Non-lethal projectile

Information

  • Patent Grant
  • 6209461
  • Patent Number
    6,209,461
  • Date Filed
    Tuesday, May 25, 1999
    25 years ago
  • Date Issued
    Tuesday, April 3, 2001
    23 years ago
Abstract
The present invention relates to a non-lethal projectile. The projectile (1) comprises a longitudinal body (5) having internally a longitudinal striker (55) suitable for perforating a container (47) of fluid under pressure in controlled manner, in particular by impact of the projectile (1) on a target. The striker (55) has an internal passage (59) opening to the outside of the body (5) via channels (60) made through a rigid wall (35) secured to the body (5) such that the outlet offered to the fluid under pressure remains disengaged even if the impact is accompanied by the deformation of the container (47). The fluid contained in the container (47) can thus escape and spread over the target even in such a case.
Description




FIELD OF THE INVENTION




The present invention relates to a non-lethal projectile adapted to be projected, in particular fired from a tube in a predetermined longitudinal direction, and to disperse a pressurized fluid in a controlled manner, in particular by impacting on a target in said direction.




BACKGROUND OF THE INVENTION




In the present context “tube” means either a weapon barrel housing the projectile directly until it is fired or a tubular case surrounding the projectile at least locally within the weapon barrel and remaining in the barrel when The projectile is fired.




European Patent Application No. 96400608.4 filed Mar. 22, 1996 by the Applicant describes an embodiment of a projectile of the above kind for dispersing a pressurized incapacitating or marking fluid in which the fluid dispersing means comprise a plurality of transverse orifices in a part of the body housing the container in the immediate proximity of the transverse wall carrying the striker. This prior art projectile is designed to be fired in a particular longitudinal direction from a weapon barrel and to release the pressurized fluid from the container as a result of inertial striking on impact on a target in that direction.




The above solution is not totally satisfactory in that the impact energy can be sufficient to cause not only striking (i.e. perforation) of the container by the striker, but also crushing of the container against the transverse wall carrying the striker, with the effect of crimping the container inside the body and/or to the striker in the immediate proximity of the aforementioned transverse wall, i.e. in the area in which the orifices are located.




This causes at least partial blocking of the orifices, making the projectile less effective. It is important for the fluid not only to exit the projectile but also to exit it in an extremely short time period, i.e. before the projectile falls to the ground after striking its target.




Also known, from FIG. 7 of British patent No. 1 354 307 is a projectile comprising, inside a body, a container which, on impact of the projectile on a target in a determined longitudinal direction, breaks against a striker so that its content escapes via lateral vents formed through the wall of the projectile body around the container, i.e. on the same side as the latter of a wall carrying the striker, as in the case of the projectile described in the above-mentioned European patent application.




Nevertheless, the container described in British patent No. 1 354 307 is not suitable for being perforated, but breaks into numerous pieces when it hits the striker, thereby making it necessary to provide firstly a cushion behind the container, in particular to protect it while the projectile is being fired, and secondly grids inside the vents to prevent pieces of the container from escaping together with the content thereof, since that would run the risk of injuring people in the vicinity.




In contrast, the present invention relates to projectiles in which the container is suitable for being perforated and opens on being perforated by means of the striker, as taught in the above-mentioned European patent application.




Also known, from U.S. Pat. No. 1,671,364, is a projectile having a tube that dips permanently into a volume containing a fluid to be expelled and communicating with channels formed in a rigid wall of the projectile.




The volume described in that document is no more a container suitable for being perforated than is the container described in the above-mentioned British patent, and the volume does not contain a fluid under pressure which is released by such a container being perforated. Release is performed by the effect of the volume telescoping and disengaging stoppers that initially closed a T-shaped end of the tube remote from the rigid wall in which the outlet channels are provided.




Consequently, neither British patent No. 1 354 307 nor U.S. Pat. No. 1,671,364 relates to a projectile implementing a container suitable for being perforated by the effect of a striker, i.e. of the type described in the above-mentioned European patent application. In particular, neither of those documents teaches means for remedying the above-mentioned drawback of the projectile described in said European patent application.




SUMMARY OF THE INVENTION




The present invention aims to remedy that drawback of the projectiles described in European Patent Application No. 9640068.4, and to this end it proposes a projectile of the type indicated in the preamble characterized in that the fluid dispersing means include a blind longitudinal passage through the striker open at the end towards the container and closed inside said wall, and a plurality of transverse passages in said wall radiating from said passage and discharging externally of the body.




The skilled person will readily see that under these conditions any crushing of the container against the transverse wall carrying the striker has no effect on the exit of the pressurized fluid and that it is therefore certain that the projectile in accordance with the invention will release the fluid that it contains in a very short time period after impact on its target if striking is caused by inertia on impact.




An embodiment of the fluid dispersing means of the above kind naturally accommodates any mode of striking the container, i.e. the use of any phenomenon able to bring about longitudinal movement towards each other of the container and the striker under conditions such as to cause the striker to perforate the container, in particular on impact on a target and given that the impact energy is intentionally limited to assure the non-lethal character of the projectile.




Striking can involve longitudinal movement of the striker relative to the transverse wall that carries it but it is preferable for the striker to be attached to that wall. Striking can then result from longitudinal crushing of the body, in which case the means for enabling or causing longitudinal movement towards each other of the container and the striker and perforation of the container by the striker include a longitudinally compressible area of the body between the container and the transverse wall in the longitudinal direction or such crushing is complemented or replaced by inertial sliding of the container inside the body towards the striker, in which case the means for enabling or causing longitudinal movement towards each other of the container and the striker and perforation of the container by the striker include mounting the container so as to slide longitudinally relative to the body, the striker and the wall being in front of the container.




