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EP3507565B1 - Projectile with penetrator - Google Patents

Projectile with penetrator Download PDF

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Publication number
EP3507565B1
EP3507565B1 EP17764359.0A EP17764359A EP3507565B1 EP 3507565 B1 EP3507565 B1 EP 3507565B1 EP 17764359 A EP17764359 A EP 17764359A EP 3507565 B1 EP3507565 B1 EP 3507565B1
Authority
EP
European Patent Office
Prior art keywords
penetrator
retaining element
bullet
holding element
length
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
EP17764359.0A
Other languages
German (de)
French (fr)
Other versions
EP3507565A1 (en
Inventor
Roger August STADELMANN
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Saltech AG
Original Assignee
Saltech AG
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 Saltech AG filed Critical Saltech AG
Priority to HRP20221423TT priority Critical patent/HRP20221423T1/en
Priority to SM20220501T priority patent/SMT202200501T1/en
Priority to RS20221187A priority patent/RS63869B1/en
Priority to SI201731290T priority patent/SI3507565T1/en
Publication of EP3507565A1 publication Critical patent/EP3507565A1/en
Application granted granted Critical
Publication of EP3507565B1 publication Critical patent/EP3507565B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/06Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators

Definitions

  • the present invention relates to a projectile according to the preamble of claim 1.
  • a hard-core projectile or impact projectile is understood to be a projectile with high penetrating power, which has an armor-piercing effect.
  • Such projectiles are used in particular by snipers and are intended for precise penetration of armored targets such as protective vests for people, armored glass, steel plates or light metal armor. These projectiles use the kinetic energy of their projectile to penetrate the target surface, eliminating the need for explosives or fuses in the projectile itself.
  • the term penetrator is therefore a common term for the projectile.
  • Bullets that have a core with a jacket are referred to as jacketed bullets. The jacket not only protects the barrel but also prevents the core from deforming or shattering when it hits a target.
  • WO 97/41404 discloses a small caliber bullet having a bullet core made of a hard and heavy material, the bullet core being disposed within a hollow bullet jacket.
  • the US 6,374,743 B1 discloses a small caliber projectile with a hard core arranged at the front and a soft core arranged at the rear.
  • the rimfire bullet has a jacket made of steel, plated steel or brass.
  • a hard-core projectile which has a projectile core.
  • a penetrator is inserted into the bullet core and protrudes from the bullet core.
  • the U.S. 2016/153757 A1 relates to a projectile comprising a cylindrical body and a nose connected to the body.
  • the nose includes a tip at a foremost portion and a plurality of cutout portions and cutting edges.
  • a projectile with a carrier body and a high density penetrator is known.
  • a front portion of the carrier body is tapered and extends beyond the front of the penetrator.
  • the EP 0 343 389 A1 relates to a projectile core for a sabot projectile, which has a projectile core tip, a projectile core rear part and a projectile core middle part, which are connected to one another by a mandrel.
  • the core of the bullet is made of brittle tungsten.
  • a particularly preferred object is a Specify a projectile that has a high penetration power and increased precision.
  • a projectile comprising a retaining element and a penetrator is therefore specified, the penetrator being at least partially accommodated in a receiving opening of the retaining element running centrally to the projectile axis and having a penetrator front and a penetrator rear.
  • the penetrator rear is cylindrical and the penetrator front is designed to taper conically from the penetrator rear in the direction of a penetrator tip towards the projectile axis.
  • the length of the penetrator front is in relation to the length of the penetrator rear in an aspect ratio of about 1 to 1, preferably about 1 to 1.5, more preferably about 1 to 2.2.
  • the penetrator has a cylindrical tail and a conical or conical front, with the tail being longer than the front as viewed along the bullet axis.
  • a conical or cone-shaped front means in particular that the front is conical or cone-shaped in the geometric sense. That is, the outer surface preferably runs at a constant angle to the central axis of the penetrator.
  • the cylindrical penetrator tail and the conical penetrator front are formed in a weight ratio of about 2 to 12, preferably about 4 to 10, to each other.
  • the cylindrical penetrator tail has a weight which is about 2 to 12 times greater, preferably about 4 to 10 times greater than the weight of the conical penetrator front.
  • the penetrator front preferably has a cone angle of between 10° and 20°, preferably 13°. This means that the penetrator front, which tapers conically from the rear of the penetrator in the direction of the penetrator tip, has a diameter which becomes smaller along this direction, so that the penetrator front has a smaller diameter in its front area than in its rear area.
  • the penetrator tip may have a flat face extending perpendicular to the bullet axis.
  • the penetrator may have a pointed end.
  • the conically tapering penetrator front thus preferably opens into a penetrator tip, which forms a straight angle.
  • the penetrator tip can be a so-called flat tip.
  • the diameter of the penetrator tip is preferably between about 0.4 and 1.2 mm, more preferably about 0.8 mm.
  • the total length of the penetrator is between 35 mm and 55 mm, preferably 45 mm, and/or that the length of the penetrator front is between 12 mm and 17 mm, preferably 14 mm, and/or that the length of the penetrator tail is between 15 mm and 44 mm, preferably 31 mm.
  • the diameter of the penetrator tail is preferably between 6 mm and 9 mm, preferably 7 mm.
  • the total length of the penetrator ie the sum of the length of the penetrator front and the length of the penetrator tail, and the diameter of the penetrator tail are in a ratio of about 4 to 10, preferably about 5 to 9, to one another.
  • the overall length of the penetrator is about 4 to 10 times longer, preferably about 5 to 9 times longer than the diameter of the penetrator tail.
  • the penetrator is preferably formed in one piece from the penetrator front and the penetrator rear and preferably consists of a material with a higher density than the holding element, in particular tungsten carbide.
  • the penetrator consisting of a material with a high density, which gives the penetrator great strength or hardness.
  • the penetrator is preferably made of an alloy whose main component is tungsten, e.g. However, it is also possible for the penetrator to consist of a single element, e.g. tungsten.
  • the penetrator front and the penetrator rear are not designed as different components, but it is an integrally formed penetrator whose outer shape, viewed from the penetrator tip, is designed in a conical shape and merges into a cylindrical rear area.
  • the penetrator in particular the penetrator front, protrudes from the holding element at the end.
  • the penetrator tail is received with a precise fit in the receiving opening of the holding element.
  • the penetrator can be fastened in the holding element by means of a non-positive connection, such as a press fit, in which the penetrator is pressed into the receiving opening in the holding element.
  • the holding element preferably has a plurality of grooves with a reduced diameter in the region of the middle of the holding element.
  • Other options for attachment are a material connection by soldering or gluing or a form-fitting attachment.
  • the holding element preferably has a frustoconical holding element rear, a cylindrical holding element center and a holding element front, which is designed to taper conically from the holding element center in the direction of the penetrator tip towards the projectile axis.
  • the retaining element front forms an extension of the conical tip of the penetrator and runs in the same direction as the conical tip of the penetrator.
  • the front of the holding element has a cone angle of between 10° and 20°, preferably 13°, and/or that the front of the holding element has a wall thickness which decreases continuously in the direction of the penetrator tip and preferably in the transition area between the penetrator front and the penetrator tail is zero so that the entire penetrator front is exposed.
  • the lateral surface of the penetrator front can thus be seen as an extension of the lateral surface of the front of the holding element, which extends along the bullet axis and adjoins the lateral surface of the front of the holding element without a transition.
  • Such a configuration of the projectile's outer surface results in good aerodynamic and ballistic properties.
  • the entire penetrator front therefore preferably protrudes from the holding element and already penetrates the target object before the holding element hits the target object, so that the projectile can very effectively deliver its kinetic energy to the target object.
  • the front of the retaining element it is also possible for the front of the retaining element to also extend at least in regions over the rear of the penetrator, leaving both the penetrator tip and part of the rear of the penetrator uncovered, for example.
  • the rear of the holding element preferably has a truncated cone angle of between 5° and 15°, preferably 9°, and/or the diameter at the end of the truncated cone of the rear of the holding element is preferably between 9 mm and 11 mm, preferably 10 mm, and/or the holding element Tail preferably has a conical indentation.
  • the conical indentation is preferably located in the rear area of the rear of the holding element and serves to improve the flight characteristics of the projectile by stabilizing it.
  • the diameter of the middle of the holding element is preferably between 12.5 mm and 13.5 mm, preferably 12.98 mm, and/or the lateral surface of the middle of the holding element preferably has circumferential grooves.
  • the grooves can be arranged in a rear area of the middle of the holding element.
  • a front area of the center of the retaining element or the entire center of the retaining element is provided with grooves.
  • Two or more grooves are preferably provided, which are formed directly adjacent to one another in the lateral surface of the middle of the holding element, starting from the rear end of the middle of the holding element in the direction of the front end of the holding element. It is possible that the grooves are each arranged at the same distance from one another on the lateral surface. Alternatively, however, the grooves can also be at different distances from one another. For example, four grooves can be provided, with the distance between two adjacent grooves increasing progressively, starting from the rear end in the direction of the front end of the center of the holding element.
  • first two grooves in relation to the rear end of the middle of the holding element can be arranged at a first distance from one another and the last two grooves in relation to the rear end of the middle of the holding element can be arranged at a second distance from one another, which is greater or smaller than the first distance be.
  • the grooves each have an identical groove profile, ie have the same groove depth or extend into the lateral surface by the same amount and have the same groove shape.
  • Conceivable groove shapes are, for example, semicircular or U-shaped grooves or rectangular grooves.
  • a semicircular, U-shaped or rectangular groove is understood to mean a groove which delimits a semicircular, U-shaped or rectangular recess.
  • the grooves each have different groove profiles.
  • the clear width of the recess can be the same or different in each case.
  • the groove depth is preferably between 0.5 mm and 2.0 mm, in particular 1.5 mm, and/or the clear width of the grooves is preferably between 1.0 mm and 2.0 mm, in particular 1.6 mm, and/or the distance between two adjacent grooves is preferably between 1 mm up to 2 mm, in particular 1.2 mm. Or to put it another way, the groove depth is preferably about one third of the clear width up to twice the clear width, in particular half the clear width up to once the clear width of the recess. The distance between two adjacent grooves is preferably half the clear width up to twice the clear width, in particular the distance corresponds approximately to the clear width.
  • the circumferential grooves are designed to interact with correspondingly designed trains in a gun barrel and serve to reduce the friction of the bullet in the gun barrel, lead to less barrel erosion and thus increase the service life of the weapon.
  • the grooves lead to an increase in performance.
  • the friction reduction of the grooves and the material hardness and mass of the penetrator mean that the projectile hits a target with a high penetrating power and can penetrate steel plates, for example.
  • the holding element is preferably formed in one piece from the rear holding element, the center holding element and the front holding element and is preferably made of brass and/or brass alloys.
  • the retaining element front, the retaining element center and the retaining element rear are not formed as different components but are formed integrally, with the outer shape of the retaining element, viewed from the penetrator tip, in is conical in shape and merges into a cylindrical central area and then into a truncated cone-shaped rear area.
  • the overall length of the holding element is preferably between 35 mm and 55 mm, preferably 43 mm, and/or the length of the front of the holding element is preferably between 3 mm and 21 mm, preferably 13 mm, and/or the length of the middle of the holding element is preferably between 14mm and 42mm, preferably 21mm.
  • the penetrator is preferably accommodated completely, and in particular with a precise fit, in the holding element.
  • the penetrator completely fills the receiving opening in the holding element.
  • the holding element preferably has a truncated cone-shaped rear holding element, a cylindrical holding element center and an ogival holding element front, with the holding element front transitioning into a truncated cone shape or dome shape in its front area.
  • the front of the retaining element, the middle of the retaining element and also the rear of the retaining element at least in some areas are encased in a sleeve, with the sleeve preferably being made of brass.
  • the rear area of the rear retaining element can be free of a cover.
  • a rear end of the retaining element that is completely encased that is to say a retaining element that is completely encased overall, is also possible.
  • the cover is preferably designed in such a way that it has the respective shape of the covered holding element area, namely ogival, cylindrical or truncated cone. In this case, it is preferred that the sleeve is directly adjacent to the holding element and is therefore applied directly to it.
  • a compact, rotationally symmetrical and dimensionally accurate projectile which has good penetration properties can be provided by a casing which is in positive contact with the holding element.
  • the sleeve preferably has a thicker wall in the front area of the holding element front, and/or the sleeve preferably has a groove in the area of the middle of the holding element, and/or the sleeve preferably has a rear flange in the area of the holding element rear.
  • the cover encloses an air space with the rear of the retaining element in the region of the rear of the retaining element.
  • the indentation can interact with correspondingly designed rifling in a gun barrel and serves to reduce the friction of the bullet in the gun barrel.
  • the front thickening of the shell reduces ricochets when firing at oblique angles on hard targets and also serves to determine the center of mass of the bullet.
  • the holding element center preferably has a truncated cone with a cone angle between 30° and 50°, preferably 45°, on the front side, and the holding element front preferably has an inner flange with the same cone angle on the rear side and is placed positively on the truncated cone.
  • These cone angles allow an optimal, rotationally symmetrical centering of the front of the holding element on the middle of the holding element and thus also of the penetrator accommodated therein.
  • the center of the retaining element extends beyond the center of the penetrator, starting from the rear of the penetrator in the direction of the penetrator front, and/or that the front of the retaining element extends beyond the tip of the penetrator. In other words, the penetrator tip is completely surrounded by the front of the holding element.
  • the rear holding element and the middle holding element are preferably formed in one piece and consist of a plastic, in particular PET, or steel, and/or the front holding element consists of powdered substances or mixtures such as borax, incendiary or explosive devices.
  • the rear holding element and the center holding element are formed integrally, while the front holding element is a component formed separately therefrom.
  • the penetrator consists of a material with a very high density
  • the holding element has a material or materials with a lower density than the penetrator.
  • the overall length of the holding element is preferably between 53 mm and 55 mm, preferably 54 mm, and/or the length of the front of the holding element is preferably between 22 mm and 28 mm, preferably 26 mm, and/or the length the middle of the holding element is preferably between 19 mm and 25 mm, preferably 21 mm.
  • 10% are retaining element, 50% penetrator and 40% casing, and/or preferably, with a total retaining element mass of 100%, 40% are front retaining element, 50% are middle retaining element and 10% are retaining element -Rear.
  • the Figures 1 to 4 each show a projectile 1, 1' comprising a retaining element 2, 2' and a penetrator 3, which has a penetrator front 4 and a penetrator rear 5.
  • the penetrator rear 5 is cylindrical and the penetrator front 4 is designed to taper conically, starting from the penetrator rear 5 in the direction of a penetrator tip 6 towards the projectile axis A.
  • the overall length LP of the penetrator 3 is 45 mm, the length LPF of the penetrator front 4 being 13 mm and the length LPH of the penetrator rear 5 being 32 mm.
  • the penetrator front 4 has a cone angle aPF of approximately 13° and the penetrator tip 6 has a flat end face 7 which extends perpendicularly to the bullet axis A. Furthermore, the diameter DPH of the penetrator tail 5 is about 7 mm.
  • the penetrator 3 is formed in one piece from the penetrator front 4 and the penetrator rear 5 and consists entirely of tungsten carbide.
  • the holding element 2 has a frustoconical holding element rear 8, a cylindrical holding element center 9 and a holding element front 10, the holding element front 10 tapering conically from the holding element center 9 in the direction of the penetrator tip 6 towards the projectile axis A is trained.
  • the conical holding element front 10 is designed with a cone angle aKF of about 13° and has a wall thickness which tapers continuously in the direction of the penetrator tip 6 and is zero at the point of transition from the penetrator front 4 to the penetrator rear 5 .
  • the whole Penetrator front 4 is therefore exposed.
  • There is a seamless transition between the front retaining element front 10 and the rear penetrator front 4 so that the lateral surface of the penetrator front 4 can be seen as an extension of the lateral surface of the retaining element front 10 .
  • the truncated cone-shaped retaining element rear 5 has a truncated cone angle ⁇ KH of about 9° and the diameter DKH at the truncated cone end of the retaining element rear 8 is about 10 mm.
  • the rear holding element 8 has a conical indentation 11 at the rear, which extends centrally into the rear holding element 8 .
  • the holding element center 9 has a diameter DKM of about 13 mm and circumferential grooves 13 are provided in areas on the outer surface of the holding element center 9, which can interact with correspondingly designed trains in a gun barrel (not shown).
  • four grooves 13a, 13b, 13c, 13d are formed in the lateral surface of the middle holding element 9, with the grooves 13a, 13b, 13c, 13d starting from the rear end of the middle holding element 9 in the direction of the front end of the Retaining element center 9 seen along about half of the lateral surface are arranged immediately adjacent to each other.
  • the first two grooves 13a, 13b seen with respect to the rear end of the holding element center 9 are of identical design here. Both have the same U-shaped groove shape and extend with the same groove depth RTa, RTb into the lateral surface of the middle 9 of the holding element.
  • the clear width of these grooves is the same in each case.
  • the distance RTa between these two grooves 13a, 13b corresponds approximately to the groove depth RTa, RTb or the clear height of these grooves 13a, 13b.
  • the two further two grooves 13c, 13d arranged following these two grooves 13a, 13b each have a rectangular groove shape and differ in their clear width both from the first two grooves 13a, 13b and from each other.
  • the rectangular grooves 13c, 13d each have a smaller groove depth RTc, RTd than the U-shaped ones Grooves 13a, 13b.
  • the rectangular groove 13c arranged adjacent to the U-shaped groove 13b extends into the lateral surface by a much smaller amount than is the case with the other rectangular groove 13d. While the rectangular groove 13c and the U-shaped groove 13b arranged adjacent to it are arranged at a distance RAb from one another which approximately corresponds to the distance RAa between the two U-shaped grooves, the distance RAc between the two rectangular grooves 13c, 13d however, significantly smaller.
  • the groove depth RTa, RTb of the first and second U-shaped grooves 13a, 13b is approximately one eighth of the diameter DKM of the middle of the holding element.
  • the groove depths RTc, RTd of the third groove 13c, which is arranged adjacent to the U-shaped groove 13b, and the fourth groove 13d, which is arranged adjacent to the third groove 13c, are approximately a factor of 30 and 15 respectively smaller than the diameter DKM Retainer center.
  • groove arrangement and groove design is not limited to the grooves shown here. Instead, fewer or more than four grooves can be provided, which have the same or different groove profiles and/or are arranged at the same or varying distances from one another.
  • the holding element 2 is formed in one piece from the holding element rear 8, the holding element center 9 and the holding element front 10 and consists entirely of brass.
  • the total length LK of the holding element 2 is about 46 mm here, the length LKF of the holding element front 10 being about 14 mm, the length LKM of the holding element middle 9 being about 22 mm, and the length LKH of the holding element rear 8 being about 10 mm .
  • the projectile 1 here consists solely of the holding element 2 and the penetrator 3 and is in particular designed without a casing.
  • the retaining element 2' of the projectile 1' has, analogously to the retaining element 2 of the projectile 1, a frustoconical retaining element rear 8' and a cylindrical retaining element center 9'.
  • the retaining element 2' of the projectile 1' has an ogival retaining element front 10' which transitions into a dome shape in its front region 14.
  • the diameter DKM' of the middle 9' of the holding element is approximately 11 mm.
  • the rear holding element 8' has a truncated cone angle ⁇ KH' of approximately 9°, the diameter DKH' at the truncated cone end of the rear holding element 8' being approximately 8.5 mm.
  • the holding element center 9' has a truncated cone 19 with a cone angle ⁇ KM of approximately 45° at the front and the holding element front 10' has an inner cone 20 with the same cone angle ⁇ KF of approximately 45° at the rear, with the inner cone 20 forming a positive fit on the truncated cone 19 is put on.
  • the holding element center 9' extends in the direction of the penetrator front 4 beyond the center M of the penetrator 3, and the holding element front 10' extends in the same direction beyond the penetrator tip 6.
  • the rear holding element 8' and the middle holding element 9' are designed in one piece and consist of PET or steel.
  • the separately formed holding element front 10' consists of borax.
  • the overall length LK' of the holding element 2' is approximately 54 mm, the length LKF' of the holding element front 10' being approximately 26 mm and the length LKM' of the holding element center 9' being approximately 21 mm.
  • the penetrator tail 5 of the projectile 1′ has a groove with a reduced diameter in the area of its base and is accommodated with a precise fit in a receiving opening 12′ of the holding element 2′.
  • the receiving opening 12' extends centrally through the holding element center 9' into the holding element rear 8'.
  • the penetrator front 4 is accommodated in a precisely fitting recess in the holding element front 10 ′, which progressively narrows starting from the penetrator rear 5 in the direction of the penetrator front 4 .
  • the holding element front 10', the holding element middle 9' and in some areas also the holding element rear 8' are encased by a cover 15 which corresponds to the respective shape of the encased holding element 2', i.e. ogival in the front area, cylindrical in the middle area and truncated in the rear area.
  • the sleeve 15 consists here entirely of brass and rests directly on the lateral surface of the holding element front 10' and the holding element center 9'.
  • the shell 15 also partially surrounds the rear holding element 8′ and encloses an air space 18 with the rear holding element 8′, which increases in size from the front area to the rear area of the rear holding element 8′.
  • the distance between the sleeve 15 and the lateral surface of the rear holding element 8' is thus increasingly increased in this direction.
  • the sleeve 15 ends at the rear on the rear holding element 8' in a flange 17, leaving a section of the rear holding element 8' free of a sleeve.
  • the penetrator 3 is never in contact with the shell 15.
  • the shell 15 has a thicker wall in the front area of the holding element front 10' and has a groove 16 in the area of the holding element center 9', which has correspondingly designed grooves Trains in a gun barrel (not shown) can interact.
  • the projectile 1' consists here of the holding element 2', the penetrator 3 and the casing 15.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Particle Accelerators (AREA)
  • Toys (AREA)

