EP1766322B1 - Hard core jacketed bullet comprising an illuminant composition, and method for the production thereof - Google Patents
Hard core jacketed bullet comprising an illuminant composition, and method for the production thereof Download PDFInfo
- Publication number
- EP1766322B1 EP1766322B1 EP05758705A EP05758705A EP1766322B1 EP 1766322 B1 EP1766322 B1 EP 1766322B1 EP 05758705 A EP05758705 A EP 05758705A EP 05758705 A EP05758705 A EP 05758705A EP 1766322 B1 EP1766322 B1 EP 1766322B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bore
- core
- jacket
- opening
- hard
- 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
Links
- 238000000034 method Methods 0.000 title claims abstract description 7
- 238000004519 manufacturing process Methods 0.000 title claims description 5
- 239000000463 material Substances 0.000 claims abstract description 16
- 239000000700 radioactive tracer Substances 0.000 claims description 6
- 238000003825 pressing Methods 0.000 abstract description 2
- 239000007789 gas Substances 0.000 description 11
- 239000011257 shell material Substances 0.000 description 10
- 239000011258 core-shell material Substances 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000002689 soil Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
Images
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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
Definitions
- the invention relates to a hard core shell projectile with flare and a method for its preparation.
- Tracer bullets are bullets that contain a set of flares that is ignited on launch, allowing it to track the trajectory of the projectiles due to its burnup. Especially during nighttime shooting, tracer bullets make it easier to track the target and sight.
- the flare is located in a arranged in the longitudinal axis of the projectile bore in the projectile core. If the projectile is a mantle projectile, the mantle in the rear of the projectile must be open in the area of the opening of the bore. In this case, the opening must be designed so that the resulting gas during combustion of the flare gas can not get between the shell and core and ruptured by the resulting gas pressure of the mantle or even separated from the core. Damage to the mantle or gas slippage negatively affect the trajectory of the projectile and lead to misses.
- the object of the present invention is to ensure a gastight seal between the shell and the core in the case of a hard core shell projectile with flare in the region of the opening of the hole for the flare.
- the object is achieved according to the invention in that after pulling the shell on the core of the jacket in the rear of the projectile, the bottom of the shell, in the center of the opening of the hole for the flare is pierced by means of a provided with a conical tip punch and when immersing of the punch in the bore of the shell material is pressed uniformly against the wall of the hole. The jacket is therefore not just bent over the edge of the hole.
- the process is similar to reshaping.
- the material of the lying in the rear of the sleeve Soil, which is thicker than the mantle, is pushed into the bore by means of the punch, so that the drawing or forming process begins and the strength of the extending into the bore bottom significantly reduced, the opening to the bore is formed.
- the diameter of the punch for the production of the opening is adapted to the wall thickness, which must have the pressed against the wall of the bore material of the shell to withstand the expected gas pressure and not be infiltrated by the gas.
- the wall thickness of the pressed against the wall of the bore material is between 0.1 mm and 1.5 mm, depending on the occurring gas pressure, which may be about 3500 bar to 4000 bar.
- the hard core shell 1 comprises a core 2, which is enclosed in its cylindrical, the leadership of the projectile in the barrel serving part 3 of a jacket 4.
- a flare 7 which is preceded by an ignition charge 9 in the direction of the rear 8 of the projectile 1.
- the opening 10 to the bore 6 in the bottom 11 of the shell 4 is closed by a cover 12.
- the bore 6 is stepped.
- the area 13 of the bore 6 in the rear 8 of the hard core, in which the material of the bottom 11 is pressed in, has a diameter 14 which is widened by approximately the wall thickness of the displaced material 15.
- the opening 10 has the same diameter 16 as the bore 6, whereby the pressing of the flare 7 and the ignition charge 9 is facilitated.
- the hard core shell projectile with flare invention is easy to produce.
- the tightness between the shell and core in the opening to the hole for the flare is achieved without soldering, solely by the interference fit of the displaced to the wall of the bore material of the soil during the piercing of the hole in the ground by means of a similar processing forming step.