The above two designs of the means for enabling or causing longitudinal movement towards each other of the container and the striker and perforation of the container by the striker can be combined and different means can be chosen, for example pyrotechnic means initiated by the impact or by firing the projectile, with a time-delay in the latter case, these examples being in no way limiting on the invention. Striking by longitudinal crushing of the body is associated with striking caused by the inertia of the body itself upon impact on a target in a particular longitudinal direction while striking by sliding of the container towards the striker is compatible with any mode of striking, in particular one relying on the inertia of the container on impact on a target in a particular longitudinal direction or on pyrotechnic or mechanical-pyrotechnic means that generally do not require an impact to supply the striking energy.




The skilled person will readily see that applications of the present invention are not limited to projectiles designed to be fired from a tube in a particular longitudinal direction and to release the pressurized fluid from the container on impact on a target in that direction and that projectiles can be made in accordance with the present invention that are designed to be projected by other means, in particular to be launched by hand in the manner of hand grenades. In such cases striking preferably relies on mounting the container to slide longitudinally relative to the body towards the striker but is advantageously achieved by means other than inertia, in particular by pyrotechnic means or mechanical-pyrotechnic means known in themselves and actuated intentionally by a user prior to launching to cause release of a gas causing the container to slide towards the striker and to be perforated by it, generally with a time-delay relative to such intentional actuation. The concepts of longitudinal and a particular longitudinal direction and derived concepts such as transverse, front and rear, nose and tail of the projectile, refer to the direction of movement of the container within the body towards the striker.




If striking relies on mounting the container to slide longitudinally relative to the body and in the case of a projectile designed to be fired from a weapon barrel the projectile in accordance with the invention advantageously includes locking means which immobilize the container relative to the body while the projectile is inside the barrel and release the container automatically so that it can slide longitudinally relative to the body when the projectile exits the barrel.




In one particularly simple but effective embodiment of such locking means the body is in the form of a wall of an elastically deformable material between the nose and the tail and has a smooth inside face to guide the container as it slides longitudinally in the body and a smooth outside face to guide the projectile as it slides longitudinally in the tube, the outside face having a localized protuberance adapted to be depressed to form a projection on the inside face when the projectile is engaged in the tube and to project from the outside face, eliminating the projection on the inside face, when the projectile has left the tube and the container has a localized transverse depression facing this protuberance when the container is juxtaposed to the striker.




The localized depression in the container can advantageously be in the form of a transverse annular groove and the protuberance on the wall of the body can then be in the form of a transverse bead joined to that wall without any discontinuity. The wall of the body of the projectile can incorporate at least one elastically flexible tongue having one end attached to the wall and offset relative to the protuberance and a free end carrying the protuberance and to which the protuberance is attached: there is preferably a plurality of tongues equi-angularly distributed around the wall of the body and the tongues are advantageously longitudinally oriented.




In all its embodiments the aforementioned protuberance not only prevents the container from sliding inside the tube, which could lead to accidental striking, but also contributes to retaining the projectile inside the tube in that it is urged elastically towards the exterior of the body and presses against the inside of the tube. In a particular instance where the protuberance is in the form of a transverse bead joined without discontinuity to the wall of the body, the protuberance further provides a seal between the projectile and the tube so that the projectile is fired by gas pressure developed inside the tube behind the projectile, for example the pressure of a gas such as compressed air introduced into the tube or the pressure of gases produced by combustion of a pyrotechnic charge.




In a manner that is widely known in the field of projectiles, when the projectile in accordance with the invention is designed to be fired from a weapon barrel in a particular longitudinal direction it advantageously has stabilizing fins attached to the tail end of the body and adapted to occupy a retracted position in which they are retained in an elastically stressed manner by the barrel when the projectile is engaged therein, their elasticity deploying them when the projectile has left the barrel.




The fins are advantageously made from an elastically deformable material and have one end attached to the body and a free end tending by virtue of its elasticity to spread transversely outwards relative to the end attached to the body, which is particularly simple, economic and reliable, and can advantageously be shaped to produce a whistling sound when the projectile is in flight which indicates firing and imminent impact.




The projectile in accordance with the invention can further include arrangements known in themselves such as a nose cone attached to its nose and made from an elastically compressible material, for example a material with a Shore A hardness in the range approximately 10 to approximately 30, preferably in the range 12 to 15, for example silicone.











BRIEF DESCRIPTION OF THE DRAWINGS




Further features and advantages of a projectile in accordance with the invention emerge from the following description given by way of non-limiting example and from the accompanying drawings that form an integral part of the description.





FIG. 1

shows a projectile in accordance with the invention after it has left the tube but before it has impacted on a target, half in elevation and half in section on a half-plane defined by a longitudinal axis of the projectile.





FIG. 2

shows the detail II from

FIG. 1

to a larger scale.





FIG. 3

shows the same detail when the projectile is still inside the tube.





FIG. 4

is a view similar to that of

FIG. 1

showing the projectile after impact on its target, two different behaviors of the projectile on impact being shown in respective halves of this figure.





FIGS. 5 through 8

are views respectively corresponding to those of

FIGS. 1 through 4

and show a different embodiment of the projectile,

FIG. 6

showing a detail VI from FIG.


5


.





FIGS. 9 and 10

are sectional views analogous to those of

FIGS. 1

,


4


,


5


and


8


of two preferred embodiments of a component combining the striker and the transverse wall carrying it.





FIGS. 11 and 12

are perspective view of these two preferred embodiments.





FIGS. 13 and 14

are views corresponding to those of

FIGS. 4 and 8

but localized to the striker and the transverse wall carrying it and showing the co-operation of the container with the aforementioned two preferred embodiments after it is perforated following impact of the projectile on its target.











DETAILED DESCRIPTION OF THE INVENTION




The respective embodiments of a projectile in accordance with the invention shown in

FIGS. 1 through 4

and in

FIGS. 5 through 8

are highly similar and their common parts are described first and are identified by the same reference numbers in all the figures. The description initially refers to all the figures.




The projectile


1


has a longitudinal axis


2


which, before the projectile is fired, lies concentric with a tube, for example a weapon barrel


3


, in which it is initially inserted and from which it emerges in a predetermined longitudinal direction


4


when fired. In the present context longitudinal and transverse are relative to the axis


2


, and front and rear are relative to the firing direction


4


.