Description

TECHNISCHES GEBIETTECHNICAL AREA

Die vorliegende Erfindung betrifft ein Geschoss nach dem Oberbegriff von Anspruch 1.The present invention relates to a projectile according to the preamble of claim 1.

STAND DER TECHNIKSTATE OF THE ART

Unter einem Hartkerngeschoss oder Wuchtgeschoss wird ein Projektil mit hoher Durchschlagskraft verstanden, welches über eine panzerbrechende Wirkung verfügt. Solche Geschosse werden insbesondere von Scharfschützen eingesetzt und bezwecken eine präzise Durchdringung von gepanzerten Zielen wie beispielsweise Schutzwesten für Personen, Panzerglas, Stahlplatten oder Leichtmetallpanzerungen. Bei diesen Geschossen wird die kinetische Energie ihres Projektils genutzt, um die Zieloberfläche zu durchdringen, so dass im Geschoss selbst auf Sprengstoff oder Zünder verzichtet werden kann. Der Ausdruck Penetrator ist daher ein gebräuchlicher Begriff für das Projektil. Geschosse, welche einen Kern mit einem Mantel aufweisen, werden als Mantelgeschosse bezeichnet. Der Mantel schützt einerseits den Lauf und verhindert ausserdem eine Verformung oder ein Zersplittern des Kerns beim Auftreffen auf ein Zielobjekt. Während Vollmantelgeschosse den Kern vollständig umgeben und hohe Geschossgeschwindigkeiten erlauben, ist der Kern bei Teilmantelgeschossen an der Spitze nicht von Mantelmaterial umschlossen, so dass beim Auftreffen auf ein Zielobjekt die weniger stabile Spitze des Geschosses durch den hohen Druck beim Aufschlag und beim Durchdringen des Ziels verformt wird und eine effektive Energieabgabe im Zielobjekt bewirkt. Derartige Munition ist in diversen Ausführungen bekannt.A hard-core projectile or impact projectile is understood to be a projectile with high penetrating power, which has an armor-piercing effect. Such projectiles are used in particular by snipers and are intended for precise penetration of armored targets such as protective vests for people, armored glass, steel plates or light metal armor. These projectiles use the kinetic energy of their projectile to penetrate the target surface, eliminating the need for explosives or fuses in the projectile itself. The term penetrator is therefore a common term for the projectile. Bullets that have a core with a jacket are referred to as jacketed bullets. The jacket not only protects the barrel but also prevents the core from deforming or shattering when it hits a target. While full-metal jacketed bullets completely enclose the core and allow high bullet velocities, with soft-jacketed bullets the core is not surrounded by jacket material at the tip, so that when it hits a target, the less stable tip of the bullet is deformed by the high pressure of impact and penetration of the target and causes an effective energy release in the target object. Such ammunition is known in various designs.