- the method of making the opening in the bottom of the shell shell is applicable to all calibers.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Adornments (AREA)
- Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
- Stringed Musical Instruments (AREA)
- Gasket Seals (AREA)
- Polymerisation Methods In General (AREA)
- Insulated Conductors (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
Description
Die Erfindung betrifft ein Hartkern-Mantelgeschoss mit Leuchtsatz und ein Verfahren zu seiner Herstellung.The invention relates to a hard core shell projectile with flare and a method for its preparation.
Leuchtspurgeschosse sind Geschosse, die einen Leuchtsatz enthalten, der beim Abschuss gezündet wird und aufgrund seines Abbrands ermöglicht, die Flugbahn der Geschosse zu verfolgen. Insbesondere beim nächtlichen Schießen erleichtern Leuchtspurgeschosse das Erfassen des Ziels und das Anvisieren.Tracer bullets are bullets that contain a set of flares that is ignited on launch, allowing it to track the trajectory of the projectiles due to its burnup. Especially during nighttime shooting, tracer bullets make it easier to track the target and sight.
Der Leuchtsatz befindet sich in einer in der Längsachse des Geschosses angeordneten Bohrung im Geschosskern. Ist das Geschoss ein Mantelgeschoss, muss der Mantel im Heckbereich des Geschosses im Bereich der Öffnung der Bohrung offen sein. Dabei muss die Öffnung so gestaltet sein, dass das beim Abbrand des Leuchtsatzes entstehende Gas nicht zwischen Mantel und Kern gelangen kann und durch den entstehenden Gasdruck der Mantel aufreißt oder gar vom Kern getrennt wird. Eine Beschädigung des Mantels oder ein Gasschlupf beeinflussen die Flugbahn des Geschosses negativ und führen zu Fehlschüssen.The flare is located in a arranged in the longitudinal axis of the projectile bore in the projectile core. If the projectile is a mantle projectile, the mantle in the rear of the projectile must be open in the area of the opening of the bore. In this case, the opening must be designed so that the resulting gas during combustion of the flare gas can not get between the shell and core and ruptured by the resulting gas pressure of the mantle or even separated from the core. Damage to the mantle or gas slippage negatively affect the trajectory of the projectile and lead to misses.
Aus der österreichischen Patentschrift
Aufgabe der vorliegenden Erfindung ist es, bei einem Hartkern-Mantelgeschoss mit Leuchtsatz im Bereich der Öffnung der Bohrung für den Leuchtsatz einen gasdichten Abschluss zwischen dem Mantel und dem Kern zu gewährleisten.The object of the present invention is to ensure a gastight seal between the shell and the core in the case of a hard core shell projectile with flare in the region of the opening of the hole for the flare.
Die Lösung der Aufgabe erfolgt erfindungsgemäß dadurch, dass nach Aufziehen des Mantels auf den Kern der Mantel im Heckbereich des Geschosses, der Boden des Mantels, im Mittelpunkt der Öffnung der Bohrung für den Leuchtsatz mittels eines mit einer kegelförmigen Spitze versehenen Stempels angestochen wird und beim Eintauchen des Stempels in die Bohrung der Mantelwerkstoff gleichmäßig gegen die Wand der Bohrung gepresst wird. Der Mantel wird also nicht nur über die Kante der Bohrung umgebogen. Der Vorgang ist dem Umformen vergleichbar. Der Werkstoff des im Heckbereich der Hülse liegenden Bodens, der dicker ist als der Mantel, wird mittels des Stempels in die Bohrung hineingeschoben, so dass der Zieh- oder Umformvorgang beginnt und sich die Stärke des in die Bohrung hineinreichenden Bodens wesentlich verringert, wobei die Öffnung zur Bohrung entsteht. Die Dichtigkeit gegen die Gase erfolgt bereits, wenn der Werkstoff auf etwa einem Millimeter Länge an die Wandung der Bohrung hineingedrückt worden ist. Selbst beim exzentrischen Einreissen des Mantels ist die Dichtigkeit noch gewährleistet und führt zu keinem Gasschlupf. Es ist an der Öffnung kein Verlöten des Mantels mit dem Kern erforderlich.The object is achieved according to the invention in that after pulling the shell on the core of the jacket in the rear of the projectile, the bottom of the shell, in the center of the opening of the hole for the flare is pierced by means of a provided with a conical tip punch and when immersing of the punch in the bore of the shell material is pressed uniformly against the wall of the hole. The jacket is therefore not just bent over the edge of the hole. The process is similar to reshaping. The material of the lying in the rear of the sleeve Soil, which is thicker than the mantle, is pushed into the bore by means of the punch, so that the drawing or forming process begins and the strength of the extending into the bore bottom significantly reduced, the opening to the bore is formed. The seal against the gases already takes place when the material has been pressed to about one millimeter in length to the wall of the bore. Even with the eccentric tearing of the shell, the tightness is still guaranteed and does not lead to gas slippage. It is not necessary to solder the jacket to the core at the opening.
