GB2316471A - Method for the manufacture of a projectile, and a projectile - Google Patents

Method for the manufacture of a projectile, and a projectile Download PDF

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Publication number
GB2316471A
GB2316471A GB9715994A GB9715994A GB2316471A GB 2316471 A GB2316471 A GB 2316471A GB 9715994 A GB9715994 A GB 9715994A GB 9715994 A GB9715994 A GB 9715994A GB 2316471 A GB2316471 A GB 2316471A
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GB
United Kingdom
Prior art keywords
core
projectile
jacket
cavity
nose
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
GB9715994A
Other versions
GB9715994D0 (en
GB2316471B (en
Inventor
Markku Koivumaeki
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.)
LAPUA Oy
Original Assignee
LAPUA Oy
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 LAPUA Oy filed Critical LAPUA Oy
Publication of GB9715994D0 publication Critical patent/GB9715994D0/en
Publication of GB2316471A publication Critical patent/GB2316471A/en
Application granted granted Critical
Publication of GB2316471B publication Critical patent/GB2316471B/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/06Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Forging (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

A projectile comprises a core 2 and a jacket 1 surrounding the core. It is the object of the present invention to provide a solution by which as uniform projectiles as possible may be made rapidly and simply of as few structural parts as possible. In the invention, grip means 12 are arranged on the projectile core 2, and corresponding receiving means eg notches 9 are arranged in the jacket 1. The co-operation of such means 9, 12 eliminates a relative movement between the jacket 1 and the core 2 when the core is arranged within the jacket.

