EP3507565A1 - Projectile muni d'un pénétrateur - Google Patents

Projectile muni d'un pénétrateur

Info

Publication number
EP3507565A1
EP3507565A1 EP17764359.0A EP17764359A EP3507565A1 EP 3507565 A1 EP3507565 A1 EP 3507565A1 EP 17764359 A EP17764359 A EP 17764359A EP 3507565 A1 EP3507565 A1 EP 3507565A1
Authority
EP
European Patent Office
Prior art keywords
holding element
penetrator
projectile
tail
center
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.)
Granted
Application number
EP17764359.0A
Other languages
German (de)
English (en)
Other versions
EP3507565B1 (fr
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 RS20221187A priority Critical patent/RS63869B1/sr
Priority to HRP20221423TT priority patent/HRP20221423T1/hr
Priority to SI201731290T priority patent/SI3507565T1/sl
Priority to SM20220501T priority patent/SMT202200501T1/it
Publication of EP3507565A1 publication Critical patent/EP3507565A1/fr
Application granted granted Critical
Publication of EP3507565B1 publication Critical patent/EP3507565B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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 projectile with high penetrating power which has an armor piercing effect.
  • Such projectiles are used in particular by snipers and aim for a precise penetration of armored targets such as personal protection vest, bulletproof glass, steel plates or light metal armor.
  • the kinetic energy of their projectile is used to penetrate the target surface, so that can be dispensed in the projectile even on explosives or detonators.
  • the term penetrator is therefore a common term for the projectile.
  • Projectiles which have a core with a jacket are referred to as jacket bullets. The jacket protects the barrel on the one hand and also prevents deformation or splitting of the core when hitting a target object.
  • WO 97/41404 discloses a small-caliber projectile having a bullet core of a hard and heavy material, wherein the bullet core is disposed within a hollow bullet jacket.
  • an armor-piercing projectile with a projectile casing is known, a hard-metal core and a filling material being arranged in the projectile casing.
  • No. 6,374,743 B1 discloses a small caliber projectile with a hard core arranged on the front side and a soft core arranged on the rear side.
  • the small caliber bullet has a steel, clad steel or brass cladding.
  • a hard core projectile which has a bullet core.
  • a penetrator is inserted, which protrudes from the bullet core.
  • a particularly preferred object is to provide a bullet, which has a high penetration and increased precision.
  • a projectile comprising a retaining element and a penetrator
  • the penetrator being accommodated at least partially in a receiving opening of the retaining element running concentric with the projectile axis and having a penetrator front and a penetrator tail.
  • the penetrator tail is cylindrical and the penetrator front is tapered starting from the penetrator in the direction of a penetrator tip to the projectile axis.
  • the length of the penetrator front is in terms of the length of the Penetratorhecks 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 rear seen along the projectile axis is longer than the front.
  • a conical or conical front is understood in particular to mean that the front is conical or conical in the geometrical sense. That is, the outer surface preferably extends 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 larger, preferably about 4 to 10 times larger, than the weight of the conical penetrator front.
  • the penetrator front has a cone angle between 10 ° and 20 °, preferably 13 °. This means that the penetrator front tapering from the penetrator tail 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 region than in its rear region.
  • the penetrator tip may have a flat end surface which extends perpendicular to the projectile axis.
  • the penetrator may alternatively have a pointed end.
  • the tapered penetrator front thus preferably opens into a penetrator tip, which forms an elongated 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 Penetratorhecks 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 so the sum of the length of the penetrator front and the length of the Penetratorhecks, and the diameter of the Penetratorhecks in a ratio of about 4 to 10, preferably from about 5 to 9 to each other.
  • the total length of the penetrator is about 4 to 10 times longer, preferably about 5 to 9 times longer than the diameter of the penetrator back.
  • the penetrator is preferably formed in one piece from the penetrator front and the penetrator tail and is preferably made of a material with a higher density than the holding element, in particular of tungsten carbide.
  • the penetrator consisting of a material with high density, which gives the penetrator a high strength or hardness.
  • the penetrator is preferably made of an alloy whose main constituent is tungsten, e.g. Tungsten carbide.
  • the penetrator consists of a single element, e.g. Tungsten, exists.
  • the penetrator front and the penetrator tail are not designed as different components, but rather an integrally formed penetrator whose outer shape, viewed from the penetrator tip, is formed in a conical shape and merges into a cylindrical rear region.
  • the penetrator in particular the penetrator front, projects out of the holding element on the face side. If such a bullet with projecting penetrator impinges on the target object, the penetrator unfolds its effect immediately, whereby energy, which would be required in the case of a fully covered penetrator for the deformation or disassembly of the holding element, is completely available to the penetrator. It is preferred that the penetrator tail is received precisely in the receiving opening of the holding element.
  • the penetrator protrudes from the front side of the receiving opening of the holding element, the rear-side region of the penetrator is received in the receiving opening.