The projectile


1


has a body


5


defined in the example shown by:




a longitudinal tubular wall


6


defined by circular cylindrical inside and outside faces


7


and


8


which are concentric with the axis


2


and smooth, with one exception to be described later, and by two plane circular transverse faces concentric with the axis


2


, namely a front face


9


and a rear face


10


, respectively connecting the faces


7


and


8


at the front and at the rear of the body


5


;




a nose


11


defining a front end of the body


5


and fixed to the wall


6


, for example by nesting and gluing it in an area of its inside face


7


directly adjoining the front face


9


, the nose


11


being generally circular and concentric with the axis


2


apart from exceptions described below; and




a tail


12


defining a rear end of the body


5


and fixed to the wall


6


, for example by nesting and gluing it in an area of its inside face


7


directly adjoining its rear face


10


, the tail


12


having a generally circular tubular shape concentric with the axis


2


.




The tubular wall


6


is made from an elastically flexible material such as a plastics material from which the tail


12


can also be made.




The tail


12


has a wall


13


delimited by circular frustoconical outside and inside faces


14


and


15


which are concentric with the axis


2


and decrease in size towards the rear. Towards the front each of the faces


14


and


15


is joined to a respective circular cylindrical face concentric with the axis


2


, namely an outside face


16


having the same diameter as the outside face


8


of the wall


6


and an inside face


17


having a smaller diameter than the inside face


7


of the wall


6


. Towards the front, the outside face


16


is joined to a plane circular annular shoulder


18


concentric with the axis


2


, facing towards the front and abutting towards the front against the rear face


10


of the wall


6


. The shoulder


18


connects the outside face


16


to another outside face


19


of the tail


12


. The outside face


19


is a circular cylinder concentric with the axis


2


and substantially the same diameter as the inside face


7


of the wall


6


so as to espouse an area of the inside face


7


directly adjacent the rear face


10


of the wall


6


. The inside and outside faces


17


and


19


of the tail


12


therefore define, relative to the wall


13


, a tubular nesting rim


20


inside the wall


6


. Towards the front inside and outside faces


17


and


19


of the rim


20


are joined by a plane circular annular shoulder


81


concentric with the axis


2


and delimiting the rim


20


towards the front. The longitudinal distance between the shoulders


18


and


81


is much less than the longitudinal dimension of the wall


6


between its front and rear faces


9


and


10


.




Towards the rear, the outside and inside faces


14


and


15


of the wall


13


are joined to a respective circular cylindrical face concentric with the axis


2


, namely an outside face


22


and an inside face


21


joined at the rear by a plane circular annular shoulder


23


concentric with the axis


2


and facing towards the rear, delimiting a tubular end-piece


24


.




The tubular end-piece


24


is used to fix to the body


5


a tail fin assembly


25


adapted to spin the projectile


1


about the axis


2


after it is fired in order to stabilize its trajectory.




The tail fin assembly


25


is advantageously made by pressing and heat-forming a sheet of elastically flexible plastics material to define:




a flat fixing base


26


oriented transversely to and concentric with the axis


2


and having a central longitudinal hole


27


through it delimited by a circular cylindrical inside face


28


concentric with the axis


2


and substantially the same diameter as the inside face


21


of the end-piece


24


and an outside periphery


29


in the form of a regular polygon, to be more precise one with four sides in the example shown, inscribed within a circle having a diameter less than that of the outside face


8


of the wall


6


, referred to the axis


2


; the central hole


27


and the inside face


21


of the end-piece


24


, which are appropriately screwthreaded, receive, from the rear, a bolt coaxial


30


for clamping the base


26


flat against the shoulder


23


of the end-piece


24


in order to attach the tail fin assembly


25


to the body


5


; and




the same number of elastically flexible fins


31


as there are sides on the polygon defined by the periphery


29


of the base


26


, namely four fins


31


in the example shown, each fin having a front end


82


attached to the base


26


along one side of the polygon and a free end


83


at the rear which, by virtue of the elasticity of the material from which the tail fin assembly


25


is made, tends to spread transversely outwards relative to the front end


82


, in other words to a greater distance from the axis


2


than the front end, with the result that the tail fin assembly


25


has a rearwardly flared shape with a diameter greater than that of the outside face


8


of the wall


6


referred to the axis


2


. However, fins


31


can be folded towards that axis to a diameter corresponding to that of the outside face


8


of the wall


6


, which is the configuration of the tail fin assembly


25


when the projectile


1


is engaged in the weapon barrel


3


; by virtue of their elasticity the fins


31


automatically return to the rearwardly flared position of the tail fin assembly


25


as soon as the projectile


1


has left the weapon barrel


3


when it is fired.




The fins


31


are helically shaped to spin the projectile


1


about the axis


2


during its flight between the weapon barrel


3


and its impact on the target in order to stabilize its trajectory. For example, each fin


31


has a first plane flat


32


the shape of a right-angle trapezium the side of which perpendicular to the bases coincides with a side of the periphery


29


of the base


26


to constitute the front end


82


of the fin


31


and the longer base of which extends to the free end


83


thereof, so that the first flat


32


has the oblique side of the trapezium towards the rear, defining a rectilinear fold


33


in the fin


31


, and a second plane flat


34


the shape of a right-angle triangle the hypotenuse of which coincides with the fold


33


, the longer side adjoining the right angle extending the shorter base of the right-angle trapezium defined by the first flat


32


at an angle to the shorter base so that the flat


34


is offset outwards relative to the flat


32


and the shorter side adjoining the right angle defining the free end


83


of the fin


31


.




The choice of the material for the tail fin assembly


25


and the conformation of the fins


31


will be advantageously made, in the field on the normal aptitude of the skilled person, such that the flight of the projectile


1


is accompanied by a whistling noise.