Description

2316471 METHOD FOR THE MANUFACTURE OF A PROJECTILE, AND A PROJECTILE The
present invention relates to a method for the manufacture of a projectile comprising a jacket and a core.
The invention also relates to a projectile manufactured with the method described.
It is previously known to manufacture projectiles, particularly those comprising a hard metal core, e.g. by forming a jacket portion with a nose of a copper mixture or copper coated steel. A core performing the actual penetra tion is provided within the jacket. The projectile core is centred in a cavity pro vided by the jacket such that the nose of the core is pressed against the front portion of the jacket. Thereafter the core is centred in the jacket cavity by a cup made of aluminium or other similar material and disposed at the open rear portion of the jacket. Such solutions are known from e.g. publications SE 116804 and SE 116856. Such a cup serves not only to centre the core but also to fill the empty space left between the jacket and the core.
Another conventional way to make similar so-called armour projec tiles is to arrange the core in a cup-like jacket that is open at the nose of the projectile. Such a solution is known e.g. from publication NO 164131. There after the jacket is usually provided with a separate nose portion that centres the projectile in the jacket and is made e.g. by traction of a copper mixture.
In addition to a rear or front portion arranged in connection with the core, at times separate support rings have to be employed to centre and lock the core immobile in the jacket.
The problem with these prior solutions has, however, been that centring the projectile core is extremely difficult and laborious, and can even occasionally fail.
In addition, making a projectile of three, even four, parts is expen sive and time-consuming. It is difficult to maintain the dimensional accuracy and accurate joining of these various structural parts in order to eliminate bal ancing problems. Dimensional variations in the rear portion, for example, es sentially affect the performance of the projectile upon firing, whereby it is vital to retain a uniform shape. When a projectile is made of a separate jacket cov ering the front portion and a separate rear portion, the rear portion of the pro jectile is often subjected to dimensional variations.
It is an object of the present invention to eliminate prior art draw backs and to provide a novel solution by which as uniform projectiles as pos- 2 sible may be made rapidly and simply of as few structural parts as possible.
This aim is achieved by a method for the manufacture of a projectile conforming with the characteristics disclosed in the claims of the present in vention. More exactly, the method according to the present invention is chiefly characterized in that a cup-like billet is made of metal, whereby a jacket is pro vided by the billet, the jacket comprising a base and an essentially cylindrical wall attached to the base and surrounding a cavity which has a bottom at the end facing the base, and that further, an elongate, essentially cylindrical or polyhedral projectile core is also made of metal, a first end of the core being provided with a tapered nose, and a second end being provided with grip means, and that receiving means for receiving the grip means are arranged in the area of the jacket bottom, and the core is arranged in the jacket cavity from an opening in the billet such that the end comprising the grip means is guided to the receiving means receiving the grip means and thereafter the core nose is encapsulated by the jacket end facing the opening, and the projectile nose end is given the desired shape.
Thus the invention is based on the realization that by arranging in terlinked means in the jacket and the core, any movement between them is eliminated and thus the manufacturing process of the projectile becomes sig nificantly simpler.
In this way a projectile is provided which has the characteristics de fined in the claims of the present invention. More exactly, the projectile ac cording to the present invention is mainly characterized in that the jacket com prises a base and a cylindrical wall attached to the base and surrounding a cavity, whereby the base end of the cavity comprises a bottom with receiving means, the cavity being provided with an elongate cylindrical or polyhedral core, whereby a first end of the core comprises a nose and a second end comprises grip means arranged in the receiving means at the bottom, and the core nose being encapsulated by the nose portion of the projectile.
Significant advantages are achieved with the method for the manu facture of a projectile and the projectile according to the invention. Thus, the projectile according to the invention is made of only two components, i.e. a jacket and a core. This way a projectile with a simple structure is achieved, the manufacture of which is possible to realize by a simple production technique.
Assembling the projectile using required dimensional accuracy is easy. Thus the projectile, particularly its base portion, is very accurately di3 mensioned providing uniform operating characteristics.
The projectile nose according to the invention is easily shaped as desired in order to provide different operating characteristics.
In the following the invention will be described in more detail by means of the attached drawings, in which Figure 1 shows a ready formed cup-like jacket billet, Figure 2 shows the jacket billet after deep drawing of the cylindrical walls, Figure 3 shows how a tool is led into the billet according to Figure 2 for arranging receiving means to the bottom of the cavity, the billet being shown in partial section, Figure 4 shows an arrangement of a core in a ready formed billet according to the invention, Figure 5 shows a side view of an embodiment of a projectile ac cording to the invention with the nose portion finished and the jacket in sec tion, Figure 6 shows a side view of an embodiment of a projectile core according to the invention, and Figure 7 shows a back view of the core according to Figure 6.
Figure 5 shows a preferred embodiment of a projectile according to the invention. The projectile comprises a jacket 1 made of a suitable metal, e.g. a copper mixture, and a core 2 arranged in the jacket and made of e. g.
steel, hard metal or heavy metal.
A projectile conforming with the invention is made according to Fig ures 1 to 4 so that a cup-like billet 3 shown in Figure 1 is made of a suitable metal e.g. by lathe work or by forming. The billet is deep drawn such that an essentially cylindrical wall 4 is provided therein in accordance with Figure 2, the wall surrounding a cavity 6 provided with a bottom 5. One end of the billet comprises a base 7, and an opening 8 opening to the cavity is arranged at the other end.
Receiving means 9, such as notches, are arranged at the billet bottom by introducing a pressing tool 10 into the billet through the opening 8.
By pressing the tool against the cavity bottom, said receiving means are formed therein.
The manufacture of the projectile continues such that a projectile core 2 according to Figures 6 and 7 is arranged in the billet 3 e.g. by pressing.
4 A first end of the core comprises a nose 11 and a second end grip means 12. The grip means are e.g. edges or grooves arranged at the end of the projectile. In a preferred embodiment according to Figure 6 and 7, one end of the core 2 comprises eight planar bevels adapted to serve as grip means. The core end comprising the grip means is first directed into the billet 3 cavity 6, whereby the grip means get in contact with the receiving means 9 at the cavity bottom 5 and lock the core in position thus efficiently preventing turning movements of the core relative to the jacket.
Because of the co-operation between the receiving means 9 and the grip means 12, the core always rotates with the jacket 1 when the projectile, forced by the rifling in the barrel of the gun, starts to rotate around its longitudinal axis. In the projectile of the invention, the location of the core 2 is also extremely accurately dimensioned, whereby projectiles made with this method always have a uniform performance upon firing.
Finally the core nose 11 is encased by the billet 3 opening 8 by a method known per se, and the nose portion 13 of the projectile is given the desired shape in accordance with Figure 5.
This way a simple procedure has provided a projectile with a cylindrical jacket 1 wall 4 with accurate dimensions, a base portion 7 with extremely accurate dimensions, and a core 2 arranged in the jacket immobile relative thereto.
According to another embodiment of the invention, the receiving means 9 to be formed at the billet 3 bottom 5 can also be pressed via the core 2. In this case the projectile core, its end comprising grip means 12, is led to the drawn billet 3. The core is pressed against the billet bottom, the grip means bearing against the surroundings of the bottom 5 and forming grooves and simultaneously locking the core end firmly into the jacket base 7. The billet opening 8 is then closed in the manner described above.
It is to be understood that the above description and the related drawings are only intended to illustrate the present invention. Thus the invention is not restricted solely to the embodiment described above or in the claims, but to those skilled in the art many modifications and variations will be apparent within the scope of the inventive idea disclosed in the attached claims.

