NZ733335B2 - Projectile with reduced ricochet risk - Google Patents

Abstract

The invention relates to a projectile (5) with a frangible material for short-trajectory ammunition. In order that there are no great losses of precision and that the internal ballistic loading is not so great as to lead to destruction of the projectile, it is proposed according to the invention that the projectile (5) consists of a brass casing (4), the casing (4) has, seen in the direction of flight, a front cylindrical receiving space (4a) and a rear cylindrical receiving space (4b), the two receiving spaces (4a, 4b) are arranged coaxially in relation to the longitudinal axis (15) of the projectile and are separated from one another by a separating wall (16), the separating wall (16) forms the base (18) of the front receiving space (4a) and a core (1) of a frangible material is inserted in the front receiving space (4a), the core (1) protrudes with its tip (17) out of the front receiving space (4a) and, in the region of the separating wall (16), the casing (4) incorporates at least one predetermined breaking location (2), running around the casing (4). t the projectile (5) consists of a brass casing (4), the casing (4) has, seen in the direction of flight, a front cylindrical receiving space (4a) and a rear cylindrical receiving space (4b), the two receiving spaces (4a, 4b) are arranged coaxially in relation to the longitudinal axis (15) of the projectile and are separated from one another by a separating wall (16), the separating wall (16) forms the base (18) of the front receiving space (4a) and a core (1) of a frangible material is inserted in the front receiving space (4a), the core (1) protrudes with its tip (17) out of the front receiving space (4a) and, in the region of the separating wall (16), the casing (4) incorporates at least one predetermined breaking location (2), running around the casing (4).

Description

Projectile with reduced ricochet risk 1. FIELD OF THE INVENTION The invention relates to a projectile which is partly made of a frangible material, for range ammunition. 2. BACKGROUND OF THE INVENTION Short-range ammunition has the purpose of enabling the use of larger calibers in smaller training areas. A r drop in speed is generated by structural measures. This can be realized with a low tile weight. A further option is a cation of the external projectile geometry.

There are various basic principles in this case, such as a reduction of the stabilization (GD) resulting from an aerodynamically unfavorable front or rear end, or a desired pressure reduction over the firing process, thereby reducing the acceleration of the projectile.

Frangibility is a property of special projectiles, and means that the projectile material is designed so that the projectiles nt into small particles upon impacting hard targets.

Frangible tion already exists in an enormous variety. In particular, projectiles with a polymer matrix or with a metal matrix are known. The purpose in this case is to achieve crumbling of the projectile into the smallest le particles upon impact on a hard surface. The particles have low sectional density. The result is a l potential hazard for nearby objects. However, frangible projectiles are relatively difficult to use. For larger rs, the radial force arising from the spin can result in the projectile bursting in the air.

Figure 1 shows a cartridge with a frangible projectile 12 according to the prior art. The frangible projectile 12 is inserted into a casing 13, n the ogive of the projectile 12 protrudes from the casing 13. After the frangible projectile 12 impacts, by way of example, a steel plate, the frangible projectile 12 breaks apart into dust 14.

One or more of the following problems exist with short-range projectiles: - Short-range projectiles can have significant losses of precision due to the modified geometry.

- Light short-range projectiles demonstrate a problematic reloading behavior, since a consistent recoil is required for the reloading nt.

- If a range ricochet occurs, there is a considerable danger for the shooter and for third parties.

- Degradation on the rotor blade or propellers of aircraft and helicopters due to plastic caps discharging.

- Purely frangible projectiles have the problem, in the case of large ammunition types, that the internal ballistic load is so great that it leads to the destruction of the projectile. t this background, it would advance frangible projectile development by making available a tile that tes or fully addresses one or more of the aforementioned disadvantages. 3. SUMMARY OF THE INVENTION In accordance with the present invention there is ed a projectile sing (i.e. having) a frangible core and a shell made of brass, n the shell, viewed in flight direction of the projectile, has a front cylindrical receiving space and a rear cylindrical receiving space, both receiving spaces being arranged coaxially with a longitudinal axis of the projectile and separated from each other by a partition wall, the partition wall forming a floor of the front receiving space, wherein the core made of a frangible material is inserted into the front receiving space and has a core tip protruding out of the forward receiving space, and wherein at least one predetermined breaking point which runs around the circumference of the shell is formed in the shell in the region of the partition. Due to the modified geometry there is no loss of precision and the internal ballistic load is not so great that it leads to the destruction of the projectile. In addition, a groove or spiral formed in the front space can have further predetermined breaking points.

