1 en contact avec une des faces 3, 4 de la cible 1. Le plan de lancement 20 peut être horizontal ou incliné, en particulier pour varier les effets de projection de la cible et la zone de l'espace dans laquelle la cible est projetée. A cet effet, la machine 19 peut être pourvue de moyens permettant son inclinaison. Lorsqu'une cible 1 est sur le plan de lancement 20, son lancement est réalisé par l'intermédiaire d'un dispositif d'éjection ici sous forme d'un bras 21 monté rotatif autour d'un axe x2. Dans l'exemple, le bras 21 est configuré pour s'appliquer sur une partie de tranche 2 de la cible 1 pour lui conférer une énergie cinétique permettant de l'envoyer. On peut utiliser un système d'armement pour le bras 21 et notamment un système tel qu'utilisé dans les machines de ball-trap par exemple mettant en jeu un ressort tendu par une motorisation et détendu sur commande pour produire une rotation rapide du bras 21 lors de la phase de lancement. La machine 19 comporte en outre une surface d'application périphérique 22 de la cible 1 et apte à coopérer avec la tranche 2 de la cible 1. De cette façon, la cible 1 peut être guidée au cours de son déplacement sur le plan de lancement 20 jusqu'à son éjection. En outre, la surface 22 peut constituer une zone d'adhérence qui permet dans un mode de réalisation préféré de mettre efficacement la cible 1 en rotation propre. On verra ultérieurement l'intérêt de cette rotation propre pour produire un effet technique visuel accru. La forme de la surface d'application 22 n'est pas limitée mais est préférentiellement curviligne avec un profil en virgule. In these figures, the machine 19 has a launching surface advantageously in the form of a plane 20 for receiving at least one target 1 in contact with one of the faces 3, 4 of the target 1. The launching plane 20 can be horizontal or inclined, in particular to vary the projection effects of the target and the area of the space in which the target is projected. For this purpose, the machine 19 may be provided with means for tilting it. When a target 1 is on the launch plane 20, its launch is achieved by means of an ejection device here in the form of an arm 21 rotatably mounted about an axis x2. In the example, the arm 21 is configured to be applied on a portion of wafer 2 of the target 1 to give it a kinetic energy to send it. It is possible to use a cocking system for the arm 21 and in particular a system as used in ballooning machines, for example involving a spring tensioned by an operator and expanded on command to produce a rapid rotation of the arm 21. during the launch phase. The machine 19 further comprises a peripheral application surface 22 of the target 1 and adapted to cooperate with the slice 2 of the target 1. In this way, the target 1 can be guided during its movement on the launch plan 20 until ejection. In addition, the surface 22 may constitute an adhesion zone which allows in a preferred embodiment to effectively put the target 1 in clean rotation. We will see later the interest of this own rotation to produce an increased visual technical effect. The shape of the application surface 22 is not limited but is preferably curvilinear with a comma profile.
Les composants précédemment décrits pour la machine 19 sont, dans le cas des figures 7 à 9, montés sur un châssis 23. Le châssis 23 peut être articulé de sorte à produire les moyens d'inclinaison précédemment indiqués et notamment posséder une capacité d'articulation en rotation selon au moins un axe.  The components previously described for the machine 19 are, in the case of Figures 7 to 9, mounted on a frame 23. The frame 23 can be articulated so as to produce the aforementioned inclination means and in particular to have an articulation capacity in rotation along at least one axis.
Pour permettre l'exercice du tir avec des cibles successives, la machine 19 comporte avantageusement une pluralité de cibles stockées dans un chargeur 24. Dans le cas représenté, le chargeur 24 est sensiblement équivalent à ceux utilisés pour lancer des cibles du type « pigeon d'argile » et comporte à cet effet au moins une colonne 25 permettant la mise en superposition des cibles 1 lors de leur stockage et comporte une zone de délivrance 26 en partie inférieure de la ou les colonnes 25, de sorte que, sur commande, une cible 1 peut être évacuée de la colonne 25 qui la stockait pour être dirigée vers le plan de lancement 20. Ce cheminement de cible 1 peut être opéré par gravité et/ou par l'intermédiaire de système de poussée.  To allow the exercise of shooting with successive targets, the machine 19 advantageously comprises a plurality of targets stored in a charger 24. In the case shown, the charger 24 is substantially equivalent to those used to launch targets of the "pigeon dart" type. "clay" and comprises for this purpose at least one column 25 for the superposition of the targets 1 during storage and has a delivery zone 26 in the lower part of the or columns 25, so that, on command, a target 1 can be evacuated from the column 25 which stored it to be directed towards the launching plane 20. This target path 1 can be operated by gravity and / or thrust system.
La cible 1 employée dans l'invention peut présenter différentes formes et configurations. Néanmoins au vu de ce qui précède en référence à la machine de lancement 19, il est avantageux que la cible 1 présente un pourtour extérieur sous forme de tranche 2 de forme sensiblement circulaire. En outre, il est avantageux que la cible 1 comporte une symétrie axiale suivant l'axe par lequel elle est amenée à être mise en rotation propre. La symétrie peut être par ailleurs centrale, de sorte que la cible 1 est complètement équilibrée autour de son centre. The target 1 used in the invention may have different shapes and configurations. However, in view of the above with reference to the launching machine 19, it is advantageous for the target 1 to have an outer periphery in the form of a slice 2 of substantially circular shape. In addition, it is advantageous for the target 1 to have an axial symmetry along the axis through which it is brought to be setting in own rotation. The symmetry can be otherwise central, so that the target 1 is completely balanced around its center.
En outre, la cible 1 est préférentiellement réutilisable et l'impact du projectile ne l'affecte pas fondamentalement. Cela n'exclut pas que des points d'impact persistent après les tirs, mais ces altérations sont avantageusement mineures de sorte que la cible peut fonctionner plusieurs fois.  In addition, the target 1 is preferably reusable and the impact of the projectile does not affect it fundamentally. This does not exclude that impact points persist after the shots, but these alterations are advantageously minor so that the target can operate multiple times.
