NZ720372B2 - Cartridge - Google Patents
Cartridge Download PDFInfo
- Publication number
- NZ720372B2 NZ720372B2 NZ720372A NZ72037214A NZ720372B2 NZ 720372 B2 NZ720372 B2 NZ 720372B2 NZ 720372 A NZ720372 A NZ 720372A NZ 72037214 A NZ72037214 A NZ 72037214A NZ 720372 B2 NZ720372 B2 NZ 720372B2
- Authority
- NZ
- New Zealand
- Prior art keywords
- projectile
- case mouth
- receiving space
- guide band
- case
- Prior art date
Links
- 239000000700 tracer Substances 0.000 claims description 6
- UONOETXJSWQNOL-UHFFFAOYSA-N Tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 3
- 239000004922 lacquer Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 3
- 239000010936 titanium Substances 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- 230000000977 initiatory Effects 0.000 claims description 2
- 239000000565 sealant Substances 0.000 claims 2
- 238000010304 firing Methods 0.000 abstract description 5
- 238000007789 sealing Methods 0.000 description 5
- 210000001331 Nose Anatomy 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 230000000875 corresponding Effects 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/02—Driving bands; Rotating bands
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/025—Cartridges, i.e. cases with charge and missile characterised by the dimension of the case or the missile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/067—Mounting or locking missiles in cartridge cases
Abstract
The invention relates to a cartridge (10) with a projectile (11) and a case (12), which is drawn onto the projectile (11) from behind and has a case mouth (13) at the front end. The projectile (11) has a tip (1) which goes over at the rear into a circumferential front guide band (4). The projectile further has a circumferential rear guide band (8). A circumferential case mouth receiving space (15) is located between the front (4) and rear (8) guide bands, and is engaged by the case mouth (13) of the cartridge (10). The front (4) and rear (8) guide bands defines the outside diameter of the projectile. An exposed portion (16) of the case mouth receiving space (15) of the projectile (11) is situated between the front guide band (4) and the case mouth such that the case mouth does not completely fill the case mouth receiving space (15) in the direction of the tip (1) of the projectile. The projectile advantageously occupies greater amount of the firearm barrel twistless freebore, enabling early build up of gas pressure during firing of the cartridge. further has a circumferential rear guide band (8). A circumferential case mouth receiving space (15) is located between the front (4) and rear (8) guide bands, and is engaged by the case mouth (13) of the cartridge (10). The front (4) and rear (8) guide bands defines the outside diameter of the projectile. An exposed portion (16) of the case mouth receiving space (15) of the projectile (11) is situated between the front guide band (4) and the case mouth such that the case mouth does not completely fill the case mouth receiving space (15) in the direction of the tip (1) of the projectile. The projectile advantageously occupies greater amount of the firearm barrel twistless freebore, enabling early build up of gas pressure during firing of the cartridge.
Description
– 1 –
Cartridge
1. FIELD OF THE INVENTION
The invention relates to a cartridge, such as but not limited to a firearm cartridge.
2. BACKGROUND OF THE INVENTION
Patent document EP 1 774 251 B1 discloses a cartridge comprised of a projectile
and a case which is drawn onto a rear of the projectile from behind. To this end,
the case has a case mouth at the front end. The projectile has a tip, a
circumferential front guide band into which a rear of the tip merges and which
defines an outside diameter of the projectile, and a circumferential case mouth
receiving space directly adjoining this front guide band in a direction towards the
projectile base, the case mouth receiving space extending in an axial direction of
the projectile engaging with the case mouth of the cartridge’s case.
It would be advantageous to make available a cartridge which improves upon
the cartridge disclosed in the EP document in such a way that the twistless
freebore is reduced to a minimum during firing. Likewise, it would be
advantageous to provide a projectile – case arrangement enabling early build up
of gas pressure during firing of the cartridge. A further benefit would follow by an
arrangement which seals off the case mouth with respect to the projectile against
moisture ingress.
