EP3060875B1 - Cartouche - Google Patents

Cartouche Download PDF

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Publication number
EP3060875B1
EP3060875B1 EP14787204.8A EP14787204A EP3060875B1 EP 3060875 B1 EP3060875 B1 EP 3060875B1 EP 14787204 A EP14787204 A EP 14787204A EP 3060875 B1 EP3060875 B1 EP 3060875B1
Authority
EP
European Patent Office
Prior art keywords
projectile
receiving space
cartridge
tip
casing mouth
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
EP14787204.8A
Other languages
German (de)
English (en)
Other versions
EP3060875A1 (fr
Inventor
Stephan GELFERT
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.)
RWS GmbH
Original Assignee
RUAG Ammotec GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by RUAG Ammotec GmbH filed Critical RUAG Ammotec GmbH
Priority to HRP20190623TT priority Critical patent/HRP20190623T1/hr
Publication of EP3060875A1 publication Critical patent/EP3060875A1/fr
Application granted granted Critical
Publication of EP3060875B1 publication Critical patent/EP3060875B1/fr
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
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/067—Mounting or locking missiles in cartridge cases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
    • F42B14/02—Driving bands; Rotating bands
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/025—Cartridges, i.e. cases with charge and missile characterised by the dimension of the case or the missile

Definitions

  • the invention relates to a cartridge with a projectile and a rear-mounted on the bullet sleeve with a sleeve mouth at the front end, wherein the projectile has a tip and this tip on the rear side in a circumferential front guide band, which defines the projectile outer diameter passes, and immediately adjacent to this front guide band is arranged in the direction of the floor of the floor in the axial direction of the projectile extending circumferential sleeve mouth receiving space in the projectile, in which the sleeve mouth engages.
  • Such a projectile is from the EP 1 774 251 B1 known.
  • NL 7203827 discloses a projectile sleeve connection for ammunition.
  • the invention has for its object to improve a cartridge according to the preamble of claim 1 so that when shooting the non-rotating bullet path is reduced to a minimum.
  • the gas pressure should be built up early.
  • the exposed section of the sleeve mouth receiving space is provided with a sealing means, such as e.g. a varnish sealed.
  • the bullet tip passes ogivally or conically over one or more shapes into the leading guide band, i. on the bullet outside diameter over.
  • the transitional shape of the tip to the guide band on the guide band has a conical shape at the angle of the transition cone of the cartridge chamber. The increase to the outside diameter of the projectile thus reduces the non-rotating projectile path and builds up the gas pressure.
  • the conical shape on the guide belt causes the centering of the projectile to Laufseelenachse. A centering thus produced causes a precision improvement.
  • the exposed portion of the sleeve mouth receiving space according to the invention goes straight into the front guide band and extends at an angle less than or equal to 16 degrees to the projectile axis. For aerodynamic reasons, this angle of ⁇ 16 ° to the projectile axis is preferred.
  • An embodiment is characterized in that from the radially lowest point in the sleeve mouth receiving space, ie the Feldtown tellmesser or smaller, the projectile shape in the direction of the rear concave, convex or rectilinear, over one or more forms, on the projectile diameter or smaller passes.
  • the front guide band in the bullet outside diameter allows for a smaller design of the rear bullet, since this is not required for pressure build-up. It also reduces the running load (Friction resistance and associated warming, running deposits).
  • the bullet shape is designed to be suitable for sealing the mouth of the mouth to the bullet and for pinching the mouth of the bullet.
  • a receiving space is arranged in the rear of the projectile, in which there is a substance that generates a tracer path upon initiation. It is then a tracer or a tracer cartridge.
  • the embodiment with the guide band displaced to the front can be transferred to further types of projectile.
  • FIG. 1a shows a cartridge 10 according to the invention and FIG. 1b a section A of FIG. 1a increased.
  • FIG. 2 shows the projectile 11 according to FIGS. 1a and 1b but without sleeve 12.
  • FIG. 3 shows in section a cartridge 10 according to the invention, inserted into a barrel 23 of a weapon.
  • Like reference numerals also show the same subject matter and in all figures.