The nose


11


includes a flat rigid transverse wall


35


, for example a metal wall, delimited in the direction away from the axis


2


by an outside face


36


having a diameter substantially equal to that of the inside face


7


of the wall


6


inside which the wall


35


therefore nests with intimate mutual contact between the faces


36


and


7


in the immediate proximity of the front face


9


of the wall


6


.




Towards the front, the outside face


36


is joined to a plane circular annular shoulder


37


concentric with the axis


2


, the shoulder


37


facing towards the rear and bearing flat against the front face


9


of the wall


6


to limit entry of the wall


35


inside the wall


6


. In the direction away from the axis


2


the shoulder


37


is itself joined to a circular cylindrical outside face


38


concentric with the axis


2


and having the same diameter as the outside face


8


of the wall


6


, which the face


38


extends towards the front with no apparent discontinuity. In the direction away from the axis


2


the outside face


38


delimits a circular annular rim


39


concentric with the axis


2


, in one piece with the wall


35


and projecting towards the front. In the direction towards the axis


2


the rim


39


is delimited by a circular cylindrical inside face


40


concentric with the axis


2


; towards the front it is delimited by a plane circular annular face


41


concentric with the axis


2


and which is joined to the outside face


38


by a rounded edge (no reference number) and to the inside face


40


by a circular annular flange


42


concentric with the axis


2


and projecting towards it relative to the inside face


40


in an area at the front end of that face. Towards the rear the inside face


40


of the rim


39


is joined to a flat front face


43


of the wall


35


which is transverse to the axis, to be more precise in the form of a disc perpendicular to and concentric with the axis


2


; the face


43


is coplanar with the shoulder


37


, for example.




The face


43


, the face


40


and the flange


42


therefore define immediately in front of the wall


35


a cavity


44


to receive a nose cone


45


and to immobilize it, for example by crimping it by means of the flange


42


and gluing it; the nose cone is circular, concentric with the axis


2


and designed to withstand impact with the target and to this end is made from a material having the elasticity of rubber, for example silicone having a Shore A hardness in the range 10 to 30, preferably in the range 12 to 15, although this example is in no way limiting on the invention. To this end the nose cone


45


has a hemispherical shape projecting towards the front relative to the front face


41


of the rim


39


, the center of this hemisphere (no reference number) being located at the intersection of the axis


2


with a geometrical plane defined by the rim


41


and, projecting rearwardly into the cavity


44


, a cylindrical tenon prestressed in compression inside the flange


42


to achieve a crimping effect and glued flat against the front face


43


of the wall


35


, these examples of its fixing being in no way limiting on the invention.




Towards the rear, the wall


35


is delimited by a plane transverse face


46


parallel to the face


43


and in the shape of a circular annulus concentric with the axis


2


. In the direction away from the latter axis the face


46


is joined to the face


36


, the distance between the faces


43


and


46


also defining the longitudinal direction of the face


36


and consequently the depth to which the wall


35


is pressed inside the wall


6


, which distance is small in comparison to the longitudinal dimension of that wall between its front and rear faces


9


and


10


so that the longitudinal distance between the face


46


of the wall


35


and the shoulder


81


of the tail


12


essentially constitutes the free longitudinal dimension of the wall


6


.




A sealed container


47


of a pressurized fluid, in particular an incapacitating fluid or a marking fluid, to be dispersed by the projectile


1


after its impact on a target in the direction


4


is mounted to slide longitudinally inside the wall


6


, guided by the inside face


7


thereof over this longitudinal distance.




The shape of the container


47


is such that it can co-operate either with a slide attached to the container


47


and sliding longitudinally against the inside face


7


of the wall


6


, in a manner that is not shown but will be obvious to the skilled person, the inside face


7


of the wall o guiding this longitudinal relative sliding, or directly with the inside face


7


of the wall


6


, as in the example shown in which the container


47


is in the form of an aerosol cartridge having a circular tubular lateral wall


48


concentric with the axis


2


and essentially delimited in the direction away from that axis by a circular cylindrical outside face


49


concentric with that axis and having a diameter substantially identical to that of the inside face


7


of the wall


6


so that sliding contact is established between the faces


49


and


7


to guide fins relative longitudinal sliding. Towards the front the wall


48


is joined to (or advantageously made in one piece with) a flat end wall


50


perpendicular to the axis


4


and delimited towards the front by a plane face


51


in the form of a disc concentric with the axis


2


and in the direction away from the axis


2


joined to the face


49


by a rounded edge. Towards the rear the wall


48


is firmly and sealingly crimped to a filler valve mechanism


52


disposed on the axis


2


and facing towards the rear, the crimping producing to the rear of the outside face


49


a plane circular annular shoulder


53


concentric with the axis


2


and facing towards the rear. Nearer this shoulder


53


than the front face


51


the wall


48


is locally deformed towards the axis


2


so as to form inside the container


47


a rib limiting penetration of the valve mechanism


52


, which will be familiar to the skilled person, and this deformation creates in the outside face


49


of the wall


48


a depression in the form of a circular annular groove


54


concentric with the axis


2


and nearer the shoulder


53


than the front face


51


.




The longitudinal distance between the shoulder


53


and the front face


51


is less than the longitudinal distance between the shoulder


81


and the rear face


46


of the wall


35


, with the result that the container


47


can occupy the position shown in

FIGS. 1 and 2

inside the body


5


and the projectile


1


in which the shoulder


53


bears rearwardly on the shoulder


81


of the tail


12


, the valve mechanism


52


being freely received in a coaxial arrangement inside the tail, and in which its front face


51


is spaced longitudinally from the rear face


46


of the wall


35


, which corresponds to the position that the container


47


occupies inside the body


5


of the projectile


1


before it is fired and in flight after it is fired and until impact occurs.




For such impact to perforate the end wall


50


of the container


47


, i.e. to release the fluid that it contains, the rear face


46


of the wall


35


has a striker


55


on its rear face


46


in the form of a hollow longitudinal needle projecting towards the rear along the axis


2


, the needle being beveled towards the rear and having a longitudinal dimension parallel to the face


46


substantially equal to the difference between the longitudinal distance between the shoulder


81


and the face


46


and the distance between the shoulder


53


and the face


51


; as a result, in the position shown in

FIGS. 1 and 2

, i.e. in the position prior to impact, the striker


35


is brought into contact with the front face


51


of the container


47


with its shoulder


53


resting on the shoulder


81


of the tail


12


, as yet without any force.




