warhead

Abstract

The present invention relates to a method for manufacturing a warhead component having an inner shell, the method comprising the steps of: i.) placing a thermoplastic first casing surrounding the inner shell, ii.) placing a preformed projectile between the thermoplastic first casing and the inner shell, and iii.) heat treating the first casing to shrink it and secure the preformed projectile to the inner shell. The present invention further relates to warheads, projectiles and bombs.

Description

[Technical field]

[0001] The present invention relates to a method for manufacturing a component of a warhead, a projectile equipped with a warhead, and a bomb equipped with a warhead. [Background technology]

[0002] The fact that warheads are equipped with preformed fragmentation / shrapnel / projectiles has been known by experts for a long time. The choice of preformed projectiles used allows the effect of the warhead to be tailored to the purpose. Depending on the type of target involved, the number of preformed projectiles, the size of the preformed projectiles, the material of the preformed projectiles, the shape of the preformed projectiles can be determined. When the warhead breaks up, the preformed projectiles and preformed fragments scatter with a predetermined size, speed and mass. It is also possible to influence the direction of dispersion by the location and arrangement of the preformed projectiles.

[0003] According to experts, besides the placement of preformed projectiles, another way to produce projectiles of a given size and mass is to produce controlled fragmentation of the warhead. This is usually achieved by placing a weak spot in the warhead, such as by machining a groove into the warhead material / shell, which upon fragmentation / explosion will cause the warhead to split depending on the location of said weak spot. The grooves can be added to the warhead by machining or can be added directly during manufacturing, for example by casting, additive manufacturing, or other manufacturing methods.

[0004] It is also common to combine preformed projectile arrangements with controlled fragmentation of a single warhead.

[0005] Rubber fixtures are often used as part of the manufacturing process to position preformed projectiles. Manufacturing the rubber fixtures themselves is relatively costly and labor intensive. Flexibility to develop new products or adapt / modify existing products is also limited, as new shapes and geometries require new rubber molding tooling, resulting in long lead and development times and high costs. Similarly, milling grooves into warhead material to achieve controlled fragmentation is often difficult and labor intensive.

[0006] An example of a method for manufacturing a warhead with a preformed projectile is contained in US Patent Specification No. 3,815,504, which shows a method for manufacturing a warhead / projectile and also discloses a warhead / projectile manufactured by placing two tubular bodies coaxially with each other and with a distance between the two tubular bodies corresponding to the diameter of the component / fragment / bullet placed therebetween. When the device is placed with an external resistance, the internal pressure forms the tubular body around the fragment / fragment / charge.

[0007] Another example of a method for manufacturing a warhead with a preformed projectile is described in U.S. Patent Specification No. 4,032,335, which shows a process for manufacturing a composite material consisting of metal powder and fragments / preformed projectiles placed together against a metal structure, the composite material being subjected to hydrostatic compression, whereby the metal powder becomes embedded in the surrounding metal.

[0008] A further example of an alternative method for producing a warhead having a preformed projectile is described in U.S. Patent Application Publication No. 2009 / 0211484, which shows a component and method for producing a workpiece component having individual preformed pieces embedded in a reactive material or an inert material such as a polymer.

[0009] A common aspect of the above known techniques is the fact that the deployment of preformed projectiles is time consuming, technically challenging, costly and / or difficult to repeat at the same power output. Furthermore, the known techniques involve manufacturing problems related to occupational health and safety issues. Summary of the Invention

[0010] It is an object of the present invention to provide a simpler, faster and more cost-effective means of manufacturing warhead components with preformed projectiles and / or controlled fragmentation, thereby producing warheads. Additionally, the new method provides an improved working environment compared to known methods for manufacturing warhead components.

[0011] The present invention relates to a method for manufacturing a warhead component having an inner shell, the method comprising the steps of: i.) a thermoplastic first casing is disposed around the inner shell; ii.) a preformed projectile is disposed between a first thermoplastic casing and an inner shell; iii.) The first casing is heat treated to shrink it and secure the preformed projectile to the inner shell.

[0012] According to a further aspect of the method for adjusting the attachment of warhead parts, the following applies: The first casing includes an opening through which a preformed projectile can be placed. After the preformed projectile is placed between the first casing and the inner shell, a second casing is placed over the first casing with the opening. The inner shell is the shell body frame. The metal casing is placed on the connecting parts, including the first casing and, optionally, the second casing, and surrounds the projectile preformed against the inner shell. The metal powder is placed on a common warhead component having a first casing and optionally a second casing by hot isostatic pressing to attach the preformed projectile to the inner shell, whereby the first casing and optionally the second casing are vaporized during the hot isostatic pressing process. The mantle surface of the inner shell is disposed with recesses in the form of bullet bowls.