D'une manière générale, la cible 1 comporte une paroi périphérique constituant sa surface extérieure et disposant avantageusement d'une tranche 2 et d'une première face 3 et d'une deuxième face 4. La figure 1 montre un exemple de réalisation de cette typologie de cible 1. Dans le cas illustré, les première et deuxième faces 3, 4 sont sensiblement planes mais ce cas n'est pas limitatif comme on le verra ultérieurement en référence aux figures 5 et 6 notamment. La tranche 2 est avantageusement sous la forme de la surface externe d'un cylindre de révolution. Ainsi, dans le cas des figures 1 à 4, la cible 1 a essentiellement la forme d'une portion de cylindre relativement aplatie à savoir que la hauteur est inférieure à son diamètre.  In general, the target 1 comprises a peripheral wall constituting its outer surface and advantageously having a wafer 2 and a first face 3 and a second face 4. FIG. 1 shows an exemplary embodiment of this invention. target typology 1. In the case illustrated, the first and second faces 3, 4 are substantially planar but this case is not limiting as will be seen later with reference to Figures 5 and 6 in particular. The slice 2 is advantageously in the form of the outer surface of a cylinder of revolution. Thus, in the case of Figures 1 to 4, the target 1 has essentially the shape of a relatively flattened cylinder portion, namely that the height is less than its diameter.
A titre d'exemple, aussi bien dans le mode de réalisation des figures 1 et 2 que dans les autres modes de réalisation, on peut utiliser une cible 1 de section circulaire ayant un diamètre compris entre 25 et 33 centimètres et une hauteur (dimension en épaisseur) comprise entre 25 et 50 millimètres.  By way of example, both in the embodiment of FIGS. 1 and 2 and in the other embodiments, it is possible to use a target 1 of circular section having a diameter of between 25 and 33 centimeters and a height (dimension in thickness) between 25 and 50 millimeters.
En revenant aux figures 1 et 2, la cible 1 porte un corps 12 préférentiellement à base de mousse polymère haute ou basse densité. A titre d'exemple, donnent satisfaction des mousses du type polyéthylène ou polychlorure de vinyle. La densité de ces mousses est par exemple inférieure à 275 kg/m3. On forme ainsi un corps 12 de cible 1 donnant une tenue à la cible 1 sans pour autant présenter une rigidité trop importante de sorte à limiter la dangerosité du lancement de la cible 1. Par ailleurs, la capacité d'écrasement de la cible 1 sous forme de déformation élastique au niveau de sa tranche 2 peut permettre, dans certains modes de réalisation, d'accentuer l'effet de mise en rotation propre par l'intermédiaire de la machine de lancement 19. Returning to Figures 1 and 2, the target 1 carries a body 12 preferably based on high or low density polymer foam. By way of example, satisfactory foams of polyethylene or polyvinyl chloride type. The density of these foams is, for example, less than 275 kg / m 3 . Thus, a body 12 of target 1 giving a resistance to the target 1 without forming too much rigidity so as to limit the danger of the launch of the target 1. Moreover, the crushing capacity of the target 1 under In some embodiments, the elastic deformation form at its edge 2 may make it possible to accentuate the effect of self-rotation by means of the launching machine 19.
Le corps de cible peut être d'un seul tenant et en une seule matière ou présenter plusieurs matériaux. Par exemple, on peut réaliser un corps 12 multicouches, avec notamment une couche centrale dans l'épaisseur du corps 12 et, de chaque côté de la couche centrale, une couche latérale en matériau moins dense que la couche centrale.  The target body can be in one piece and in one material or have multiple materials. For example, it is possible to produce a multilayer body 12, in particular with a central layer in the thickness of the body 12 and, on each side of the central layer, a lateral layer made of a material less dense than the central layer.
Dans le même temps, compte tenu de la nécessité de provoquer la rupture d'un projectile lors de son impact sur la cible 1 , cette dernière comporte avantageusement une surface d'impact dont la conception est définie de sorte à assurer la rupture. En particulier, la surface d'impact 8 est avantageusement configurée pour limiter l'absorption de l'énergie de l'impact de sorte que cette énergie est suffisamment réfléchie vers le projectile pour provoquer sa rupture, c'est-à-dire dépasser sa limite de résistance à la rupture. Pour y parvenir, la surface d'impact 8 est dans le cas des figures 1 et 2 réalisée à partir d'au moins un revêtement 10, chaque revêtement 10 pouvant coopérer avec l'une parmi la première et la deuxième faces 3, 4. At the same time, given the need to cause the rupture of a projectile during its impact on the target 1, the latter advantageously comprises an impact surface whose design is defined to ensure rupture. In particular, the impact surface 8 is advantageously configured to limit the absorption of the energy of the impact so that this energy is sufficiently reflected towards the projectile to cause its rupture, that is to say to exceed its limit of resistance to rupture. To achieve this, the impact surface 8 is in the case of Figures 1 and 2 made from at least one coating 10, each coating 10 can cooperate with one of the first and second faces 3, 4.
La figure 1 montre que le revêtement 10 peut présenter la forme d'un disque applicable sur une face 3, 4 de manière centrée sur celle-ci et délimitant une bordure 9 sur la face 3, 4 équipée, de sorte à préserver un pourtour qui peut être dans un matériau moins dense et/ou moins rigide.  FIG. 1 shows that the coating 10 may have the shape of a disc that can be applied on a face 3, 4 in a centered manner and delimits an edge 9 on the face 3, 4 equipped so as to preserve a periphery which may be in a less dense material and / or less rigid.
On a représenté en figure 2 un exemple de revêtement 10 sous forme d'une nappe en matériau suffisamment souple pour être positionné facilement sur la face 3. A titre préféré, la nappe est en matériau élastomère ce qui comprend à la fois les matériaux polymères élastomères et les matériaux naturels en particulier le caoutchouc. La fixation de la nappe peut s'opérer par tous moyens mécaniques ou encore par collage. La surface extérieure de la nappe ainsi formée constitue ou participe à constituer la surface d'impact 8. Avantageusement, le matériau de la nappe est choisi pour assurer une bonne coopération avec le projectile.  FIG. 2 shows an example of a coating 10 in the form of a sheet of material that is sufficiently flexible to be easily positioned on the face 3. As a preference, the sheet is made of elastomer material which comprises both the elastomeric polymer materials. and natural materials especially rubber. Fixing the web can be done by any mechanical means or by gluing. The outer surface of the sheet thus formed constitutes or participates in constituting the impact surface 8. Advantageously, the material of the sheet is chosen to ensure good cooperation with the projectile.
