The present invention relates to the field of spin stabilized projectiles containing a releasable payload. More particularly the invention relates to a device for counteracting contact-impact events upon firing of a projectile leading to improved effect/penetration of the sub-projectiles to the target.
When elongated sub-projectiles (rods, flechettes, sub-munitions etc.) are fired out of a barrel, separated from a carrier shell or cylinder, the sub-projectiles rotate either relative to a stationary barrel, or the barrel, carrier shell or cylinder rotates together with the sub-projectiles. The sub-projectiles are affected by the centrifugal forces which give rise to a tumbling motion when the centre of gravity of the projectiles/sub-projectiles pass the muzzle of the barrel/cylinder, or are released from a carrier shell, (see
U.S. Pat. No. 3,656,433 provides a method for reducing shot dispersion by using a viscoelastic matrix utilized to hold flechettes or other types of small missiles or shots in a unitary projectile form until the unit are released from the gun barrel and until it has substantially passed through the blast region area.
U.S. Pat. No. 5,817,969 discloses a method to avoid contact-impact event of the payload, i.e., sub-projectiles, when the payload is released from a carrier shell, i.e., the payload chamber opens essentially along a casing line from the bottom to the top (cap) and the sub-projectiles are released from the carrier shell when the shell opens up, thereby avoiding contact-impact events. The construction is complex and heavy; the aim is also to fill the casing with maximum number of sub-projectiles for improved hit rate, i.e., quantity.
In view of the background there is a need of developing a device that allows the sub-projectiles to leave the barrel, carrier shell or the like with decreased interference of the centrifugal forces leading to decreased tumbling of the sub-projectiles thereby obtaining increased effect/penetration.
It is desirable to provide a device that decreases and/or counter-acts the tumbling effect of projectiles/sub-projectiles fired from a barrel, cylinder, carrier shell or the like.
According to an aspect of the present invention, a holding device counteracts the contact-impact event on sub-projectiles when they are fired from a barrel, cylinder, carrier shell or the like. The holding device comprises a core having at least two legs. The legs enclose at least partially at least one sub-projectile each.
In one embodiment the number of legs is in the range of two to twelve. In yet another embodiment the number of legs is in the range of two to six. The number and design of the legs varies and depends on the type of projectile to be used. The number and the design of the legs depend on the type of sub-projectiles to be enclosed.
Generally, the holding device comprises a core from where at least two legs are protruding. The legs are protruding from the core in a circular symmetric manner and evenly distributed around the core. If two legs are utilized they are separated by 180 degrees, three legs 120 degrees, four legs 90 degree, etc.
The holding device may for example be made of plastics. In another embodiment it may be made of aluminium. In yet another embodiment the holding device may be made of magnesium. A holding device made of steel, preferably soft steel, is also provided.
The holding device may in another embodiment be made of a combination of material.
The holding device of the present invention may be manufactured by molding, but other processes known by the art is also possible.
In one embodiment of the holding device each leg can enclose up to S sub-projectiles.
The holding device may in one embodiment be enclosed by a cover. A cover may surround the holding device, e.g., surrounding the outside on the legs. In another embodiment a cover can be used for preventing the sub-projectiles from falling out from the holding device, e.g., as top or bottom cover. The holder may also be used in combination with a payload container.
It is also desirable to provide the holding device, as described above, comprising sub-projectiles. The sub-projectiles may be of any suitable kind.
A payload container comprising a holding device of the present invention and sub-projectiles can be arranged in a projectile, preferably in the payload chamber of a carrier shell.
It is also desirable to provide a projectile comprising said holding device comprising sub-projectiles as described above. In one example the projectile is a dividable projectile, comprising a payload chamber, a time fuze and a separation charge arranged behind the payload chamber for separating the payload chamber from the projectile in the forward direction of the projectile.
It is also desirable to provide a process for decreasing the tumbling effect when firing projectiles/sub-projectiles from a barrel, cylinder, carrier shell or the like. The tumbling effect of a sub-projectile is counteracted or decreased when the holding device described above is used. A leg of the holding device encloses at least partly a sub-projectile. The rotation implies that the sub-projectile loads the leg which is deformed and opens up, which results in that the sub-projectile is released outside the muzzle or opening without tumbling, i.e., in a controlled manner.
The present invention also provides a process for adapting a commercial projectile for firing sub-projectiles without or decreased contact-impact events when passing a barrel/cylinder, carrier shell or the like. The process comprises the steps of
The loading of the sub-projectiles is due to the centrifugal forces and the rotation that implies that the sub-projectiles load the legs.
The holding device is preferably arranged in a payload chamber of a projectile.
In general, the holding device of the present invention can be arranged in any suitable commercial projectile, thereby providing a projectile that does not suffer from contact-impact events upon firing the projectile from a barrel or the like.
The invention is now described, by way of example, with reference to the accompanying drawings, in which:
Before the invention is disclosed and described in detail, it is to be understood that this invention is not limited to particular materials or configurations disclosed herein as such configurations and materials may vary. It is also to be understood that the terminology employed herein is used for the purpose of describing particular embodiments only and is not intended to be limiting since the scope of the present invention is limited only by the appended claims.
