IL154032A

IL154032A - Non-penetrating projectile

Info

Publication number: IL154032A
Application number: IL154032A
Authority: IL
Original assignee: Richard Ian Brydges Price
Priority date: 2000-07-28
Filing date: 2003-01-19
Publication date: 2007-07-04
Also published as: JP2004505230A; GB0118011D0; GB2365100B; WO2002010671A1; AU7266501A; EP1307700B1; EP1307700A1; ES2261440T3; ATE323274T1; AU2001272665B2; NZ523823A; CA2417602A1; DE60118753T2; IL154032A0; CZ299005B6; DK1307700T3; GB2365100A; CN1466672A; CA2417602C; GB2365100C

Abstract

A non-lethal projectile or a projectile for delivery of a substance has a casing 1 which surrounds a compartment 2 for containment of the substance 3. A hollow tube 5 projects forward within an ogival nose cap 8. An inflatable membrane 7 is located within the nose cap 8. The rear end of the compartment 2 has a piston 4 the rear side of which communicates through passageway 14, valve 12 and orifice 11 with the rear end of the projectile whereby propulsive gases on firing are stored in the cavity 15 to the rear of the piston. The nose cap 8 is of a readily breakable plastics material. On target impact the nose is displaced and permits a small amount of substance from compartment 2 to bleed through opening 6 allowing piston 4 to move forward uncovering ports 16. This action allows pressure gas to pass through the ports 16 and ducts to inflate the membrane 7 to spread the impact over a wide area. The piston is also free to move forward to discharge the substance through needle 5. In another construction (Fig. 6) a membrane 33 forms the nose of a non-lethal bullet and contains a gel 36. On impact the gel moves valve plate 38 back to allow pressure gas in casing 30 to act through ports 40 to inflate the membrane 33.

Description

NON-PENETRATING PROJECTILE Eitan, Pearl, Latzer & Cohen-Zedek P-5655-IL Title: Non-penetrating Projectile This invention relates to a non-penetrating projectile which may be adapted for use as a medication delivery system, for example for delivering a tranquillising substance, drug, vaccine, medication, identification means or tracking device to an animal or to any other target. The system may also be used to take a sample of tissue. Such projectiles are commonly referred to as tranquilliser darts and their primary purpose is to provide means for remotely delivering and injecting a tranquillising fluid or medication into an animal without causing undue harm or stress.

This invention also relates to a projectile which can be adapted for use as a non-lethal projectile commonly referred to as a "baton round" or "rubber bullet".

With reference to the first mentioned us, there has long been a need to capture, study, relocate or medicate animals and various means are used. The most commonly used method being by means of some form of adapted syringe containing a tranquilliser which is propelled and injected on impact into the animal. These tranquilliser dart devices have serious disadvantages primarily being lack of range and accuracy due to poor ballistic properties and the highly parabolic trajectory making range estimation critical. As a projectile the devices are inherently unstable due to length and weight and cannot be spin stabilised to any useful degree due to the low velocity which is required to avoid deep penetration which is a major factor. The known devices are also complex to assemble and load often with highly toxic drugs and are heavy in relation to the delivered payload.

It is one object of this invention to provide a tranquilliser or other medication delivery system using a projectile, being preferably spin stabilised having improved range and accuracy and of an inherently stable ballistic shape, being an improvement and a modification of the projectile described and claimed in WO 00/71967A1 and GB2350414 A1.

Another alternative object is to provide a projectile which has limited, controlled or no penetration into a target.

Yet a further alternative object is to provide a projectile which itself does not include an explosive or gas producing charge.

A further alternative object of this invention to provide a non-lethal projectile which may be fired with accuracy at a soft target directly and even at close ranges and which is designed not to penetrate to any significant extent and which should only cause minimal injury to the limbs or torso.

Another alternative object is to provide a projectile which is capable of marking the target for subsequent identification.

In accordance with a first aspect of this invention there is provided a projectile including means to effectively retard the velocity of the projectile on impact with a target wherein the velocity is retarded in such a way as to prevent excess injury or penetration by deployment of means, following impact with a target, which rapidly expands to produce a large increase in the area at the nose of the projectile to spread the kinetic energy over a large area, characterised in that said expansion of said means is effected using a pressurised gaseous medium carried in the projectile.