  • the attachment of the penetrator in the holding element can via a frictional connection such as a press fit, in which the penetrator is pressed into the receiving opening in the holding element, take place.
  • the retaining element has several Einrillungen reduced diameter in the region of the holding element center.
  • Other ways of attachment are a cohesive connection by soldering or gluing or a positive attachment.
  • the retaining element preferably has a frustoconical holding element tail, a cylindrical holding element center and a holding element front, which is formed tapering from the holding element center in the direction of the penetrator tip to the projectile axis.
  • the holding element front forms an extension of the conical tip of the penetrator and extends in the same direction as the conical tip of the penetrator. It is preferred that the holding element front has a cone angle between 10 ° and 20 °, preferably 13 °, and / or that the holding element front has a wall thickness which decreases continuously in the direction of the penetrator tip and preferably in the transition region between the penetrator front and the penetrator tail Zero is so that the entire penetrator front is exposed.
  • the entire penetrator front preferably projects out of the holding element and already penetrates into the target object before the holding element impinges on the target object, so that the projectile can deliver its kinetic energy very effectively to the target object.
  • the holding element front extends at least partially over the penetrator rear and leaves uncovered, for example, both the penetrator tip and a part of the penetrator back.
  • the retaining element rear has a truncated cone angle between 5 ° and 15 °, preferably 9 °, and / or the diameter at the truncated cone end of the retaining element tail is preferably between 9 mm and 11 mm, preferably 10 mm, and / or Garelement-
  • the stern preferably has a conical indentation.
  • the conical indentation is preferably in the rear region of the retaining element tail and serves to improve the flight characteristics of the projectile by stabilization.
  • the diameter of the holding element center between 12.5 mm and 13.5 mm, preferably 12.98 mm, and / or the lateral surface of the holding element center preferably has circumferential grooves.
  • the grooves may be arranged in a rear region of the holding element center.
  • only a front-side region of the holding element center or the entire holding element center is provided with grooves.
  • two or more grooves are preferably provided, which are formed starting from the rear end of the holding element center in the direction of the front end of the holding element center immediately adjacent to each other in the lateral surface of the holding element center. It is possible that the grooves are each arranged at the same distance from each other on the lateral surface. Alternatively, however, the grooves may also have different distances from each other. For example, four grooves may be provided, wherein the distance between two adjacent grooves, starting from the rear end in the direction of the front end of the holding element center increases increasingly.
  • first two grooves with respect to the rear end of the holding element center can be arranged at a first distance from one another and the last two grooves with respect to the rear end of the holding element center at a second distance 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 grout over 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 clearance of the recess can also be the same or different.
  • the groove depth is preferably between 0.5 mm to 2.0 mm, in particular 1.5 mm, and / or the clear width of the grooves is preferably between 1.0 mm to 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 in other words, the groove depth is preferably about one third of the clear width up to twice the clear width, in particular half of 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 adapted to cooperate with appropriately trained trains in a gun barrel and serve to reduce the friction of the projectile in the gun barrel, lead to a lower erosion and thus increase the life of the weapon. Together with the rest of the design of the projectile, in particular due to the penetrator, the grooves also lead to an increase in performance. Thus, the friction reduction of the grooves and the hardness of the material as well as the mass of the penetrator cause the projectile to impinge on a target with a high penetration force and, for example, penetrate steel plates.
  • the holding element is preferably formed integrally from the retaining element rear, the holding element center and the holding element front and is preferably made of brass and / or brass alloys.
  • the holding element front, the holding element center and the Halteelement- tail are therefore not formed as different components but integrally molded
  • the outer shape of the holding element viewed from the Penetrator dictate, in is conical shape and merges into a cylindrical central region and then in a frustoconical rear area.
  • the total length of the holding element is preferably between 35 mm and 55 mm, preferably 43 mm, and / or the length of the holding element front is preferably between 3 mm and 21 mm, preferably 13 mm, and / or the length of the holding element center is preferably between 14 mm and 42 mm, preferably 21 mm.
  • the penetrator is preferably completely, and in particular accurately fitting, received in the holding element.
  • the penetrator fills the receiving opening in the holding element completely.
  • the holding element has a frustoconical holding element rear, a cylindrical holding element center and an ogival holding element front, wherein the holding element front merges in its front region into a truncated cone shape or dome shape.