So wird in der WO 97/41404 ein kleinkalibriges Geschoss mit einem Geschosskern aus einem harten und schweren Material offenbart, wobei der Geschosskern innerhalb eines hohlen Geschossmantels angeordnet ist.So will in the WO 97/41404 discloses a small caliber bullet having a bullet core made of a hard and heavy material, the bullet core being disposed within a hollow bullet jacket.

Aus der US 3,782,287 ist ein panzerbrechendes Geschoss mit einem Geschossmantel bekannt, wobei ein Hartmetallkern sowie ein Füllmaterial im Geschossmantel angeordnet sind.From the U.S. 3,782,287 an armor-piercing projectile with a projectile jacket is known, with a hard metal core and a filling material being arranged in the projectile jacket.

Die US 6,374,743 B1 offenbart ein Kleinkalibergeschoss mit einem frontseitig angeordneten Hartkern und einem heckseitig angeordneten Weichkern. Das Kleinkalibergeschoss verfügt über einen Mantel aus Stahl, plattiertem Stahl oder Messing.the US 6,374,743 B1 discloses a small caliber projectile with a hard core arranged at the front and a soft core arranged at the rear. The rimfire bullet has a jacket made of steel, plated steel or brass.

Aus der WO 2006/010424 ist ein Hartkerngeschoss bekannt, welches über einen Geschosskern verfügt. In den Geschosskern ist ein Penetrator eingesetzt ist, welcher aus dem Geschosskern herausragt.From the WO 2006/010424 a hard-core projectile is known which has a projectile core. A penetrator is inserted into the bullet core and protrudes from the bullet core.

Die US 2016/153757 A1 betrifft ein Projektil umfassend einen zylindrischen Körper und eine Nase, welche mit dem Körper verbunden ist. Die Nase umfasst an einem vordersten Abschnitt eine Spitze sowie eine Vielzahl von Ausschnittabschnitten und Schneidkanten.the U.S. 2016/153757 A1 relates to a projectile comprising a cylindrical body and a nose connected to the body. The nose includes a tip at a foremost portion and a plurality of cutout portions and cutting edges.

Aus der IL 79 191 A ist ein Geschoss mit einem Trägerkörper und einem Penetrator von hoher Dichte bekannt. Ein Frontbereich des Trägerkörpers ist abgeschrägt und erstreckt sich über die Front des Penetrators hinaus.From the IL 79 191 A a projectile with a carrier body and a high density penetrator is known. A front portion of the carrier body is tapered and extends beyond the front of the penetrator.

Die EP 0 343 389 A1 betrifft einen Geschosskern für ein Treibspiegelgeschoss, der eine Geschosskern-Spitze, einen Geschosskern-Heckteil und einen Geschosskern-Mittelteil aufweist, die durch einen Dorn miteinander verbunden sind. Der Geschosskern-Mittelteil ist aus sprödem Wolfram hergestellt.the EP 0 343 389 A1 relates to a projectile core for a sabot projectile, which has a projectile core tip, a projectile core rear part and a projectile core middle part, which are connected to one another by a mandrel. The core of the bullet is made of brittle tungsten.

Viele der aus dem Stand der Technik bekannten Geschosse weisen aufgrund ihrer Geometrie und ihren ballistischen Eigenschaften eine ungenügende Durchdringungsfähigkeit oder Treffer-Wahrscheinlichkeit des gepanzerten Zielobjekts auf.Due to their geometry and their ballistic properties, many of the projectiles known from the prior art have an insufficient penetration capability or hit probability of the armored target object.

DARSTELLUNG DER ERFINDUNGPRESENTATION OF THE INVENTION

Es ist daher eine Aufgabe der Erfindung, ein Geschoss anzugeben, welches die Nachteile des Standes der Technik überwindet. Eine besonders bevorzugte Aufgabe ist es, ein Geschoss anzugeben, welches eine hohe Durchschlagskraft und eine gesteigerte Präzision aufweist.It is therefore an object of the invention to provide a projectile which overcomes the disadvantages of the prior art. A particularly preferred object is a Specify a projectile that has a high penetration power and increased precision.

Erfindungsgemäss wird diese Aufgabe durch ein Geschoss gemäss Anspruch 1 gelöst. Weitere Ausführungsformen sind in den abhängigen Ansprüchen angegeben.According to the invention, this object is achieved by a projectile according to claim 1. Further embodiments are specified in the dependent claims.

Es wird also ein Geschoss umfassend ein Halteelement und einen Penetrator angegeben, wobei der Penetrator zumindest teilweise in einer zentrisch zur Geschossachse verlaufenden Aufnahmeöffnung des Halteelements aufgenommen ist und eine Penetratorfront und ein Penetratorheck aufweist. Das Penetratorheck ist zylinderförmig ausgebildet und die Penetratorfront ist ausgehend vom Penetratorheck in Richtung einer Penetratorspitze zu der Geschossachse hin konisch zulaufend ausgebildet. Die Länge der Penetratorfront ist bezüglich der Länge des Penetratorhecks in einem Längenverhältnis von etwa 1 zu 1, vorzugsweise etwa 1 zu 1.5, besonders bevorzugt etwa 1 zu 2.2.A projectile comprising a retaining element and a penetrator is therefore specified, the penetrator being at least partially accommodated in a receiving opening of the retaining element running centrally to the projectile axis and having a penetrator front and a penetrator rear. The penetrator rear is cylindrical and the penetrator front is designed to taper conically from the penetrator rear in the direction of a penetrator tip towards the projectile axis. The length of the penetrator front is in relation to the length of the penetrator rear in an aspect ratio of about 1 to 1, preferably about 1 to 1.5, more preferably about 1 to 2.2.

In anderen Worten verfügt der Penetrator über ein zylindrisches Heck und eine konische oder kegelförmige Front, wobei das Heck entlang der Geschossachse gesehen länger als die Front ist. Unter einer konischen oder kegelförmigen Front wird insbesondere verstanden, dass die Front im geometrischen Sinne konisch bzw. kegelförmig ist. Das heisst, die Aussenfläche verläuft vorzugsweise in einem konstanten Winkel zur Mittelachse des Penetrators.In other words, the penetrator has a cylindrical tail and a conical or conical front, with the tail being longer than the front as viewed along the bullet axis. A conical or cone-shaped front means in particular that the front is conical or cone-shaped in the geometric sense. That is, the outer surface preferably runs at a constant angle to the central axis of the penetrator.

Es ist bevorzugt, dass das zylindrische Penetratorheck und die konische Penetratorfront in einem Gewichtsverhältnis von etwa 2 bis 12, vorzugsweise von etwa 4 bis 10, zueinander ausgebildet sind. In anderen Worten ist es bevorzugt, dass das zylindrische Penetratorheck ein Gewicht aufweist, welches etwa 2 bis 12 mal grösser, vorzugsweise etwa 4 bis 10 mal grösser, als das Gewicht der konischen Penetratorfront ist.It is preferred that the cylindrical penetrator tail and the conical penetrator front are formed in a weight ratio of about 2 to 12, preferably about 4 to 10, to each other. In other words, it is preferred that the cylindrical penetrator tail has a weight which is about 2 to 12 times greater, preferably about 4 to 10 times greater than the weight of the conical penetrator front.

Diese Gewichtsverteilungen bewirken eine gesteigerte Präzision.These weight distributions result in increased precision.

Vorzugsweise weist die Penetratorfront einen Konuswinkel zwischen 10° und 20°, vorzugsweise 13° auf. Das heisst, die ausgehend vom Penetratorheck in Richtung der Penetratorspitze konisch zulaufende Penetratorfront verfügt über einen Durchmesser, welcher entlang dieser Richtung geringer wird so dass die Penetratorfront in ihrem Frontbereich einen kleineren Durchmesser aufweist als in ihrem Heckbereich.The penetrator front preferably has a cone angle of between 10° and 20°, preferably 13°. This means that the penetrator front, which tapers conically from the rear of the penetrator in the direction of the penetrator tip, has a diameter which becomes smaller along this direction, so that the penetrator front has a smaller diameter in its front area than in its rear area.

Die Penetratorspitze kann eine flache Stimfläche aufweisen, welche sich senkrecht zur Geschossachse erstreckt. Die Penetrator kann alternativ über ein spitzes Ende verfügen.The penetrator tip may have a flat face extending perpendicular to the bullet axis. Alternatively, the penetrator may have a pointed end.

Die konisch zulaufende Penetratorfront mündet also vorzugsweise in eine Penetratorspitze, welche einen gestreckten Winkel bildet. Das heisst, bei der Penetratorspitze kann es sich um eine sogenannte Flachspitze handeln. Der Durchmesser der Penetratorspitze ist bevorzugterweise zwischen etwa 0.4 und 1.2 mm, besonders bevorzugt etwa 0.8 mm.The conically tapering penetrator front thus preferably opens into a penetrator tip, which forms a straight angle. This means that the penetrator tip can be a so-called flat tip. The diameter of the penetrator tip is preferably between about 0.4 and 1.2 mm, more preferably about 0.8 mm.

Es ist bevorzugt, dass die Gesamtlänge des Penetrators zwischen 35 mm und 55 mm, vorzugsweise 45 mm beträgt, und/oder dass die Länge der Penetratorfront zwischen 12 mm und 17 mm, vorzugsweise 14 mm beträgt, und/oder dass die Länge des Penetratorhecks zwischen 15 mm und 44 mm, vorzugsweise 31 mm beträgt.It is preferred that the total length of the penetrator is between 35 mm and 55 mm, preferably 45 mm, and/or that the length of the penetrator front is between 12 mm and 17 mm, preferably 14 mm, and/or that the length of the penetrator tail is between 15 mm and 44 mm, preferably 31 mm.

Der Durchmesser des Penetratorhecks beträgt vorzugsweise zwischen 6 mm und 9 mm, vorzugsweise 7 mm.The diameter of the penetrator tail is preferably between 6 mm and 9 mm, preferably 7 mm.

Es ist bevorzugt, dass die Gesamtlänge des Penetrators, also die Summe der Länge der Penetratorfront und der Länge des Penetratorhecks, und der Durchmesser des Penetratorhecks in einem Verhältnis von etwa 4 bis 10, vorzugsweise von etwa 5 bis 9 zueinander sind. In anderen Worten ist es bevorzugt, dass die Gesamtlänge des Penetrators etwa 4 bis 10 mal länger, vorzugsweise etwa 5 bis 9 mal länger, als der Durchmesser des Penetratorhecks ist.It is preferred that the total length of the penetrator, ie the sum of the length of the penetrator front and the length of the penetrator tail, and the diameter of the penetrator tail are in a ratio of about 4 to 10, preferably about 5 to 9, to one another. In other words, it is preferred that the overall length of the penetrator is about 4 to 10 times longer, preferably about 5 to 9 times longer than the diameter of the penetrator tail.

Diese Längenverhältnisse beeinflussen die Durchschlagsleistung positiv, das heisst, der Penetrator erhält eine hohe Durchschlagskraft und kann in einem Zielobjekt einen grösseren Weg zurücklegen bevor er gestoppt wird.These length ratios have a positive effect on the penetrating power, which means that the penetrator has a high penetrating power and can cover a longer distance in a target object before it is stopped.

Der Penetrator ist vorzugsweise einstückig aus der Penetratorfront und dem Penetratorheck gebildet und besteht vorzugsweise aus einem Material mit höherer Dichte als das Halteelement, insbesondere aus Wolframkarbid.The penetrator is preferably formed in one piece from the penetrator front and the penetrator rear and preferably consists of a material with a higher density than the holding element, in particular tungsten carbide.

Eine grosse Auftreffwucht auf dem Zielobjekt und eine panzerbrechende Wirkung können durch den Penetrator bestehend aus einem Material mit hoher Dichte erreicht werden, welches dem Penetrator eine grosse Festigkeit bzw. Härte verleiht. So besteht der Penetrator vorzugsweise aus einer Legierung, deren Hauptbestandteil Wolfram ist, z.B. Wolframkarbid. Es ist aber auch möglich, dass der Penetrator aus einem einzigen Element, z.B. Wolfram, besteht.A large impact force on the target object and an armor-piercing effect can be achieved by the penetrator consisting of a material with a high density, which gives the penetrator great strength or hardness. Thus, the penetrator is preferably made of an alloy whose main component is tungsten, e.g. However, it is also possible for the penetrator to consist of a single element, e.g. tungsten.

