EP0787969A1 - Projectile avec noyau et chemise - Google Patents

Projectile avec noyau et chemise Download PDF

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Publication number
EP0787969A1
EP0787969A1 EP97100478A EP97100478A EP0787969A1 EP 0787969 A1 EP0787969 A1 EP 0787969A1 EP 97100478 A EP97100478 A EP 97100478A EP 97100478 A EP97100478 A EP 97100478A EP 0787969 A1 EP0787969 A1 EP 0787969A1
Authority
EP
European Patent Office
Prior art keywords
projectile
core
blank
shaft
diameter
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
EP97100478A
Other languages
German (de)
English (en)
Other versions
EP0787969B1 (fr
Inventor
Albert Wernz
Wolfgang Katzmaier
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.)
Heckler und Koch GmbH
Original Assignee
Heckler und Koch 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 Heckler und Koch GmbH filed Critical Heckler und Koch GmbH
Publication of EP0787969A1 publication Critical patent/EP0787969A1/fr
Application granted granted Critical
Publication of EP0787969B1 publication Critical patent/EP0787969B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • 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
    • F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
    • F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
    • F42B12/78—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing of jackets for smallarm bullets ; Jacketed bullets or projectiles
    • 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

Definitions

  • the invention relates to a core projectile for handguns, with a solid projectile core and a jacket.
  • Such a projectile has been known for a long time and is particularly suitable for firing in machine guns, sniper rifles, tank rifles or the like, the core being said to achieve armor-piercing effect.
  • a soft, coated bullet tip is provided.
  • the custom-made projectile core is surrounded in a pressing process with a lead shirt and then with a thin jacket that takes over the leadership.
  • Such conventional cores are usually introduced from behind, but sometimes also from the front (German patent 205 734).
  • the invention has for its object to further develop the above-mentioned core storey in such a way that its performance is improved.
  • the projectile according to the invention thus differs from the known projectile in that it does not have an additional, soft tip preventing the projectile core from slipping, and preferably from the known precision projectile in that the core does not have the largest possible diameter, but a significantly smaller diameter.
  • the projectile core of the projectile according to the invention forms a slim penetrator which, because of its great length and its high mass, achieves an extraordinarily large cross-sectional load in the target, and thus a high armor-piercing effect.
  • the projectile according to the invention thus has a particularly good penetration effect on light armor.
  • the diameter of the projectile core is only part of the diameter of the entire projectile over most of its length.
  • no lead shirt is arranged between the projectile core and the jacket, which in turn consists of the State of the art is known.
  • the centricity of the projectile is improved because a layer which is subject to tolerances is dispensed with, and thus the shot precision is also improved.
  • the jacket has a considerably greater thickness than is otherwise customary and sits directly on the core of the projectile.
  • the thickness of the core is only about 2/3 of the diameter of the entire floor (claim 2). This increases the slenderness of the projectile core and thus its penetration.
  • the projectile according to the invention In the conventional projectile with a lead shirt, the latter never centers the projectile core with sufficient accuracy; moreover, the material of the lead shirt is never completely homogeneous. In the case of the projectile according to the invention, on the other hand, this lead shirt is omitted, and with it the inaccuracy caused by it. Thus, the projectile according to the invention is also particularly suitable for firing from precision weapons, also because it can be manufactured centrically with the highest accuracy.
  • the projectile core forms the projectile tip, that is to say it is exposed, and that the jacket, starting from the projectile rear, extends only over part of the length of the projectile core (claim 3).