Der Durchmesser des Stempels zur Herstellung der Öffnung ist auf die Wandstärke abgestimmt, die der an die Wand der Bohrung gepresste Werkstoff des Mantels aufweisen muss, um den zu erwartenden Gasdruck standzuhalten und nicht vom Gas unterwandert zu werden. Die Wandstärke des an die Wand der Bohrung gepressten Werkstoffs liegt zwischen 0,1 mm und 1,5 mm, in Abhängigkeit von dem auftretenden Gasdruck, der etwa 3500 bar bis 4000 bar betragen kann.The diameter of the punch for the production of the opening is adapted to the wall thickness, which must have the pressed against the wall of the bore material of the shell to withstand the expected gas pressure and not be infiltrated by the gas. The wall thickness of the pressed against the wall of the bore material is between 0.1 mm and 1.5 mm, depending on the occurring gas pressure, which may be about 3500 bar to 4000 bar.
Anhand eines figürlich dargestellten Ausführungsbeispiels wird die Erfindung erläutert und ihre Vorteile gegenüber dem Stand der Technik dargelegt.Reference to a figuratively illustrated embodiment, the invention will be explained and set forth its advantages over the prior art.
Das Hartkern-Mantelgeschoss 1 umfasst einen Kern 2, der in seinem zylindrischen, der Führung des Geschosses im Lauf dienenden Teil 3 von einem Mantel 4 umschlossen ist. In einer zentrisch zur Geschossachse 5 verlaufenden Bohrung 6 befindet sich ein Leuchtsatz 7, dem in Richtung zum Heck 8 des Geschosses 1 ein Anzündsatz 9 vorgelagert ist. Die Öffnung 10 zur Bohrung 6 im Boden 11 des Mantels 4 wird durch eine Deckel 12 verschlossen.The hard core shell 1 comprises a
Wie aus der Figur ersichtlich, ist die Bohrung 6 abgestuft. Der Bereich 13 der Bohrung 6 im Heck 8 des Hartkerns, in den der Werkstoff des Bodens 11 hineingepresst wird, hat einen Durchmesser 14 der jeweils um etwa die Wandstärke des verdrängten Werkstoffs 15 erweitert ist. Dadurch hat die Öffnung 10 den gleichen Durchmesser 16 wie die Bohrung 6, wodurch das Einpressen des Leuchtsatzes 7 und des Anzündsatzes 9 erleichtert wird.As can be seen from the figure, the
Außerdem wird verhindert, dass die Ränder des in den Bereich 13 verdrängten Mantelwerkstoffs 15 eine Angriffsfläche für die Gase bilden, die beim Abbrand der pyrotechnischen Ladungen 7 und 9 entstehen.In addition, it is prevented that the edges of the displaced in the
Weiterhin hat das Heck 17 des Hartkems 2 innen und außen abgerundete Ränder 18 im Bereich der Öffnung 10. Dadurch wird verhindert, dass bei der Bildung der Öffnung 10 im Boden 13 des Mantels 4 der durch den Umformvorgang über den inneren Rand 18 fließende Werkstoff abreißt.Furthermore, the rear 17 of the
Das erfindungsgemäße Hartkern-Mantelgeschoss mit Leuchtsatz ist einfach herzustellen. Die Dichtigkeit zwischen Mantel und Kern im Bereich der Öffnung zur Bohrung für den Leuchtsatz wird ohne Löten erreicht, allein durch den Presssitz des an die Wand der Bohrung verdrängten Werkstoff des Bodens beim Einstechen des Lochs in den Boden mittels eines dem Umformen vergleichbaren Bearbeitungsschritts.The hard core shell projectile with flare invention is easy to produce. The tightness between the shell and core in the opening to the hole for the flare is achieved without soldering, solely by the interference fit of the displaced to the wall of the bore material of the soil during the piercing of the hole in the ground by means of a similar processing forming step.