Bei einem einstückig ausgebildeten Penetrator sind die Penetratorfront und das Penetratorheck also nicht als verschiedene Bauteile ausgebildet, sondern es handelt sich um einen integral geformten Penetrator, dessen Aussenform, von der Penetratorspitze aus betrachtet, in konischer Form ausgebildet ist und in einen zylindrischen Heckbereich übergeht.In the case of a one-piece penetrator, the penetrator front and the penetrator rear are not designed as different components, but it is an integrally formed penetrator whose outer shape, viewed from the penetrator tip, is designed in a conical shape and merges into a cylindrical rear area.

Gemäss einer nicht erfindungsgemäßen Ausführungsform ragt der Penetrator, insbesondere die Penetratorfront, stirnseitig aus dem Halteelement heraus.According to an embodiment not according to the invention, the penetrator, in particular the penetrator front, protrudes from the holding element at the end.

Wenn ein solches Geschoss mit hervorstehendem Penetrator auf das Zielobjekt auftrifft, entfaltet der Penetrator sofort seine Wirkung, wobei Energie, welche im Falle eines vollständig bedeckten Penetrators für die Verformung oder Zerlegung des Halteelements erforderlich wäre, dabei gänzlich dem Penetrator zur Verfügung steht.If such a projectile with a protruding penetrator hits the target object, the penetrator unfolds its effect immediately, the energy which would be required for the deformation or disintegration of the holding element in the case of a completely covered penetrator being completely available to the penetrator.

Es ist bevorzugt, dass das Penetratorheck passgenau in der Aufnahmeöffnung des Halteelements aufgenommen ist.It is preferred that the penetrator tail is received with a precise fit in the receiving opening of the holding element.

Während der Penetrator also stirnseitig aus der Aufnahmeöffnung des Halteelements herausragt, ist der heckseitige Bereich des Penetrators in der Aufnahmeöffnung aufgenommen. Die Befestigung des Penetrators im Halteelement kann über eine kraftschlüssige Verbindung wie zum Beispiel eine Presspassung, bei welcher der Penetrator in die Aufnahmeöffnung im Halteelement eingepresst wird, erfolgen. Vorzugsweise weist das Halteelement dabei im Bereich der Halteelement-Mitte mehrere Einrillungen mit reduziertem Durchmesser auf. Weitere Möglichkeiten einer Befestigung sind eine stoffschlüssige Verbindung durch Löten oder Kleben oder eine formschlüssige Befestigung.While the penetrator protrudes from the receiving opening of the holding element at the end, the rear area of the penetrator is received in the receiving opening. The penetrator can be fastened in the holding element by means of a non-positive connection, such as a press fit, in which the penetrator is pressed into the receiving opening in the holding element. The holding element preferably has a plurality of grooves with a reduced diameter in the region of the middle of the holding element. Other options for attachment are a material connection by soldering or gluing or a form-fitting attachment.

Das Halteelement weist vorzugsweise ein kegelstumpfförmiges Halteelement-Heck, eine zylindrische Halteelement-Mitte und eine Halteelement-Front auf, welche von der Halteelement-Mitte ausgehend in Richtung der Penetratorspitze zu der Geschossachse hin konisch zulaufend ausgebildet ist. Vorzugsweise bildet die Halteelement-Front eine Verlängerung der konischen Spitze des Penetrators und verläuft in die gleiche Richtung wie die konische Spitze des Penetrators.The holding element preferably has a frustoconical holding element rear, a cylindrical holding element center and a holding element front, which is designed to taper conically from the holding element center in the direction of the penetrator tip towards the projectile axis. Preferably, the retaining element front forms an extension of the conical tip of the penetrator and runs in the same direction as the conical tip of the penetrator.

Es ist bevorzugt, dass die Halteelement-Front einen Konuswinkel zwischen 10° und 20°, vorzugsweise 13° aufweist, und/oder dass die Halteelement-Front eine Wandstärke aufweist, welche in Richtung der Penetratorspitze kontinuierlich abnimmt und vorzugsweise im Übergangsbereich zwischen der Penetratorfront und dem Penetratorheck Null ist, so dass die gesamte Penetratorfront freiliegt.It is preferred that the front of the holding element has a cone angle of between 10° and 20°, preferably 13°, and/or that the front of the holding element has a wall thickness which decreases continuously in the direction of the penetrator tip and preferably in the transition area between the penetrator front and the penetrator tail is zero so that the entire penetrator front is exposed.

In anderen Worten besteht vorzugsweise ein nahtloser Übergang zwischen der Halteelement-Front und der Penetratorfront. Die Mantelfläche der Penetratorfront kann also als eine sich entlang der Geschossachse erstreckende Verlängerung der Mantelfläche der Halteelement-Front gesehen werden, welche übergangslos an die Mantelfläche der Halteelement-Front angrenzt. Eine solche Ausgestaltung der Geschossaussenfläche ergibt gute aerodynamische und ballistische Eigenschaften.In other words, there is preferably a seamless transition between the front of the holding element and the front of the penetrator. The lateral surface of the penetrator front can thus be seen as an extension of the lateral surface of the front of the holding element, which extends along the bullet axis and adjoins the lateral surface of the front of the holding element without a transition. Such a configuration of the projectile's outer surface results in good aerodynamic and ballistic properties.

Vorzugsweise ragt also die gesamte Penetratorfront aus dem Halteelement heraus und dringt bereits ins Zielobjekt ein, bevor das Halteelement auf dem Zielobjekt auftrifft, so dass das Geschoss seine kinetische Energie sehr effektiv an das Zielobjekt abgeben kann. Es ist aber auch möglich, dass sich die Halteelement-Front zumindest bereichsweise auch über das Penetratorheck erstreckt und dabei zum Beispiel sowohl die Penetratorspitze als auch einen Teil des Penetratorhecks unbedeckt lässt.The entire penetrator front therefore preferably protrudes from the holding element and already penetrates the target object before the holding element hits the target object, so that the projectile can very effectively deliver its kinetic energy to the target object. However, it is also possible for the front of the retaining element to also extend at least in regions over the rear of the penetrator, leaving both the penetrator tip and part of the rear of the penetrator uncovered, for example.

Bevorzugterweise weist das Halteelement-Heck einen Kegelstumpfwinkel zwischen 5° und 15°, vorzugsweise 9° auf, und/oder der Durchmesser am Kegelstumpfende des Halteelement-Hecks beträgt bevorzugterweise zwischen 9 mm und 11 mm, vorzugsweise 10 mm, und/oder das Halteelement-Heck weist bevorzugterweise eine konische Einbuchtung auf.The rear of the holding element preferably has a truncated cone angle of between 5° and 15°, preferably 9°, and/or the diameter at the end of the truncated cone of the rear of the holding element is preferably between 9 mm and 11 mm, preferably 10 mm, and/or the holding element Tail preferably has a conical indentation.

Die konische Einbuchtung befindet sich vorzugsweise im Heckbereich des Halteelement-Hecks und dient dazu, die Flugeigenschaften des Geschosses durch Stabilisierung zu verbessern.The conical indentation is preferably located in the rear area of the rear of the holding element and serves to improve the flight characteristics of the projectile by stabilizing it.

Bevorzugterweise beträgt der Durchmesser der Halteelement-Mitte zwischen 12.5 mm und 13.5 mm, vorzugsweise 12.98 mm, und/oder die Mantelfläche der Halteelement-Mitte weist vorzugsweise umlaufende Rillen auf. Die Rillen können in einem heckseitigen Bereich der Halteelement-Mitte angeordnet sein. Es ist jedoch auch denkbar, dass nur ein frontseitiger Bereich der Halteelement-Mitte oder die gesamte Halteelement-Mitte mit Rillen versehen ist. Insbesondere ist etwa ein Drittel bis die Hälfte der Mantelfläche, ausgehend vom heckseitigen Ende in Richtung des frontseitigen Endes der Halteelement-Mitte gesehen, mit Rillen versehen. Dabei sind vorzugsweise zwei oder mehr Rillen vorgesehen, welche ausgehend vom heckseitigen Ende der Halteelement-Mitte in Richtung des frontseitigen Endes der Halteelement-Mitte unmittelbar benachbart zueinander in der Mantelfläche der Halteelement-Mitte ausgebildet sind. Es ist möglich, dass die Rillen jeweils im selben Abstand zueinander auf der Mantelfläche angeordnet sind. Alternativ können die Rillen aber auch unterschiedliche Abstände zueinander aufweisen. Zum Beispiel können vier Rillen vorgesehen sein, wobei sich der Abstand zwischen zwei benachbarten Rillen ausgehend vom heckseitigen Ende in Richtung des frontseitigen Endes der Halteelement-Mitte zunehmend vergrössert. Oder aber die bezüglich dem heckseitigen Ende der Halteelement-Mitte ersten zwei Rillen können in einem ersten Abstand zueinander und die bezüglich dem heckseitigen Ende der Halteelement-Mitte letzten zwei Rillen in einem zweiten Abstand zueinander, welcher grösser oder kleiner als der erste Abstand ist, angeordnet sein. Zudem ist es denkbar, dass die Rillen jeweils über ein identisches Rillenprofil verfügen, also dieselbe Rillentiefe aufweisen respektive sich um denselben Betrag in die Mantelfläche hineinerstrecken sowie über dieselbe Rillenform verfügen. Denkbare Rillenformen sind beispielsweise halbkreisförmige beziehungsweise U-förmige Rillen oder rechteckige Rillen. Unter einer halbkreisförmigen, U-förmigen respektive rechteckigen Rille wird eine Rille verstanden, welche eine halbkreisförmige, U-förmige respektive rechteckige Aussparung begrenzt. Es ist jedoch auch möglich, dass die Rillen jeweils über unterschiedliche Rillenprofile verfügen. Nebst denselben oder unterschiedlichen geometrischen Formen der Aussparung kann auch die lichte Weiter der Aussparung jeweils dieselbe oder eine unterschiedliche sein.The diameter of the middle of the holding element is preferably between 12.5 mm and 13.5 mm, preferably 12.98 mm, and/or the lateral surface of the middle of the holding element preferably has circumferential grooves. The grooves can be arranged in a rear area of the middle of the holding element. However, it is also conceivable that only a front area of the center of the retaining element or the entire center of the retaining element is provided with grooves. In particular, about a third to half of the lateral surface, starting from the rear end in the direction of the front end, is the middle of the holding element seen, provided with grooves. Two or more grooves are preferably provided, which are formed directly adjacent to one another in the lateral surface of the middle of the holding element, starting from the rear end of the middle of the holding element in the direction of the front end of the holding element. It is possible that the grooves are each arranged at the same distance from one another on the lateral surface. Alternatively, however, the grooves can also be at different distances from one another. For example, four grooves can be provided, with the distance between two adjacent grooves increasing progressively, starting from the rear end in the direction of the front end of the center of the holding element. Or the first two grooves in relation to the rear end of the middle of the holding element can be arranged at a first distance from one another and the last two grooves in relation to the rear end of the middle of the holding element can be arranged at a second distance from one another, which is greater or smaller than the first distance be. In addition, it is conceivable that the grooves each have an identical groove profile, ie have the same groove depth or extend into the lateral surface by the same amount and have the same groove shape. Conceivable groove shapes are, for example, semicircular or U-shaped grooves or rectangular grooves. A semicircular, U-shaped or rectangular groove is understood to mean a groove which delimits a semicircular, U-shaped or rectangular recess. However, it is also possible that the grooves each have different groove profiles. In addition to the same or different geometric shapes of the recess, the clear width of the recess can be the same or different in each case.

Die Rillentiefe beträgt vorzugsweise zwischen 0.5 mm bis 2.0 mm, insbesondere 1.5 mm, und/oder die lichte Breite der Rillen beträgt vorzugsweise zwischen 1.0 mm bis 2.0 mm, insbesondere 1.6 mm, und/oder der Abstand zwischen zwei benachbarten Rillen beträgt vorzugsweise zwischen 1 mm bis 2 mm, insbesondere 1.2 mm. Oder anders gesagt beträgt die Rillentiefe vorzugsweise etwa einen Drittel der lichten Breite bis zu zweimal die lichte Breite, insbesondere die Hälfte der lichten Breite bis zu einmal die lichte Breite der Aussparung. Der Abstand zwischen zwei benachbarten Rillen ist vorzugsweise die Hälfte der lichten Breite bis zu zweimal die lichte Breite, insbesondere entspricht der Abstand in etwa der lichten Breite.The groove depth is preferably between 0.5 mm and 2.0 mm, in particular 1.5 mm, and/or the clear width of the grooves is preferably between 1.0 mm and 2.0 mm, in particular 1.6 mm, and/or the distance between two adjacent grooves is preferably between 1 mm up to 2 mm, in particular 1.2 mm. Or to put it another way, the groove depth is preferably about one third of the clear width up to twice the clear width, in particular half the clear width up to once the clear width of the recess. The distance between two adjacent grooves is preferably half the clear width up to twice the clear width, in particular the distance corresponds approximately to the clear width.