  • the outer surface of the projectile tip is accordingly formed by the outer surface of the projectile core. If the core is made of hard metal, the projectile tip is not deformed in the weapon even if it is subjected to a considerable load in the weapon reloading mechanism.
  • the geometry of the projectile tip which is particularly important for the precision of the projectile flight, remains completely unchanged from storey to storey, unlike in the case of a full-coat storey. This further reduces the spread due to the bullet.
  • the jacket only extends over approximately 3/4 of the length of the projectile core (claim 4).
  • the shape of a pointed, cylindrical rod is favorable for the projectile core.
  • the projectile tip formed by the projectile core preferably has a larger diameter at its rear end than the shank of the projectile core lying behind it and forms an annular step toward it (claim 5).
  • the jacket sits on the ring step and its outer surface is flush with that of the core tip. This creates a visually and geometrically flawless transition from the jacket to the core. This prevents a thinning of the sheath, which would occur if the sheath continuously changed into a smooth core surface, with resulting strength problems.
  • This ring step also offers the possibility of arranging a guide element, which can be immovably fixed, particularly in the longitudinal direction of the projectile, when the shaft of the projectile core is tapered towards the ring step (claim 6). Then the projectile core forms a ring notch, so to speak, in which a guide element can engage in a form-fitting manner.
  • the rear end portion of the shaft is preferably stepped and has a smaller diameter than the main part of the shaft (claim 7).
  • a driving mirror-like guide element which engages behind the projectile core in a form-fitting manner and can therefore apply driving forces for the projectile core.
  • the guide elements mentioned can be formed independently of the jacket. However, the storey core is preferred undercut by the jacket itself on the ring step and on the rear step (claim 8). The coat can not slide off the bullet core.
  • a material is particularly expedient for the projectile core, which gives it a density of approximately 14 kg / dm 3 (sintered hard metal) to approximately 19 kg / dm 3 (tungsten) (claim 9).
  • the hardness of the metal is less important, but rather both hard and soft heavy metal is suitable.
  • toxic materials such as uranium alloys and strongly oxidizing materials can only be used if it is possible to apply a thin and permanent protective coating to the core, such as a galvanic coating.
  • the core and sheath can be made from a variety of suitable materials, depending on the intended use of the projectile according to the invention.
  • Tombac is particularly suitable for the jacket (claim 10).
  • the invention relates not only to a core projectile, but also to a method for its production, which is characterized by the production of a projectile core blank, in which the shaft and the foremost end of the tip are manufactured to final dimensions, preferably ground, and the remaining part of the tip is made with oversize; by producing the jacket blank and applying it to the shank of the projectile core blank, the jacket blank being oversized in diameter and interlocking in the ring step and, if appropriate, in the rear shoulder; and by picking up the blank thus produced between Pointing and creating the final floor contour.
  • the finished outer contour is thus achieved by clamping the projectile core and turning. It is thereby achieved that the axis of rotation of the finished projectile coincides exactly with the clamping axis of the projectile core, and that the projectile contour can be produced with virtually any precision.
  • the projectile core blank can be produced, for example, by all common manufacturing processes. It is particularly advantageous, however, that for the manufacture of the projectile core blank, a blank is provided on the front with a centering tip and on the rear side with a centering hole and is then received and processed between centers (claim 12).
  • the projectile core thus has an axis of rotation which coincides with its clamping axis and - due to the method according to the invention - also with the longitudinal axis of the finished projectile axis.
  • the jacket blank can be manufactured separately from the projectile core or can be produced by application to the projectile core.
  • the separately manufactured jacket blank is preferably pushed onto the shank of the projectile core blank and there is plastically deformed radially inwards (claim 13).