  • the cartridge 10 consists of a projectile 11 and a rearwardly mounted on the projectile 11 sleeve 12 with a sleeve mouth 13 at the front end, wherein the projectile 11 has a tip 1 and this tip 1 rear side in a circumferential front guide band 4, which the projectile outer diameter defined, passes.
  • an exposed partial section 16 of the sleeve mouth receiving space 15 is arranged which extends in the axial direction of the projectile 11.
  • the sleeve mouth 13 therefore does not completely fill the sleeve mouth receiving space 15 in the direction of the nose of the projectile 11.
  • the sleeve mouth 13 thus fills only a part of the sleeve mouth receiving space 15 and the remaining part is arranged outside the sleeve 12.
  • the rotationally free projectile path during firing is reduced to a minimum.
  • the gas pressure is built up early by the front guide strip 4, whereby the possibility arises to make the area behind the front guide strip 4 smaller in diameter. Reducing the diameter reduces bullet friction in run 23. Less friction results in less heat energy. The heating of the barrel 23 is thus delayed in time. The precision is increased and retained longer. Due to the reduced bullet friction, the speed increases, creating a stretched trajectory.
  • the exposed portion 16 of the sleeve mouth receiving space 15 of the sleeve mouth 13 and a portion 7 of the sleeve mouth receiving space 15 can be easily sealed against moisture of any shape, for example by a paint in this exposed portion 16 of the sleeve mouth receiving space 15th
  • the bullet tip 1 can be round, flat or pointed.
  • the projectile nose 1 extends ogival 2 or conically over one or more forms, such as concave, convex or rectilinear 3 to the projectile outer diameter, or to the front guide 4.
  • the transition form of tip to the guide band on the guide band has a cone shape at the angle of the transition cone the cartridge warehouse.
  • the conical shape on the guide belt causes the centering of the projectile to Laufseelenachse. A centering thus produced additionally causes a precision improvement.
  • the increase to the outside diameter of the projectile is supposed to reduce the non-rotating projectile path and build up the gas pressure.
  • the bullet outside diameter or front guide band 4 is defined in each caliber over the largest permissible bullet diameter. In CIP member countries, this is the value for "G1" on "Patrons Maxi.”
  • the defined maximum permissible projectile outside diameter is used in the military and government sector.
  • the tolerance range at the front guide band 4 is - 0.1 mm to the permissible projectile diameter.
  • the projectile outer diameter or the axial extent of the front guide strip is held only briefly and runs for aerodynamic reasons slowly straight 5 expiring, to a diameter corresponding to Feldtown devismesser 6 or smaller.
  • the distance between the foremost guide belt 4 and the Feldtown choir bemesser 6 depends on the caliber with different transition lengths. However, the front guide band 4 is positioned so that as possible Little to no rotating bullet path is available. In this case, a distance between the sleeve mouth 13 and the foremost guide band 4 is essential.
  • the Feldassisomer 6 at the lowest point of the sleeve mouth receiving space 15 is defined in each caliber. In CIP member countries, this is the value for "F" in "Cartridge Mini.” Deviating from the above-mentioned field diameter 6, the minimum permissible field size is used in the military and government sector.
  • the expiring form can be concave, convex or rectilinear. For aerodynamic reasons, an angle 9 of ⁇ 16 ° to the projectile axis 17 is preferred. For radii, the angle of the resulting straight line between the front guide band 4 and the Felddemand messr 6 is used.
  • the projectile shape is concave, convex or straight 7 toward the rear (see FIG. 1b ), via one or more shapes, on the bullet diameter.
  • the bullet mold 7 is at best designed so that it is suitable for sealing the sleeve neck 24 and for pinching the sleeve 12.
  • the projectile 11 is cylindrical or provided with rear guide bands 8 in the region of the sleeve neck 24.
  • a substance may be contained, which generates a tracer. In this case we speak of a tracer bullet.
  • a projectile core 21 made of tungsten or tungsten carbide and the bore 20 is closed by a bullet tip insert 22 made of titanium or zirconium, wherein the outer shell of the bullet tip insert 22 is part of the tip 1 of the projectile 11.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Switches With Compound Operations (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Claims (5)