The striker


55


is advantageously made in one piece with the wall


35


and is delimited in the direction away from the axis


2


by a circular cylindrical outside face


56


concentric with that axis and having a diameter significantly less than that of the inside face


7


of the wall


6


. The outside face


56


is joined towards the front to the rear face


46


of the wall


35


and towards the rear to a plane annular face


57


which is inclined to the axis


2


, for example at 45°, and faces downwards, which defines for the striker


55


a beveled free rear end and connects the outside face


56


to a circular cylindrical inside face


58


concentric with the axis


2


and delimiting inside the striker


55


a longitudinal passage


59


open towards the rear inside the beveled face


57


and extending towards the front as far as the inside of the wall


35


, where it is closed at the front. However, inside the wall


35


the passage


59


discharges into a plurality of passages


60


, of which there are eight in the example shown, and which radiate from it, radially relative to the axis


2


, as far as the outside face


36


of the wall


35


onto which they open. Each passage


60


is defined by a circular cylindrical inside face


61


concentric with a respective axis


62


perpendicular to the axis


2


, for example, the various axes


62


being equi-angularly distributed around that axis and the respective diameters of the inside faces


61


being equal to each other but less than the diameter of the inside face


58


of the striker


55


. The wall


6


has a hole


63


through it facing and coaxial with each of the passages


60


and delimited by a circular cylindrical inside face


64


concentric with the respective axis


62


and having a diameter identical to that of the inside face


61


of a passage


60


so that the passage


59


, the passages


60


and the holes


63


establish communication between the outside of the body


5


and a sealed cavity


65


defined by the walls


6


and


35


and the tail


12


and in which the container


47


is housed. Naturally other arrangements of the passages


60


in the wall


35


and other numbers of passages can be chosen without departing from the scope of the invention.




Accordingly, when the projectile


1


impacts on its target


66


in the direction


4


after leaving a weapon barrel, as shown in

FIG. 4

, because of its inertia the container


47


tends to continue to move forwards inside the wall


6


, which is immobilized in this direction by the target


66


, and bears with a high force towards the front on the striker


55


which perforates the end wall


50


. This frees the container


47


to slide towards the front relative to the wall


6


with the result that the container


47


moves forwards in the body


1


until the face


51


of its end wall


50


is pressed flat against the rear face


46


of the wall


35


, as shown in FIG.


4


. The pressurized fluid


68


initially enclosed in the container


57


escapes from it through the perforation


67


produced in this way in the end wall


50


, flowing towards the front through the longitudinal passage


59


in the striker


55


and then in the centrifugal direction relative to the axis


2


through each of the passages


60


and the holes


63


until it escapes transversely from the body


5


of the projectile


1


to spread over the target


66


.




This process, relying exclusively on sliding of the container


47


towards the front inside the body


5


, is shown in the right-hand half of FIG.


4


.




The left-hand half of the figure shows a different embodiment of the projectile in which the above effect is complemented or replaced by longitudinal crushing of the wall


6


on impact.




Longitudinal compression of the wall


6


can be encouraged at least in an area longitudinally between the container


47


and the transverse wall


35


, for example as shown in the left-hand half of

FIG. 1

, by making longitudinal cuts


69


part-way through the outside face


8


of the wall


6


and localized immediately to the rear of the rear face


46


of the wall


35


, the cuts having a longitudinal dimension preferably corresponding to approximately twice the longitudinal distance between the front face


51


of the container


47


and the rear face


46


of the wall


35


when, as shown in the right-hand half of

FIG. 1

, the front face


51


bears towards the front against the striker


55


with no force and without causing perforation. On impact, and as shown in the left-hand half of

FIG. 4

, the cuts


69


open and allow the formation in the wall


6


of folds


70


on the outside face


8


of the wall


6


projecting away from the axis


2


. This is accompanied by apparent shortening of the wall


6


between the shoulder


81


and rear face


46


of the wall


35


, forcing the end wall


50


of the container


47


against the striker


55


, which perforates it. The formation of the outward folds


70


prevents the presence of the container


47


inside the wall


6


impeding the apparent shortening of the wall


6


and impeding longitudinal sliding of the container


47


inside the wall


6


when the effects of apparent shortening of that wall and of sliding of the container


47


towards the front inside it combine to cause the striker


55


to perforate the end wall


50


. In all cases the arrangement of the passage


59


through the striker


55


, of the passages


60


inside the wall


35


and of the holes


63


facing the passages


60


prevents any impediment to the exit of the fluid initially contained in the container


47


.




Because of the high ductility generally evidenced by the materials, such as aluminum or aluminum-based alloys, from which the walls of the aerosol cartridges preferably used for the container


47


are made, imperfect tearing of the end wall


50


of the container


47


around the perforation


67


can occur, in the sense that the tearing produces in the end wall


50


a tongue that remains attached to the rest of the end wall and is pressed against the annular face


57


on which the passage


59


discharges longitudinally towards the rear, which blocks the passage


59


and consequently prevents the fluid reaching the passages


60


and the holes


63


.




This risk can be overcome or eliminated by shaping the striker


55


differently, for example as in a variant shown in

FIGS. 9

,


11


,


13


or a variant shown in

FIGS. 10

,


12


,


14


, it being understood that the other components of the projectile can be the same as in either of the embodiments described above.

FIGS. 9 through 14

therefore show, identified by the same reference numbers as used in

FIGS. 1 through 8

, various components identical to components described with reference to those figures with the exception of localized differences that will now be described.




