EP0716285B1 - Training projectile for gun barrel - Google Patents

Training projectile for gun barrel Download PDF

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Publication number
EP0716285B1
EP0716285B1 EP95113344A EP95113344A EP0716285B1 EP 0716285 B1 EP0716285 B1 EP 0716285B1 EP 95113344 A EP95113344 A EP 95113344A EP 95113344 A EP95113344 A EP 95113344A EP 0716285 B1 EP0716285 B1 EP 0716285B1
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EP
European Patent Office
Prior art keywords
projectile
training
floor
fact
practice
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.)
Expired - Lifetime
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EP95113344A
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German (de)
French (fr)
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EP0716285A1 (en
Inventor
Gero Wähner
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Mauser Werke Oberndorf Waffensysteme GmbH
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Mauser Werke Oberndorf Waffensysteme GmbH
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Publication of EP0716285A1 publication Critical patent/EP0716285A1/en
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Publication of EP0716285B1 publication Critical patent/EP0716285B1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00Practice or training ammunition
    • F42B8/12Projectiles or missiles
    • F42B8/14Projectiles or missiles disintegrating in flight or upon impact

Definitions

  • the invention relates to a practice projectile for barrel weapons, which is essentially one in shape and mass Standard practice floor or a combat floor, with a bullet hood and a bullet tail with guide band.
  • Shattered bullets are generally known an impact or hitting a target medium disassemble more or less and thereby the danger area reduce.
  • DE 39 02 112 C1 is a disassembly projectile head for practice ammunition revealed in a thin Hood a core is inserted, which one to the top of the floor has facing recess. On this recess there is a ball in the recess so immersed far that the center of the sphere above the top of the recess. In the event of an impact of the cutting head on a target medium the ball is in driven the recess. This is the core split up and disassembled when it bursts open Core surrounding hood.
  • a dismantling projectile head with a different design for practice ammunition is known from DE 36 42 414 Al.
  • a core is made of a pressed one or soaked metal powder in the floor hood introduced in the impact area conical with a flattened tip is formed. If this known Practice projectile hits a target medium, so the bullet hood bursts and the core is covered by the Impact forces almost broken down into powder form. Thereby becomes most of the energy of the practice floor reduced.
  • disassembling the core in particular prevents the practice bullet from the target medium bounces off and possibly people on a practice area injured.
  • cutting heads of the aforementioned It is particularly suitable in the event of an oblique impact not reliably disassemble on a target medium and thereby represent a hazard, as described at the beginning.
  • a training floor for barrel weapons to create which is easy to manufacture and at Impact is broken down into at least two parts and thereby the risk of ricochets and the hazardous area noticeably reduced.
  • disassembly element as a so-called Separating element is it with technically simple and economically viable means possible to reach from rebounding practice projectiles by separation into to drastically reduce at least two parts, thereby practice shooting is also possible on smaller practice areas becomes.
  • the range reduction is essentially through achieved two physical laws. On the one hand put the two remaining parts after separation of the practice floor by ballistic disassembly unfavorable, d. H. with a higher drag coefficient afflicted bodies whose flight speed is different degrades much faster than a whole floor. A new stabilization of such fragments of floors is also unlikely. To the others are the two or more story fragments after disassembling the practice floor easier than the entire floor. This is the floor parts remaining speed very quickly reduced.
  • the practice floor essentially consists of a floor hood 2 and a bullet tail 3, which is the guide band 4 accommodates in an annular groove.
  • the storey hood 2 and the tail 3 are by a disassembly element 5, which is hollow cylindrical and to both Sides of a central area 6 thread approaches 7 and 8 has connected.
  • the threaded approach 7 that is Disassembly element 6 in a corresponding internal thread a blind hole 9 of the projectile hood 2 is screwed in.
  • the tailgate 3 is with an internal thread of the recess 10 screwed onto the threaded attachment 8.
  • the central region 6 of the Disassembly element 5 has the same outer diameter 11 like the hood 2 and the tail 3. This means that the central region 6 of the disassembly element 5 ring-shaped between the facing end faces the floor hood 2 and the rear floor 3 is located.
  • the dismantling element 5 according to FIG. 1 has one in the middle part 6 inner circumferential radial groove 12, which as Radial set point serves, as clearly shown in Figure 2 is highlighted.
  • the disassembly element 5 is made of a high-strength wrought aluminum alloy manufactured which has a lower Temperature dependence of the notch toughness as Steel.
  • the remaining wall thickness 13 of the radial breaking point 12 is dimensioned so that the practice floor in the event of a collision with a target medium disassembled at least two parts. This is also guaranteed if the practice floor 1 in a relative flat impact angle of, for example, 10 ° degrees hits a target medium.
  • FIG. 3 is a disassembling element 14 in a slightly modified Design shown.
  • This disassembling element 14 differs from the disassembly element 5 according to FIG. 2 or according to Figure 1 in that the central region is radial does not protrude beyond the two threaded lugs 7 and 8.
  • the middle area 15, on the inside again a circumferential radial breaking point 12 is introduced is in the outer diameter with the Inner diameter of the blind bore 9 of the projectile hood 2 or with the recess 10 in the tail end.
  • the central region 15 of the disassembly element 14 according to FIGS. 6 and 7 within the floor covering, the radial breaking point 12 directly below the dividing line 16 between the floor hood 2 and the tail 3 is located.
  • the disassembly element 17 according to FIG. 4 has a similar structure as the disassembly element 14 in Figure 3. As the only one The difference is that this dismantling element 17 has an outer circumferential one Radial set point 18.
  • FIG 5 is again a disassembling element 19 in half section shown which the disassembling element from the building 14 corresponds. However, are in the disassembly element 19 now an inner circumferential and an outer circumferential Radial set point 20 or 21 introduced.
  • FIG. 6 again shows a practice floor 22 with a Missile hood 2 and a missile tail 3 with a guide band 4.
  • the projectile hood 2 and the projectile tail 3 are in turn by a disassembly element 23 connected, only the threaded lugs 7 and 8 have different diameters.
  • the radial breaking point 12 is located directly below the parting line 16 between the hood 2 and the tail 3.
  • In the front area of exercise floor 2 are located one or more compacts 24, 25 and 26 made of an iron powder.
  • the exercise floor 22 according to FIG. 7 is again with a Disassembly element 23 provided as the only difference 6 are in this case according to FIG. 7 between the disassembling element 23 and the pressing body 24 spherical shaped bodies 27 and 28 of different Diameters used.
  • a Disassembly element 23 provided as the only difference 6 are in this case according to FIG. 7 between the disassembling element 23 and the pressing body 24 spherical shaped bodies 27 and 28 of different Diameters used.
  • Through the use of compacts 24, 25 and 26 and shaped bodies 27 and 28 is the Disassembly of practice levels 1 and 22 further optimized.
  • Ballistic-optimized storey hood 2 in several uncritical ones Parts disassembled on target impact.
  • For the tailgate 3 remains only a relative lighter, ballistically unfavorable cylinder-like flying Residual body.
  • the disassembly element serves 23 not just connecting and disconnecting Bullet hood 2 and tailgate 3, but allowed at the same time also a backlash free and to the tailgate 3 fixation of packing elements independent of length tolerance 24, 25, 26, 27 and 28 in the floor hood 2.
  • One construction 6 or 7 is technically more complex than that Construction of practice level 1 according to Figure 1. Here it is left to the specialist, taking into account the right demands on him Construction variant for a practice floor 1 or 22 to choose which one at least in the event of a target impact disassembled two parts.