3. SUMMARY OF THE INVENTION
In accordance with the present invention, there is provided a cartridge,
comprising a projectile and a case drawn from behind onto the projectile, a front
end of the case having a case mouth, the projectile having a tip merging at a rear
thereof into a circumferential front guide band, the projectile further having a
– 2 –
circumferential case mouth receiving space directly adjoining the front guide
band and extending in an axial direction of the projectile toward a base of the
projectile, the projectile further having a circumferential rear guide band between
the case mouth receiving space and the base of the projectile, the front guide
band and the rear guide band defining an outside diameter of the projectile, the
case mouth engaging the projectile in the case mouth receiving space, wherein
an exposed portion of the case mouth receiving space extending in the axial
direction of the projectile is situated between the front guide band and the case
mouth such that the case mouth does not completely fill the case mouth
receiving space in the direction of the tip of the projectile.
Due to the exposed portion of the case mouth receiving space which extends in
the axial direction of the projectile being situated between the front guide band
and the case mouth, i.e., the case mouth not completely filling the case mouth
receiving space towards the nose of the projectile, the front guide band is shifted
forward toward the tip, as a result of which the twistless freebore is reduced to a
minimum. In addition, a receiving space is thus created which may be filled with a
sealing means, thus sealing off the case mouth with respect to the projectile
against moisture ingress.
It is thus preferred for the exposed portion of the case mouth receiving space to
be sealed off with a sealing means, for example a lacquer.
In one embodiment, the projectile tip merges via one or more shapes into the
front guide band, i.e., on the outside diameter of the projectile, in an ogival or
conical manner. The transitional shape at the guide band from the tip to the guide
band optimally has a conical shape at the angle of the transition cone of the
cartridge chamber. The increase in the outside diameter of the projectile thus
achieved reduces the twistless freebore and builds up the gas pressure. The
– 3 –
conical shape at the guide band brings about centering of the projectile with
respect to the barrel bore axis. Centering produced in this way results in
improved precision.
The exposed portion of the case mouth receiving space may merge into the front
guide band in a concave, convex, or linear manner. If the exposed portion of the
case mouth receiving space merges linearly into the front guide band, this linear
transition preferably extends at an angle of less than or equal to 16 degrees with
respect to the projectile axis. This angle of ≤ 16° with respect to the projectile
axis is preferred for aerodynamic reasons.
One embodiment is characterized in that from the radially lowest location in the
case mouth receiving space, i.e., the field diameter or smaller, the shape of the
projectile toward the rear transitions via one or more shapes to the diameter of
the projectile or smaller in a concave, convex, or linear manner. The front guide
band in the outside diameter of the projectile allows a smaller design of the rear
part of the projectile, since this part is not necessary for the pressure build-up. In
addition, the barrel load (frictional resistance and associated barrel heating and
barrel deposits) are thus also reduced. The projectile is ideally shaped in such a
way that it is suitable for sealing off the case mouth with respect to the projectile
and for pinching the case mouth.
In one design, a receiving space containing a material that produces a tracer
upon initiation is situated at the rear of the projectile. This is referred to as a
tracer projectile or a tracer cartridge.
In one embodiment, a borehole which is coaxial with respect to the projectile axis
is provided in the projectile, the borehole being open toward the projectile tip, and
a projectile core made of tungsten or tungsten carbide is situated in the borehole,
– 4 –
and the borehole is closed by a projectile tip insert made of titanium or zirconium,
the outer shell of the projectile tip insert being a part of the tip of the projectile.
This is referred to as an armor-piercing incendiary (API) projectile or API
cartridge.
In principle, the embodiment with the guide band shifted to the front is
transferable to other types of projectiles. Examples of other types of projectiles
are armor-piercing (AP) projectiles, partial fragmentation projectiles, full metal
jacket projectiles, monolithic projectiles, deformation projectiles, and others.
The above and other features of the invention’s cartridge are explained in greater
detail below with reference to a number of preferred, non-limiting cartridge
embodiments illustrated in the accompanying drawings.
4. BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1a shows a side plan view, partially in section, of a cartridge according
to the invention;
Figure 1b shows an enlarged detail view A from Figure 1a;
Figure 2 shows the projectile of the cartridge according to Figures 1a and
1b; and
Figure 3 shows in longitudinal section the cartridge according to the
invention, inserted into a barrel of a weapon.
. DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
Same reference numerals are used throughout the figures to denote same
features.
The cartridge 10 is made up of a projectile 11 and a case 12 which is mounted
on the projectile 11 from behind and which has a case mouth 13 at the front end,
– 5 –
wherein the projectile 11 has a tip 1, and at the rear this tip 1 merges into a
circumferential front guide band 4 which defines the outside diameter of the
projectile. Directly adjoining this front guide band 4 in the direction of the
projectile base 14, a circumferential case mouth receiving space 15, which
extends in the axial direction of the projectile 11 and in which the case mouth 13
engages, is situated in the projectile 11. An exposed portion 16 of the case
mouth receiving space 15 extending in the axial direction of the projectile 11 is
situated between the front guide band 4 and the case mouth 13. Therefore, the
case mouth 13 does not completely fill the case mouth receiving space 15 in the
direction of the nose of the projectile 11. The case mouth 13 thus fills only a
portion of the case mouth receiving space 15, and the remaining portion is
situated outside the case 12.
Due to the front guide band 4, also referred to below as the outside diameter of
the projectile, being shifted to the front on the projectile 11, the twistless freebore
is reduced to a minimum during firing. Likewise, due to the front guide band 4,
the gas pressure is built up early, thus making it possible to design the area
behind the front guide band 4 with a smaller diameter. A decrease in the
diameter reduces the projectile friction in the barrel 23. Less heat energy is
generated due to the lower friction, thus delaying the heating of the barrel 23.
The precision is increased and is maintained for a longer time. The reduced
projectile friction results in increased velocity, which produces a longer trajectory.
As a result of the exposed portion 16 of the case mouth receiving space 15, the
case mouth 13 and an area 7 of the case mouth receiving space 15 may be
easily sealed off from any form of moisture, for example by means of a lacquer in
this exposed portion 16 of the case mouth receiving space 15.
The projectile tip 1 may be round, flat, or pointed.
– 6 –
The projectile tip 1 extends via one or more shapes in an ogival 2 or conical
manner, such as concave, convex, or linear 3, up to the outside diameter of the
projectile, i.e., up to the front guide band 4. The transitional shape at the guide
band from the tip to the guide band is optimally conical at the angle of the
transition cone of the cartridge chamber. The conical shape at the guide band
brings about centering of the projectile with respect to the barrel bore axis.
Centering produced in this way results in improved precision.
The increase in the outside diameter of the projectile thus achieved is intended to
reduce the twistless freebore and build up the gas pressure. The outside
diameter of the projectile or the front guide band 4 in any caliber is defined by the
largest permissible diameter of the projectile. In CIP member states, this is the
value "G1" for a "maxi cartridge."
In a departure from the outside diameter mentioned above, the defined maximum
permissible diameter of the projectile is used in the military and governmental
sectors. The tolerance range at the front guide band 4 is -0.1 mm with respect to
the permissible diameter of the projectile.
The outside diameter of the projectile or the axial extension of the front guide
band is maintained only temporarily, and for aerodynamic reasons gradually
tapers linearly 5 to a diameter corresponding to the field diameter 6 or smaller.
The distance between the frontmost guide band 4 and the field diameter 6
depends on the caliber, with different transition lengths. However, the front guide
band 4 is positioned in such a way that preferably little or no twistless freebore is
present. It is essential to have a distance between the case mouth 13 and the
frontmost guide band 4.
– 7 –
The field diameter 6 at the lowest point of the case mouth receiving space 15 is
defined in each caliber. In CIP member states, this is the value "F" for "mini
cartridge chamber." In a departure from the field diameter 6 mentioned above,
the minimum permissible field diameter of the projectile is used in the military and
governmental sectors. The tapering shape may extend in a concave, convex, or
linear manner. An angle 9 of ≤ 16° with respect to the projectile axis 17 is
preferred for aerodynamic reasons. For radii, the angle of the resulting straight
lines between the front guide band 4 and the field diameter 6 is used.