  • the material of the later sheath is applied to the shank of the projectile core blank in composite casting, by spraying, sintering, casting, vapor deposition, galvanic application or the like until the excess is reached (claim 14).
  • the shell blank as a whole and the projectile core blank in the area of the exposed projectile tip are manufactured with oversize and finally removed together concentrically to the final dimension, so that not only for a particularly high dimensional accuracy, but also for a completely smooth and paragraph-free transition between the projectile tip and Coat is taken care of.
  • the projectile shown consisting of a core 2 and a jacket 1, is designed as a relatively long mezzanine with a conical rear and set up for firing from a barrel provided with swirl.
  • the finished bullet (Fig. 1 and the solid outline in Fig. 2 and Fig. 3) has a bullet tip 3, the length of which forms part of the total length of the bullet; further a projectile body and a projectile tail 9, which together take up a further part of the projectile length and are penetrated in the middle by a projectile core shaft 4.
  • the projectile core shaft 4 is substantially cylindrical and has an outer diameter which is smaller, e.g. 2/3 than the largest outside diameter of the bullet.
  • the shaft 4 is surrounded by the jacket 1, the outer contour of which continues continuously in the outer contour of the projectile tip 3.
  • the jacket 1 can be smooth on the outside or have punctures (floating), one of which can be seen in FIGS. 1 and 2 and is delimited by the front and rear guide zones 11.
  • the shaft 4 ends via a shoulder 6 in a rear section 4a, the diameter of which is smaller than that of the shaft 4 and is, for example, 2/3 of the shaft diameter.
  • the shaft 4 ends in a conically tapered section 4b which opens into the tip 3 in one piece.
  • the maximum diameter of the tip 3 is considerably larger in this area than that of the shaft 4, so that the rear end of the tip 3 projects beyond the shaft 4 and forms an annular step 5.
  • the end surface of the tip 3 facing the tapered shaft section 4b forms a very flat conical surface.
  • the angle between the contour of the conically tapered shaft section 4b and the adjacent flat conical surface of the tip 3 is preferably approximately 90 °.
  • the jacket 1 lies closely against the outer surface of the shaft 4 and thus engages positively both in the tapered shaft section 4b behind the ring step 5 and in the rear shaft section 4a.
  • the rear floor surface 12 of the projectile forms a flat, round transom, the ring-shaped outer area of which is formed by the casing 1 and the inner area of which is formed by the shaft 4 of the core 2.
  • a center hole 10 is located in the middle of the inner region.
  • the core 2 is formed at the foremost end of the tip 3 as a pointed nose cone.
  • a core blank 7 is first produced with the contour of the tip 3 shown in dash-dotted lines, the shaft 4 with the ring step 5, its tapered section 4b, the shoulder 6 and its rear section 4a being produced to final dimensions.
  • the nose cone in the core blank 7 extended towards the rear and merges into a cylindrical section, the outside diameter of which is larger than the largest outside diameter of the core 2 after completion.
  • the outwardly enlarged ring step 5 ends this cylindrical section.
  • the end face of the core blank 7 is provided with the center hole 10.
  • the nose cone and the centering bore 10 are first formed thereon, then the round material is picked up between them and further processed.
  • a jacket blank 8 is formed into a tubular sleeve, which is pushed onto the shaft and pressed there so that the material of the jacket blank 8 (dash-double-dotted contour) around the paragraph 6 in the taper at the ring step 5, against this, as well as against the entire length of the outside of the shaft.
  • the projectile blank thus formed is again received between the centering bore 10 and the nose cone and machined along an outer surface in such a way that the solid contour line is reached, a constant transition between tip 3 and jacket 1 being produced. If necessary, the bottom surface 12 is also reworked.
  • the projectile core 4 of the embodiment shown in FIG. 2 forms a shoulder 6 on the mirror side, this is missing in the projectile core 4 of the embodiment shown in FIG. 3.
  • the cylindrical floor core 4 extends continuously without any step to the floor mirror or floor (floor surface 12).