Preferably the velocity retarding means comprises an inflatable membrane which is subject to the pressurised medium through means actuated on impact with a target, for example by a impact sensor or by means of a proximity sensing means, or by physical displacement actuating a valve device, the membrane being inflated using said pressure, preferably being gas pressure, stored in the projectile and preferably derived from the propulsive charge gases occurring on firing the projectile from a weapon.

In accordance with a second aspect of this invention there is also provided a projectile with means to effectively retard the velocity of the projectile on impact with the target for the purpose of preventing penetration, wherein the velocity retarding means comprises an inflatable membrane actuated on or close to impact, for example by a impact sensor or by means of a proximity sensing means, the membrane being inflated using gas pressure stored in the projectile, said pressure being preferably derived from the propulsive charge gases occurring on firing from a weapon.

In accordance with a third aspect of this invention there is provided a projectile comprising a rear canister part and a forward nose part connected therewith, the canister part containing or adapted to contain a pressure gas, the forward end of the canister part having a valve means, the nose part comprising a profiled impact deformable material with a portion to act on and open the valve following impact, the nose part having a membrane around the deformable material, the membrane being inflated on release of the pressure gas through opening of the valve.

The velocity is retarded in such a way as to prevent excess injury or penetration and may be achieved by means which rapidly produces a large increase in area at the nose of the projectile thus spreading and dissipating the kinetic energy over a large area.

Preferably the projectile is adapted to be fired from a barrel weapon which may be rifled to impart spin. The projectile may be of sub-calibre design using a discarding sabot and be fired in a barrel having progressive rifled pitch to attain a velocity greater than 500 m/s.

In one preferred construction the projectile has a body with a cavity containing a payload, such as a marker fluid or dye and an ogival nose.

The velocity retarding means comprises a means to significantly increase the area of the projectile nose portion on initial impact by inflation to produce unfurling or unfolding, or by expansion through stretching or by a combination of both.

In one construction the velocity retarding means comprises an inflatable membrane which opens up or expands through gas pressure and actuated by a sensor on initial impact or using a proximity sensing means.

In an alternative the membrane is pre-pressurised and expands following discarding of an overlaying covering forming a constraining means.

The membrane may be inflated through a detonator and gas producing explosive charge or through use of stored gas pressure. This charge or stored pressure may also serve for the purpose of dissipating the marker by driving a piston in the containing cavity.

The membrane can be located in the nose of the projectile comprising a readily broken, fragmenting, unfurling or deployable cap. The membrane may be in the form of a bag attached to and around a forward end of the projectile nose thus preventing penetration beyond a predetermined depth.

The nose part of the projectile may include a solid foam-like or gel-like substance forming an energy absorbing material which spreads on impact. More specifically the gel may comprise a nano-porous open cell foam of the kind known by the trade mark Aerogel.

This invention is further described and illustrated with reference to the drawings showing a modification of the embodiment disclosed in patent application WO 00/71967A1 and further embodiments according to this invention all shown by way of examples only. In the drawings: Fig 1 shows an embodiment of projectile, in longitudinal section, which uses stored gas pressure, Fig 2 shows a detail of the nose of the projectile of Fig 1 , Fig 3 shows a detail of the base of the projectile of Fig 1.

Fig 4 shows a longitudinal cross-section of a non-lethal disabling or marking projectile, which may optionally use stored gas pressure, Fig 5 shows a longitudinal cross-section of a non-lethal disabling or marking projectile which uses stored gas pressure derived from the propulsive charge, and Fig 6 shows a construction of baton round according to this invention using stored gas pressure.

The embodiment is shown Figs 1 to 3 of the drawings is similar to that disclosed in WO 00/71967A1 but here gas pressure for inflating the bag and injecting the substance is derived from propulsion gases on firing the projectile. This arrangement avoids the need for the projectile itself to contain a gas producing charge.

As shown in Figs 1 to 3 the projectile has a casing 1 surrounding a cavity 2 to contain the substance 3 and a piston 4 which serves to drive the substance 3 forward through the hollow tube 5 which in this embodiment is a needle to exit via one or more opening at the end of the needle 6. Surrounding the hollow tube 5 is an expandable membrane 7 which may be of rubber or the like and capable of inflating in the manner of a balloon. The nose cap 8 of the projectile has a casing which supports a stopper 9 of the membrane 7, this stopper 9 also supporting the end of hollow tube 5.

The base of the projectile comprises and end cap 10 ultrasonically welded to the casing 1. The end cap 10 has an orifice 1 with an internal seat against which a deformable, for example rubber, bead or cone 12 is pressed by an internal bridge 13. The bridge 13 has apertures 14.

