[0001] The present invention is concerned with ammunition projectiles having frangible bodies
(that is, bodies which fragment upon impact with a target).
[0002] It is known that ricochet of ammunition projectiles, such as target practice rounds,
can give rise to undesirable hazards, particularly when the projectile is fired from
an aircraft at a low angle relative to the target. This phenomenon of ricochet is
illustrated, by way of example, in Figure 1 of the accompanying drawings, in which
the dimensions shown are illustrative of those encountered using 20 mm. ammunition.
[0003] Projectiles having frangible bodies (instead of bodies of conventional materials
such as steel) have been proposed, for example, in U.S. Patents 2,995,090, 3,570,406,
3902,683 and 3,951,035. Such projectiles generally have a body which is encapsulated
in a polymeric material and/or formed from metal particles bonded with a polymeric
binder. Such bodies require special processing.
[0004] We have now developed a frangible ammunition projectile which requires neither a
polymeric binder nor an encapsulating polymer.
[0005] According to the invention, there is provided a frangible ammunition projectile,
at least the body of which is a die-casting formed of a brittle zinc-based alloy.
[0006] The projectiles according to the invention may be, for example, target practice rounds
or rounds for short-range use.
[0007] The zinc-based alloy which constitutes the body of the projectile according to the
invention should be one which consists of a zinc matrix and one or more embrittling
alloying elements (that is, elements which provide easy paths of fracture,for example,
along grain boundaries of intermetallic compounds formed by the zinc matrix and the
alloying element(s) ). The alloy preferably contains at least 80% by weight, more
preferably, at least 85% by weight of zinc. Such a zinc-based alloy preferably contains
aluminium in an amount of up to 12% by weight (more preferably 8 to 12% by weight)
and, optionally, a minor amount of other metals such as copper or copper and magnesium,
the latter being preferably present in an amount of up to 0.1% by weight. Other zinc-based
alloys which may be employed include alloys containing manganese,cadmium, antimony,
tin, magnesium, copper, nickel, cobalt, or iron.
[0008] The exact choice of ingredients for the brittle alloy depends on a number of criteria,
such as the size and design of the projectile body, the ; nature of the expected impact
with the target and the launch stresses to be encountered. In particular, the alloy
preferably has a dynamic yield strength ; of more than 35 ksi; this enables the body
to survive typical launch stresses consistently, so that ballistically consistent
results can be obtained.
[0009] Examples of suitable zinc-based alloys for use according to the invention are given
in the I following Table, together with their dymamic yield strengths and, in some
cases, their ability to survive a typical launch stress.
[0010]

[0011] The physical properties of such alloys may be modified, for example, by heat treating,
or quenching cycles. Such modifying treatments are desirably effected when they increase
the dynamic yield strength and thereby promote resistance to launch stress. For example,
we have found that heat treatment of certain alloys (such as alloys 5 and 8 identified
in the above Table) at 360°C for 1 to 4 hours results in improved physical properties
for use according to the invention.
[0012] As mentioned above, the body of the projectile is a die casting. This may constitute
the whole of the projectile or there may be a separate nose-tip of the same material
or of a different material, or a core of a different material. When a core or separate
nose-tip is employed, it may be of aluminium, graphite-epoxy (or other plastics material)
or graphite, for example.
[0013] A rotating band (for example, of zinc, copper or plastics) may be applied to the
projectile, as is conventional.
[0014] An embodiment of the present invention will now be described with reference to Figure
2 of the accompanying drawings, which is an exploded view of a projectile having a
hollow die-cast frangible body and a frangible body cap adapted to fit in the hollow
body.
[0015] The frangible body shown is trimmed, sized and machined as necessary to the desired
dimensions after die casting and then a rotating band is applied as described above.
[0016] The body cap may be fabricated from a variety of materials, including aluminium alloys
(such as 6061) or the same zinc-based alloy as the body. The cap may be a die casting,
but it may also be made by screw machining. After fabrication, the cap is press-fitted
into the body.
1. A frangible ammunition projectile, characterised in that at least the body of the
projectile is a die-casting formed of a brittle zinc-based alloy.
2. A projectile according to claim 1, in which the alloy contains up to 12% by weight
of aluminium.
3. A projectile according to claim 2, in which the alloy contains a minor amount of
copper.
4. A projectile according to claim 2 or 3, in which the alloy contains up to 0.1%
by weight of magnesium.
5. A projectile according to any of claims 1 to 4, in which the alloy has a dynamic
yield strength of more than 35 ksi.