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)
  • Soft Magnetic Materials (AREA)
  • Developing Agents For Electrophotography (AREA)
  • Optical Fibers, Optical Fiber Cores, And Optical Fiber Bundles (AREA)
  • Inks, Pencil-Leads, Or Crayons (AREA)
EP97100478A 1996-02-05 1997-01-14 Procédé de fabrication d'un projectile à noyau et à chemise Expired - Lifetime EP0787969B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19604061A DE19604061C2 (de) 1996-02-05 1996-02-05 Geschoß
DE19604061 1996-02-05

Publications (2)

Publication Number Publication Date
EP0787969A1 true EP0787969A1 (fr) 1997-08-06
EP0787969B1 EP0787969B1 (fr) 1999-05-26

Family

ID=7784517

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97100478A Expired - Lifetime EP0787969B1 (fr) 1996-02-05 1997-01-14 Procédé de fabrication d'un projectile à noyau et à chemise

Country Status (7)

Country Link
US (1) US5794320A (fr)
EP (1) EP0787969B1 (fr)
KR (1) KR970062648A (fr)
AT (1) ATE180564T1 (fr)
DE (2) DE19604061C2 (fr)
DK (1) DK0787969T3 (fr)
ES (1) ES2132976T3 (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6186072B1 (en) 1999-02-22 2001-02-13 Sandia Corporation Monolithic ballasted penetrator
US6363856B1 (en) 1999-06-08 2002-04-02 Roscoe R. Stoker, Jr. Projectile for a small arms cartridge and method for making same
US6279214B1 (en) 1999-07-14 2001-08-28 Alliant Techsystems Inc. Moisture seal for composite sabot with depleted uranium penetrator
US7311046B2 (en) * 2001-04-19 2007-12-25 Ruag Ammotec Gmbh Bullet for infantry ammunition
DE10257590B4 (de) * 2002-12-09 2005-03-24 Wilhelm Brenneke Gmbh & Co. Kg Büchsengeschoss für Jagdzwecke
DE10305721A1 (de) * 2003-02-12 2004-09-02 Rheinmetall W & M Gmbh Verfahren zur Herstellung eines Mantelpenetrators
FR2865272A1 (fr) * 2004-01-20 2005-07-22 Serge Ladriere Dispositif pour projectile a energie embarquee
US20050183617A1 (en) * 2004-02-23 2005-08-25 Macdougall John Jacketed ammunition
US7451705B2 (en) * 2004-03-17 2008-11-18 Fry Grant R Non-discarding sabot projectile system
DE102004036148A1 (de) * 2004-07-24 2006-02-16 Ruag Ammotec Gmbh Hartkerngeschoss mit Penetrator
US8707868B2 (en) * 2006-11-30 2014-04-29 The United States Of America As Represented By The Secretary Of The Navy Pre-compressed penetrator element for projectile
US8028626B2 (en) 2010-01-06 2011-10-04 Ervin Industries, Inc. Frangible, ceramic-metal composite objects and methods of making the same
CA2786331C (fr) 2010-01-06 2018-05-01 Ervin Industries, Inc. Objets composites ceramique-metal cassables et leurs procedes de fabrication
US8783187B2 (en) 2010-02-09 2014-07-22 Amick Family Revocable Living Trust Firearm projectiles and cartridges and methods of manufacturing the same
US8567297B2 (en) 2010-09-21 2013-10-29 Adf, Llc Penetrator and method of manufacture same
USD813974S1 (en) 2015-11-06 2018-03-27 Vista Outdoor Operations Llc Cartridge with an enhanced ball round
US10551154B2 (en) 2017-01-20 2020-02-04 Vista Outdoor Operations Llc Rifle cartridge with improved bullet upset and separation
DE102017106526A1 (de) * 2017-03-27 2018-10-11 Rheinmetall Waffe Munition Gmbh Geschoss, insbesondere im Mittelkaliberbereich
USD848569S1 (en) 2018-01-20 2019-05-14 Vista Outdoor Operations Llc Rifle cartridge

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE205734C (fr)
FR336272A (fr) * 1903-10-27 1904-03-04 Krupp Ag Procédé de fabrication de projectiles en acier avec chemise et de petit calibre
FR496867A (fr) * 1918-09-24 1919-11-19 Fernand Louis Roux Projectile
US1767308A (en) * 1929-11-27 1930-06-24 John T Phillips Bullet
FR800016A (fr) * 1935-04-02 1936-06-25 Projectile de guerre
US2303449A (en) * 1939-11-21 1942-12-01 Copperweld Steel Co Jacketed bullet
CH318865A (de) * 1953-07-02 1957-01-31 Inst Nacional De Ind Infanteriegeschoss
US3599573A (en) * 1968-05-31 1971-08-17 Whittaker Corp Composite preformed penetrators
US3720170A (en) * 1970-10-12 1973-03-13 W Godfrey Heavy small arms projectile
DE2525230A1 (de) * 1975-06-06 1976-12-23 Dynamit Nobel Ag Verfahren zum herstellen von mantelgeschossen
US4387492A (en) * 1980-10-02 1983-06-14 Omark Industries, Inc. Plated jacket soft point bullet
GB1605224A (en) * 1972-07-12 1984-10-31 Rheinmetall Gmbh Armour piercing projectiles
EP0279732A1 (fr) * 1987-02-11 1988-08-24 Societe Francaise De Munitions (S.F.M.) Projectile perforant à noyau dur et guide ductile et son procédé de fabrication
GB2244119A (en) * 1990-05-18 1991-11-20 Rheinmetall Gmbh Jacketed penetrators