Referring at first to

FIGS. 9

,


11


,


13


there is shown a variant of the striker


55


that differs from the embodiment thereof previously described only in that it has at least one transverse orifice through it, extending between its inside and outside faces


58


and


56


and therefore opening into the passage


59


and into the body


5


to the rear of the wall


35


, to be more precise at a longitudinal distance from the rear face


46


of that wall at least equal to and preferably greater than the thickness of the end wall


50


.




In the non-limiting example shown there are three such orifices


85


,


86


,


87


each of which is oriented along a respective axis perpendicular to the axis


2


and has a circular cylindrical periphery concentric with the respective axis and a diameter that is as large as possible within limits compatible with the mechanical strength of the striker


55


so as to offer to the fluid a cumulative flow cross-section that is as close as possible to that of the passage


59


.




To be more precise, in the example shown in

FIGS. 9 and 13

in which the annular face


57


is oriented perpendicularly to the section plane, the orifice


85


is on an axis


88


in that plane and intersects the axis


2


perpendicularly where that axis intersects the geometrical plane (no reference number) of the face


57


; the orifices


86


and


87


have a common axis


89


perpendicular to the plane of

FIGS. 9 and 13

and intersecting the axis


2


perpendicularly between the intersection of the axis


88


with the axis


2


and the rear face


46


of the wall


35


; they have the same diameter, which is less than that of the orifice.




Accordingly, even if striking the end wall


50


upon impact of the projectile


1


on its target produces a tongue


84


from the end wall


50


that is pressed against the face


57


and therefore blocks the passage


59


towards the rear, as shown in

FIG. 13

, the latter communicates with the interior of the container


47


via the orifices


85


,


86


,


87


which are to the rear of the end wall


50


and so enable the fluid in the container


47


to escape from it and exit the projectile


1


via the passage


50


, the passages


60


and the holes


63


.




Naturally, the scope of the invention would not be exceeded by choosing other arrangements to preserve communication between the inside of the container


47


after it is perforated and the passage


59


, even if a tongue


84


formed from the material of the end wall


50


should block it towards the rear.




Nor would the scope of the present invention be exceeded by conforming the striker


55


to prevent the formation of any such tongue


84


or at least blocking of the passage


59


thereby, and a variant of the striker


55


with this aim in view will now be described with reference to

FIGS. 10

,


12


,


14


. The skilled person will readily realize that, although this variant is described independently of that shown in

FIGS. 9

,


11


,


13


, the two variants could easily be combined.




In the variant shown in

FIGS. 10

,


12


,


14


the striker


55


differs from that described with reference to

FIGS. 1 through 8

only in that its free end at the rear is hollowed out by a step


90


offset towards the front relative to its annular face


57


in the area thereof nearest the wall


35


and opens longitudinally towards the rear in this area and transversely onto the inside and outside faces


58


and


56


.




To be more precise, in the example shown the annular face


57


has a localized interruption


91


in its area nearest the wall


35


, symmetrical about a plane perpendicular to the annular face


57


and including the axis


2


, namely the plane of

FIG. 11

, and the step


90


is delimited by two plane longitudinal faces


92


,


93


symmetrical to each other about that plane and joined towards the rear to the annular face


57


on respective opposite sides of the interruption


91


therein and by a plane transverse face


94


facing towards the rear and connecting the two longitudinal faces


92


,


93


together in front of the annular face


57


. However, the transverse face


94


is preferably at a longitudinal distance to the rear of the face


46


of the partition


35


greater than the thickness of the end wall


50


of the container


47


.




The two longitudinal faces


92


,


93


are in a common plane (no reference number) parallel to the axis


2


and perpendicular to the plane of

FIG. 11

, for example. As shown here, the plane of the faces


92


,


93


is preferably on the same side of the axis


2


as the area of the annular face


57


nearest the wall


35


so that the interruption


91


in the annular face


57


, and with it the step


90


, extends over less than half the periphery of the annular face


57


, for example over 120° referred to the axis


2


, this value being given purely by way of non-limiting example.




The skilled person will readily understand that other shapes can be adopted for the step


90


without departing from the scope of the invention.




When, as the projectile impacts on its target, the end wall


50


of the container


47


moves forwards, towards the wall


35


, it comes into contact with the striker


55


first by means of the area of the beveled face


57


at the greatest distance from the wall


35


, what perforates it and can lead to the progressive formation of a tongue


84


as the end wall


50


comes into contact with areas of the face


57


progressively closer to the wall


35


; the tongue


84


tends to remain pressed against the face


57


in an oblique orientation relative to the axis


2


. When the end wall


50


reaches the interruption


91


in the face


57


it crosses the step


90


, the longitudinal faces


92


,


93


and then the transverse face


94


of which straighten the tongue


84


, in such away as to tend to orient it parallel to the axis


2


before the end wall


50


abuts towards the front against the face


46


of the wall


35


, as shown in

FIG. 14

; when the container


47


stops against the face


46


of the wall


35


any tongue


84


that may have been formed from its end wall


50


is therefore oriented so that there is no risk of it blocking the mouth of the passage


59


of the striker


55


on the annular face


57


, i.e. it cannot in any way impede exit of the fluid initially contained in the container


47


via the passage


59


, the passages


60


and the holes


63


.




To prevent accidental perforation of the container before impact on a target


66


, and in particular during storage of the projectile, during loading of the weapon (not shown) and when the weapon is being handled, locking means are preferably provided to immobilize the container


47


relative to the body


5


while the projectile


1


is inside the weapon barrel


3


and to release the container


47


automatically so that it can slide longitudinally relative to the body


3


when the projectile


1


leaves the weapon barrel


3


.

FIGS. 1 through 4

show a first embodiment of the locking means and

FIGS. 5 through 7

show a second embodiment and it is to be understood that these embodiments are also compatible with the variants of the striker shown in

FIGS. 8 through 14

.




Refer firstly to

FIGS. 1 through 4

, which show the locking means in the form of a circular annular transverse bead


71


concentric with the axis


2


, projecting on the outside face


8


of the wall


6


of the body


5


in an area transversely facing the groove


54


and forming a depression in the outside face


49


of the wall


48


of the container


47


when the shoulder


53


bears towards the rear on the shoulder


81


of the tail


12


of the body


5


.