Die umlaufenden Rillen sind dazu ausgebildet, mit entsprechend dazu ausgebildeten Zügen in einem Gewehrlauf zusammenzuwirken und dienen der Reibungs-Reduzierung des Geschosses im Gewehrlauf, führen zu einer geringeren Lauferosion und erhöhen somit die Lebensdauer der Waffe. Zusammen mit der übrigen Ausgestaltung des Geschosses, insbesondere aufgrund des Penetrators, führen die Rillen zudem zu einer Leistungssteigerung. So bewirken die Reibungs-Reduzierung der Rillen und die Materialhärte sowie Masse des Penetrators, dass das Geschoss mit einer hohen Durchschlagskraft auf ein Ziel auftrifft und beispielsweise Stahlplatten durchdringen kann.The circumferential grooves are designed to interact with correspondingly designed trains in a gun barrel and serve to reduce the friction of the bullet in the gun barrel, lead to less barrel erosion and thus increase the service life of the weapon. In addition, together with the rest of the design of the bullet, in particular due to the penetrator, the grooves lead to an increase in performance. The friction reduction of the grooves and the material hardness and mass of the penetrator mean that the projectile hits a target with a high penetrating power and can penetrate steel plates, for example.

Das Halteelement ist vorzugsweise einstückig aus dem Halteelement-Heck, der Halteelement-Mitte und der Halteelement-Front gebildet und besteht vorzugsweise aus Messing und/oder Messinglegierungen.The holding element is preferably formed in one piece from the rear holding element, the center holding element and the front holding element and is preferably made of brass and/or brass alloys.

Bei einem einstückig ausgebildeten Halteelement, analog zum einstückig ausgebildeten Penetrator, sind die Halteelement-Front, die Halteelement-Mitte und das Halteelement-Heck also nicht als verschiedene Bauteile ausgebildet sondern integral geformt, wobei die Aussenform des Halteelements, von der Penetratorspitze aus betrachtet, in konischer Form ausgebildet ist und in einen zylindrischen Mittelbereich und alsdann in einen kegelstumpfförmigen Heckbereich übergeht.In the case of a one-piece retaining element, analogous to the one-piece penetrator, the retaining element front, the retaining element center and the retaining element rear are not formed as different components but are formed integrally, with the outer shape of the retaining element, viewed from the penetrator tip, in is conical in shape and merges into a cylindrical central area and then into a truncated cone-shaped rear area.

Die Gesamtlänge des Halteelements beträgt bevorzugterweise zwischen 35 mm und 55 mm, vorzugsweise 43 mm, und/oder die Länge der Halteelement-Front beträgt bevorzugterweise zwischen 3 mm und 21 mm, vorzugsweise 13 mm, und/oder die Länge der Halteelement-Mitte beträgt bevorzugterweise zwischen 14 mm und 42 mm, vorzugsweise 21 mm.The overall length of the holding element is preferably between 35 mm and 55 mm, preferably 43 mm, and/or the length of the front of the holding element is preferably between 3 mm and 21 mm, preferably 13 mm, and/or the length of the middle of the holding element is preferably between 14mm and 42mm, preferably 21mm.

Vorzugsweise sind bei einer gesamten Geschossmasse von 100 % davon 60 % Halteelement und 40 % Penetrator.Preferably, with a total projectile mass of 100%, 60% of these are holding elements and 40% are penetrators.

Diese Längenverhältnisse und Massenverteilung ergeben für das vorliegende Geschoss mit herausragendem Penetrator eine ideale Gewichtsverteilung, wobei der Schwerpunkt des Geschosses für eine ballistische Flugbahn optimal ist.These aspect ratios and mass distribution result in an ideal weight distribution for the present projectile with outstanding penetrator, with the center of gravity of the projectile being optimal for a ballistic trajectory.

Gemäss einer erfindungsgemäßen Ausführungsform ist der Penetrator vorzugsweise vollständig, und insbesondere passgenau, im Halteelement aufgenommen.According to one embodiment of the invention, the penetrator is preferably accommodated completely, and in particular with a precise fit, in the holding element.

In anderen Worten füllt der Penetrator die Aufnahmeöffnung im Halteelement vollständig aus.In other words, the penetrator completely fills the receiving opening in the holding element.

Vorzugsweise weist das Halteelement ein kegelstumpfförmiges Halteelement-Heck, eine zylindrische Halteelement-Mitte und eine ogivale Halteelement-Front auf, wobei die Halteelement-Front in ihrem Frontbereich in eine Kegelstumpfform oder Kalottenform übergeht.The holding element preferably has a truncated cone-shaped rear holding element, a cylindrical holding element center and an ogival holding element front, with the holding element front transitioning into a truncated cone shape or dome shape in its front area.

Erfindungsgemäß sind die Halteelement-Front, die Halteelement-Mitte und zumindest bereichsweise auch das Halteelement-Heck von einer Hülle umhüllt, wobei die Hülle vorzugsweise aus Messing besteht.According to the invention, the front of the retaining element, the middle of the retaining element and also the rear of the retaining element at least in some areas are encased in a sleeve, with the sleeve preferably being made of brass.

Bei einem nur bereichsweise umhüllten Halteelement-Heck kann zum Beispiel der Heckbereich des Halteelement-Hecks hüllenfrei sein. Anstelle eines nur bereichsweise umhüllten Halteelement-Hecks ist auch ein vollständig umhülltes Halteelement-Heck, also ein insgesamt vollständig umhülltes Halteelement, möglich. Die Hülle ist vorzugsweise derart ausgestaltet, dass sie die jeweilige Form des umhüllten Halteelementbereichs, nämlich ogival, zylindrisch beziehungsweise kegelstumpfförmig, aufweist. Dabei ist es bevorzugt, dass die Hülle unmittelbar an das Halteelement angrenzt und somit direkt auf diesem aufgebracht ist. Durch eine formschlüssig an dem Halteelement anliegende Hülle kann ein kompaktes, rotationssymmetrisches und massgenaues Geschoss bereitgestellt werden, welches gute Durchdringungseigenschaften aufweist.In the case of a rear retaining element that is only covered in some areas, for example, the rear area of the rear retaining element can be free of a cover. Instead of a rear retaining element that is only partially encased, a rear end of the retaining element that is completely encased, that is to say a retaining element that is completely encased overall, is also possible. The cover is preferably designed in such a way that it has the respective shape of the covered holding element area, namely ogival, cylindrical or truncated cone. In this case, it is preferred that the sleeve is directly adjacent to the holding element and is therefore applied directly to it. A compact, rotationally symmetrical and dimensionally accurate projectile which has good penetration properties can be provided by a casing which is in positive contact with the holding element.

Die Hülle weist vorzugsweise im Frontbereich der Halteelement-Front eine verdickte Wandstärke auf, und/oder die Hülle weist vorzugsweise im Bereich der Halteelement-Mitte eine Einrillung auf, und/oder die Hülle weist vorzugsweise im Bereich des Halteelement-Hecks eine heckseitige Bördelung auf. Erfindungsgemäß schliesst die Hülle im Bereich des Halteelement-Hecks einen Luftraum mit dem Halteelement-Heck ein.The sleeve preferably has a thicker wall in the front area of the holding element front, and/or the sleeve preferably has a groove in the area of the middle of the holding element, and/or the sleeve preferably has a rear flange in the area of the holding element rear. According to the invention, the cover encloses an air space with the rear of the retaining element in the region of the rear of the retaining element.

Die Einrillung kann mit entsprechend dazu ausgebildeten Zügen in einem Gewehrlauf zusammenwirken und dient der Reibungs-Reduzierung des Geschosses im Gewehrlauf.The indentation can interact with correspondingly designed rifling in a gun barrel and serves to reduce the friction of the bullet in the gun barrel.

Die frontseitige Verdickung der Hülle verringert Abpraller bei schiefwinkligem Beschuss an harten Zielobjekten und dient zudem einer Festlegung des Massenschwerpunktes des Geschosses.The front thickening of the shell reduces ricochets when firing at oblique angles on hard targets and also serves to determine the center of mass of the bullet.

Vorzugsweise weist die Halteelement-Mitte frontseitig einen Kegelstumpf mit einem Kegelwinkel zwischen 30° und 50°, vorzugsweise 45° auf, und die Halteelement-Front weist vorzugsweise heckseitig einen Innengekel mit gleichem Kegelwinkel auf und ist formschlüssig auf den Kegelstumpf aufgesetzt. Diese Kegelwinkel erlauben eine optimale rotationssymmetrische Zentrierung der Halteelement-Front an der Halteelement-Mitte und somit auch des darin aufgenommenen Penetrators.The holding element center preferably has a truncated cone with a cone angle between 30° and 50°, preferably 45°, on the front side, and the holding element front preferably has an inner flange with the same cone angle on the rear side and is placed positively on the truncated cone. These cone angles allow an optimal, rotationally symmetrical centering of the front of the holding element on the middle of the holding element and thus also of the penetrator accommodated therein.

Es ist bevorzugt, dass sich die Halteelement-Mitte ausgehend vom Penetratorheck in Richtung der Penetratorfront über die Mitte des Penetrators hinaus erstreckt, und/oder dass sich die Halteelement-Front über die Penetratorspitze hinaus erstreckt. In anderen Worten wird die Penetratorspitze vollständig von der Halteelement-Front umgeben.It is preferred that the center of the retaining element extends beyond the center of the penetrator, starting from the rear of the penetrator in the direction of the penetrator front, and/or that the front of the retaining element extends beyond the tip of the penetrator. In other words, the penetrator tip is completely surrounded by the front of the holding element.

Vorzugsweise sind das Halteelement-Heck und die Halteelement-Mitte einstückig ausgebildet und bestehen aus einem Kunststoff, insbesondere PET, oder Stahl, und/oder die Halteelement-Front besteht aus pulverförmigen Substanzen oder Gemischen wie Borax, Brand- oder Explosivsätzen.The rear holding element and the middle holding element are preferably formed in one piece and consist of a plastic, in particular PET, or steel, and/or the front holding element consists of powdered substances or mixtures such as borax, incendiary or explosive devices.

Hierbei sind also das Halteelement-Heck und die Halteelement-Mitte integral ausgebildet, während es sich bei der Halteelement-Front um ein separat davon ausgebildetes Bauteil handelt. Während der Penetrator aus einem Material mit sehr hoher Dichte besteht, weist das Halteelement ein Material bzw. Materialien mit einer geringeren Dichte als der Penetrator auf.In this case, therefore, the rear holding element and the center holding element are formed integrally, while the front holding element is a component formed separately therefrom. While the penetrator consists of a material with a very high density, the holding element has a material or materials with a lower density than the penetrator.

Die Gesamtlänge des Halteelements beträgt bevorzugterweise zwischen 53 mm und 55 mm, vorzugsweise 54 mm, und/oder die Länge der Halteelement-Front beträgt bevorzugterweise zwischen 22 mm und 28 mm, vorzugsweise 26 mm, und/oder die Länge der Halteelement-Mitte beträgt bevorzugterweise zwischen 19 mm und 25 mm, vorzugsweise 21 mm.The overall length of the holding element is preferably between 53 mm and 55 mm, preferably 54 mm, and/or the length of the front of the holding element is preferably between 22 mm and 28 mm, preferably 26 mm, and/or the length the middle of the holding element is preferably between 19 mm and 25 mm, preferably 21 mm.

Vorzugsweise sind bei einer gesamten Geschossmasse von 100% davon 10% Halteelement, 50 % Penetrator und 40 % Hülle, und/oder vorzugsweise sind bei einer gesamten Halteelementmasse von 100% davon 40% Halteelement-Front, 50% Halteelement-Mitte und 10 % Halteelement-Heck.Preferably, with a total projectile mass of 100%, 10% are retaining element, 50% penetrator and 40% casing, and/or preferably, with a total retaining element mass of 100%, 40% are front retaining element, 50% are middle retaining element and 10% are retaining element -Rear.