Dans un mode de réalisation, le projectile est sous forme d'une bille ou balle présentant une coque en matériau souple et par exemple en gélatine. Dans cet exemple, l'utilisation d'un revêtement 10 en élastomère assure une capacité de frottement accrue entre la coque du projectile et la surface d'impact 8 de sorte à faciliter la rupture de la coque. Par ailleurs, on peut utiliser un revêtement 10 de sorte à faciliter le nettoyage lorsque la coque en matériau souple renferme un produit liquide colorant tel de la peinture. La surface de la surface d'impact 8 est à cet effet avantageusement lisse. Dans cet exemple, il suffit de frotter le revêtement 10 avec un chiffon pour faire disparaître facilement la peinture déposée par le projectile. A titre d'alternative, le revêtement 10 peut se présenter sous forme de plaque en matériau polymère rigide rapportée sur l'une ou l'autre des faces 3, 4.  In one embodiment, the projectile is in the form of a ball or ball having a shell of flexible material and for example gelatin. In this example, the use of an elastomeric coating provides increased frictional capability between the shell of the projectile and the impact surface 8 to facilitate rupture of the shell. Moreover, a coating 10 can be used so as to facilitate cleaning when the shell of flexible material contains a liquid dye product such as paint. The surface of the impact surface 8 is advantageously smooth for this purpose. In this example, it suffices to rub the coating 10 with a cloth to easily remove the paint deposited by the projectile. As an alternative, the coating 10 may be in the form of a rigid polymer material plate attached to one or other of the faces 3, 4.
Dans le cas des figures 3 et 4, le montage s'opère par des organes de fixation coopérant avec des organes de fixation 1 1 sur la face interne du revêtement 10 et des organes complémentaires 13 dans le corps de cible 12 ou une autre partie de cible. Les organes complémentaires 13 comprennent avantageusement des logements femelles formés dans le corps de cible 12 alors que les organes 1 1 sont des parties mâles susceptibles de s'insérer dans les logements. Au moins un organe de fixation 1 1 peut être formé ou plusieurs. Dans le cas illustré, au moins quatre organes sont situés à quatre points cardinaux, de sorte à répartir l'effort de fixation sur la cible 1 . Les organes de fixation sont insérés dans les logements et peuvent s'accrocher sur la paroi de ces derniers. En outre, au moins un organe de fixation 1 1 peut présenter un relief à sa surface de sorte à augmenter l'effet d'accroché dans l'organe de fixation complémentaire 13. Cet exemple de montage peut être complété ou remplacé par toute autre forme de fixation et notamment par un collage. In the case of FIGS. 3 and 4, the assembly is effected by fixing members cooperating with fastening members 1 1 on the internal face of the coating 10 and complementary members 13 in the target body 12 or another part of target. The complementary members 13 advantageously comprise female housings formed in the target body 12 while the members 1 1 are male parts capable of being inserted into the housings. At least one fastener 1 1 may be formed or more. In the illustrated case, at least four members are located at four cardinal points, so as to distribute the fixing force on the target 1. The fasteners are inserted in the housing and can hang on the wall of the latter. In addition, at least one fastening member January 1 can have a relief on its surface so as to increase the effect of hanging in the complementary fastening member 13. This mounting example can be completed or replaced by any other form fixing and in particular by a collage.
A titre de variante, la figure 4 montre en section le résultat obtenu dans le mode de réalisation de la figure 3 avec le passage des organes de fixation 1 1 au travers de l'épaisseur du corps de cible 12. Cette figure montre par ailleurs que l'on peut équiper chaque face 3, 4 de la cible 1 avec un revêtement 10 de sorte que l'impact du projectile peut se produire par les deux côtés de la cible 1 . Dans ce cadre, il peut être avantageux de faire coopérer les organes de fixation 1 1 des deux revêtements 10. C'est le sens du cas illustré dans lequel chaque revêtement 10 porte des organes de fixation, d'une part sous forme de tiges mâles, d'autre part sous forme de tiges présentant un conduit intérieur. On s'arrange pour que les tiges des organes de fixation 1 1 d'un des revêtements 10 puissent s'insérer dans les conduits intérieurs des organes de fixation de l'autre revêtement 10 situé sur la face opposée. De la sorte, le corps de cible 12 est pris en étau entre les deux revêtements 10 placés de part et d'autre de ce dernier et se fixant conjointement au travers de l'épaisseur comme le montre la figure 4. Dans le cas où le revêtement 10 est en matériau polymère, il s'agit avantageusement d'un matériau polymère thermodurcissable. A titre d'exemple, le revêtement 10 peut être dans les matériaux suivants : polycarbonate, polyamide ou ABS. Toujours à titre d'exemple, l'épaisseur du revêtement 10 peut être dans tous les cas de figures compris entre 0,5 et 3 millimètres et avantageusement de 1 millimètre.  As a variant, FIG. 4 shows in section the result obtained in the embodiment of FIG. 3 with the passage of the fastening members 11 through the thickness of the target body 12. This figure also shows that one can equip each face 3, 4 of the target 1 with a coating 10 so that the impact of the projectile can occur by both sides of the target 1. In this context, it may be advantageous to cooperate the fasteners 1 1 of the two coatings 10. This is the sense of the illustrated case in which each coating 10 carries fasteners, on the one hand in the form of male rods on the other hand in the form of rods having an inner conduit. It is arranged that the rods of the fasteners 1 1 of one of the coatings 10 can be inserted into the inner conduits of the fasteners of the other coating 10 on the opposite side. In this way, the target body 12 is clamped between the two coatings 10 placed on either side of the latter and is fixed together through the thickness as shown in FIG. coating 10 is made of polymeric material, it is advantageously a thermosetting polymer material. By way of example, the coating 10 may be in the following materials: polycarbonate, polyamide or ABS. Still as an example, the thickness of the coating 10 may be in all cases between 0.5 and 3 millimeters and preferably 1 millimeter.
Surtout dans le cas de l'utilisation de projectile présentant un marqueur sous forme de liquide colorant, il est avantageux d'utiliser un revêtement 10 présentant une surface extérieure de couleur foncée et préférentiellement noire, cela permet d'accentuer l'effet visuel par contraste lors de la libération du marqueur.  Especially in the case of the use of a projectile having a marker in the form of a coloring liquid, it is advantageous to use a coating 10 having an outer surface of dark color and preferentially black, this makes it possible to accentuate the visual effect by contrast. when the marker is released.
Comme précédemment indiqué, le mode de réalisation présenté aux figures 1 à 4 ménage une bordure 9 autour du revêtement 10. La bordure 9 peut participer à la sécurité de l'exercice du tir en évitant de rendre la cible trop dangereuse notamment dans le cas où les revêtements sont rigides et présentent une densité supérieure à la densité du corps de cible 12. Dans ce cadre, à titre d'exemple, on notera que l'épaisseur du rebord peut correspondre à entre 10 et 30% du diamètre des faces 3, 4 des cibles.  As previously indicated, the embodiment shown in FIGS. 1 to 4 includes a border 9 around the covering 10. The edge 9 can participate in the safety of the exercise of the shot by avoiding making the target too dangerous especially in the case where the coatings are rigid and have a density greater than the density of the target body 12. In this context, by way of example, it will be noted that the thickness of the rim may correspond to between 10 and 30% of the diameter of the faces 3, 4 targets.