Description

Die Erfindung betrifft ein Übungsgeschoß für Rohrwaffen, welches in Form und Masse im wesentlichen einem Standard-Übungsgeschoß bzw. einem Kampfgeschoß entspricht, mit einer Geschoßhaube und einem Geschoßheck mit Führungsband.The invention relates to a practice projectile for barrel weapons, which is essentially one in shape and mass Standard practice floor or a combat floor, with a bullet hood and a bullet tail with guide band.

Das Übungsschießen mit Rohrwaffen von bodengebundenen oder luftgestützten Waffensystemen ist durch die zur Verfügung stehende Schießanlage und den für die jeweilige Munition gültigen Gefahrenbereich begrenzt. Es ist bekannt, daß sich vom Boden abprallende Geschosse nach kurzer Zeit wieder stabilisieren können und danach in undefinierter Richtung weiter fliegen. Dabei ist es möglich, daß solche wiederstablisierten Geschoßteile auch den zulässigen Gefahrenbereich verlassen.Practice shooting with barrel weapons from ground-based or airborne weapon systems is due to the Available shooting range and the one for the respective Ammunition valid danger zone limited. It is known that bullets bouncing off the floor after can stabilize again for a short time and then in continue flying in an undefined direction. It is possible that such re-established floor parts also leave the permissible danger zone.

Allgemein bekannt sind Zerschellgeschosse, die sich bei einem Aufschlag bzw. dem Auftreffen in einem Zielmedium mehr oder weniger stark zerlegen und dadurch den Gefährdungsbereich verringern. Durch Radial- und Längssollbruchstellen in Verbindung mit Metallpulver- oder anderen Füllkörpern in der Geschoßhaube sind solche Zerschellgeschosse technisch aufwendig und wirtschaftlich ungünstiger herstellbar als herkömmliche Übungsgeschosse.Shattered bullets are generally known an impact or hitting a target medium disassemble more or less and thereby the danger area reduce. Through radial and longitudinal breaking points in connection with metal powder or other fillers in the floor hood are such Shatter projectiles are technically complex and economical less favorable to manufacture than conventional practice projectiles.