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1072515B (fr) *
DE211778C (fr) *
US388496A (en) * 1888-08-28 Francis p
US622582A (en) * 1899-04-04 Bullet or projectile
US36449A (en) * 1862-09-16 Improvement in the
US182278A (en) * 1876-09-19 Improvement in projectiles for rifled ordnance
CH754A (fr) * 1889-04-24 1889-07-05 Perrin P H Balle Compound
US644361A (en) * 1899-06-27 1900-02-27 Jacques Luciani Projectile.
US776056A (en) * 1903-12-17 1904-11-29 Krupp Ag Process of producing small-caliber jacketed steel projectiles.
US932014A (en) * 1907-12-14 1909-08-24 Krupp Ag Projectile.
DE1017493B (de) * 1953-07-04 1957-10-10 Inst Nac De Ind Und Guenther V Langgeschoss fuer Handfeuerwaffen
US4256039A (en) * 1979-01-02 1981-03-17 Allied Chemical Corporation Armor-piercing projectile
GB2052693A (en) * 1979-06-26 1981-01-28 Earl H A Pellet for an Air, Gas or Spring Gun
PT77697B (fr) * 1982-11-24 1986-02-12 Ladriere Serge Projectile perfectionne destine a etre decharge par des armes a feu
FR2647201B3 (fr) * 1989-05-19 1991-10-31 Munitions Ste Fse Projectile a gorges profilees
DE4024543C2 (de) * 1990-08-02 1998-10-08 Diehl Stiftung & Co Geschoß

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE205734C (fr)
FR336272A (fr) * 1903-10-27 1904-03-04 Krupp Ag Procédé de fabrication de projectiles en acier avec chemise et de petit calibre
FR496867A (fr) * 1918-09-24 1919-11-19 Fernand Louis Roux Projectile
US1767308A (en) * 1929-11-27 1930-06-24 John T Phillips Bullet
FR800016A (fr) * 1935-04-02 1936-06-25 Projectile de guerre
US2303449A (en) * 1939-11-21 1942-12-01 Copperweld Steel Co Jacketed bullet
CH318865A (de) * 1953-07-02 1957-01-31 Inst Nacional De Ind Infanteriegeschoss
US3599573A (en) * 1968-05-31 1971-08-17 Whittaker Corp Composite preformed penetrators
US3720170A (en) * 1970-10-12 1973-03-13 W Godfrey Heavy small arms projectile
GB1605224A (en) * 1972-07-12 1984-10-31 Rheinmetall Gmbh Armour piercing projectiles
DE2525230A1 (de) * 1975-06-06 1976-12-23 Dynamit Nobel Ag Verfahren zum herstellen von mantelgeschossen
US4387492A (en) * 1980-10-02 1983-06-14 Omark Industries, Inc. Plated jacket soft point bullet
EP0279732A1 (fr) * 1987-02-11 1988-08-24 Societe Francaise De Munitions (S.F.M.) Projectile perforant à noyau dur et guide ductile et son procédé de fabrication
GB2244119A (en) * 1990-05-18 1991-11-20 Rheinmetall Gmbh Jacketed penetrators

Also Published As

Publication number Publication date
ES2132976T3 (es) 1999-08-16
DK0787969T3 (da) 1999-11-08
EP0787969B1 (fr) 1999-05-26
DE19604061A1 (de) 1997-08-07
DE19604061C2 (de) 1998-07-23
US5794320A (en) 1998-08-18
DE59700168D1 (de) 1999-07-01
KR970062648A (ko) 1997-09-12
ATE180564T1 (de) 1999-06-15

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