  • the holding element front, the holding element center and at least partially the retaining element rear are enveloped by a shell, wherein the shell is preferably made of brass.
  • the rear region of the retainer tail can be sleeve-free.
  • a completely enclosed retaining element tail that is to say a retaining element which is completely enveloped in its entirety.
  • the sheath is preferably designed such that it has the respective shape of the wrapped holding element region, namely ogival, cylindrical or frustoconical. It is preferred that the sheath directly adjacent to the holding element and thus is applied directly on this.
  • a compact, rotationally symmetrical and dimensionally accurate projectile can be provided by a form-fitting fitting to the holding element sleeve, which has good fürdringungseigenschaften.
  • the casing preferably has a thickened wall thickness in the front region of the holding element front, and / or the casing preferably has a groove in the region of the holding element center, and / or the casing preferably has a rear flanging in the region of the holding element tail. and / or the shell preferably encloses an air space with the retaining element tail in the region of the retaining element tail.
  • the grooving can interact with appropriately trained trains in a gun barrel and serves to reduce the friction of the projectile in the gun barrel.
  • the thickening on the front of the case reduces bounce in the case of oblique angle bombardment on hard target objects and also serves to determine the center of mass of the projectile.
  • the holding element center front side has a truncated cone with a cone angle between 30 ° and 50 °, preferably 45 °, and the holding element front preferably has on the rear side a réellegekel with the same cone angle and is positively placed on the truncated cone.
  • These cone angles allow an optimal rotationally symmetrical centering of the holding element front on the holding element center and thus also of the penetrator accommodated therein.
  • the holding element center extends from the penetrator tail in the direction of the penetrator front beyond the center of the penetrator, and / or that the holding element front extends beyond the penetrator tip. In other words, the penetrator tip is completely surrounded by the holding element front.
  • the holding element rear and the holding element center are integrally formed and made of a plastic, in particular PET, or steel, and / or the holding element front consists of powdery substances or mixtures such as borax, fire or explosive charges.
  • the holding element rear and the holding element center are formed integrally, while it is at the holding element front to a separately formed component.
  • the penetrator is made of a very high density material
  • the retainer has a material or materials with a lower density than the penetrator.
  • the total length of the retaining element is preferably between 53 mm and 55 mm, preferably 54 mm, and / or the length of the Halteelement- front is preferably between 22 mm and 28 mm, preferably 26 mm, and / or the length the holding element center is preferably between 19 mm and 25 mm, preferably 21 mm.
  • a total floor mass of 100% thereof 10% holding element, 50% penetrator and 40% sheath, and / or preferably with a total holding element mass of 100% thereof 40% holding element front, 50% holding element center and 10% holding element -Rear.
  • FIG. 1 shows a partial sectional view through a projectile according to a first embodiment
  • FIG. 2 shows a full sectional view through the projectile according to FIG. 1;
  • Fig. 3 is a partial sectional view through a projectile according to a second
  • FIG. 4 shows a full sectional view through the projectile according to FIG. 3.
  • FIGS. 1 to 4 each show a projectile 1, comprising a holding element 2, 2 'and a penetrator 3, which has a penetrator front 4 and a penetrator tail 5.
  • the penetrator 5 is cylindrical in shape and the penetrator front 4 is formed starting from the penetrator 5 in the direction of a Penetratorspitze 6 to the projectile axis A tapered towards.
  • the total 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.
  • FIGS. 1 and 2 show a first embodiment of the projectile 1 in which the penetrator 3 is only partially received in the rear side of a receiving opening 12 of the holding element 2 which extends centrally with respect to the projectile axis A and projects out of the holding element 2 with the penetrator front 4.
  • FIGS. 3 and 4 show a second embodiment of the projectile 1 ', in which the penetrator 3 is completely accommodated in the holding element 2'.
  • identical components are provided with the same reference numerals.
  • the penetrator front 4 has a cone angle aPF of about 13 ° and the penetrator tip 6 has a flat end face 7, which extends perpendicular to the projectile axis A.
  • the diameter DPH of the penetrator 5 is about 7 mm.
  • the penetrator 3 is formed in one piece from the penetrator front 4 and the penetrator 5 and is made entirely of tungsten carbide.
  • the penetrator tail 5 of the projectile 1 according to the first embodiment is snugly received in the receiving opening 12 of the holding element 2, the rear end of the penetrator 5 having a reduced diameter recess in the region of its bottom.
  • the holding element 2 has a frustoconical holding element rear end 8, a cylindrical holding element center 9 and a holding element front 10, the holding element front 10 tapering from the holding element center 9 in the direction of the penetrator tip 6 to the projectile axis A is trained.
  • the conical holding element front 10 is formed 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 location of the transition from the penetrator front 4 to the rear 5 of the penetrator.
  • the whole Penetratorfront 4 is thus free. In this case, there is a seamless transition between the front-side holding element front 10 and the rear-side 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 holding element front 10.
