EP3507565B1 - Geschoss mit penetrator - Google Patents

Geschoss mit 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
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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)
English (en)
French (fr)
Other versions
EP3507565A1 (de
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/hr
Priority to RS20221187A priority patent/RS63869B1/sr
Priority to SI201731290T priority patent/SI3507565T1/sl
Publication of EP3507565A1 publication Critical patent/EP3507565A1/de
Application granted granted Critical
Publication of EP3507565B1 publication Critical patent/EP3507565B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04—Projectiles, 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
    • F42B12/06—Projectiles, 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)
  • Toys (AREA)
  • Particle Accelerators (AREA)
EP17764359.0A 2016-09-02 2017-09-01 Geschoss mit penetrator Active EP3507565B1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
HRP20221423TT HRP20221423T1 (hr) 2016-09-02 2017-09-01 Projektil s penetratorom
RS20221187A RS63869B1 (sr) 2016-09-02 2017-09-01 Metak sa penetratorom
SI201731290T SI3507565T1 (sl) 2016-09-02 2017-09-01 Izstrelek s penetratorjem

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP16187018 2016-09-02
PCT/EP2017/071973 WO2018042000A1 (de) 2016-09-02 2017-09-01 Geschoss mit penetrator

Publications (2)

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

Family

ID=56853523

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17764359.0A Active EP3507565B1 (de) 2016-09-02 2017-09-01 Geschoss mit penetrator

Country Status (18)

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

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DE102017126442A1 (de) * 2017-11-10 2019-05-16 Johann Fimbinger Geschoss für Schusswaffen
CN113916063A (zh) * 2020-07-07 2022-01-11 东莞梵铃材料科技有限公司 穿甲弹头及其制造方法
LV15696B (lv) * 2021-06-04 2023-03-20 Baltic Bullets, Sia Bruņsitēju lode

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* Cited by examiner, † Cited by third party
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DE102023105715A1 (de) 2023-03-08 2024-09-12 Swissp Defence Ag Mantelgeschoss

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FI3507565T3 (fi) 2023-01-31
HUE060908T2 (hu) 2023-04-28
PL3507565T3 (pl) 2023-03-20
RS63869B1 (sr) 2023-01-31
WO2018042000A1 (de) 2018-03-08
BR112019004186B1 (pt) 2022-11-16
EP3507565A1 (de) 2019-07-10
CN109791036A (zh) 2019-05-21
AU2017320928B2 (en) 2023-02-02
CA3035079A1 (en) 2018-03-08
BR112019004186A2 (pt) 2019-05-28
SI3507565T1 (sl) 2023-02-28
AU2023200529A1 (en) 2023-03-02
PT3507565T (pt) 2022-12-20
DK3507565T3 (da) 2022-12-19
US10890423B2 (en) 2021-01-12
ES2933679T3 (es) 2023-02-13
CN109791036B (zh) 2021-11-16
US20190242680A1 (en) 2019-08-08
LT3507565T (lt) 2022-12-27
HRP20221423T1 (hr) 2023-01-06

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