The projectile may be integrated with a propellant charge carrying casing or may be caseless. The operation is as follows: When the projectile is fired from weapon gas pressure from the propulsive charge will be about 600 atmospheres sufficient to deform the bead 12 thus allowing pressure gas to enter via orifices 11 and apertures 14 to the reservoir space 15 behind piston 4. Once the projectile leaves the muzzle of the weapon internal pressure in the reservoir space 15 forces bead 12 back onto the seat and closes the orifice 11.

On impact with a target the stopper 9 is moved back over the hollow tube 5 exposing the needle 6 to permit some substance 3 in the cavity 2 to bleed thus allowing piston 4 to move forward. This movement uncovers ports 6 in the wall of cavity 2 and permits stored gas pressure in reservoir space 15 to enter the cavity between casing 1 and cavity 2. This compartment connects through passageways with the compartment 17 inside the membrane 7 and thus rapidly inflates same. Where the membrane is of rubber it will stretch and expand. The membrane could be of a non-or partly-stretchable material which is folded into the nose cone. During this action the nose cap 8 is split open and is discarded or peels back.

It will be appreciated that the sequence of events occurs rapidly in relation the velocity of the projectile resulting in minimum penetration of the needle. The balloon-like inflation of the membrane 7 also has the effect of pushing the projectile back relative to the target thus withdrawing the hollow tube 5 with the projectile falling to the ground. Modifications to the form of the membrane on inflation may be made in order to permit the projectile to be retained in the target if required.

Referring to Fig 4 of the drawings the projectile shown comprises a tubular body casing 1 which may, if required, define a cavity 2 for containment of a marker or dye for example a fluid. The fluid may be stabilised by means of a sponge or similar material to prevent inertia to spin which may create instability in flight.

Located towards the tip of a nose cap 8 is a gas producing detonator 54 fired by an impact fuse 55. In an alternative arrangement two, or more, otherwise inert substances are to be brought together to initiate an action. Attached to the detonator 54 is the neck 56 of an inflatable membrane or bag 7 of which an opposed end 57 is attached to the plug 53. A hollow tube 5 which in this embodiment is readily deformable, connects the detonator 54 to the plug 53 and acts as a support.

The rear end of the cavity 2 has a piston 4 the rear end of which communicates through concentric passageways 58 around the cavity 2 and ducts 59 in the plug 53 with the interior of the bag 7. The rear end of the casing 1 is closed off by a tail piece 510.

The projectile has an inherently stable ballistic shape and may have a mass of about 8 to 10 grammes and be some 1.5 cm in calibre. Larger or smaller calibre may be used as appropriate to the circumstances. The projectile may be embraced by a discarding sabot of plastics material and may be fired from a standard or progressive pitch rifled barrel giving a muzzle velocity of about 500 m/s. The range under these conditions should be of the order of 150 m with a mid range trajectory fall of less than 20 cm.

The nose cap 8 is of a readily frangible plastics material and may include structural lines of weakness to facilitate fragmentation. The inflatable bag 7 may be of Kevlar material, latex or silicone as examples of suitable materials. An impact absorbing material such as Aerogel may be contained in the nose cap. A marking dye substance may also be included.

In use, and following discharge from the weapon, the nose 8 will make initial impact and the detonator 54 is driven back along the support tube and fired via the ignition and retention cuff forming a fixed pin assembly to thus inflate the bag 7 rapidly. The bag 7 expands and prevents excess penetration whilst spreading the impact energy over a wide area. On inflation of the bag the nose cap 8 is broken open and may be discarded. In an alternative arrangement the nose cap 8 may spread open in a petaline manner and add to the retardation effect. The bag may be striated longitudinally or laterally and coated or impregnated with gas producing chemical compounds to both accelerate expansion and strengthen the bag membrane. The bag inflation gas bleeds through ducts 59 and passageways 58 to drive piston 4 forward thus ejecting the marker through the tube 6.

In a modification excess gas pressure is used to further retard the projectile by forward facing discharge nozzles.

In a modification of this embodiment the cavity behind piston 4 or the cavity 2 is charged with a pressurised gas which may be collected from rearward ports which are exposed to the propulsive charge on firing and trapped by one-way valve means. The gas is released to inflate the bag 7 on impact.