Das Verfahren zur Herstellung der Öffnung in dem Boden des Geschossmantels ist für alle Kaliber anwendbar.The method of making the opening in the bottom of the shell shell is applicable to all calibers.
Claims (7)
- A hard-core jacketed bullet having a tracer composition that is loaded into a bore of the core, characterized in that in the region of the opening (10) to the bore (6) in the hard core (2) for receiving the tracer composition (7) the material (15) of the base (11) that is displaced into the bore (6) during the creation of the opening (10) in the base (11) of the jacket (4) by forming is pressed against the wall of the bore, simultaneously reducing the wall thickness of the base (11).
- A hard-core jacketed bullet according to claim 1, characterized in that the bore (6) in the region of the opening (10) has a widened region (13) for receiving the material (15) of the base (11) of the jacket (4) that is displaced during the production of the opening (10).
- A hard-core jacketed bullet according to claim 2, characterized in that the diameter (15) of the widened region (13) is greater by twice the wall thickness of the displaced material (15) of the jacket (4) than the diameter (16) of the bore (6).
- A hard-core jacketed bullet according to one of claims 1 to 3, characterized in that the wall thickness of the displaced material (15) is between 0.1 mm and 1.5 mm depending on the gas pressure that occurs.
- A hard-core jacketed bullet according to one of claims 1 to 4, characterized in that the diameter of the bore (6) and the diameter in the region of the opening (10) are of equal size.
- A method of manufacturing a hard-core jacketed bullet having a tracer composition that is loaded into a bore of the core according to one of claims 1 to 5, characterized in that after mounting of the jacket onto the core the jacket in the rear region of the bullet, the base of the jacket, is broached in the centre of the opening of the bore for the tracer composition by means of a punch provided with a conical tip and that during engagement of the punch into the bore the jacket material is displaced by means of an operation comparable to forming and is pressed uniformly against the wall of the bore, simultaneously reducing the wall thickness of the base.
- A method according to claim 6, characterized in that it is usable for all calibres.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004033017A DE102004033017A1 (en) | 2004-07-08 | 2004-07-08 | Hard core shell with flare and process for its production |
PCT/EP2005/006941 WO2006005439A1 (en) | 2004-07-08 | 2005-06-28 | Hard core jacketed bullet comprising an illuminant composition, and method for the production thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1766322A1 EP1766322A1 (en) | 2007-03-28 |
EP1766322B1 true EP1766322B1 (en) | 2009-04-01 |
Family
ID=34975136
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05758705A Active EP1766322B1 (en) | 2004-07-08 | 2005-06-28 | Hard core jacketed bullet comprising an illuminant composition, and method for the production thereof |
Country Status (8)
Country | Link |
---|---|
US (1) | US7661368B2 (en) |
EP (1) | EP1766322B1 (en) |
AT (1) | ATE427474T1 (en) |
DE (2) | DE102004033017A1 (en) |
DK (1) | DK1766322T3 (en) |
ES (1) | ES2325125T3 (en) |
NO (1) | NO338240B1 (en) |
WO (1) | WO2006005439A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004036148A1 (en) * | 2004-07-24 | 2006-02-16 | Ruag Ammotec Gmbh | Hard core bullet with penetrator |