Les figures 5 et 6 présentent une variante de réalisation de la cible 1 selon l'invention. En particulier, la figure 6 révèle qu'au moins une des faces 3, 4 peut ne pas être plane et présenter, en particulier dans l'exemple illustré, une cavité centrale entourée à sa périphérie par une portion de surface d'impact 8 située à un niveau plus élevé. Cette configuration peut permettre de limiter le poids de la cible 1 mais aussi de favoriser la rupture en proposant des éléments de surface ayant différentes orientations de sorte à éviter une application trop tangentielle du projectile sur la face 3,4 considérée. Dans le cas où le revêtement 10 est en matériau polymère, il s'agit avantageusement d'un matériau polymère thermodurcissable. A titre d'exemple, le revêtement 10 peut être dans les matériaux suivants : polycarbonate, polyamide ou ABS. Figures 5 and 6 show an alternative embodiment of the target 1 according to the invention. In particular, FIG. 6 reveals that at least one of the faces 3, 4 may not be flat and have, particularly in the example shown, a central cavity surrounded at its periphery by an impact surface portion 8 located at a higher level. This configuration can make it possible to limit the weight of the target 1, but also to promote breakage by proposing surface elements having different orientations so as to avoid too much tangential application of the projectile on the face 3.4 considered. In the case where the coating 10 is of polymeric material, it is advantageously a thermosetting polymer material. By way of example, the coating 10 may be in the following materials: polycarbonate, polyamide or ABS.
Le mode de réalisation des figures 5 et 6 comporte une ceinture 14 apte à constituer un organe périphérique pour le reste de la cible 1. A titre avantageux et dans l'exemple représenté, la ceinture 14 est sous forme annulaire, la surface extérieure de l'anneau constituant la tranche 2 alors que la surface intérieure de l'anneau permet la coopération avec le reste de la cible 1 . Le reste de la cible 1 peut comprendre, comme dans le cas illustré, un cœur 15 présentant une portion de coopération avec la ceinture 14 et une portion centrale dénommée « âme » 16. Dans le cas représenté, l'âme 16 présente une épaisseur moindre que le reste du cœur 15. La partie périphérique du cœur 15 comprend un élargissement 17 encadrant l'âme 16 et pouvant servir de base à la réception de deux ailes 18 situées de part et d'autre de l'élargissement et apparaissant chacune au niveau de l'une parmi la première et la deuxième faces 3, 4. Les ailes 18 sont avantageusement sensiblement parallèles et permettent de coopérer avec les flancs 2 de la ceinture 14 de sorte que les deux éléments s'imbriquent pour former un ensemble solidaire.  The embodiment of FIGS. 5 and 6 comprises a belt 14 capable of constituting a peripheral member for the remainder of the target 1. As an advantage and in the example shown, the belt 14 is in annular form, the outer surface of the ring constituting the slice 2 while the inner surface of the ring allows cooperation with the rest of the target 1. The remainder of the target 1 may comprise, as in the case illustrated, a heart 15 having a portion of cooperation with the belt 14 and a central portion called "soul" 16. In the case shown, the core 16 has a lower thickness That the rest of the heart 15. The peripheral part of the heart 15 comprises an enlargement 17 framing the core 16 and can serve as a basis for the reception of two wings 18 located on either side of the enlargement and appearing at each level. one of the first and second faces 3, 4. The wings 18 are preferably substantially parallel and cooperate with the sidewalls 2 of the belt 14 so that the two elements interlock to form a unitary assembly.
Dans le cas représenté, le cœur 15 est constitué d'une seule pièce mais ce cas n'est pas limitatif. De même, la ceinture 14 est ici monobloc mais pourrait être réalisée en plusieurs parties assemblées.  In the case shown, the heart 15 consists of a single piece but this case is not limiting. Similarly, the belt 14 is here monobloc but could be made of several parts assembled.
Comme dans les modes de réalisation précédemment présentés, le cas des figures 5 et 6 révèle la capacité de sélectionner des matériaux spécifiques pour constituer la surface d'impact 8 relativement à la surface de la tranche 2. En particulier, le cœur 15 peut être réalisé en un matériau plus dense que le matériau de la ceinture 14 et/ou un matériau présentant un module de Young plus élevé que celui de la ceinture 14. On dispose ainsi d'une surface d'impact 8 favorisant la réflexion de l'énergie d'impact sur le projectile pour produire sa rupture alors que le reste de la cible 1 et en particulier le matériau situé à sa tranche 2 est moins dense et/ou plus déformable élastiquement (moins rigide) pour limiter les risques d'accident et favoriser la mise en rotation par adhérence. Dans tous les cas de figures évoqués précédemment, on peut sélectionner pour la tranche 2 un ou des matériaux dont le module de Young est inférieur ou égal 0,1 Gpa (gigaPascal). En complément ou de manière séparée, on peut sélectionner un ou des matériaux pour la surface d'impact 8 dont le module de Young est supérieur à 0,8 Gpa. As in the embodiments previously presented, the case of FIGS. 5 and 6 reveals the ability to select specific materials for constituting the impact surface 8 relative to the surface of the slice 2. In particular, the core 15 can be realized in a material that is denser than the material of the belt 14 and / or a material having a Young's modulus higher than that of the belt 14. This provides an impact surface 8 that promotes the reflection of the energy of the body. impact on the projectile to produce its break while the rest of the target 1 and in particular the material located at its slice 2 is less dense and / or more elastically deformable (less rigid) to limit the risk of accident and promote the rotation by adhesion. In all the cases mentioned above, it is possible to select for unit 2 one or more materials whose Young's modulus is less than or equal to 0.1 Gpa (gigaPascal). In addition or separately, one or more materials may be selected for the impact surface 8, the Young's modulus of which is greater than 0.8 Gpa.
Suivant une possibilité, la surface d'impact (8) est en un matériau polymère et particulièrement en polyuréthane. Ce matériau est avantageusement choisi pour disposer d'une dureté Shore de plus de 90 et plus préférentiellement d'au moins 99 ; il peut se présenter sous forme de plaque d'au moins 1 mm, et préférentiellement de 1 mm plus ou moins 10%.  According to one possibility, the impact surface (8) is made of a polymer material and particularly of polyurethane. This material is advantageously chosen to have a Shore hardness of more than 90 and more preferably of at least 99; it may be in the form of a plate of at least 1 mm, and preferably of 1 mm plus or minus 10%.