  1. Cartouche (10) avec un projectile (11) et une douille (12) emmanchée de l'arrière sur le projectile (11) avec une bouche de douille (13) à l'extrémité avant, le projectile (11) comportant une pointe (1) et cette pointe (1) passant à l'arrière dans une bande de guidage avant périphérique (4), laquelle définit le diamètre extérieur du projectile et un espace de réception de bouche de douille (15) périphérique s'étendant directement adjacent à cette bande de guidage avant (4) en direction de la base du projectile (14) est disposé dans le projectile (11), dans lequel la bouche de douille (13) vient en prise, une section partielle (16) dégagée de l'espace de réception de bouche de douille (15) s'étendant en direction axiale du projectile (11) étant disposée entre la bande de guidage avant (4) et la bouche de douille (13) de telle sorte que la bouche de douille (13) ne remplit pas complètement l'espace de réception de bouche de douille (15) en direction de l'avant du projectile (11), caractérisée en ce que la section partielle dégagée (16) de l'espace de réception de la bouche de douille (15) est bouchée hermétiquement avec un agent d'étanchéification, comme par ex. : une laque et en ce que la section partielle dégagée (16) de l'espace de réception de bouche de douille (15) passe dans la bande de guidage avant (4) en ligne droite sous un angle inférieur ou égal à 16 degrés par rapport à l'axe du projectile (17).
  2. Cartouche selon la revendication 1, caractérisée en ce que la pointe du projectile (1) passe de façon ogivale (2) ou conique par une ou plusieurs formes dans la bande de guidage avant (4) et sur le diamètre extérieur du projectile.
  3. Cartouche selon l'une quelconque des revendications 1 à 2 avec un diamètre de projectile, caractérisée en ce que de l'emplacement radialement le plus profond dans l'espace de réception de la bouche de douille (15), ceci correspondant au diamètre agraire ou plus petit (6), la forme du projectile passe en direction arrière de façon concave, convexe ou en ligne droite (18), par une ou plusieurs formes, sur le diamètre de projectile ou inférieur.
  4. Cartouche selon l'une quelconque des revendications 1 à 3 avec un diamètre de projectile, caractérisée en ce qu'à l'arrière du projectile (11) est disposé un espace de réception (19) dans lequel se trouve une matière, qui produit une trace lumineuse lors de l'amorçage.
  5. Cartouche selon l'une quelconque des revendications 1 à 4, caractérisée en ce qu'un trou coaxial (20) à l'axe du projectile (17) est disposé dans le projectile (11), qui est ouvert vers la pointe du projectile (11) et un noyau de projectile (21) en carbure de tungstène est disposé dans le trou (20) et le trou (20) est fermé par un embout de pointe de projectile (22) en titane, l'enveloppe extérieure de l'embout de pointe de projectile (22) faisant partie de la pointe (1) du projectile (11).
EP14787204.8A 2013-10-25 2014-10-24 Cartouche Active EP3060875B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
HRP20190623TT HRP20190623T1 (hr) 2013-10-25 2014-10-24 Patrona

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013017672 2013-10-25
PCT/EP2014/072866 WO2015059282A1 (fr) 2013-10-25 2014-10-24 Cartouche

Publications (2)

Publication Number Publication Date
EP3060875A1 EP3060875A1 (fr) 2016-08-31
EP3060875B1 true EP3060875B1 (fr) 2019-03-27

Family

ID=51790703

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14787204.8A Active EP3060875B1 (fr) 2013-10-25 2014-10-24 Cartouche

Country Status (13)