In this embodiment the bag 7 is folded in the manner of a bellows as shown, to provide greater expansion capability, and retained at the nose, within the nose cap 8, by an annular support 50 holding the detonator 54. This support 50 also centralises the opening et the end of the tube 6 and closes the nose completely. The tail piece 510 comprises a removable plug 51 to permit filling of the cavity 2. The casing 1 here is a removable module carrying the hollow tube 5 and is housed within the projectile outer case 52.

The propellant charge for the projectile may be included within an integral cartridge casing forming a single piece round. The projectile may be a single use device pre-loaded with a defined marker and charge with different charges being coded for ease of field use. The casing may comprise a carbon fibre material or glass bonded hydrocarbon matrix.

The projectile may be packaged in such a way that arming only occurs when removed from the pack.

The projectile has a particular use for soft targets presently require firing at close range typically 20 m.

A further advantageous embodiment is shown in Fig 5 and is similar in concept to the embodiment of Figure 1 , with gas pressure for inflating the bag and ejecting the marker substance being derived from propulsion gases formed on firing the projectile. This arrangement also avoids the need for the projectile itself to contain a gas producing charge. The previously described embodiment of Fig 4 may be modified to include a pressurised gas compartment or capsule rather than an explosive gas producing compound. This would make distribution and compliance with regulations easier.

As shown in Fig 5 the projectile is in many respects similar to that of Fig 1 and includes a pressure gas storage chamber. The projectile has a casing 1 surrounding a cavity 2 to contain the marker substance 3 to be ejected and a piston 4 which serves to drive the marker substance 3 forward through the tube 5. Details are otherwise similar to Figs 1 to 3.

Fig 6 shows a construction of baton round according to this invention using stored gas pressure.

Referring to Fig 6 the projectile has an inherently stable ballistic shape and may have a mass of about 10 to 150 grammes and be some 10 to 50 mm in calibre. Larger or smaller calibre may be used as appropriate to the circumstances. The projectile may be embraced by a discarding sabot of plastics material and may be fired from a standard or progressive pitch rifled barrel giving a muzzle velocity of about 500 m/s. The range under these conditions should be of the order of 150 m with a mid range trajectory fall of less than 20 cm.

In the construction shown the projectile comprises a rear canister 30 forming a pressure gas reservoir 31 either pre-filled or filled by combustion gases on firing or by gases from a detonator and gas producing charge unit 37 and with a forward closure 32 retaining an expandable membrane or cover bag 33. The bag 33 is connected by an interlock 34 to a rim 35 on the closure 32. The shape of the bag 33 is maintained and supported by a viscous filler 36 such as Aerogel (a Trade Mark). The bag 33 may be protected by a nose cone being relatively thin and easily deformed or broken on initial impact.

On impact with a target the Aerogel deforms and crushes initially and a valve 38 opens by rearward movement of the stub part 36a of the Aerogel. Pressure gas from the reservoir 31 or alternatively generated by the detonator and gas producing charge unit 37 on impact, for example using an inertia detonator, enters cavity 39 past the valve 38 and passes through ducts 40 to expand the bag 33.

As described the pressure gas for inflating the bag 33 may be derived from either an inertia detonator with gas producing charge unit 37, from gas stored in the container or from the gases produced from the propulsive charge on firing using ports at the base which are exposed to the propulsive gases with intervening valve means to retain the gas pressure.

In another option the inertia detonator will initiate filling of the rear cavity 31 with pressurised gas on firing and this pressure is retained during flight against the valve 38. In another alternative a pressurised capsule may be incorporated to replace the inertia detonator.

A marker dye could be included between the nose cone and the inflatable membrane.

In a modification excess gas pressure is used to further retard the projectile by forward facing discharge nozzle The propellant charge for the projectile may be included within an integral cartridge casing forming a single piece round. The projectile may be a single use device pre-loaded with a defined marker and charge with different charges being coded for ease of field use. The casing may comprise a carbon fibre material or glass bonded hydrocarbon matrix.

The projectile may be integrated with a propellant charge carrying casing or caseless.

It will be appreciated that the sequence of events occurs rapidly in relation the velocity of the projectile resulting in no, or minimal, penetration of the nose. The balloon-like inflation of the membrane also has the effect of pushing the projectile back relative to the target thus adding to the blow inflicted on the target.

The membrane used may comprise an expandable rubber material which stretches or the material may comprise KEVLAR (a registered Trade Mark) weft which initially inflates, then expands and finally allows gas pressure to bleed due to opening-up of the weave. In all embodiments a pressure relief system may be included to avoid over extending the inflation of the membrane.