Un autre mode de réalisation de la cible 1 , qui n'est pas présenté aux figures, consiste à partir d'une cible 1 présentant un corps de cible 12 sensiblement comme dans le cas des figures 1 et 2, à réaliser une réticulation d'une partie de la surface de l'une au moins parmi la première et la deuxième faces 3, 4, de sorte à durcir cette partie et former une surface d'impact 8 absorbant moins l'énergie d'impact que le reste du corps de cible 12. On peut néanmoins préserver une bordure 9 autour de la surface d'impact 8 lors de la phase de réticulation en apposant un cache sur la surface à protéger lors de cette réticulation. La surface d'impact 8 est alors constituée directement dans le corps de cible 12, et avantageusement dans une mousse polymère, mais avec un matériau transformé qui présente des propriétés mécaniques différentes du reste de la cible 1 et qui notamment absorbe moins l'énergie de l'impact que le reste de la cible 1 . La réticulation est faite préférentiellement suivant une profondeur correspondant à l'épaisseur du corps de cible. La cible 1 ainsi décrite assure à la fois l'efficacité et la sécurité de son lancement et l'efficacité de coopération avec le projectile. En effet, la surface d'impact 8 est avantageusement configurée dans les exemples précédents pour moins absorber l'énergie de l'impact que la partie de tranche 2 de la cible 1 , si bien que l'énergie renvoyée au projectile est suffisante pour provoquer la rupture de la coque et libérer le marqueur.  Another embodiment of the target 1, which is not shown in the figures, consists of a target 1 having a target body 12 substantially as in the case of Figures 1 and 2, to perform a crosslinking of a part of the surface of at least one of the first and second faces 3, 4, so as to harden this portion and form an impact surface 8 absorbing less impact energy than the rest of the body of target 12. It is nevertheless possible to preserve a border 9 around the impact surface 8 during the crosslinking phase by affixing a cover on the surface to be protected during this crosslinking. The impact surface 8 is then formed directly in the target body 12, and advantageously in a polymer foam, but with a transformed material which has mechanical properties different from the rest of the target 1 and which in particular absorbs less the energy of the target. the impact that the rest of the target 1. The crosslinking is preferably done at a depth corresponding to the thickness of the target body. The target 1 thus described ensures both the efficiency and safety of its launch and the effectiveness of cooperation with the projectile. Indeed, the impact surface 8 is advantageously configured in the previous examples to less absorb the energy of the impact than the slice portion 2 of the target 1, so that the energy returned to the projectile is sufficient to cause break the shell and release the marker.
On notera que les différentes possibilités de réalisation de cibles indiquées ci- dessus peuvent être combinées suivant toutes associations de leurs caractéristiques.  It should be noted that the different target realization possibilities indicated above can be combined according to any combination of their characteristics.
Selon l'invention, la cible 1 est amenée à coopérer avec un projectile non représenté.  According to the invention, the target 1 is brought to cooperate with a projectile not shown.
Comme précédemment indiqué, dans un mode de réalisation, le projectile comporte un marqueur sous forme de matériau pulvérulent qui peut être par exemple à base de carbonate de calcium coloré ou non. Dans cet exemple, la coque renfermant le marqueur est avantageusement une coque rigide et préférentiellement une coque de forme sphérique. Par ailleurs, la surface de la coque est avantageusement lisse de sorte à favoriser la précision du tir même si cela peut pénaliser la portée du tir. Il faut souligner que la présente invention s'adresse avantageusement à un exercice de tir dans lequel le projectile est lancé par l'intermédiaire d'une arme pouvant faire partie de la présente invention, la distance entre l'arme et la cible lancée étant comprise entre dix et vingt mètres et avantageusement inférieure à quinze mètres. As previously indicated, in one embodiment, the projectile comprises a marker in the form of a powdery material which may for example be based on colored calcium carbonate or not. In this example, the shell enclosing the marker is advantageously a rigid shell and preferably a shell of spherical shape. Moreover, the surface of the shell is advantageously smooth so as to promote the accuracy of the shot even if it can penalize the range of the shot. It should be emphasized that the present invention is advantageously aimed at a firing exercise in which the projectile is launched via a weapon that can be part of the present invention, the distance between the weapon and the target being launched being included between ten and twenty meters and advantageously less than fifteen meters.
On cherche donc préférentiellement à accroître la précision du tir plutôt que la portée du projectile. La coque rigide, indiquée ci-dessus, peut par exemple être en matériau polymère avec une épaisseur inférieure à un millimètre et avantageusement comprise entre 0,5 et 1 millimètre et avoir un diamètre compris entre un et deux centimètres et avantageusement 1 ,5 centimètre. La coque est par exemple obtenue par le procédé suivant: un mélange en poudre de polyéthylène glycol et de carbonate de calcium est placé dans un moule à la forme du projectile souhaitée ; on procède à un échauffement du moule de sorte à provoquer une fusion périphérique du mélange ; on stoppe réchauffement après un délai configuré pour permettre la formation d'une couche d'enveloppe de l'épaisseur voulue après refroidissement (le refroidissement peut être forcée, par trempe par exemple).  We therefore preferentially seek to increase the accuracy of the shot rather than the scope of the projectile. The rigid shell, indicated above, may for example be of polymeric material with a thickness of less than one millimeter and advantageously between 0.5 and 1 millimeter and have a diameter of between one and two centimeters and advantageously 1, 5 centimeters. The shell is for example obtained by the following method: a powder mixture of polyethylene glycol and calcium carbonate is placed in a mold in the shape of the desired projectile; the mold is heated to cause a peripheral melting of the mixture; heating is stopped after a delay configured to allow the formation of an envelope layer of the desired thickness after cooling (the cooling may be forced, for example by quenching).
Dans un autre mode de réalisation, la coque est en matériau souple et par exemple en gélatine. Elle constitue un enrobage délimitant le volume de stockage du marqueur. Cette solution est particulièrement adaptée, même si ce n'est pas limitatif, à un marqueur du type colorant liquide. Dans ce cas, le projectile a une conformation plus souple et est amené à se déformer plus facilement lors de l'impact sur la cible 1 . La coque souple peut être de la gélatine avec une épaisseur du même ordre que les épaisseurs données pour le cas de coques rigides.  In another embodiment, the shell is of flexible material and for example gelatin. It constitutes a coating delimiting the storage volume of the marker. This solution is particularly suitable, although not limiting, to a marker of the liquid dye type. In this case, the projectile has a more flexible conformation and is made to deform more easily during the impact on the target 1. The flexible shell may be gelatin with a thickness of the same order as the thicknesses given for the case of rigid shells.