The bead


71


is continuous, joined with no discontinuity to the wall


6


and advantageously made in one piece with that wall. When, as shown in

FIG. 3

, the projectile


1


is inserted into the weapon barrel


3


, which has a circular cylindrical inside face


72


concentric with an axis coincident with the axis


2


and a diameter substantially identical to that of the outside face of the wall


6


in order to co-operate with the outside face


8


to guide the body


5


as it slides longitudinally in the weapon barrel


3


when fired, the bead


71


bears on the inside face


72


which compresses it towards the axis


2


which causes at least partly elastic deformation, and where necessary slightly plastic deformation, of the wall


6


in the direction towards the axis


2


. This forms on the inside face


7


of the wall


6


a circular annular bead


73


concentric with the axis


2


and projecting towards that axis relative to the inside face


7


of the wall


6


, i.e. entering the groove


54


to immobilize the container


57


relative to the wall


6


in the position with the shoulder


53


bearing on the shoulder


21


.




The bead


71


, which is stressed against the inside face


72


of the weapon barrel


3


because of the elasticity of the material of which the wall


6


is made, retains the projectile


1


because of friction between the inside face


72


, on the one hand, and a seal between the projectile


1


and the face


72


, on the other hand, in a manner that is particularly advantageous when, as is frequently the case, the projectile


1


is fired by accumulating pressurized gas between it and a bolt (not shown) closing the rear end of the barrel


3


, whether by introducing a pressurized gas or by generating a pressurized gas, for example by combustion of a suitable pyrotechnic substance.




When the projectile has left the weapon barrel


3


, as shown in

FIGS. 1

,


2


,


4


, the elasticity of the wall


6


causes the bead


71


, which has been relieved of the pressure previously applied to it by the inside face


72


, to return to its original configuration, i.e. projecting on the outside face


8


of the wall


6


, which eliminates the bead


73


projecting on its inside face


7


and allows the container


47


to slide forwards inside the wall


6


.




Referring now to

FIGS. 5 through 8

, the bead


71


is dispensed with but appropriate cuts form elastically flexible tongues


74


in the wall


6


. There are eight such tongues, for example, oriented longitudinally and equip-angularly distributed around the axis


2


, although other arrangements and other numbers of tongues can be chosen without departing from the scope of the invention.




Each tongue


74


, which is therefore in one piece with the wall


6


, has one end


75


, here the front end, attached to the remainder of the wall


6


and a free end


76


, here the rear end, carrying and having fastened to it, for example in one piece with it, a protuberance


77


projecting away from the axis


2


on the outside face


8


of the wall


6


when, as shown in

FIGS. 5

,


6


,


8


, the projectile


1


has left the weapon barrel


3


. Because of its elasticity the tongue


74


tends to retain a shape in which the corresponding part of the inside and outside faces


7


and


8


remains on the same respective geometrical cylinder as the remainder of the peripheral wall respectively inside or outside the wall


6


.




On the other hand, when the projectile


1


is inside the weapon barrel


3


, as shown in

FIG. 7

, the inside face


72


of the barrel bearing on the respective protuberance


77


eliminates the projection that the latter constitutes relative to the outside face


8


of the wall


6


, i.e. it causes each tongue


74


to flex towards the axis


2


at the position of the protuberance


77


, with the result that the free end


76


of each tongue


74


forms a projection towards the axis


2


on the inside face


7


of the wall


6


. Because the protuberances


77


have exactly the same location as the bead


71


, i.e. they coincide with the groove


54


in the wall


48


of the container


47


bearing through a shoulder


53


on the shoulder


81


of the tail


12


of the body


5


of the projectile


1


, the free ends


76


of the tongues


74


enter the groove


54


and constitute an abutment opposing movement of the container


47


towards the front inside the body


5


.




When the projectile


1


has left the weapon barrel


3


the force applied to its face


72


by the protuberances


77


is removed and the elasticity of the tongues


74


returns them to a position in which each protuberance


77


projects on the outside face


8


. The free ends


76


of the tongues


74


are therefore retracted away from the axis


2


relative to the inside face


7


of the wall


6


, freeing the container


47


to slide towards the front inside the body


5


.




Assuming that, instead of sliding directly inside the body


5


, the container


47


is mounted in a slide adapted to slide inside the body


5


, the bead


71


or the tongues


74


could co-operate in exactly the same way as described with reference to the groove


54


with a similar groove in the slide. A solution of the above kind is not shown but how to put it into effect will be evident to the skilled person.




Naturally, other modes of locking the container


47


or the slide carrying it inside the body


5


can be chosen without departing from the scope of the invention, in particular if the movement of the container


47


leading to its end wall


50


being perforated by the striker


55


is brought about not by inertial displacement of the container


47


or by apparent shortening of the wall


6


, as shown, but by other means such as pyrotechnic means with a time-fuse initiated when the projectile is fired. In this case, for example, the container


47


could be retained temporarily against sliding inside the body


5


by shear pins that break when the gas pressure generated by the aforementioned pyrotechnic means exceeds a predetermined threshold or when the combination of this effect and an inertia of the container


47


on impact exceeds the predetermined threshold at which the pins shear. How to construct this variant of the projectile


1


, and likewise of the other variants, will be evident to the skilled person and is within the scope of the invention.




Likewise, although applications of the invention to a projectile


1


adapted to be fired in a given longitudinal direction


4


from a weapon barrel


3


and to release the pressurized fluid


68


from the container


47


on impact on a target


66


in this direction have been described with reference to

figs. 1 through 14

, it will be obvious to the skilled person how to adapt these to the case of a projectile


1


adapted to be projected by some other means, in particular launched by hand, and/or how to release the pressurized fluid from the container in a manner other than in response to impact on a target in the particular longitudinal direction, in particular by striking of the container


47


as a consequence of its longitudinal sliding inside the body


5


of the projectile


1


towards the striker


55


and towards the transverse partition


35


carrying it by action of pyrotechnic or mechanical-pyrotechnic means known in themselves, in particular intentionally operated by a user prior to launching the projectile


1


.