  • the frustoconical holding element rear 5 in this case has a truncated cone angle aKH of about 9 ° and the diameter DKH at the truncated cone end of the holding element tail 8 is about 10 mm.
  • the rear retaining element 8 has a conical indentation 11 at the rear, which extends centrally into the retaining element rear 8.
  • the holding element center 9 has a diameter DKM of about 13 mm and on the lateral surface of the holding element center 9 in some areas circumferential grooves 13 are provided, which can cooperate with appropriately trained trains in a gun barrel (not shown).
  • the clear width of these grooves that is, together with the groove depth RTa, RTb or clear height and the clear width RBa, RBb, each is the same.
  • the distance RTa between these two grooves 13a, 13b corresponds approximately to the groove depth RTa, RTb or clear height of these grooves 13a, 13b.
  • the two further two grooves 13c, 13d arranged subsequent to these two grooves 13a, 13b each have a rectangular groove shape and differ in their clear width from both 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-shape. shaped grooves 13a, 13b.
  • the rectangular groove 13c disposed adjacent to the U-shaped groove 13b extends into the circumferential surface by a much smaller amount than the other rectangular groove 13d. While the rectangular groove 13c and the U-shaped groove 13b adjacent thereto are arranged at a distance RAb from each other which is approximately equal to the distance RAa of the two U-shaped grooves, the distance RAc is between the two rectangular grooves 13c, 13d however, much smaller.
  • the groove depth RTa, RTb of the first and second U-shaped grooves 13a, 13b is here about one eighth of the diameter DKM of the holding element center.
  • the groove depths RTc, RTd of the third groove 13c disposed adjacent to the U-shaped groove 13b and the fourth groove 13d located adjacent to the third groove 13c are about a factor of 30 and 15, respectively, smaller than the diameter DKM holding-center.
  • the holding element 2 is integrally formed from the retaining element rear 8, the holding element center 9 and the Halteelement- front 10 and is made entirely of brass.
  • the total length LK of the holding element 2 here amounts to approximately 46 mm, the length LKF of the holding element front 10 being approximately 14 mm, the length LKM of the holding element center 9 approximately 22 mm, and the length LKH of the holding element tail 8 being approximately 10 mm ,
  • the projectile 1 here therefore consists solely of the holding element 2 and the penetrator 3 and is in particular formed without a casing.
  • the holding element 2 'of the projectile has, analogously to the holding element 2 of the projectile 1, a frustoconical holding element tail 8' and a cylindrical holding element center 9 '.
  • the holding element 2 'of the projectile has an ogival holding element front 10', which merges into a dome shape in its front region 14.
  • the diameter DKM 'of the holding element center 9' is about 11 mm.
  • the holding element tail 8 ' has a cone obtuse angle aKH' of about 9 °, wherein the diameter DKH 'at the truncated cone end of the holding element tail 8' is about 8.5 mm.
  • the holding element center 9 ' has front side over a truncated cone 19 with a cone angle ßKM of about 45 ° and the holding element front 10' has the rear side on a réellegekel 20 with the same cone bevel 1 ßKF of about 45 °, the inner cone 20 on a form fit the truncated cone 19 is placed.
  • the holding element center 9 ' extends starting from the penetrator tail 5 in the direction of the penetrator front 4 beyond the center M of the penetrator 3, and the holding element front 10' extends along the same direction beyond the penetrator tip 6.
  • the retaining element tail 8 'and the holding element center 9' are integrally formed and made of PET or steel.
  • the separately formed holding element front 10 ' is made of borax.
  • the total 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 'on the rear side in the region of its bottom has a recess with a reduced diameter and is snugly received in a receiving opening 12' of the holding element 2 '.
  • the receiving opening 12 ' extends centrally through the holding element center 9' in the holding element tail 8 'into it.
  • the penetrator front 4 is accommodated in a precisely fitting recess of the holding element front 10 ', which increasingly tapers starting from the penetrator 5 in the direction of the penetrator front 4.
  • the holding element front 10 ', the holding element center 9' and partially the retaining element tail 8 'enveloped by a shell 15, which is the respective shape of the wrapped support member 2', ie ogival in the front, cylindrical in the central region and frustoconical in the rear area, has.
  • the shell 15 is made entirely of brass here and lies directly on the lateral surface of the holding element front 10 'and the holding element center 9'.
  • the envelope 15 also partially surrounds the holding element tail 8 'and encloses with the retaining element rear end 8' an air space 18, which increasingly increases from the front region to the rear region of the holding element tail 8 '.
  • the distance between the shell 15 and the lateral surface of the retaining element tail 8 ' is thus increasingly increased in this direction.
  • the shell 15 ends at the rear on the retaining element rear end 8 'in a flange 17 and leaves a portion of the retaining element rear 8' without sheaths.
  • the penetrator 3 is never in contact with the sheath 15.
  • the sheath 15 has a thickened wall thickness in the front region of the holding element front 10 'and has a grooving 16 in the region of the holding element center 9', which has a recess 16 corresponding thereto Trains in a gun barrel (not shown) can cooperate.