In an advantageous embodiment according to the invention, a tracer composition is arranged in the rear receiving space of the tile shell. The rear receiving space lends itself to this, and the tracer composition even desirably shifts the center of y slightly toward the rear, thereby improving the flight path.

The core is preferably glued or press-fitted into the front receiving space. Both are appropriate fixing methods which lead to a desired anchoring of the core at the shell.

To direct away compressed air, in particular in the case of press-fitted cores, in an ageous embodiment the core has bevels or s on its outer surface running from the rear end up to the front end of the shell, el to the projectile longitudinal axis. In another embodiment, a bore hole is arranged in the partition wall, connecting the front receiving space to the rear receiving space. This also directs away the compressed air formed during impact of the projectile on a hard e. A blind hole with a connection to the front receiving space can also be constructed in the partition wall. This blind hole also functions to reduce pressure.

In a specific embodiment, two circumferential predetermined breaking points g around the circumference of the shell are formed in the shell in the region of the ion, wherein one predetermined breaking point is formed in the rear end of the partition wall, as seen in the direction of flight. The predetermined breaking points are preferably formed at a right angle to the projectile longitudinal axis, and are V-shaped or U-shaped in cross-section. These predetermined breaking points improve the tation behavior.

In a specific embodiment, the inner wall of the front receiving space has one or more s which are parallel to the projectile axis or run in a spiral pattern. This improves the anchoring of the frangible core in the front ing space.

The invention and other features thereof are explained in greater detail below by way of nonlimiting embodiments and with reference to the accompanying drawings. 4. BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 illustrates a prior art projectile, one in partial section, as described above; Figure 2 illustrates in longitudinal section a first embodiment of a projectile according to the invention; Figure 3 illustrates schematically forces and res arising upon impact of a projectile according to the ion on a hard surface; and Figure 4 illustrates in udinal section another embodiment of a projectile according to the invention.

. DETAILLED DESCRIPTION OF PREFERRED EMBODIMENTS OF THE INVENTION Figure 2 rates in longitudinal section a first embodiment of a projectile according to the invention, ting of a shell 4 made of brass and a frangible core 1. The shell 4 has, seen in the direction of flight 19, a front cylindrical receiving space 4a and a rear cylindrical receiving space4b in the projectile tail 11. The front receiving space 4a is formed from the front, and the rear receiving space 4b is formed from the rear, of the shell 4. Both receiving spaces 4a, 4b are arranged coaxially with the projectile longitudinal axis 15 of the projectile, and are separated from each other by a ion wall 16. The partition wall 16 forms the floor of the front receiving space 4a. The ble core 1 is inserted into the front receiving space 4a, and anchored therein, preferably via a press fit. The front tip 17 of the frangible core 1 projects out of the front receiving space 4a and/or the shell 4. A tracer composition (not shown in the figure) is inserted in one ment of the invention in the rear receiving space 4b. A groove providing a predetermined breaking point 2 is formed in the shell 4 adjoining the partition wall 16 and extends around the circumference of the shell 4. This predetermined breaking point 2 is formed at a right angle to the projectile longitudinal axis 15, and can have a rectangular cross-section, as shown. However, a V-shaped predetermined breaking point 2 is preferred, as shown in the tile embodiment of Fig 4.

The external geometry of the projectile, consisting of ble core 1 and shell 4, largely corresponds to a known and proven short-range projectile of the applicant. This projectile meets requirements in terms of precision, loading safety, and trajectory. The risk to the surroundings is reduced by two systems. On the one hand, core 1 which is made of frangible material is inserted into the shell 4 from the front, as seen in the shooting direction. A “frangible core” means a core which breaks apart—for e, to dust—upon impact with a hard target. On the other hand, predetermined breaking points 2 are formed at the tile tail 11 so that the residual mass of the individual parts corresponds at most to the mass of a conventional small-caliber projectile.