Claims (8)

1. Method for the manufacture of a projectile comprising a jacket and a core wherein: - - a cup-like billet is made of metal, whereby a jacket is pro vided by the billet, the jacket comprising a base and an essentially cylindri cal wall attached to the base and surrounding a cavity which has a bottom at the end facing the base, - further, an elongate, essentially cylindrical or polyhedral projectile core is also made of metal, a first end of the core being provided with a tapered nose, and a second end being provided with grip means, - receiving means for receiving the grip means are arranged in the area of the jacket bottom and the core is arranged in the jacket cavity from an opening in the billet such that the end corn prising the grip means is guided to the receiving means receiving the grip means and thereafter the core nose is encapsulated by the jacket end facing the opening, and the projectile nose end is given the desired shape.
2. A method as claimed in claim 1, w h e r e i n t h e receiving means for receiving the grip means are formed by pressing the core to the jacket cavity from its openin g, whereby the end provided with the grip means is guided to the cavity bottom. such that the grim means form the receiving means for receiving the grip means into the area of the bottom.
3. Projectile comprising a core and a surrounding jacket, w h e r e i n t h e jacket comprises a base and a cylin drical wall attached to the base and syrrounding a cavity, whereby the base end of the cavity comprises a bottom with receiving means, the cavity being provided with an elongate cylindrical or polyhedral core, whereby a first end of the core comprises a nose and a second end corn prises grip means arranged in the receiving means at the bottom, and the core nose being encapsulated by the nose portion of the projectile.
4. Projectile as claimed in claim 3, w h e r. e i n t h e grip means comprise planar bevels formed at one end of the core.
5. Projectile as claimed in claim 3 or 4, w h e r e i n the the core is of armour penetrating metal.
6 6. Projectile as claimed in claim 3, 4 or 5, w h e r e i n the cylindrical wall of the jacket - is provided by deep drawing from the cuplike billet.
7. Method for the manufacture of a projectile, substantially as herein described with reference to the accompanying drawings.
8. Projectile substantially as herein described with reference to the accompanying drawings.
GB9715994A 1996-08-14 1997-07-29 Method for the manuacture of a projectile,and a projectile Expired - Lifetime GB2316471B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FI963189A FI100917B (en) 1996-08-14 1996-08-14 Procedure for the manufacture of a ball and a ball

Publications (3)

Publication Number Publication Date
GB9715994D0 GB9715994D0 (en) 1997-10-01
GB2316471A true GB2316471A (en) 1998-02-25
GB2316471B GB2316471B (en) 2000-08-02

Family

ID=8546489

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9715994A Expired - Lifetime GB2316471B (en) 1996-08-14 1997-07-29 Method for the manuacture of a projectile,and a projectile

Country Status (4)

Country Link
DE (1) DE19730968B4 (en)
FI (1) FI100917B (en)
GB (1) GB2316471B (en)
SE (1) SE518433C2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000068636A1 (en) * 1999-05-06 2000-11-16 Gosudarstvennoe Unitarnoe Predpriyatie Konstruktorskoe Bjuro Priborostroeniya Armour-piercing bullet
EP1718921A1 (en) * 2004-02-23 2006-11-08 SNC Technologies Inc. Jacketed one-piece core ammunition
CN114207376A (en) * 2019-08-05 2022-03-18 卢阿格现代科技股份有限公司 Projectile, method of manufacturing projectile, die for manufacturing projectile and method of rotationally fixing core of projectile relative to sheath of projectile