Claims
  • 1. A non-lethal projectile for projecting from a tube in a given longitudinal direction, and to disperse a pressurized fluid in a controlled manner by impact on a target in said direction, said non-lethal projectile comprising:a longitudinal body having a nose at the front and a tail at the rear, a container for the pressurized fluid disposed in said body between said nose and said tail, a longitudinal striker for perforating said container juxtaposed longitudinally thereto and carried by a transverse wall attached to the body, means for enabling longitudinal movement towards each other of the container and the striker and controlled perforation of the container by the striker, by impact on the target in said direction, means for dispersing the fluid to enable the fluid to exit the body in a transversely-distributed manner on perforation of the container by the striker, wherein the means for dispersing the fluid include a blind longitudinal passage through the striker open at the end towards the container and closed inside said wall, and a plurality of transverse passages in said wall radiating from said blind longitudinal passage and opening to the exterior of the body through holes in said body.
  • 2. A projectile according to claim 1, wherein the striker has longitudinally opposite said wall a free end in the form of a bevel onto which said blind passage opens longitudinally.
  • 3. A projectile according to claim 1, wherein the striker has longitudinally opposite said wall a free end that includes a step set back longitudinally towards said wall and onto which said blind passage opens longitudinally.
  • 4. A projectile according to claim 1, wherein the striker has longitudinally opposite said wall a free end in the form of a bevel onto which said blind passage opens longitudinally, said free end includes a step set back longitudinally towards said wall and onto which said blind passage opens longitudinally, the step is formed in the area of the bevel closest to said wall in the longitudinal direction.
  • 5. A projectile according to claim 4, wherein the step extends over at least half the periphery of the bevel.
  • 6. A projectile according to claim 1, wherein the striker has, longitudinally on the same side of said wall as the container, at least one transverse orifice that opens into said blind longitudinal passage.
  • 7. A projectile according to claim 1, wherein the striker is attached to said transverse wall and the means for enabling longitudinal movement of the container and the striker towards each other and perforation of the container by the striker include a longitudinally compressible area of the body longitudinally between the container and said transverse wall.
  • 8. A projectile according to claim 1, wherein the striker is attached to said transverse wall and the means for enabling longitudinal movement of the container and the striker towards each other and perforation of the container by the striker include mounting the container to slide longitudinally relative to the body, the striker and said wall being disposed in front of the container.
  • 9. A projectile according to claim 8, further comprising locking means for immobilizing the container relative to the body when the projectile is inside the tube and to release the container automatically to slide longitudinally relative to the body when the projectile exits the tube.
  • 10. A projectile according to claim 9, wherein the body is in the form of an elastically deformable material wall between the nose and the tail and has a smooth inside face for guiding the container when it slides longitudinally in the body and a smooth outside face for guiding the projectile when it slides longitudinally in the tube, in that said outside face has a localized protuberance to be depressed and form a projection on said inside face when the projectile is engaged in the tube and to project on the outside face and eliminate the projection on the inside face when the projectile has left the tube, and in that the container has a localized depression in it transversely facing said protuberance when the container is juxtaposed to the striker.
  • 11. A projectile according to claim 10, wherein said localized depression is in the form of a transverse annular groove.
  • 12. A projectile according to claim 11, wherein the protuberance is in the form of a transverse bead connected without discontinuity to the wall of the body.
  • 13. A projectile according to claim 10, wherein said wall includes at least one elastically flexible tongue having one end attached to the wall and offset relative to said protuberance and a free end carrying said protuberance which is attached to it.
  • 14. A projectile according to claim 8, wherein said means for enabling longitudinal movement towards each other of the container and the striker and perforation of the container by the striker are controlled by inertia.
  • 15. A projectile according to claim 1, further comprising stabilizing fins attached to the tail of the body and to occupy a retracted position in which they are retained and elastically stressed by the tube when the projectile is engaged therein and to be deployed by virtue of their elasticity when the projectile has left the tube.
  • 16. A projectile according to claim 15, wherein the fins are made from an elastically deformable material and have one end attached to the body and a free end tending by virtue of its elasticity to spread transversely outwards relative to the end attached to the body.
  • 17. A projectile according to claim 15, wherein the fins are shaped to cause a whistling sound when the projectile is in flight.
  • 18. A non-lethal projectile comprising:a body having a nose at the front and a tail at the rear; a container to contain a pressurized fluid, said container disposed in said body between said nose and said tail; a striker to perforate said container, wherein said striker is enabled to automatically strike the container upon impact of said body with a target to cause perforation of the container; and a fluid passage arrangement to enable the fluid from said container to exit the body in a transversely-distributed manner upon perforation of the container by the striker, wherein said fluid passage arrangement includes a blind passage through the striker open at the end towards the container and closed at the other end, and a plurality of transverse passages extending from said blind passage to the exterior of the body.
Priority Claims (1)
Number Date Country Kind
96 07780 Jun 1996 FR
PCT Information
Filing Document Filing Date Country Kind 102e Date 371c Date
PCT/FR97/01109 WO 00 5/25/1999 5/25/1999
Publishing Document Publishing Date Country Kind
WO97/49969 12/31/1997 WO A
US Referenced Citations (6)
Number Name Date Kind
1671364 Gangnes May 1928
3091365 Horner et al. May 1963
4195572 Knapp Apr 1980
4667601 Diamond et al. May 1987
5078117 Cover Jan 1992
5415845 Brede et al. May 1995
Foreign Referenced Citations (5)
Number Date Country
506770 Jan 1969 CH
0733875 Sep 1996 EP
2598215 May 1986 FR
1354307 Jun 1971 GB
WO 9101479 Feb 1991 WO
Non-Patent Literature Citations (1)
Entry
Navy Technical Disclosure Bulletine, vol. V, No. 3, Mar. 1980, Arlington Virginia, pp. 43-46.