Claims

13 154032/2 ims

1. A projectile including means to effectively retard the velocity thereof on impact with a target in such a way as to prevent excess damage, injury or penetration, the means rapidly expanding to produce a large increase in the area at the nose of the projectile following impact with a target, characterised in that said expansion is effected by release of a pressurised medium stored in the projectile.

2. A projectile in accordance with claim 1 , including a device for delivery of a substance to a target, the projectile including a cavity to contain such substance, means to release the said substance at a point of impact with a target, and means to effectively retard the velocity of the projectile on impact with the target, the velocity retarding means comprises an inflatable membrane actuated on or close to impact with the target, the membrane being inflated by release of the pressurised medium being gas pressure stored in the projectile.

3. A projectile in accordance with Claim 2, wherein the gas pressure also serves the purpose of ejecting the substance.

4. A projectile in accordance with any of the preceding Claims, wherein the rear of the projectile includes a valved orifice leading to a gas pressure storage chamber for storing the pressurised medium derived from propulsive gas pressure on firing the projectile from a weapon.

5. A projectile in accordance with Claim 2 or 3 as limited by Claim 4, wherein the gas pressure storage chamber acts on a piston serving to discharge the substance and which chamber communicates with the membrane to inflate same following impact with a target. 14 154032/2

6. A projectile in accordance with Claim 5, wherein on impact with a target the substance within the cavity is permitted to bleed thus allowing the piston to initially move by which action gas pressure is released to the membrane.

7. A projectile in accordance with Claim 1 or Claim 4 having a body defining a cavity and a nose connected therewith, the body having a container to store a pressurised medium comprising a pressure gas, the nose including a deformable or malleable substance and an outer casing including an overlying membrane internally communicating with the container and forming the expanding means to effectively retard the velocity of the projectile on impact with a target, the membrane being inflatable by release of said pressure gas on or close to impact with a target.

8. A projectile in accordance with any one of Claims 1 to 7, wherein pressure gas is stored in the projectile and derived from the propulsive charge gases occurring on firing from a weapon.

9. A projectile in accordance with any one of Claims 1 to 7, wherein the pressure gas is generated and stored prior to impact by a gas producing charge ignited by a detonator.

10. A projectile in accordance with any preceding Claim 1 to 9, wherein the gas pressure, on release, also disperses a payload carried by the projectile.

11. A projectile in accordance with any of the preceding Claims, wherein the membrane is in the form of an inflatable bag, or a stretchable material or a combination of both attached to and provided around a forward end of the projectile nose. 15 154032/2

12. A projectile in accordance with Claim 11 , wherein the membrane forms the external profile of the nose.

13. A projectile in accordance with any of the preceding Claims, wherein the membrane is of an expandable material or is folded or pleated to permit expansion and comprises a reinforced fabric being semipermeable to gases.

14. A projectile in accordance with any of the preceding Claims, wherein the nose part of the projectile includes a deformable or malleable substance and forming an impact absorbing material which spreads on impact, or a dye marker or other device.

15. A projectile in accordance with Claim 14, wherein the substance is a solid foam-like or gel-like gel formulation and comprises a nano-porous open cell foam.

16. A projectile in accordance with any one of Claims 1 , 4 or 7 to 9 comprising a rear canister part and a forward nose part connected therewith, the canister part containing or adapted to contain a pressure gas, the forward end of the canister part having a valve means, the nose part comprising a profiled impact deformable material with a portion to act on and open the valve following impact with a target, the nose part having a membrane around the deformable material, the membrane being inflated on release of the pressure gas through opening of the valve.

17. A projectile in accordance with claim 16, wherein the membrane is protected by a nose cone or covering.

18. A projectile in accordance with any of the preceding Claims, constructed as a sub-calibre discarding sabot projectile. 16 154032/2

19. A projectile in accordance with any preceding Claim 1 to 18, wherein the pressure gas is derived and stored prior to impact from a pressurised capsule.

20. A projectile in accordance with any preceding Claim 1 to 18, wherein the pressure gas is generated and stored prior to impact by means of an inertia activated detonator, preferably activated on firing of the projectile from a weapon.

21. A projectile in accordance with any preceding Claim 1 to 18, wherein the inflatable membrane is pre-pressurised by the pressure gas and is constrained against inflation by an overlying covering which is discarded at, or close to, impact with a target.

22. A projectile in accordance with any preceding Claim 1 to 18, wherein the pressure gas is stored prior to the firing of the projectile from a weapon.