[0013] The present invention further comprises a warhead produced by the above-described method.

[0014] The present invention further comprises a projectile including a warhead.

[0015] The present invention is further a bomb having a combat component. Effect of the Invention

[0016] By manufacturing preformed warhead / projectile components and / or projectiles according to the demonstrated methods, projectiles can be manufactured faster, cheaper, easier, and with fewer issues regarding the working environment than previously known manufacturing methods. [Brief description of the drawings]

[0017] The present invention will now be described with reference to the drawings. [Figure 1] FIG. 1 shows a perspective view of a shell body for a warhead according to one embodiment of the present invention. [Diagram 2] FIG. 2 shows a perspective view of a shell body for a warhead disposed around a first casing according to one embodiment of the present invention. [Diagram 3] FIG. 3 shows a perspective view of a shell body for a warhead disposed surrounding a first casing and surrounding a second casing according to one embodiment of the present invention. [Figure 4] FIG. 4 shows a perspective view of a first casing according to an embodiment of the present invention. [Diagram 5]FIG. 5 shows a perspective view of a second casing according to an embodiment of the present invention. [Figure 6] FIG. 6 shows a perspective view of a shell body for a warhead arranged to surround a first casing according to another embodiment of the present invention. [Figure 7] FIG. 7 shows a perspective view of a shell body for a warhead disposed around a first casing according to another embodiment of the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0018] The present invention provides numerous embodiments of methods for manufacturing warheads / fuzes, as well as projectiles and grenades.

[0019] FIG. 1 shows the inner shell 1 of a warhead according to a first embodiment of the invention. The inner shell 1, which is the main body of the warhead, when the warhead is also called the fuse or shell body, is manufactured, for example, by cutting, such as turning, or by additive manufacturing, but can also be manufactured, for example, by casting, pressing or drawing. The inner shell 1 can also be made of a spacer material that can be used as a part in the manufacture of the projectile, in which case the inner shell can be placed in the warhead frame as a stage of the manufacturing process to manufacture the warhead / fuze. The warhead is a device adapted for combating a target, also called a fuse, and can consist of a projectile such as a grenade or can be a component of a projectile such as a grenade or a submunition. The inner shell 1 is hollow and can contain an explosive. The inner shell 1 is also designed to receive a nose section and an aft section in the front part 2 and the rear part 3, respectively. The nose and stern sections can have different designs, depending on the desired characteristics of the warhead, for example nose sections with different fuse forms, for example stern sections adapted to the cartridge or other stern sections suitable for the projectile. The inner shell 1 is preferably made of any material that the expert considers suitable for the purpose, usually a metallic material, but it can also be plastic or composite materials, various examples of materials are already known in the field of engineering. In the inner shell 1, recesses 4, also called bullet bowls, can be arranged, in which a preformed projectile can be placed. The inner shell acts as a driving mirror for the preformed projectile placed in the recess 4, influencing the ballistic trajectory of the preformed projectile when detonating the fuse.

[0020] Fig. 2 shows the inner shell, which is preferably made of metal, for example machined by conventional turning, or manufactured by additive manufacturing methods. The recess 4 of each projectile is provided in the inner shell 1 of the embodiment shown. Around the inner shell 1, an enclosed first casing 10 is arranged, in which the outlet 12, which is a slot, is arranged. The first casing 10 is arranged around the inner shell 1, i.e. around the outer diameter of the inner shell 1, meaning that it surrounds it radially along the axial extension of the inner shell, as also shown in the figure.

[0021] In FIG. 2, the enclosure casing is shown with an opening showing the location of the recesses 4 under the enclosure casing 10. The preformed projectiles are placed through the outlet 12 so that they are partially placed in the recesses 4. In the illustrated embodiment, bullet-shaped projectiles are used, so the recesses are bullet bowls, i.e., a bowl-shaped design that fits bullets. In one embodiment, the spherical projectiles are placed through the outlet 12 so that all the recesses 4 have a spherical projectile, then the inner shell 1 is rotated so that the next row of recesses 4 is visible to the outlet 12, then the spherical projectiles are placed in the next row, and then the inner shell 1 is rotated again to expose the next row of recesses 4 to the outlet 12. This process is repeated until all the recesses 4 have a spherical projectile. Preferably, the outlet 12 is positioned vertically with the opening facing upwards so that the balls mounted in the recesses 4 are held by gravity. As the inner shell 1 is rotated, the spherical projectiles already mounted are held by the first casing 10. The preformed projectiles are sometimes called fragmentation and / or shrapnel. In the embodiment shown in FIG. 2, the preformed projectile is bullet / spherical, but this can vary depending on the application.