Landscapes

  • 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)

Abstract

L'invention concerne un projectile (1, 1') comprenant un élément de retenue (2, 2') et un pénétrateur (3), le pénétrateur (3) étant logé au moins en partie dans une ouverture de logement (12, 12') de l'élément de retenue (2, 2') s'étendant centralement par rapport à l'axe (A) du projectile, et le pénétrateur présentant une partie avant (4) de pénétrateur et une partie arrière (5) de pénétrateur. La partie arrière (5) du pénétrateur est de forme cylindrique, et la partie avant (4) du pénétrateur s'étend sous forme conique par rapport à l'axe (A) du projectile à partir de la partie arrière (5) du pénétrateur en direction d'une pointe (6) du pénétrateur. Le rapport de longueur entre la longueur (LPF) de la partie avant (4) du pénétrateur et la longueur (LPH) de la partie arrière (5) du pénétrateur est d'environ 1 pour 1, de préférence d'environ 1 pour 1,5, de préférence encore d'environ 1 pour 2,2.
EP17764359.0A 2016-09-02 2017-09-01 Projectile comprenant un penetrateur Active EP3507565B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
RS20221187A RS63869B1 (sr) 2016-09-02 2017-09-01 Metak sa penetratorom
HRP20221423TT HRP20221423T1 (hr) 2016-09-02 2017-09-01 Projektil s penetratorom
SI201731290T SI3507565T1 (sl) 2016-09-02 2017-09-01 Izstrelek s penetratorjem
SM20220501T SMT202200501T1 (it) 2016-09-02 2017-09-01 Proiettile con penetratore

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP16187018 2016-09-02
PCT/EP2017/071973 WO2018042000A1 (fr) 2016-09-02 2017-09-01 Projectile muni d'un pénétrateur

Publications (2)

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

Family

ID=56853523

Family Applications (1)

Application Number Title Priority Date Filing Date
EP17764359.0A Active EP3507565B1 (fr) 2016-09-02 2017-09-01 Projectile comprenant un penetrateur

Country Status (20)