The present invention will now be described in more detail with reference to the accompanying figures, in which different embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein.
In context of the present invention the term sub-projectile means a small weapon or device that is part of a larger warhead and separates from it prior to impact, e.g., rods, flechettes, or arrow-like darts, i.e., not only munitions of various kinds, but all kinds of payloads, from which a specific continued flight on a determined flight path is expected after its release.
In context of the present invention the term contact-impact events means the event when the projectile/sub-projectile is fired/released from a barrel, carrier shell, cylinder or the like and pass the muzzle-edge resulting in disturbances and tumbling of the sub-projectile.
In context of the present invention the term holding device defines devices that at least partly enclose and arrange sub-projectiles.
When a sub-projectile is emerging from a muzzle or opening of a barrel or being separated forward from a carrier shell or a cylinder, the sub-projectiles will rotate either in relation to a stationary barrel, or the barrel or carrier shell rotates together with the sub projectiles. Due to the rotation, the sub-projectiles are influenced by the centrifugal force (F,
An ideal solution would be that the sub-projectiles are released from the barrel/cylinder, or carrier shell without tumbling.
The holding device 5 comprises a core 3 with protruding legs 2 arranged to it. The core 3 and legs 2 can be manufactured in one piece, or the legs 2 may be arranged to the core 3 in a separate step.
In some embodiments the centre of the core 3 it is a bore for arrangement of a continuous detonator wire, for example a shock tube or an electric wire.
The legs 2 are in this embodiment six, but in other embodiments the number may vary between 2-50 depending on the type of carrier shell, holder or purpose. Usually, the number of legs is in the range of 2-50, or 2-25, 2-12 2-6, 2-4 or only 2.
The legs 2 are in this embodiment at least partially enclosing the sub-projectiles 1, and in this example there is one sub-projectile 1 enclosed per leg 2.
When sub-projectiles 1 are released from a barrel/cylinder, carrier shell or the like, the device is deformed due to the centrifugal forces and the rotation implies that the sub-projectiles 1 load the legs 2 which are deformed and opens up (
The holding device 5 may for example be made of plastics, aluminium, magnesium, or steel, or a combination of said materials. The core 3 and the legs 2 can be made of different materials. The holding device (5) may be manufactured by molding.
In the embodiment of
The embodiment shown in
The embodiment in
The number of legs 2 and/or sub-projectiles 1 is scalable and is not intended to be limiting.
In the embodiments shown here the legs 2 enclose the sub-projectiles 1 from the left, but other embodiments are also possible.
Generally, the holding device 5 comprises a core 3 from where at least two legs 2 are protruding. The legs 2 are protruding from the core in a circular symmetric manner and evenly distributed around the core. If two legs 2 are utilized they are separated by 180 degrees, three legs 120 degrees, four legs 90 degree, etc.
Clockwise as shown in
The payload chamber 80 arranged in the front projectile body 20 comprises at least one holding device 5 comprising sub-projectiles 1. A time fuze comprising an activation unit for activating the primer device 60 is arranged in the nose part 100 of the front projectile body 20, in front of the payload chamber 80. The nose part 100 is fitted to the front projectile body 20 by a second drive plate 110 and by for example shear pins 90, which are designed to rupture under the effect of the pressure on the separation of the payload chamber 80 from the projectile 10. In an alternative embodiment a continuous detonator wire 120, for example a shock tube, is arranged between the pyrotechnic primer device 60 and the front part 20 for separating the nose part (fuze) 100 from the projectile 10.
The holding device 5 of the present invention is intended to be used in commercially available projectiles. The holding device 5 is manufactured separately, and suitable sub-projectiles 1 are inserted into the holding device. At least one holding device 5 comprising sub-projectiles is thereafter arranged in a suitable projectile/carrier.
Sub-projectiles suitable for the holding device of the present invention are for example small calibre e.g. 12 gauge shotgun: rods, flechettes, medium calibre e.g. 40 mm, 57 mm: rods, flechettes, armor-piercing wolfram carbide projectiles and large calibre e.g. 120 mm, 155 mm sub-munitions, flechettes, rods.
In summary, the invention provides a holding device 5 for decreasing or eliminating contact-impact events that occur when sub-projectiles are released from a barrel, cylinder or a carrier shell. Advantages of the present invention are among other things: reduced or eliminated tumbling leading to improved penetration into and effect on the target; the size of the fins and the stabilization distance can be reduced of aerodynamic stabilized sub-projectiles; the sub-projectiles are fixed in a carrier shell when it is fired and before separation.
Number | Date | Country | Kind |
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1700293-2 | Nov 2017 | SE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/SE2018/050973 | 9/26/2018 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2019/108104 | 6/6/2019 | WO | A |
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Entry |
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International Search Report (dated Dec. 13, 2018) for corresponding international App. PCT/SE2018/050973. |
Number | Date | Country | |
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20200355479 A1 | Nov 2020 | US |