[0022] Figure 3 shows the manufacturing process of the warhead according to the invention. A second casing 20 is placed on top of the first casing 10. Both the first casing 10 and the second casing 20 extend axially along part or all of the inner shell 1, but in a preferred embodiment the ends of the forward 2 and aft 3 sections are left free for connection to the nose and stern sections, respectively. The second casing 20 is not provided with an opening 12, so that the second casing 20 surrounds the first casing 10 and prevents the preformed projectiles placed between the inner shell 1 and the first casing 10 from falling out, separating or dislodging from their respective recesses 4. The manufacturing material of the first casing 10 and the second casing 20 is preferably a polymer selected for the properties such as the thermal properties / melting point, strength, ability of the material not to affect subsequent manufacturing steps.

[0023] FIG. 4 shows the first casing 10 with an opening 12. The first casing is preferably made of a polymer, also called a plastic, such as a thermoplastic, for example a thermoplastic polyester. Examples of suitable materials include high molecular weight thermoplastic polymers, such as polyethylene terephthalate, also known as PET, and HDPE (high density polyethylene). The first casing is designed to fit the inner shell in which the preformed projectile is placed, i.e., it can be placed on the inner shell 1 by the inner radius of the first casing 10. It is designed so that the preformed fragment can be placed in the inner shell and held by the first casing 10, i.e., it can be placed between the inner shell 1 and the first casing 10.

[0024] Figure 5 shows the second casing 20. The second casing is preferably made of a polymer, also called a plastic, such as a thermoplastic, e.g. a thermoplastic polyester. Examples of suitable materials are PET and HDPE. The second casing 20 is designed to fit over the first casing 10.

[0025] During the manufacture of the first casing 10 and the second casing 20, the plastic is stretched in an expanded state into a shape suitable for placement in the inner shell 1. The plastic can be thermoformed, extruded or blow molded into the desired shape. In blow molding, the raw material, for example in the form of an extruded polymer tube, can be placed in a chamber having the desired shape. Once the polymer tube is placed in the mold, the chamber is completely closed and gas flows into the polymer tube while it is heated. The gas fills the polymer tube and is attached to a threaded fitting placed at one end of the polymer tube, squeezing the polymer tube so that it settles according to the shape of the chamber. The mold is then cooled and the product is removed. When manufacturing casings such as the first casing 10 and the second casing 20, the casing may be manufactured in the shape of a bottle and then machined into the shape of the casing by removing the top and bottom parts. In shape-blown molding, when the stretched first casing 10 and / or second casing 20 are exposed to heat, the first casing 10 and / or second casing 20 will attempt to return to the shape of a polymer tube. In other words, the first casing 10 and / or second casing 20 will shrink. The covered part will return to its original shape if the temperature is above the glass transition temperature but below the melting point of the plastic.

[0026] In an alternative embodiment, as shown in FIG. 6, a first casing 10' arranged without an outlet is placed on the inner shell 1, which creates a distance between the first casing 10' and the inner shell 1, between which a preformed projectile, such as a charge, can be loaded. When a preformed projectile, such as a charge 30, is loaded between the first casing 10', the first casing 10' is heat treated to shrink relative to the inner shell 1, thereby holding and fixing the preformed projectile charge 30 relative to the inner shell 1. The heat treatment can be performed with hot air, an oven, or an IR heater. To facilitate loading of the preformed projectile, the first casing 10' may be provided with a funnel-shaped opening 14, in which the preformed projectile is placed. The funnel-shaped opening can be removed after placing the preformed projectile between the first casing 10' and the inner shell 1. The projectile shown in FIG. 6, and thus the inner shell 1, is provided with a rear end 40 and a threaded portion 50 for placing a primer tube. When the preformed projectile 30 is placed between the first casing 10' and the inner shell 1, a plug 52 may be placed in or on the threads 50 to prevent the preformed projectile 30 from terminating inside the inner shell 1. The material of choice for the first casing 10' is preferably a thermoplastic, such as a thermoplastic polyester. Examples of suitable materials include PET and HDPE.