Diese Längenverhältnisse und Massenverteilung ergeben für das vorliegende, umhüllte Geschoss mit vollständig aufgenommenem Penetrator eine ideale Gewichtsverteilung, wobei der Schwerpunkt des Geschosses für eine ballistische Flugbahn optimal ist.These aspect ratios and mass distribution provide an ideal weight distribution for the present fully seated penetrator jacketed bullet with the bullet's center of gravity optimal for ballistic trajectory.

KURZE BESCHREIBUNG DER ZEICHNUNGENBRIEF DESCRIPTION OF THE DRAWINGS

Bevorzugte Ausführungsformen der Erfindung werden im Folgenden anhand der Zeichnungen beschrieben, die lediglich zur Erläuterung dienen und nicht einschränkend auszulegen sind. In den Zeichnungen zeigen:

Fig. 1
eine Teilschnittansicht durch ein Geschoss gemäss einer nicht erfindungsgemäßen Ausführungsform;
Fig. 2
eine Vollschnittansicht durch das Geschoss gemäss Figur 1;
Fig. 3
eine Teilschnittansicht durch ein Geschoss gemäss einer erfindungsgemäßen Ausführungsform;
Fig. 4
eine Vollschnittansicht durch das Geschoss gemäss Figur 3.
Preferred embodiments of the invention are described below with reference to the drawings, which are for explanation only and are not to be interpreted as restrictive. In the drawings show:
1
a partial sectional view through a projectile according to an embodiment not according to the invention;
2
a full sectional view through the bullet according to figure 1 ;
3
a partial sectional view through a projectile according to an embodiment of the invention;
4
a full sectional view through the bullet according to figure 3 .

BESCHREIBUNG BEVORZUGTER AUSFÜHRUNGSFORMENDESCRIPTION OF PREFERRED EMBODIMENTS

Die Figuren 1 bis 4 zeigen jeweils ein Geschoss 1, 1' umfassend ein Halteelement 2, 2' und einen Penetrator 3, welcher eine Penetratorfront 4 und ein Penetratorheck 5 aufweist. Das Penetratorheck 5 ist zylinderförmig ausgebildet und die Penetratorfront 4 ist ausgehend vom Penetratorheck 5 in Richtung einer Penetratorspitze 6 zu der Geschossachse A hin konisch zulaufend ausgebildet. In diesen Figuren ist das Längenverhältnis zwischen der Länge LPF der Penetratorfront 4 bezüglich der Länge LPH des Penetratorhecks 5 etwa 1 zu 2, d.h. das Penetratorheck ist um etwa einen Faktor zwei länger als die Penetratorfront. Insbesondere ist hierbei die Gesamtlänge LP des Penetrators 3 45 mm, wobei die Länge LPF der Penetratorfront 4 13 mm und die Länge LPH des Penetratorhecks 5 32 mm betragen.the Figures 1 to 4 each show a projectile 1, 1' comprising a retaining element 2, 2' and a penetrator 3, which has a penetrator front 4 and a penetrator rear 5. The penetrator rear 5 is cylindrical and the penetrator front 4 is designed to taper conically, starting from the penetrator rear 5 in the direction of a penetrator tip 6 towards the projectile axis A. In these characters it is Aspect ratio between the length LPF of the penetrator front 4 with respect to the length LPH of the penetrator tail 5 is about 1 to 2, ie the penetrator tail is longer by about a factor of two than the penetrator front. In particular, the overall length LP of the penetrator 3 is 45 mm, the length LPF of the penetrator front 4 being 13 mm and the length LPH of the penetrator rear 5 being 32 mm.

In den Figuren 1 und 2 ist eine nicht erfindungsgemäße Ausführungsform des Geschosses 1 dargestellt, bei welcher der Penetrator 3 heckseitig nur teilweise in einer zentrisch zur Geschossachse A verlaufenden Aufnahmeöffnung 12 des Halteelements 2 aufgenommen ist und stirnseitig mit der Penetratorfront 4 aus dem Halteelement 2 herausragt. In den Figuren 3 und 4 ist eine erfindungsgemäße Ausführungsform des Geschosses 1' dargestellt, bei welcher der Penetrator 3 vollständig im Halteelement 2' aufgenommen ist. In den Figuren 1-4 sind jeweils gleiche Bauteile mit gleichen Bezugszeichen versehen.In the Figures 1 and 2 an embodiment of the projectile 1 not according to the invention is shown, in which the penetrator 3 is only partially accommodated at the rear in a receiving opening 12 of the retaining element 2 running centrally to the projectile axis A and protrudes from the retaining element 2 with the penetrator front 4 at the front. In the Figures 3 and 4 an embodiment of the projectile 1' according to the invention is shown, in which the penetrator 3 is completely accommodated in the holding element 2'. In the Figures 1-4 the same components are provided with the same reference numbers.

In beiden Ausführungsformen weist die Penetratorfront 4 einen Konuswinkel aPF von etwa 13° auf und die Penetratorspitze 6 verfügt über eine flache Stirnfläche 7, welche sich senkrecht zur Geschossachse A erstreckt. Weiter beträgt der Durchmesser DPH des Penetratorhecks 5 etwa 7 mm. In beiden Ausführungsformen ist der Penetrator 3 einstückig aus der Penetratorfront 4 und dem Penetratorheck 5 gebildet und besteht vollständig aus Wolframkarbid.In both embodiments, the penetrator front 4 has a cone angle aPF of approximately 13° and the penetrator tip 6 has a flat end face 7 which extends perpendicularly to the bullet axis A. Furthermore, the diameter DPH of the penetrator tail 5 is about 7 mm. In both embodiments, the penetrator 3 is formed in one piece from the penetrator front 4 and the penetrator rear 5 and consists entirely of tungsten carbide.

Wie aus den Figuren 1 und 2 hervorgeht, ist das Penetratorheck 5 beim Geschoss 1 gemäss der nicht erfindungsgemäßen Ausführungsform passgenau in der Aufnahmeöffnung 12 des Halteelements 2 aufgenommen, wobei das Penetratorheck 5 heckseitig im Bereich seines Bodens eine Einrillung mit reduziertem Durchmesser aufweist.How from the Figures 1 and 2 shows that the penetrator tail 5 of the projectile 1 according to the embodiment not according to the invention is accommodated with a precise fit in the receiving opening 12 of the holding element 2, the penetrator tail 5 having a groove with a reduced diameter on the rear side in the region of its base.

Das Halteelement 2 weist ein kegelstumpfförmiges Halteelement-Heck 8, eine zylindrische Halteelement-Mitte 9 und eine Halteelement-Front 10 auf, wobei die Halteelement-Front 10 von der Halteelement-Mitte 9 ausgehend in Richtung der Penetratorspitze 6 zu der Geschossachse A hin konisch zulaufend ausgebildet ist. Die konische Halteelement-Front 10 ist dabei mit einem Konuswinkel aKF von etwa 13° ausgebildet und verfügt über eine Wandstärke, welche sich in Richtung der Penetratorspitze 6 kontinuierlich verjüngt und am Ort des Übergangs von der Penetratorfront 4 zum Penetratorheck 5 Null ist. Die gesamte Penetratorfront 4 liegt somit frei. Dabei besteht ein nahtloser Übergang zwischen der frontseitigen Halteelement-Front 10 und der heckseitigen Penetratorfront 4, so dass die Mantelfläche der Penetratorfront 4 als Verlängerung der Mantelfläche der Halteelement-Front 10 gesehen werden kann.The holding element 2 has a frustoconical holding element rear 8, a cylindrical holding element center 9 and a holding element front 10, the holding element front 10 tapering conically from the holding element center 9 in the direction of the penetrator tip 6 towards the projectile axis A is trained. The conical holding element front 10 is designed with a cone angle aKF of about 13° and has a wall thickness which tapers continuously in the direction of the penetrator tip 6 and is zero at the point of transition from the penetrator front 4 to the penetrator rear 5 . The whole Penetrator front 4 is therefore exposed. There is a seamless transition between the front retaining element front 10 and the rear penetrator front 4 so that the lateral surface of the penetrator front 4 can be seen as an extension of the lateral surface of the retaining element front 10 .

Das kegelstumpfförmige Halteelement-Heck 5 weist hierbei einen Kegelstumpfwinkel αKH von etwa 9° auf und der Durchmesser DKH am Kegelstumpfende des Halteelement-Hecks 8 beträgt etwa 10 mm.The truncated cone-shaped retaining element rear 5 has a truncated cone angle αKH of about 9° and the diameter DKH at the truncated cone end of the retaining element rear 8 is about 10 mm.

Zudem verfügt das Halteelement-Heck 8 heckseitig über eine konische Einbuchtung 11, welche sich mittig in das Halteelement-Heck 8 hinein erstreckt.In addition, the rear holding element 8 has a conical indentation 11 at the rear, which extends centrally into the rear holding element 8 .

Die Halteelement-Mitte 9 verfügt über einen Durchmesser DKM von etwa 13 mm und auf der Mantelfläche der Halteelement-Mitte 9 sind bereichsweise umlaufende Rillen 13 vorgesehen, welche mit entsprechend dazu ausgebildeten Zügen in einem Gewehrlauf (nicht dargestellt) zusammenzuwirken können.The holding element center 9 has a diameter DKM of about 13 mm and circumferential grooves 13 are provided in areas on the outer surface of the holding element center 9, which can interact with correspondingly designed trains in a gun barrel (not shown).

In der hier gezeigten Ausführungsform sind vier Rillen 13a, 13b, 13c, 13d in der Mantelfläche der Halteelement-Mitte 9 ausgebildet, wobei die Rillen 13a, 13b, 13c, 13d ausgehend vom heckseitigen Ende der Halteelement-Mitte 9 in Richtung des frontseitigen Endes der Halteelement-Mitte 9 gesehen entlang etwa der Hälfte der Mantelfläche unmittelbar benachbart zueinander angeordnet sind. Die bezüglich des heckseitigen Endes der Halteelement-Mitte 9 gesehenen ersten zwei Rillen 13a, 13b sind hier identisch ausgebildet. So weisen beide dieselbe U-förmige Rillenform auf und erstrecken sich mit derselben Rillentiefe RTa, RTb in die Mantelfläche der Halteelement-Mitte 9 hinein. Auch die lichte Weite dieser Rillen, das heisst nebst der Rillentiefe RTa, RTb beziehungsweise lichten Höhe auch die lichte Breite RBa, RBb, ist jeweils dieselbe. Der Abstand RTa zwischen diesen beiden Rillen 13a, 13b entspricht in etwa der Rillentiefe RTa, RTb beziehungsweise lichten Höhe dieser Rillen 13a, 13b. Im Unterschied dazu weisen die zwei im Anschluss an diese zwei Rillen 13a, 13b angeordneten weiteren zwei Rillen 13c, 13d jeweils eine rechteckige Rillenform auf und unterscheiden sich in ihrer lichten Weite sowohl von den ersten beiden Rillen 13a, 13b als auch voneinander. Insbesondere weisen die rechteckigen Rillen 13c, 13d jeweils eine kleinere Rillentiefe RTc, RTd als die U-förmigen Rillen 13a, 13b auf. Zudem erstreckt sich die benachbart zur U-förmigen Rille 13b angeordnete rechteckige Rille 13c um einen wesentlich kleineren Betrag in die Mantelfläche hinein als es bei der anderen rechteckigen Rille 13d der Fall ist. Während die rechteckige Rille 13c und die benachbart zu dieser angeordneten U-förmige Rille 13b in einem Abstand RAb zueinander angeordnet sind, welcher in etwa dem Abstand RAa der beiden U-förmigen Rillen entspricht, ist der Abstand RAc zwischen den beiden rechteckigen Rillen 13c, 13d hingegen deutlich kleiner. Die Rillentiefe RTa, RTb der ersten und zweiten U-förmigen Rillen 13a, 13b beträgt hier etwa ein Achtel des Durchmessers DKM der Halteelement-Mitte. Die Rillentiefen RTc, RTd der dritten Rille 13c, welche benachbart zur U-förmigen Rille 13b angeordnet ist, und der vierten Rille 13d, welche benachbart zu der dritten Rille 13c angeordnet ist, sind etwa einen Faktor 30 respektive 15 kleiner als der Durchmesser DKM der Halteelement-Mitte.In the embodiment shown here, four grooves 13a, 13b, 13c, 13d are formed in the lateral surface of the middle holding element 9, with the grooves 13a, 13b, 13c, 13d starting from the rear end of the middle holding element 9 in the direction of the front end of the Retaining element center 9 seen along about half of the lateral surface are arranged immediately adjacent to each other. The first two grooves 13a, 13b seen with respect to the rear end of the holding element center 9 are of identical design here. Both have the same U-shaped groove shape and extend with the same groove depth RTa, RTb into the lateral surface of the middle 9 of the holding element. The clear width of these grooves, that is to say in addition to the groove depth RTa, RTb or clear height and also the clear width RBa, RBb, is the same in each case. The distance RTa between these two grooves 13a, 13b corresponds approximately to the groove depth RTa, RTb or the clear height of these grooves 13a, 13b. In contrast to this, the two further two grooves 13c, 13d arranged following these two grooves 13a, 13b each have a rectangular groove shape and differ in their clear width both from the first two grooves 13a, 13b and from each other. In particular, the rectangular grooves 13c, 13d each have a smaller groove depth RTc, RTd than the U-shaped ones Grooves 13a, 13b. In addition, the rectangular groove 13c arranged adjacent to the U-shaped groove 13b extends into the lateral surface by a much smaller amount than is the case with the other rectangular groove 13d. While the rectangular groove 13c and the U-shaped groove 13b arranged adjacent to it are arranged at a distance RAb from one another which approximately corresponds to the distance RAa between the two U-shaped grooves, the distance RAc between the two rectangular grooves 13c, 13d however, significantly smaller. The groove depth RTa, RTb of the first and second U-shaped grooves 13a, 13b is approximately one eighth of the diameter DKM of the middle of the holding element. The groove depths RTc, RTd of the third groove 13c, which is arranged adjacent to the U-shaped groove 13b, and the fourth groove 13d, which is arranged adjacent to the third groove 13c, are approximately a factor of 30 and 15 respectively smaller than the diameter DKM Retainer center.