From the field diameter 6 or smaller, the shape of the projectile extends via one
or more shapes to the rear in a concave, convex, or linear 7 manner (see Figure
1b) on the diameter of the projectile. The projectile 7 is ideally shaped in such a
way that it is suitable for sealing off the case mouth 24 and for pinching the case
The projectile 11 is cylindrical or is provided with rear guide bands 8 in the area
of the case neck 24.
A receiving space 19 at the rear of the projectile 11 may contain a material which
produces a tracer. This is referred to as a tracer projectile.
A borehole 20, which is coaxial with respect to the projectile axis 17, is preferably
provided in the projectile 11 (see Figure 3), the borehole being open toward the
projectile tip 1, and a projectile core 21 made of tungsten or tungsten carbide is
situated in the borehole 20, and the borehole 20 is closed by a projectile tip insert
22 made of titanium or zirconium, the outer shell of the projectile tip insert 22
being a part of the tip 1 of the projectile 11.
– 8 –
Claims (10)
1. A cartridge, comprising a projectile and a case drawn from behind onto the projectile, a front end of the case having a case mouth, the projectile having a tip merging at a rear thereof into a circumferential front guide band, the projectile further having a circumferential case mouth receiving space directly adjoining the front guide band and extending in an axial direction of the projectile toward a base of the projectile, the projectile further having a circumferential rear guide band between the case mouth receiving space and the base of the projectile, the front guide band and the rear guide band defining an outside diameter of the projectile, the case mouth engaging the projectile in the case mouth receiving space, wherein an exposed portion of the case mouth receiving space extending in the axial direction of the projectile is situated between the front guide band and the case mouth such that the case mouth does not completely fill the case mouth receiving space in the direction of the tip of the projectile.
2. The cartridge according to claim 1, wherein the exposed portion of the case mouth receiving space is sealed off with a sealant.
3. The cartridge according to claim 1 or 2, wherein the projectile tip merges via one or more shapes into the front guide band on the outside diameter of the projectile in an ogival or conical manner.
4. The cartridge according to any one of claims 1 to 3, wherein the exposed portion of the case mouth receiving space merges into the front guide band in a concave, convex, or linear manner. – 9 –
5. The cartridge according to claim 4, wherein the exposed portion of the case mouth receiving space merges linearly into the front guide band at an angle of less than or equal to 16 degrees with respect to the projectile axis.
6. The cartridge according to any one of claims 1 to 5, wherein the projectile transitions from a radially lowest location in the case mouth receiving space toward a rear of the projectile via one or more shapes, in a concave, convex, or linear manner, to the outside diameter of the projectile.
7. The cartridge according to any one of claims 1 to 6, wherein a receiving space containing a material that produces a tracer upon initiation is situated at a rear face of the projectile.
8. The cartridge according to any one of claims 1 to 7, wherein a borehole, which is coaxial with respect to an axis of the projectile, is provided in the projectile , the borehole being open toward a front of the projectile, wherein a projectile core made of tungsten carbide is situated in the borehole, and wherein the borehole is closed-off by a projectile tip insert made of titanium, an outer shell of the projectile tip insert being a part of the tip of the projectile.
9. The cartridge according to claim 2, wherein the sealant is a lacquer.
10. The cartridge according to claim 6, characterized the radially lowest location in the case mouth receiving space is a field diameter or smaller.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013017672.7 | 2013-10-25 | ||
DE102013017672 | 2013-10-25 | ||
PCT/EP2014/072866 WO2015059282A1 (en) | 2013-10-25 | 2014-10-24 | Cartridge |
Publications (2)
Publication Number | Publication Date |
---|---|
NZ720372A NZ720372A (en) | 2020-12-18 |
NZ720372B2 true NZ720372B2 (en) | 2021-03-19 |
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