[0027] Figure 7 shows an alternative embodiment in which the warhead components are prepared for further handling as part of the process of manufacturing a complete fuse / warhead. A first casing 10' is shrunk to seat the preformed projectile and the first casing is processed to remove a portion of the casing such as the funnel 14 shown in Figure 6. For example, the unwanted portion of the warhead component can be cut with a knife, heat knife, wire cutters / heat wire, or otherwise removed.

[0028] The fuze components include a first casing and sometimes additional cases such as a second casing that secures the preformed projectile to the inner shell. Once the fuze components are manufactured, additional materials can be applied to manufacture the complete fuze / projectile, for example by applying a steel or aluminum outer casing or by applying metal powder to the fuze components by hot isostatic pressing (HIP). When material is applied to the fuze components using HIP, the polymer of the first casing 10 and sometimes the second casing 20 vaporize by pyrolysis. Pyrolysis, also known as distillation, is the process of heating a substance to high temperatures in an oxygen-free environment and decomposing it without combustion. During pyrolysis, volatile materials are released in gaseous form, while solid or liquid residues remain. The inner shell 1, sometimes the tooling attached to the inner shell, the preformed projectile, the first casing 10, 10', and sometimes the second casing 20 are placed together in a HIP container. The HIP container is an apparatus that arranges the powder so that it can be formed into a HIPPAD body under high temperature and pressure. After the frame, together with the preformed projectile and the first casing 10, 10', and possibly the second casing 20, are placed in the HIP container, the powder is placed in the HIP container. After the powder material is placed in the HIP container, the HIP container is evacuated, vibrated and sealed to distribute the powder evenly in the HIP container. Then the HIP is carried out; that is, gas is supplied to a connection device attached to the HIP container to generate isostatic pressure in the HIP container. Before the gas is applied to the HIP container, the HIP container can be evacuated with a vacuum pump or evacuated using air or a filler gas / fluid placed in the HIP container before evacuation. At the same time, the entire HIP container is heated. After this process, the composite and the HIP container are created and the excess material is processed. After machining the body to be HIPed, the tool may be removed from the frame. After the processing and removal of the frame is completed, the body can be subjected to heat treatment. This means that the combined body is heated. The material after heat treatment is suitable for machining, such as cutting. After removal of the tooling, hardening of the HIPed frame is allowed to occur.

[0029] Further, to produce a complete projectile, the inner hull 1 may be filled with energetic material and a fuse may be attached to the nose of the fuse assembly, or, if the stern section is not part of the inner hull 1, the stern section or the rear section may be attached to the fuse assembly.

[0030] [Another embodiment] The invention is not limited to the embodiments shown but can be varied within the scope of the claims.

[0031] For example, the number of preformed projectiles, the choice of materials, polymers and geometric shapes, the included elements and details may obviously be adapted to the characteristics of one or several weapon systems, platforms or other relevant structures applied in each individual case.

[0032] Additionally, the present invention encompasses all types of warheads, fuses and projectiles, including grenades, high explosive shells, bombs, missiles and rockets, as well as other warheads such as grenades and various types of land mines.

Claims

1. A method for manufacturing a component for a warhead having an inner shell (1), the method comprising the following steps: i.) a thermoplastic first casing (10, 10') is disposed around the inner shell; ii.) a preformed projectile is placed between said first casing (10, 10') and said inner shell (1); iii.) shrinking said first casing (10, 10') by heat treatment to fix said preformed projectile to said inner shell (1).

2. The first casing (10) is provided with an opening (12) in which the preformed projectile can be placed. The method of claim 1.

3. After the preformed projectile is placed between the first casing (10) and the inner shell (1), a second casing (20) is placed on the first casing (10) with the opening (12). The method of claim 2.

4. The inner shell (1) is a shell body frame; The method according to claim 1 or 2.

5. a metal casing is placed on the connecting pieces including the first casing (10, 10') and possibly the second casing (20) and surrounds the preformed projectile against the inner shell (1); The method according to claim 3.

6. the metal powder is placed in a common warhead component having a first casing (10, 10') and optionally a second casing (20) by hot isostatic pressing and attaches said preformed projectile to said inner shell (1), whereby said first casing (10, 10') and optionally said second casing (20) are evaporated during the hot isostatic pressing process; The method according to claim 3.

7. A recess (4) in the form of a bullet bowl is arranged on the mantle surface of the inner shell (1). The method according to claim 1 or 2.

8. A warhead produced by the method of claim 1 or 2.

9. A projectile incorporating a warhead as claimed in claim 8.

10. A bomb incorporating a warhead as claimed in claim 8.

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