Es gilt allerdings zu verstehen, dass sich die Rillenanordnung und die Rillenausbildung nicht auf die hier gezeigten Rillen beschränken. Stattdessen können weniger oder mehr als vier Rillen vorgesehen sein, welche über dieselben oder unterschiedliche Rillenprofile verfügen und/oder in jeweils denselben oder variierenden Abständen zueinander angeordnet sind.However, it should be understood that the groove arrangement and groove design is not limited to the grooves shown here. Instead, fewer or more than four grooves can be provided, which have the same or different groove profiles and/or are arranged at the same or varying distances from one another.

In den Figuren 1 und 2 ist das Halteelement 2 einstückig aus dem Halteelement-Heck 8, der Halteelement-Mitte 9 und der Halteelement-Front 10 gebildet und besteht vollständig aus Messing. Die Gesamtlänge LK des Halteelements 2 beträgt hier etwa 46 mm, wobei die Länge LKF der Halteelement-Front 10 circa 14 mm, die Länge LKM der Halteelement-Mitte 9 circa 22 mm, und die Länge LKH des Halteelement-Hecks 8 circa 10 mm betragen.In the Figures 1 and 2 the holding element 2 is formed in one piece from the holding element rear 8, the holding element center 9 and the holding element front 10 and consists entirely of brass. The total length LK of the holding element 2 is about 46 mm here, the length LKF of the holding element front 10 being about 14 mm, the length LKM of the holding element middle 9 being about 22 mm, and the length LKH of the holding element rear 8 being about 10 mm .

Bei einer gesamten Geschossmasse von 100% sind hiervon 60% Halteelement 2 und 40 % Penetrator 3. Das Geschoss 1 besteht hier also einzig aus dem Halteelement 2 und dem Penetrator 3 und ist insbesondere hüllenfrei ausgebildet.With a total projectile mass of 100%, 60% of this is holding element 2 and 40% penetrator 3. The projectile 1 here consists solely of the holding element 2 and the penetrator 3 and is in particular designed without a casing.

Wie bereits erwähnt und aus den Figuren 3 und 4 hervorgeht, ist beim Geschoss 1' gemäss der erfindungsgemäßen Ausführungsform nicht nur das Penetratorheck 5, sondern auch die Penetratorfront 4, also der gesamte Penetrator, vollständig im Halteelement 2' aufgenommen.As already mentioned and from the Figures 3 and 4 shows, in the case of the projectile 1' according to the embodiment according to the invention, not only the penetrator rear 5 but also the penetrator front 4, i.e. the entire penetrator, is completely in the holding element 2' recorded.

Das Halteelement 2' des Geschoss 1' verfügt, analog zum Halteelement 2 des Geschoss 1, über ein kegelstumpfförmiges Halteelement-Heck 8' und eine zylindrische Halteelement-Mitte 9'. Im Unterschied zur konischen Halteelement-Front 10 des Geschoss 1 weist das Halteelement 2' des Geschoss 1' jedoch eine ogivale Halteelement-Front 10' auf, welche in ihrem Frontbereich 14 in eine Kalottenform übergeht.The retaining element 2' of the projectile 1' has, analogously to the retaining element 2 of the projectile 1, a frustoconical retaining element rear 8' and a cylindrical retaining element center 9'. In contrast to the conical retaining element front 10 of the projectile 1, however, the retaining element 2' of the projectile 1' has an ogival retaining element front 10' which transitions into a dome shape in its front region 14.

Der Durchmesser DKM' der Halteelement-Mitte 9' beträgt etwa 11 mm. Das Halteelement-Heck 8' verfügt über einen Kegelstumpfwinkel αKH' von circa 9°, wobei der Durchmesser DKH' am Kegelstumpfende des Halteelement-Hecks 8' etwa 8.5 mm beträgt. Die Halteelement-Mitte 9' verfügt frontseitig über einen Kegelstumpf 19 mit einem Kegelwinkel βKM von circa 45° und die Halteelement-Front 10' verfügt heckseitig über einen Innengekel 20 mit gleichem Kegelwinkel βKF von circa 45°, wobei der Innenkegel 20 formschlüssig auf den Kegelstumpf 19 aufgesetzt ist. Die Halteelement-Mitte 9' erstreckt sich ausgehend vom Penetratorheck 5 in Richtung der Penetratorfront 4 über die Mitte M des Penetrators 3 hinaus und die Halteelement-Front 10' erstreckt sich entlang derselben Richtung über die Penetratorspitze 6 hinaus.The diameter DKM' of the middle 9' of the holding element is approximately 11 mm. The rear holding element 8' has a truncated cone angle αKH' of approximately 9°, the diameter DKH' at the truncated cone end of the rear holding element 8' being approximately 8.5 mm. The holding element center 9' has a truncated cone 19 with a cone angle βKM of approximately 45° at the front and the holding element front 10' has an inner cone 20 with the same cone angle βKF of approximately 45° at the rear, with the inner cone 20 forming a positive fit on the truncated cone 19 is put on. Starting from the penetrator rear 5, the holding element center 9' extends in the direction of the penetrator front 4 beyond the center M of the penetrator 3, and the holding element front 10' extends in the same direction beyond the penetrator tip 6.

Das Halteelement-Heck 8' und die Halteelement-Mitte 9' sind dabei einstückig ausgebildet und bestehen aus PET oder Stahl. Die separat ausgebildete Halteelement-Front 10' besteht aus Borax. Die Gesamtlänge LK' des Halteelements 2' beträgt dabei circa 54 mm, wobei die Länge LKF' der Halteelement-Front 10' etwa 26 mm und die Länge LKM' der Halteelement-Mitte 9' etwa 21 mm betragen.The rear holding element 8' and the middle holding element 9' are designed in one piece and consist of PET or steel. The separately formed holding element front 10' consists of borax. The overall length LK' of the holding element 2' is approximately 54 mm, the length LKF' of the holding element front 10' being approximately 26 mm and the length LKM' of the holding element center 9' being approximately 21 mm.

Auch hier weist das Penetratorheck 5 des Geschoss 1' heckseitig im Bereich seines Bodens eine Einrillung mit reduziertem Durchmesser auf und ist passgenau in einer Aufnahmeöffnung 12' des Halteelements 2' aufgenommen. Die Aufnahmeöffnung 12' erstreckt sich mittig durch die Halteelement-Mitte 9'in das Halteelement-Heck 8' hinein. Die Penetratorfront 4 ist in einer passgenauen Ausnehmung der Halteelement-Front 10' aufgenommen, welche sich ausgehend vom Penetratorheck 5 in Richtung der Penetratorfront 4 zunehmend verjüngt. Aufgrund des Innenkegels 20 im Heckbereich der Halteelement-Front 10' und des Kegelstumpfs 19 im Frontbereich der Halteelement-Mitte 9' ist ein dichtes Zusammenfügen der Halteelement-Front 10' mit der Halteelement-Mitte 9', und somit eine gute Fixierung des Penetrators im Geschoss 1', ermöglicht.Here, too, the penetrator tail 5 of the projectile 1′ has a groove with a reduced diameter in the area of its base and is accommodated with a precise fit in a receiving opening 12′ of the holding element 2′. The receiving opening 12' extends centrally through the holding element center 9' into the holding element rear 8'. The penetrator front 4 is accommodated in a precisely fitting recess in the holding element front 10 ′, which progressively narrows starting from the penetrator rear 5 in the direction of the penetrator front 4 . Due to the inner cone 20 in the rear area of the holding element front 10' and the truncated cone 19 in the front area of the holding element middle 9 'a tight joining of the holding element front 10' with the holding element middle 9 ', and thus a good fixation of the penetrator in the projectile 1', is made possible.

Zudem sind die Halteelement-Front 10', die Halteelement-Mitte 9' und bereichsweise auch das Halteelement-Heck 8' von einer Hülle 15 umhüllt, welche die jeweilige Form des umhüllten Halteelements 2', also ogival im Frontbereich, zylindrisch im Mittelbereich sowie kegelstumpfförmig im Heckbereich, aufweist. Die Hülle 15 besteht hier vollständig aus Messing und liegt unmittelbar auf der Mantelfläche der Halteelement-Front 10' und der Halteelement-Mitte 9' auf.In addition, the holding element front 10', the holding element middle 9' and in some areas also the holding element rear 8' are encased by a cover 15 which corresponds to the respective shape of the encased holding element 2', i.e. ogival in the front area, cylindrical in the middle area and truncated in the rear area. The sleeve 15 consists here entirely of brass and rests directly on the lateral surface of the holding element front 10' and the holding element center 9'.

Die Hülle 15 umgibt bereichsweise auch das Halteelement-Heck 8' und schliesst dabei mit dem Halteelement-Heck 8' einen Luftraum 18 ein, welcher sich vom Frontbereich zum Heckbereich des Halteelement-Hecks 8' hin zunehmend vergrössert. Der Abstand zwischen der Hülle 15 und der Mantelfläche des Halteelement-Hecks 8' wird in dieser Richtung also zunehmend vergrössert.The shell 15 also partially surrounds the rear holding element 8′ and encloses an air space 18 with the rear holding element 8′, which increases in size from the front area to the rear area of the rear holding element 8′. The distance between the sleeve 15 and the lateral surface of the rear holding element 8' is thus increasingly increased in this direction.

Die Hülle 15 endet heckseitig auf dem Halteelement-Heck 8' in einer Bördelung 17 und lässt dabei einen Abschnitt des Halteelement-Hecks 8' hüllenfrei. Der Penetrator 3 ist dabei jedoch nie in Kontakt mit der Hülle 15. Die Hülle 15 weist im Frontbereich der Halteelement-Front 10' eine verdickte Wandstärke auf und verfügt im Bereich der Halteelement-Mitte 9' über eine Einrillung 16, welche mit entsprechend dazu ausgebildeten Zügen in einem Gewehrlauf (nicht dargestellt) zusammenwirken kann.The sleeve 15 ends at the rear on the rear holding element 8' in a flange 17, leaving a section of the rear holding element 8' free of a sleeve. However, the penetrator 3 is never in contact with the shell 15. The shell 15 has a thicker wall in the front area of the holding element front 10' and has a groove 16 in the area of the holding element center 9', which has correspondingly designed grooves Trains in a gun barrel (not shown) can interact.