Le projectile peut être lancé par l'intermédiaire d'une arme à gaz comprimé pouvant par exemple fonctionner sur la base de C02 et utilisant la détente du C02 pour réaliser l'effort de projection. Il peut s'agir de pistolets ou de fusils. The projectile can be launched via a compressed gas weapon that can for example operate on the basis of C0 2 and using the C0 2 expansion to achieve the projection effort. They may be pistols or rifles.
Le procédé d'exercice au tir s'opère de la façon suivante :  The practice of shooting practice is as follows:
- le tireur se met en position, arme à la main, l'arme étant prête à lancer un projectile du type indiqué précédemment ;  - the shooter puts himself in position, armed in the hand, the weapon being ready to launch a projectile of the type indicated previously;
- sur ordre du tireur ou sur toute autre forme de commande, la machine procède au lancement d'une cible 1 dans une portion de l'espace. Le lancer peut être configuré de sorte à exposer essentiellement l'une parmi la première ou la deuxième face 3, 4 en vis-à-vis du tireur, mais toute autre inclinaison est possible. Après le lancer de la cible 1 , le tireur cherche à l'atteindre au moyen du projectile. S'il y parvient, grâce à l'invention, un effet visuel est immédiatement produit par l'intermédiaire de la libération du marqueur. En effet, lors de l'impact, le projectile voit sa coque se rompre de sorte à libérer le matériau marqueur qui se répand rapidement de par la dynamique de la cible 1 . Cela s'opère préférentiellement tout en assurant que la cible ne soit pas substantiellement dégradée et notamment pour que l'énergie de l'impact soit plus largement reprise par le projectile que par la cible 1 , au moins dans une limite permettant de rompre le projectile et de ne pas dégrader la cible 1 . Par exemple, au moins les trois quarts de l'énergie de l'impact sont absorbés par le projectile pour favoriser la rupture de la coque ; - On the order of the shooter or on any other form of command, the machine starts launching a target 1 in a portion of the space. The throw can be configured to expose essentially one of the first or second face 3, 4 facing the shooter, but any other inclination is possible. After the throwing of the target 1, the shooter tries to reach it by means of the projectile. If it succeeds, thanks to the invention, a visual effect is immediately produced by means of the release of the marker. Indeed, during the impact, the projectile sees its hull break so as to release the marker material which spreads rapidly by the dynamics of the target 1. This operates preferentially while ensuring that the target is not substantially degraded and in particular for the energy of the impact to be more widely taken up by the projectile than by the target 1, at least within a limit to break the projectile and not to degrade the target 1. For example, at least three-quarters of the energy of the impact is absorbed by the projectile to promote rupture of the shell;
- le marqueur est libéré et se répand sur la cible 1 au niveau de la surface d'impact 8 et/ou dans une portion de l'espace. Dans le cas d'un marqueur du type peinture, c'est essentiellement sur la cible 1 que le marquage sera produit. Dans le cas d'un matériau pulvérulent, le marqueur a tendance à se dissiper sous forme d'un nuage dans une portion tridimensionnelle de l'espace. Dans tous les cas, il est avantageux de mettre en rotation la cible 1 autour de son axe de sorte à ce que lors de l'impact, un effet tangentiel se produise favorisant la répartition du marqueur sur une plus grande surface. D'une certaine manière, lors de l'impact, le point d'impact suit une trajectoire pseudo-cycloïdal ce qui permet de produire cet élargissement de la zone de l'effet visuel.  the marker is released and spreads on the target 1 at the impact surface 8 and / or in a portion of the space. In the case of a marker of the painting type, it is essentially on the target 1 that the marking will be produced. In the case of a powdery material, the marker tends to dissipate as a cloud in a three-dimensional portion of the space. In all cases, it is advantageous to rotate the target 1 about its axis so that during the impact, a tangential effect occurs promoting the distribution of the marker on a larger area. In a certain way, during the impact, the point of impact follows a pseudo-cycloid trajectory which makes it possible to produce this widening of the zone of the visual effect.
L'invention peut être employée pour un exercice au tir dans lequel le tireur tente à plusieurs reprises de toucher la cible 1. Par exemple, la cible 1 est lancée à une hauteur suffisante pour permettre un tir à répétition. Chaque fois que la cible est touchée, le tireur marque un point. Grâce à l'invention, la cible 1 n'est pas altérée lors des impacts et, avantageusement, sa trajectoire n'est pas sensiblement modifiée. De ce fait, on peut par exemple opérer au moins 5 tirs sur une cible 1 lancée. Suivant un mode de réalisation de l'invention, un système comportant plusieurs machines de lancement de préférence alignées est mis en place. Eventuellement, les machines peuvent être coordonnées avec un séquenceur apte à définir l'ordre et les intervalles (par exemple entre 3 et 10 secondes) de tirs des machines. Un schéma de tir est comme suit : chaque machine lance une cible suivant une direction qui lui est spécifique, les lancers s'enchainant dans le temps pour ne pas démarrer avant que la cible du lancer précédent ne soit plus accessible au tireur. Les lancers autorisent jusqu'à 5 possibilités d'impact. Le joueur a donc la faculté de marquer jusqu'à 15 points. Le nombre de tireurs pouvant participer à un concours n'est aucunement limité.  The invention can be used for a fire drill in which the shooter repeatedly tries to hit the target 1. For example, the target 1 is launched at a height sufficient to allow a repetitive shooting. Whenever the target is hit, the shooter scores a point. Thanks to the invention, the target 1 is not altered during the impacts and, advantageously, its trajectory is not substantially modified. Therefore, one can for example operate at least 5 shots on a target 1 launched. According to one embodiment of the invention, a system comprising several preferably aligned launching machines is set up. Optionally, the machines can be coordinated with a sequencer capable of defining the order and the intervals (for example between 3 and 10 seconds) of firing of the machines. A firing pattern is as follows: Each machine launches a target in a direction specific to it, the launches are chained in time to not start before the target of the previous throw is no longer accessible to the shooter. Throws allow up to 5 impact possibilities. The player has the ability to score up to 15 points. The number of fencers who can participate in a contest is in no way limited.