DE102011018475A1 (en) * | 2011-04-21 | 2012-10-25 | Rwm Schweiz Ag | Apparatus and method for airtight covering a tracer or the like |
US9772171B2 (en) * | 2015-03-24 | 2017-09-26 | Patrick C Henry, III | Method of modifying ammunition classification |
SE538646C2 (en) * | 2015-04-01 | 2016-10-11 | Nammo Vanäsverken Ab | Track light projectile and method of applying a track light device to a track light projectile |
US10422613B2 (en) | 2016-12-01 | 2019-09-24 | Battelle Memorial Institute | Illuminants and illumination devices |
BR112019011338A2 (en) | 2016-12-01 | 2019-10-15 | Battelle Memorial Institute | self-shining materials, tracing ammunition and lighting devices |
US10557696B2 (en) | 2016-12-01 | 2020-02-11 | Battelle Memorial Institute | Self-glowing materials and tracer ammunition |
EP3701215B1 (en) * | 2017-10-26 | 2024-04-17 | Spectra Technologies LLC | Explosive ordnance cold assembly process |
WO2020068288A2 (en) * | 2018-08-13 | 2020-04-02 | Ammo Technologies, Inc. | Methods of mass-producing luminescent projectiles and luminescent projectiles mass-produced thereby |
DE102020102159A1 (en) | 2020-01-29 | 2021-07-29 | Ruag Ammotec Gmbh | METHOD AND DEVICE FOR CHECKING THE COMBUSTION OF A LIGHT SET OF A LIGHT PLATE LIGHT, IGNITION UNIT FOR LIGHTING A LIGHT SET OF A LIGHT PLATE AND SYSTEM |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AT84321B (en) * | 1916-12-19 | 1921-06-10 | Chemische Producten Und Zuendk | Marker bullet. |
DE332279C (en) * | 1918-01-12 | 1921-01-28 | Conrad Claessen Dr | Incendiary and tracer bullet with visible trajectory for infantry rifles |
US1432669A (en) * | 1918-11-18 | 1922-10-17 | Wallace L Clay | Armor-piercing and tracer bullet |
FR622797A (en) * | 1926-01-30 | 1927-06-07 | Projectile with visible trajectory | |
US2115047A (en) * | 1936-11-30 | 1938-04-26 | Stevenson Thomas | Tracer ammunition and to an igniter mixture for tracer compositions |
BE498540A (en) * | 1949-10-07 | |||
US2958287A (en) * | 1954-07-16 | 1960-11-01 | Jean L Auxier | Projectile |
US3013495A (en) * | 1959-07-10 | 1961-12-19 | Stevenson Thomas | Spotter-tracer projectile |
US3262390A (en) * | 1964-05-29 | 1966-07-26 | Olin Mathieson | Tracer shotshell |
FR2057590A5 (en) * | 1969-08-29 | 1971-05-21 | France Etat | Disintegratable tracer practice shell for - armoured vehicles |
US5714707A (en) * | 1996-05-13 | 1998-02-03 | Talon Manufacturing Company, Inc. | Process and apparatus for demilitarization of small caliber primed cartridge cases |
-
2004
- 2004-07-08 DE DE102004033017A patent/DE102004033017A1/en not_active Withdrawn
-
2005
- 2005-06-28 ES ES05758705T patent/ES2325125T3/en active Active
- 2005-06-28 AT AT05758705T patent/ATE427474T1/en active
- 2005-06-28 US US11/571,772 patent/US7661368B2/en not_active Expired - Fee Related
- 2005-06-28 DK DK05758705T patent/DK1766322T3/en active
- 2005-06-28 EP EP05758705A patent/EP1766322B1/en active Active
- 2005-06-28 WO PCT/EP2005/006941 patent/WO2006005439A1/en active Application Filing
- 2005-06-28 DE DE502005007004T patent/DE502005007004D1/en active Active
-
2007
- 2007-02-08 NO NO20070740A patent/NO338240B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE502005007004D1 (en) | 2009-05-14 |
EP1766322A1 (en) | 2007-03-28 |
NO338240B1 (en) | 2016-08-08 |
DK1766322T3 (en) | 2009-07-27 |
ATE427474T1 (en) | 2009-04-15 |
US20080196617A1 (en) | 2008-08-21 |
WO2006005439A1 (en) | 2006-01-19 |
DE102004033017A1 (en) | 2006-02-09 |
ES2325125T3 (en) | 2009-08-26 |
NO20070740L (en) | 2007-02-08 |
US7661368B2 (en) | 2010-02-16 |
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