Country Link
US (1) US9797695B2 (fr)
EP (1) EP3060875B1 (fr)
JP (1) JP6576341B2 (fr)
KR (1) KR102220828B1 (fr)
AU (1) AU2014338927B2 (fr)
BR (1) BR112016009057B1 (fr)
CA (1) CA2928157C (fr)
DE (1) DE102014015674A1 (fr)
DK (1) DK3060875T3 (fr)
HR (1) HRP20190623T1 (fr)
HU (1) HUE044253T2 (fr)
IL (1) IL245223B (fr)
WO (1) WO2015059282A1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10048051B1 (en) * 2015-06-18 2018-08-14 Cutting Edge Bullets, LLC Firearm projectile
US10684108B2 (en) * 2015-10-21 2020-06-16 Vista Outdoor Operations Llc Reduced drag projectiles
US10222188B2 (en) * 2016-01-15 2019-03-05 Joshua M. Kunz Projectile with enhanced ballistic efficiency
US10436557B2 (en) * 2016-04-18 2019-10-08 Ammo Technologies, Inc. Armor-piercing projectile
IT201600085447A1 (it) * 2016-08-16 2018-02-16 Claudio Terrizzi Pallottola per cartuccia 6,5 x 52 mm carcano
EP3467427A1 (fr) * 2017-10-03 2019-04-10 BAE SYSTEMS plc Munitions à performance améliorée
EP3692325B1 (fr) * 2017-10-03 2022-11-30 BAE Systems PLC Munitions à performance améliorée
GB2575226B (en) * 2017-10-03 2021-12-22 Bae Systems Plc Enhanced performance ammunition
US20190120603A1 (en) * 2017-10-19 2019-04-25 Richard C. Cole Projectile with radial grooves
DE102019121984A1 (de) * 2019-08-15 2021-02-18 Rheinmetall Waffe Munition Gmbh Penetrator, Verwendung eines Penetrators und Geschoss

Family Cites Families (16)

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Publication number Priority date Publication date Assignee Title
US2120913A (en) * 1934-02-01 1938-06-14 Rene R Studler Projectile
GB576726A (en) * 1943-08-12 1946-04-17 Siegfried Keller Cartridge for automatic gun
FR899552A (fr) * 1942-11-13 1945-06-05 Oerlikon Buehrle Ag Cartouche pour canon automatique
US2872864A (en) * 1952-01-08 1959-02-10 Gladeon M Barnes Center-guide for fin-stabilized fixed round ammunition
US3720169A (en) * 1971-03-30 1973-03-13 Us Army Incendiary projectile for smooth bore special purpose individual weapon
NL144057B (nl) * 1972-03-22 1974-11-15 Nederl Wapen & Munitie Peojectielhulsverbinding voor munitie, in het bijzonder voor uiteenvaloefenmunitie.
US3968750A (en) * 1972-03-22 1976-07-13 Nederlandsche Wapen- En Munitiefabriek "De Kruithoorn" B.V. Projectile-case connection
JPS5241200U (fr) * 1975-09-17 1977-03-24
NO137297C (no) * 1976-07-01 1978-02-01 Raufoss Ammunisjonsfabrikker Prosjektil.
DE8812000U1 (de) * 1988-09-22 1990-02-08 Rheinmetall GmbH, 4000 Düsseldorf Granatengeschoß
US5686693A (en) * 1992-06-25 1997-11-11 Jakobsson; Bo Soft steel projectile
AUPN554295A0 (en) * 1995-09-20 1996-02-01 Australian Defence Industries Limited Frangible ammunition
DE102004036148A1 (de) 2004-07-24 2006-02-16 Ruag Ammotec Gmbh Hartkerngeschoss mit Penetrator
US7966937B1 (en) * 2006-07-01 2011-06-28 Jason Stewart Jackson Non-newtonian projectile
DE102007025981A1 (de) * 2007-06-04 2008-12-11 Rheinmetall Waffe Munition Gmbh Patronenmunition, insbesondere Übungsmunition
KR100843573B1 (ko) * 2008-03-13 2008-07-03 (주)한국원자력 엔지니어링 탄약

Non-Patent Citations (1)

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Title
None *

Also Published As

Publication number Publication date
NZ720372A (en) 2020-12-18
IL245223A0 (en) 2016-06-30
BR112016009057B1 (pt) 2021-02-02
DE102014015674A1 (de) 2015-04-30
HRP20190623T1 (hr) 2019-05-31
DK3060875T3 (da) 2019-05-06
KR102220828B1 (ko) 2021-02-25
WO2015059282A1 (fr) 2015-04-30
JP2016538517A (ja) 2016-12-08
KR20160087386A (ko) 2016-07-21
JP6576341B2 (ja) 2019-09-18
US20160252332A1 (en) 2016-09-01
HUE044253T2 (hu) 2019-10-28
IL245223B (en) 2020-10-29
AU2014338927A1 (en) 2016-06-09
AU2014338927B2 (en) 2018-10-18
CA2928157A1 (fr) 2015-04-30
CA2928157C (fr) 2022-06-14
EP3060875A1 (fr) 2016-08-31
US9797695B2 (en) 2017-10-24

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