L'invention n'est pas limitée aux modes de réalisation précédemment décrits mais s'étend à tous modes de réalisation conformes à son esprit. REFERENCES The invention is not limited to the previously described embodiments but extends to all embodiments in accordance with his spirit. REFERENCES
1 . Cible 1. Target
2. Tranche  2. Slice
3. Première face  3. First face
4. Deuxième face  4. Second face
5. Couche interne  5. Inner layer
6. Première couche superficielle  6. First layer superficial
7. Deuxième couche superficielle  7. Second superficial layer
8. Surface d'impact  8. Impact surface
9. Bordure  9. Border
10. Revêtement  10. Coating
1 1 . Organe de fixation  1 1. Fixing member
12. Corps de cible  12. Target body
13. Organe de fixation complémentaire 13. Complementary fastener
14. Ceinture 14. Belt
15. Cœur  15. Heart
16. Ame  16. Soul
17. Elargissement  17. Enlargement
18. Aile  18. Wing
19. Machine de lancement  19. Launch machine
20. Plan de lancement  20. Launch plan
21 . Bras  21. Arms
22. Surface d'application périphérique 22. Peripheral application area
23. Châssis 23. Chassis
24. Chargeur  24. Charger
25. Colonne  25. Column
26. Zone de délivrance  26. Issuing area

Claims

REVENDICATIONS
1 . Procédé d'exercice au tir, comprenant une étape de lancement d'une cible (1 ) dans une portion de l'espace, une étape de tir d'un projectile en direction de la cible (1 ) et une étape d'impact du projectile sur la cible (1 ), caractérisé par le fait qu'on utilise un projectile comprenant une coque délimitant un volume intérieur contenant un matériau marqueur et par le fait qu'il comporte une étape de rupture de la coque lors de l'impact du projectile sur la cible (1 ), de sorte à libérer le matériau marqueur. 1. Firing exercise method comprising a step of launching a target (1) in a portion of the space, a firing step of a projectile towards the target (1) and a step of impacting the target projectile on the target (1), characterized in that a projectile comprising a shell delimiting an interior volume containing a marker material and the fact that it comprises a step of rupture of the shell during the impact of the projectile on the target (1), so as to release the marker material.
2. Procédé selon la revendication précédente dans lequel l'étape de lancement comprend une mise en rotation propre de la cible (1 ).  2. Method according to the preceding claim wherein the launching step comprises a self-rotation of the target (1).
3. Procédé selon la revendication précédente dans lequel la vitesse de rotation propre de la cible (1 ) est au moins de 300 tours par minute au moment du lancer.  3. Method according to the preceding claim wherein the own rotational speed of the target (1) is at least 300 rpm at the time of casting.
4. Procédé selon l'une des revendications précédentes dans lequel on utilise une cible (1 ) dont la surface périphérique comporte une tranche (2) joignant une première face (3) et une deuxième face (4) et dans lequel l'étape d'impact est réalisée par contact du projectile sur une surface d'impact (8) formée sur au moins l'une parmi la première face (3) et la deuxième face (4).  4. Method according to one of the preceding claims wherein there is used a target (1) whose peripheral surface comprises a wafer (2) joining a first face (3) and a second face (4) and wherein the step of impact is achieved by contact of the projectile on an impact surface (8) formed on at least one of the first face (3) and the second face (4).
5. Procédé selon la revendication précédente dans lequel la tranche (2) de la cible (1 ) et la surface d'impact (8) sont choisis en des matériaux différents.  5. Method according to the preceding claim wherein the wafer (2) of the target (1) and the impact surface (8) are selected from different materials.
6. Procédé selon la revendication précédente dans lequel le ou les matériaux de la tranche (2) est choisi avec une densité inférieure à la densité du ou des matériaux de la surface d'impact (8).  6. Method according to the preceding claim wherein the material or materials of the wafer (2) is chosen with a density less than the density of the material or materials of the impact surface (8).
7. Procédé selon l'une des 3 revendications précédentes dans lequel la densité du ou des matériaux de la surface d'impact (8) est choisie supérieure à 500 kg/m3. 7. Method according to one of the 3 preceding claims wherein the density of the material or materials of the impact surface (8) is chosen greater than 500 kg / m 3 .
8. Procédé selon l'une des 4 revendications précédentes dans lequel la densité du ou des matériaux de la tranche (2) est choisie inférieure à 275 kg/m3. 8. Method according to one of the 4 preceding claims wherein the density of the material or materials of the wafer (2) is chosen less than 275 kg / m 3 .
9. Procédé selon l'une des cinq revendications précédentes dans lequel on utilise une cible (1 ) comprenant un corps de cible (12) de forme cylindrique dont la surface de révolution forme la tranche (2) et dans laquelle la surface d'impact (8) comprend, sur au moins l'une parmi la première face (3) et la deuxième face (4), une zone en forme de disque.  9. Method according to one of the five preceding claims in which a target (1) is used comprising a cylindrical target body (12) whose surface of revolution forms the wafer (2) and in which the impact surface (8) comprises, on at least one of the first face (3) and the second face (4), a disk-shaped area.
10. Procédé selon la revendication précédente dans lequel le diamètre de la zone en forme de disque est choisi inférieur au diamètre du corps de cible (12). 10. Method according to the preceding claim wherein the diameter of the disk-shaped region is chosen to be smaller than the diameter of the target body (12).
1 1 . Procédé selon l'une des deux revendications précédentes dans lequel on utilise une cible (1 ) dont le corps (12) est en mousse polymère et dans lequel au moins une partie de la surface d'impact (8) est réalisée par réticulation de ladite mousse. 1 1. Method according to one of the two preceding claims, in which a target (1) is used, the body (12) of which is made of polymeric foam and in which at least part of the impact surface (8) is made by crosslinking said foam.
12. Procédé selon l'une des revendications 9 à 10 dans lequel on forme au moins une partie de la surface d'impact (8) par fixation d'un revêtement (10) sur le corps de cible (12).  12. Method according to one of claims 9 to 10 wherein is formed at least a portion of the impact surface (8) by attaching a coating (10) on the target body (12).
13. Procédé selon la revendication précédente dans lequel la fixation est opérée avec au moins un organe de fixation (1 1 ) situé sur une face du revêtement (10) opposée à la face du revêtement (10) formant au moins en partie la surface d'impact (8), et avec au moins un organe de fixation complémentaire (13) formé sur le corps de cible (12).  13. Method according to the preceding claim wherein the fixing is carried out with at least one fastener (1 1) located on a face of the coating (10) opposite the face of the coating (10) forming at least partly the surface of impact (8), and with at least one complementary fastening member (13) formed on the target body (12).
14. Procédé selon l'une des deux revendications précédentes dans lequel le revêtement (10) est choisi sous forme d'une plaque de matériau polymère.  14. Method according to one of the two preceding claims wherein the coating (10) is selected in the form of a plate of polymeric material.