Country Link
US (1) US10890423B2 (fr)
EP (1) EP3507565B1 (fr)
CN (1) CN109791036B (fr)
AU (2) AU2017320928B2 (fr)
BR (1) BR112019004186B1 (fr)
CA (1) CA3035079A1 (fr)
CY (1) CY1125770T1 (fr)
DK (1) DK3507565T3 (fr)
ES (1) ES2933679T3 (fr)
FI (1) FI3507565T3 (fr)
HR (1) HRP20221423T1 (fr)
HU (1) HUE060908T2 (fr)
LT (1) LT3507565T (fr)
PL (1) PL3507565T3 (fr)
PT (1) PT3507565T (fr)
RS (1) RS63869B1 (fr)
SI (1) SI3507565T1 (fr)
SM (1) SMT202200501T1 (fr)
WO (1) WO2018042000A1 (fr)
ZA (1) ZA201901373B (fr)

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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
USD1052365S1 (en) * 2021-12-24 2024-11-26 Reuben Boyd Combined spice jar and projectile
USD1068401S1 (en) * 2021-12-25 2025-04-01 Reuben Boyd Combined snack jar and projectile
USD1070523S1 (en) * 2021-12-25 2025-04-15 Reuben Boyd Combined sugar dispenser and projectile
USD1062381S1 (en) * 2021-12-25 2025-02-18 Reuben Boyd Combined oil and vinegar bottle 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
DE102023105715A1 (de) * 2023-03-08 2024-09-12 Swissp Defence Ag Mantelgeschoss

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FR2610715A1 (fr) * 1987-02-11 1988-08-12 Munitions Ste Fse Projectile perforant a noyau dur et guide ductile
NO891580L (no) 1988-05-24 1989-11-27 Oerlikon Buehrle Ag Prosjektilkjerne for et drivspeilprosjektil.
US5009166A (en) * 1989-07-31 1991-04-23 Olin Corporation Low cost penetrator projectile
SE508476C2 (sv) 1996-04-26 1998-10-12 Bofors Carl Gustaf Ab Finkaliberprojektil
JP2001514372A (ja) 1997-08-26 2001-09-11 エス・エム・シユバイツエリツシエ・ムニツイオーンスウンターネームング・アー・ゲー ハードコアを有する被甲付き弾丸
US6085661A (en) * 1997-10-06 2000-07-11 Olin Corporation Small caliber non-toxic penetrator projectile
DE50109825D1 (de) * 2001-11-28 2006-06-22 Futurtec Ag Rotkreuz Geschosse hoher Penetrations- und Lateralwirkung mit integrierter Zerlegungseinrichtung
US20050183617A1 (en) * 2004-02-23 2005-08-25 Macdougall John Jacketed ammunition
US7150233B1 (en) * 2004-04-26 2006-12-19 Olin Corporation Jacketed boat-tail bullet
DE102004036148A1 (de) 2004-07-24 2006-02-16 Ruag Ammotec Gmbh Hartkerngeschoss mit Penetrator
US20070017409A1 (en) * 2005-06-20 2007-01-25 Alliant Techsystems Inc. Non-expanding modular bullet
EP4607141A3 (fr) * 2014-04-30 2025-11-12 G9 Holdings, LLC Projectile à balles améliorées

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AU2017320928A1 (en) 2019-03-21
PT3507565T (pt) 2022-12-20
EP3507565B1 (fr) 2022-10-26
ZA201901373B (en) 2022-09-28
CN109791036B (zh) 2021-11-16
LT3507565T (lt) 2022-12-27
FI3507565T3 (fi) 2023-01-31
WO2018042000A1 (fr) 2018-03-08
RS63869B1 (sr) 2023-01-31
AU2023200529A1 (en) 2023-03-02
CY1125770T1 (el) 2026-02-25
SMT202200501T1 (it) 2023-01-13
ES2933679T3 (es) 2023-02-13
US10890423B2 (en) 2021-01-12
CN109791036A (zh) 2019-05-21
AU2017320928B2 (en) 2023-02-02
CA3035079A1 (fr) 2018-03-08
PL3507565T3 (pl) 2023-03-20
SI3507565T1 (sl) 2023-02-28
BR112019004186A2 (pt) 2019-05-28
DK3507565T3 (da) 2022-12-19
HRP20221423T1 (hr) 2023-01-06
BR112019004186B1 (pt) 2022-11-16
HUE060908T2 (hu) 2023-04-28
US20190242680A1 (en) 2019-08-08

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