NZ720372B2 - Cartridge - Google Patents

Cartridge Download PDF

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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
Application number
NZ720372A
Other versions
NZ720372A (en
Inventor
Stephan Gelfert
Original Assignee
Ruag Ammotec Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ruag Ammotec Gmbh filed Critical Ruag Ammotec Gmbh
Priority claimed from PCT/EP2014/072866 external-priority patent/WO2015059282A1/en
Publication of NZ720372A publication Critical patent/NZ720372A/en
Publication of NZ720372B2 publication Critical patent/NZ720372B2/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/02Driving bands; Rotating bands
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/025Cartridges, i.e. cases with charge and missile characterised by the dimension of the case or the missile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/067Mounting 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)

Claims 1.
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.
NZ720372A 2013-10-25 2014-10-24 Cartridge NZ720372B2 (en)

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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