The shell 4 of the projectile is advantageously made of brass. With brass as the shell material, the projectile according to the invention will largely be broken apart to dust upon impact. This was surprising for a person skilled in the art, and not predicted. Upon the impact of the projectile 5 against a hard target 17 (see Figure 3), the frangible core 1 is pressed into the shell 4. During this pressing, the frangible core 1 abruptly produces a high hydrostatic pressure (see arrows 20 in Figure 3). This causes a splintering of the majority of the projectile. The brass of the shell 4 naturally demonstrates a brittle behavior over such a short stress period. The xial stress state when the frangible core 1 bursts also supports the brittle behavior of the brass of the shell 4. In this way, the impact energy is reduced to an extreme degree, and nearly negated. The rest of the projectile then breaks apart into lighter parts as consequence of the presence of the defined predetermined ng point 2. These individual parts have very low sectional density due to their ry. This significantly decreases the risk to the surroundings. In a particularly advantageous solution, the frangible core 1 of the projectile is a sub-caliber projectile which is simply inserted into the front receiving space 4a. The attachment between the shell 4 and the ble core 1 can be realized by means of an adhesive or through press fit. If a press fit is selected, lateral bevels on the core can direct the ssed air away. A r ility is that the ssed air is ed away, when the projectile is assembled, by a bore hole in the projectile longitudinal axis 15 through the partition 16, or by a blind bore in the partition wall, so that the pressure can be minimized. The projectile tail 11 is also made of brass, since brass is suitable for press-fitting tracer compositions.

Figure 4 shows another embodiment of a projectile 5 according to the ion, consisting of a shell 4 made of brass and a frangible core 1. The shell 4 has in this case as well, seen in the direction of flight 19, a front cylindrical receiving space 4a and a rear cylindrical receiving space 4b in the projectile tail 11. The front receiving space 4a is made through the front, and the rear receiving space 4b is made through the rear, of the shell 4. Both ing spaces 4a, 4b are arranged coaxially with the projectile longitudinal axis 15 of the projectile, and are separated from each other by a partition wall 16. The partition wall 16 in this embodiment is substantially r than in the embodiment of Fig 2. The partition wall 16 in this case also forms the floor of the front receiving space 4a. The frangible core 1 is inserted into the front receiving space 4a, and anchored therein preferably via press fit. The front tip 17 of the ble core 1 projects in this case as well out of the front receiving space 4a and/or the shell 4. A tracer composition (not shown in the figure) can be inserted in the rear receiving space 4b. A groove-like predetermined breaking point 2a running around the circumference of the shell 4 is formed on the shell 4 adjoining the rear segment—seen in the shooting direction—of the partition wall 16. In the embodiment shown here—also seen in the shooting direction—a further predetermined breaking point 2b is also formed on the front t of the partition wall 16. The se predetermined breaking points 2a, 2b are formed at a right angle to the projectile longitudinal axis 15 and are V-shaped in cross-section.

Claims (10)

Claims

1. A projectile for short-range ammunition, comprising: a shell made of brass, the shell, seen in a direction of flight of the projectile, having a front cylindrical ing space and a rear cylindrical receiving space, both receiving spaces being arranged coaxially with a longitudinal axis of the projectile and separated from each other by a partition which forms a floor of the front receiving space; and a core made of a frangible al inserted into the front ing space, the core having a tip protruding out of the front receiving space, characterized in that at least one predetermined breaking point, which runs around the circumference of the shell, is formed in the shell in the region of the partition.

2. A tile according to claim 1, characterized in that a tracer composition is received in the rear receiving space.

3. A projectile according to claim 1 or 2, characterized in that the core is glued or press-fitted into the front receiving space.

4. A projectile according to any one of the claims 1 to 3, characterized in that the core has on an outside surface thereof bevels or s g parallel to the projectile longitudinal axis from a rear end thereof to the front end of the shell.

5. A projectile according to any one of the claims 1 to 4, characterized in that a bore hole extending through the partition wall connects the front receiving space to the rear ing space of the shell.

6. A projectile according to any one of the claims 1 to 5, characterized in that a blind bore is present in the partition wall and has a connection to the front receiving space.

7. A projectile according to any one of the claims 1 to 6, characterized in that two of said predetermined breaking points, which run around the circumference of the shell, are formed on the shell in the region of the partition wall, wherein one predetermined breaking point is formed at a rear end of the partition wall as seen in the direction of flight.

8. A projectile according to any one of claims 1 to 6, characterized in that the at least one predetermined breaking point is formed at right angles to the projectile longitudinal axis and is V-shaped or U-shaped in cross-section.

9. A projectile according to claim 7, terized in that the two predetermined breaking points are formed at right angles to the projectile longitudinal axis and are V-shaped or U- shaped in cross-section.

10. A projectile according to any one of the claims 1 to 9, characterized in that the front receiving space has an inner wall with one or more notches which are el to the projectile axis or run in a spiral.