15. Procédé selon l'une des revendications 4 à 8 dans lequel on utilise une cible (1 ) comprenant une ceinture dont une partie de pourtour forme la tranche (2) de la cible (1 ) et entourant un cœur (15) de cible, et dans lequel la paroi externe du cœur (15) de cible forme au moins en partie la surface d'impact (8).  15. Method according to one of claims 4 to 8 wherein a target (1) comprising a belt including a portion of periphery forms the wafer (2) of the target (1) and surrounding a heart (15) target and wherein the outer wall of the target core (15) at least partially forms the impact surface (8).
16. Procédé selon la revendication précédente dans lequel le cœur (15) de cible est choisi tel qu'il comporte une partie de fixation d'une zone de la ceinture (14) opposée à la partie de pourtour.  16. Method according to the preceding claim wherein the heart (15) target is chosen such that it comprises a fastening portion of a zone of the belt (14) opposite the perimeter portion.
17. Procédé selon l'une des deux revendications précédentes dans lequel le cœur (15) de cible est choisi tel qu'il comporte une âme (16) centrale choisie avec une épaisseur inférieure à celle de la partie de fixation.  17. Method according to one of the two preceding claims wherein the core (15) target is chosen such that it comprises a central core (16) chosen with a thickness less than that of the fixing portion.
18. Procédé selon l'une des revendications précédentes dans lequel le module de Young du ou des matériaux de la tranche (2) est choisi inférieur à celui du ou des matériaux de la surface d'impact (8).  18. The method as claimed in one of the preceding claims, in which the Young's modulus of the material or materials of the wafer (2) is chosen to be smaller than that of the material or materials of the impact surface (8).
19. Procédé selon l'une des revendications précédentes dans lequel le module de Young du ou des matériaux de la tranche est choisi inférieur à 0,1 giga Pascal.  19. Method according to one of the preceding claims wherein the Young's modulus of the material or materials of the wafer is chosen less than 0.1 giga Pascal.
20. Procédé selon l'une des revendications 12 ou 13 dans lequel le revêtement est choisi sous forme d'une nappe de matériau élastomère.  20. Method according to one of claims 12 or 13 wherein the coating is chosen in the form of a sheet of elastomeric material.
21 . Procédé selon l'une des revendications 1 à 19 dans lequel le module de Young du ou des matériaux de la surface d'impact (8) est choisi supérieur à 0,8 giga Pascal.  21. Method according to one of claims 1 to 19 wherein the Young's modulus of the material or materials of the impact surface (8) is chosen greater than 0.8 giga Pascal.
22. Procédé selon l'une des revendications précédentes dans lequel le marqueur du projectile est choisi parmi un colorant liquide et une poudre. 22. Method according to one of the preceding claims wherein the marker of the projectile is selected from a liquid dye and a powder.
23. Procédé selon l'une des revendications précédentes dans lequel la coque du projectile est réalisée sous forme d'une coque rigide en matériau polymère ou sous forme d'une coque souple, de préférence en gélatine. 23. Method according to one of the preceding claims wherein the shell of the projectile is made in the form of a rigid shell of polymeric material or in the form of a flexible shell, preferably gelatin.
24. Procédé selon l'une des revendications précédentes dans lequel la coque est réalisée sous forme d'enveloppe sphérique lisse.  24. Method according to one of the preceding claims wherein the shell is formed as a smooth spherical envelope.
25. Système pour l'exercice au tir, comportant une machine de lancement (19) d'une cible (1 ) et un projectile destiné à impacter la cible (1 ), caractérisé par le fait que le projectile comprend une coque délimitant un volume intérieur contenant un matériau marqueur et par le fait l'impact du projectile sur la cible (1 ) est configuré pour provoquer la rupture de la coque, de sorte à libérer le matériau marqueur.  25. System for the practice of shooting, comprising a launching machine (19) of a target (1) and a projectile for impacting the target (1), characterized in that the projectile comprises a shell defining a volume interior containing a marker material and thereby the impact of the projectile on the target (1) is configured to cause the rupture of the shell, so as to release the marker material.
26. Système selon la revendication précédente configuré pour mettre en œuvre le procédé selon l'une des revendications 1 à 24.  26. System according to the preceding claim configured to implement the method according to one of claims 1 to 24.
EP13773259.0A 2012-10-10 2013-10-07 Firing practice method Active EP2906900B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1259668A FR2996633B1 (en) 2012-10-10 2012-10-10 FIRE EXERCISE METHOD
PCT/EP2013/070782 WO2014056822A1 (en) 2012-10-10 2013-10-07 Firing practice method

Publications (2)

Publication Number Publication Date
EP2906900A1 true EP2906900A1 (en) 2015-08-19
EP2906900B1 EP2906900B1 (en) 2016-11-30

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EP13773259.0A Active EP2906900B1 (en) 2012-10-10 2013-10-07 Firing practice method

Country Status (5)

Country Link
US (1) US20160040966A1 (en)
EP (1) EP2906900B1 (en)
CA (1) CA2887626A1 (en)
FR (1) FR2996633B1 (en)
WO (1) WO2014056822A1 (en)

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Publication number Priority date Publication date Assignee Title
US9568287B2 (en) * 2015-07-09 2017-02-14 Jeremy A. Nienke Recoverable and reusable aerial target

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Publication number Priority date Publication date Assignee Title
US4961585A (en) * 1989-07-27 1990-10-09 Crawford Joe T Flying target with marker
US6393992B1 (en) * 1996-11-18 2002-05-28 Jaycor Tactical Systems, Inc. Non-lethal projectile for delivering an inhibiting substance to a living target
US20020125643A1 (en) * 2001-03-08 2002-09-12 Mark Sullivan Advanced target system
US7731612B2 (en) * 2004-06-17 2010-06-08 Martin John C Arrow launched media reservoir
US20110107935A1 (en) * 2009-11-06 2011-05-12 Authement Sr Joseph Photo-luminescent shotgun projectiles
EP2381210A1 (en) * 2010-04-21 2011-10-26 Laporte Holding Air-launchable archery target made from polymeric foam
US20150137453A1 (en) * 2013-11-19 2015-05-21 Eugene Taylor Audible, reusable, illuminated skeet target

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Title
See references of WO2014056822A1 *

Also Published As

Publication number Publication date
US20160040966A1 (en) 2016-02-11
WO2014056822A1 (en) 2014-04-17
FR2996633B1 (en) 2014-11-28
EP2906900B1 (en) 2016-11-30
FR2996633A1 (en) 2014-04-11
CA2887626A1 (en) 2014-04-17

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