Bei einer gesamten Geschossmasse von 100 % sind hiervon 10 % Halteelement 2', 50 % Penetrator 3 und 40 % Hülle 15, wobei bei einer gesamten Halteelementmasse von 100 % davon 40 % Halteelement-Front 10', 50 % Halteelement-Mitte 9' und 10% Halteelement-Heck 8' sind. Das Geschoss 1' besteht hier also aus dem Halteelement 2', dem Penetrator 3 sowie der Hülle 15.With a total projectile mass of 100%, 10% of these are retaining element 2', 50% penetrator 3 and 40% casing 15, with a total retaining element mass of 100% being 40% front retaining element 10', 50% middle retaining element 9' and 10% retaining element stern 8' are. The projectile 1' consists here of the holding element 2', the penetrator 3 and the casing 15.

BEZUGSZEICHENLISTEREFERENCE LIST

1, 1'1, 1'
Geschossbullet
2,2'2.2'
Halteelementholding element
33
Penetratorpenetrator
44
Penetratorfrontpenetrator front
55
Penetratorheckpenetrator rear
66
Penetratorspitzepenetrator tip
77
Stirnflächeface
8,8'8.8'
Halteelement-HeckRetaining element rear
9,9'9.9'
Halteelement-MitteRetainer center
10,10'10,10'
Halteelement-FrontRetaining element front
1111
Einbuchtungindentation
12, 12'12, 12'
Aufnahmeöffnungintake opening
13, 13a, 13b 13c, 13d13, 13a, 13b 13c, 13d
Rillengrooves
1414
Frontbereich der Halteelement-FrontFront area of the holding element front
1515
HülleCovering
1616
Einrillunggroove
1717
Bördelungflanging
1818
Luftraumairspace
1919
Kegelstumpftruncated cone
2020
Innengekelinside frame
AA
Geschossachsebullet axis
LPFLPF
Länge der Penetratorfrontlength of the penetrator front
LPHLPH
Länge des PenetratorhecksLength of the penetrator tail
LPLP
Gesamtlänge des PenetratorsTotal length of the penetrator
LKF, LKF'LKF, LKF'
Länge der Halteelement-FrontLength of the holding element front
LKM, LKM'LKM, LKM'
Länge der Halteelement-MitteLength of the holding element center
LKH, LKH'LKH, LKH'
Länge des Halteelement-HecksLength of the rear holding element
LK, LK'LK, LK'
Gesamtlänge des HalteelementsTotal length of the holding element
DPHDPH
Durchmesser des PenetratorhecksDiameter of the penetrator tail
DKH, DKH'DKH, DKH'
Durchmesser am Kegelstumpfende des Halteelement-HecksDiameter at the truncated end of the retaining element rear
DKM, DKM'DKM, DKM'
Durchmesser der Halteelement-MitteDiameter of the holding element center
rKFrKF
Ogivenradius der Halteelement-FrontOgival radius of the holding element front
aPFaPF
Konuswinkel der PenetratorfrontCone angle of the penetrator front
aKFaKF
Konuswinkel der Halteelement-FrontCone angle of the holding element front
αKH, αKH'αKH, αKH'
Kegelstumpfwinkel des Halteelement-HecksAngle of truncated cone of the stern of the holding element
βKMβKM
Kegelwinkelcone angle
βKFβKF
Kegelwinkelcone angle
βKMβKM
Kegelstumpfwinkel der HülleFrustum angle of the hull
RTa, RTb RTc, RTdRTa, RTb RTc, RTd
Rillentiefegroove depth
RBa, RBb RBc, RBdRBa, RBb RBc, RBd
Rillenbreitegroove width
RAa, RAb RAc,RAa, RAb RAc,
Rillenabstandgroove spacing

Claims (11)

  1. A bullet (1') comprising a retaining element (2') and a penetrator (3),
    wherein the penetrator (3) is received at least partially in a receiving opening (12'), extending centrally relative to the bullet axis (A), of the retaining element (2'), and has a penetrator front (4) and a penetrator rear (5), and
    wherein the penetrator rear (5) is formed in a cylindrical manner and the penetrator front (4) is formed in a manner tapering conically toward the bullet axis (A) starting from the penetrator rear (5) in the direction of a penetrator tip (6),
    wherein the retaining element (2') has a retaining element rear (8'), a retaining element middle (9'), and a retaining element front (10'),
    wherein the retaining element front (10'), the retaining element middle (9'), and at least regionally also the retaining element rear (8') are encased by a casing (15),
    characterized in that the length (LPF) of the penetrator front (4) is in a length ratio of about 1 to 1, preferably about 1 to 1.5, particularly preferably about 1 to 2.2, with respect to the length (LPH) of the penetrator rear (5), and
    in that the casing (15) encloses an air space (18) with the retaining element rear (8') in the region of the retaining element rear (8').
  2. The bullet (1') as claimed in claim 1, wherein the penetrator front (4) has a cone angle (αPF) of between 5° and 25°, preferably 13°, and/or
    wherein the penetrator tip (6) has a flat end face (7), which extends perpendicularly to the bullet axis (A).
  3. The bullet (1') as claimed in either of the preceding claims, wherein the total length (LP) of the penetrator (3) is between 35 mm and 55 mm, preferably 45 mm, and/or
    wherein the length (LPF) of the penetrator front (4) is between 12 mm and 17 mm, preferably 14 mm, and/or
    wherein the length (LPH) of the penetrator rear (5) is between 15 mm and 44 mm, preferably 31 mm, and/or
    wherein the diameter (DPH) of the penetrator rear (5) is between 6 mm and 9 mm, preferably 7 mm.
  4. The bullet (1') as claimed in one of the preceding claims, wherein the penetrator (3) is formed in one piece from the penetrator front (4) and the penetrator rear (5), and consists of a material with a higher density than the retaining element (2'), in particular of tungsten carbide.
  5. The bullet (1') as claimed in any one of the preceding claims, wherein the penetrator (3) is received entirely, and in particular with a precise fit, in the retaining element (2').
  6. The bullet (1') as claimed in any one of the preceding claims, wherein the retaining element (2') has a frustoconical retaining element rear (8'), a cylindrical retaining element middle (9'), and an ogival retaining element front (10'), wherein the retaining element front (10') transitions into a frustum shape or calotte shape in its front region (14).
  7. The bullet (1') as claimed in any one of the preceding claims, , wherein the casing (15) consists of brass and/or brass alloys.
  8. The bullet (1') as claimed in any one of the preceding claims, wherein the casing (15) has a greater wall thickness in the front region (14) of the retaining element front (10'), and/or
    wherein the casing (15) has a notch (16) in the region of the retaining element middle (9'), and/or
    wherein the casing (15) has rear-side flanging (17) in the region of the retaining element rear (8').
  9. The bullet (1') as claimed in any one of the preceding claims, wherein the retaining element middle (9') has at its front a frustum (19) with a cone angle (βKM) of between 30° and 50°, preferably 45°, and wherein the retaining element front (10') has at its rear an internal cone (20) with an identical cone angle (βKF) and has been fitted in a form-fitting manner on the frustum (19), and/or
    wherein the retaining element middle (9') extends beyond the middle (M) of the penetrator (3) starting from the penetrator rear (5) in the direction of the penetrator front (4), and/or
    wherein the retaining element front (10') extends beyond the penetrator tip (6).
  10. The bullet (1') as claimed in any one of the preceding claims, wherein the retaining element rear (8') and the retaining element middle (9') are formed in one piece and consist of a plastic, in particular PET, or steel, and/or
    wherein the retaining element front (10') consists of pulverulent substances or mixtures such as borax, incendiary agents or explosives.
  11. The bullet (1') as claimed in any one of the preceding claims, wherein the total length (LK') of the retaining element (2') is between 53 mm and 55 mm, preferably 54 mm, and/or
    wherein the length (LKF') of the retaining element front (10') is between 22 mm and 28 mm, preferably 26 mm, and/or
    wherein the length (LKM') of the retaining element middle (9') is between 19 mm and 25 mm, preferably 21 mm, and/or
    wherein, for a total bullet mass of 100%, the retaining element (2') makes up 10%, the penetrator (3) makes up 50%, and the casing (15) makes up 40% thereof, and/or
    wherein, for a total retaining element mass of 100%, the retaining element front (10') makes up 40%, the retaining element middle (9') makes up 50%, and the retaining element rear (8') makes up 10% thereof.
EP17764359.0A 2016-09-02 2017-09-01 Projectile with penetrator Active EP3507565B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
HRP20221423TT HRP20221423T1 (en) 2016-09-02 2017-09-01 Projectile with penetrator
SM20220501T SMT202200501T1 (en) 2016-09-02 2017-09-01 Projectile with penetrator
RS20221187A RS63869B1 (en) 2016-09-02 2017-09-01 BULLET WITH PENETRATOR
SI201731290T SI3507565T1 (en) 2016-09-02 2017-09-01 Projectile with penetrator

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP16187018 2016-09-02
PCT/EP2017/071973 WO2018042000A1 (en) 2016-09-02 2017-09-01 Projectile with penetrator

Publications (2)

Publication Number Publication Date
EP3507565A1 EP3507565A1 (en) 2019-07-10
EP3507565B1 true EP3507565B1 (en) 2022-10-26

Family

ID=56853523

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Application Number Title Priority Date Filing Date
EP17764359.0A Active EP3507565B1 (en) 2016-09-02 2017-09-01 Projectile with penetrator

Country Status (19)

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US (1) US10890423B2 (en)
EP (1) EP3507565B1 (en)
CN (1) CN109791036B (en)
AU (2) AU2017320928B2 (en)
BR (1) BR112019004186B1 (en)
CA (1) CA3035079A1 (en)
DK (1) DK3507565T3 (en)
ES (1) ES2933679T3 (en)
FI (1) FI3507565T3 (en)
HR (1) HRP20221423T1 (en)
HU (1) HUE060908T2 (en)
LT (1) LT3507565T (en)
PL (1) PL3507565T3 (en)
PT (1) PT3507565T (en)
RS (1) RS63869B1 (en)
SI (1) SI3507565T1 (en)
SM (1) SMT202200501T1 (en)
WO (1) WO2018042000A1 (en)
ZA (1) ZA201901373B (en)

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DE102023105715A1 (en) * 2023-03-08 2024-09-12 Swissp Defence Ag Jacketed bullet

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DE102017126442A1 (en) * 2017-11-10 2019-05-16 Johann Fimbinger Bullet for firearms
CN113916063A (en) * 2020-07-07 2022-01-11 东莞梵铃材料科技有限公司 Armor piercing bullet and manufacturing method thereof
LV15696B (en) * 2021-06-04 2023-03-20 Baltic Bullets, Sia An armour piercing bullet
USD1052365S1 (en) * 2021-12-24 2024-11-26 Reuben Boyd Combined spice jar and projectile
USD1062381S1 (en) * 2021-12-25 2025-02-18 Reuben Boyd Combined oil and vinegar bottle and projectile
USD1070523S1 (en) * 2021-12-25 2025-04-15 Reuben Boyd Combined sugar dispenser and projectile
USD1068401S1 (en) * 2021-12-25 2025-04-01 Reuben Boyd Combined snack jar and projectile
US12305964B2 (en) * 2022-07-07 2025-05-20 Gregory Victor Finsterbusch Alternate armor piercing bullet configuration
US20240102779A1 (en) * 2022-09-26 2024-03-28 Sig Sauer, Inc. Multi-piece projectile

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Also Published As

Publication number Publication date
HUE060908T2 (en) 2023-04-28
WO2018042000A1 (en) 2018-03-08
ES2933679T3 (en) 2023-02-13
BR112019004186B1 (en) 2022-11-16
RS63869B1 (en) 2023-01-31
DK3507565T3 (en) 2022-12-19
AU2017320928B2 (en) 2023-02-02
CA3035079A1 (en) 2018-03-08
BR112019004186A2 (en) 2019-05-28
AU2017320928A1 (en) 2019-03-21
HRP20221423T1 (en) 2023-01-06
US10890423B2 (en) 2021-01-12
CN109791036A (en) 2019-05-21
PT3507565T (en) 2022-12-20
US20190242680A1 (en) 2019-08-08
EP3507565A1 (en) 2019-07-10
CN109791036B (en) 2021-11-16
FI3507565T3 (en) 2023-01-31
LT3507565T (en) 2022-12-27
AU2023200529A1 (en) 2023-03-02
PL3507565T3 (en) 2023-03-20
SMT202200501T1 (en) 2023-01-13
SI3507565T1 (en) 2023-02-28
ZA201901373B (en) 2022-09-28

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