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2821151B1 (en) * 2001-02-16 2004-05-28 Manurhin Defense PERFORATING PROJECTILE FOR A SMALL OR MEDIUM CALIBER AMMUNITION AND METHOD FOR MOUNTING SUCH A PERFORATING PROJECTILE
DE102017112889A1 (en) * 2017-06-12 2018-12-13 Rheinmetall Waffe Munition Gmbh Kleinkalibergschoss and small caliber ammunition with such a small caliber bullet
LV15696B (en) * 2021-06-04 2023-03-20 Baltic Bullets, Sia An armour piercing bullet

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB520366A (en) * 1939-02-22 1940-04-22 Graviner Manufacturing Co Improved means for stoppering and opening fluid containers or vessels
US3795196A (en) * 1972-12-27 1974-03-05 Mauser Werke Ag Projectile with a loose hard core
US4336756A (en) * 1978-08-16 1982-06-29 Hornady Manufacturing Company Jacketed bullet and method of manufacture
US5038684A (en) * 1990-06-18 1991-08-13 Petrovich Paul A Jacketed projectile for ammunition
US5069139A (en) * 1987-10-05 1991-12-03 Denis Jean Pierre Projectile intended to be fired by a fire-arm

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB520346A (en) * 1938-10-18 1940-04-22 Chester Tietig Projectile
BE542649A (en) * 1954-12-13
GB2123123A (en) * 1982-07-01 1984-01-25 Honeywell Inc Projectiles
WO1987007708A1 (en) * 1986-06-09 1987-12-17 Royal Ordnance Pld Armour piercing projectile
FR2610715A1 (en) * 1987-02-11 1988-08-12 Munitions Ste Fse PERFORATING PROJECTILE WITH HARD CORE AND DUCTILE GUIDE

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB520366A (en) * 1939-02-22 1940-04-22 Graviner Manufacturing Co Improved means for stoppering and opening fluid containers or vessels
US3795196A (en) * 1972-12-27 1974-03-05 Mauser Werke Ag Projectile with a loose hard core
US4336756A (en) * 1978-08-16 1982-06-29 Hornady Manufacturing Company Jacketed bullet and method of manufacture
US5069139A (en) * 1987-10-05 1991-12-03 Denis Jean Pierre Projectile intended to be fired by a fire-arm
US5038684A (en) * 1990-06-18 1991-08-13 Petrovich Paul A Jacketed projectile for ammunition

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000068636A1 (en) * 1999-05-06 2000-11-16 Gosudarstvennoe Unitarnoe Predpriyatie Konstruktorskoe Bjuro Priborostroeniya Armour-piercing bullet
EP1718921A1 (en) * 2004-02-23 2006-11-08 SNC Technologies Inc. Jacketed one-piece core ammunition
EP1718921A4 (en) * 2004-02-23 2010-10-20 Gen Dynamics Ordnance & Tactic Jacketed one-piece core ammunition
US7980180B2 (en) 2004-02-23 2011-07-19 General Dynamics Ordnance And Tactical Systems-Canada Inc. Jacketed one piece core ammunition
NO338077B1 (en) * 2004-02-23 2016-07-25 Gen Dynamics Ordnance & Tactic Uniformly sheathed nuclear ammunition
CN114207376A (en) * 2019-08-05 2022-03-18 卢阿格现代科技股份有限公司 Projectile, method of manufacturing projectile, die for manufacturing projectile and method of rotationally fixing core of projectile relative to sheath of projectile

Also Published As

Publication number Publication date
FI100917B (en) 1998-03-13
DE19730968A1 (en) 1998-02-19
SE518433C2 (en) 2002-10-08
FI963189A0 (en) 1996-08-14
GB9715994D0 (en) 1997-10-01
DE19730968B4 (en) 2013-09-05
SE9702868D0 (en) 1997-08-06
GB2316471B (en) 2000-08-02
SE9702868L (en) 1998-02-15

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Date Code Title Description
PE20 Patent expired after termination of 20 years

Expiry date: 20170728