Durch die DE 39 02 112 C1 ist ein Zerleger-Geschoßkopf für Übungsmunition offenbart bei dem in einer dünnen Haube ein Kern eingefügt ist, welcher eine zur Geschoßspitze gewandte Ausnehmung aufweist. Auf dieser Ausnehmung liegt eine Kugel auf, die in die Ausnehmung so weit eintaucht, daß der Kugelmittelpunkt oberhalb des oberen Randes der Ausnehmung liegt. Bei einem Aufprall des Zerlegerkopfes auf ein Zielmedium wird die Kugel in die Ausnehmung hineingetrieben. Dadurch wird der Kern aufgespalten und zerlegt beim Aufplatzen auch die den Kern umgebende Haube.DE 39 02 112 C1 is a disassembly projectile head for practice ammunition revealed in a thin Hood a core is inserted, which one to the top of the floor has facing recess. On this recess there is a ball in the recess so immersed far that the center of the sphere above the top of the recess. In the event of an impact of the cutting head on a target medium the ball is in driven the recess. This is the core split up and disassembled when it bursts open Core surrounding hood.

Ein konstruktiv anders aufgebauter Zerleger-Geschoßkopf für Übungsmunition ist aus der DE 36 42 414 Al bekannt. Bei diesem Geschoßkopf ist ein Kern aus einem gepreßten oder gesinderten Metallpulver in die Geschoßhaube eingebracht, die im Aufschlagbereich konisch mit einer abgeplatteten Spitze ausgebildet ist. Wenn dieses bekannte Übungsgeschoß auf ein Zielmedium auftrifft, so platzt die Geschoßhaube und der Kern wird durch die Aufschlagkräfte nahezu in Pulverform zerlegt. Dadurch wird der größte Teil der Energie des Übungsgeschosses abgebaut. Durch die Zerlegung des Kernes wird insbesondere verhindert, daß das Übungsgeschoß vom Zielmedium abprallt und eventuell Personen auf einem Übungsgelände verletzt.A dismantling projectile head with a different design for practice ammunition is known from DE 36 42 414 Al. In this projectile head, a core is made of a pressed one or soaked metal powder in the floor hood introduced in the impact area conical with a flattened tip is formed. If this known Practice projectile hits a target medium, so the bullet hood bursts and the core is covered by the Impact forces almost broken down into powder form. Thereby becomes most of the energy of the practice floor reduced. By disassembling the core, in particular prevents the practice bullet from the target medium bounces off and possibly people on a practice area injured.

Es ist jedoch bekannt, daß Zerlegerköpfe der vorgenannten Bauart sich insbesondere bei einem Schrägaufprall auf ein Zielmedium nicht zuverlässig zerlegen und dadurch eine Gefährdung, wie eingangs geschildert, darstellen.However, it is known that cutting heads of the aforementioned It is particularly suitable in the event of an oblique impact not reliably disassemble on a target medium and thereby represent a hazard, as described at the beginning.

Ausgehend von dem vorgenannten Stand der Technik ist es Aufgabe der Erfindung, ein Übungsgeschoß für Rohrwaffen zu schaffen, welches einfach herstellbar ist und beim Aufprall in mindestens zwei Teile zerlegt wird und dadurch die Gefahr von Abprallern und den Gefährdungsbereich spürbar reduziert. Based on the aforementioned prior art, it is Object of the invention, a training floor for barrel weapons to create which is easy to manufacture and at Impact is broken down into at least two parts and thereby the risk of ricochets and the hazardous area noticeably reduced.

Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Patentanspruches 1 gelöst. Erfinderische Weiterbildungen und Ausgestaltungen sind den Unteransprüchen 2 bis 6 zu entnehmen.This object is achieved by the features of claim 1 solved. Innovative further training and refinements are the subclaims 2 up to 6.

Durch die Verwendung des Zerlegeelementes als sogenanntes Trenn-Element ist es mit technisch einfachen und wirtschaftlich günstigen Mitteln möglich, die Reichweite von abprallenden Übungsgeschossen durch Trennung in mindestens zwei Teile drastisch zu reduzieren, wodurch das Übungsschießen auch auf kleineren Übungsplätzen ermöglicht wird.By using the disassembly element as a so-called Separating element is it with technically simple and economically viable means possible to reach from rebounding practice projectiles by separation into to drastically reduce at least two parts, thereby practice shooting is also possible on smaller practice areas becomes.

Die Reichweitenreduzierung wird im wesentlichen durch zwei physikalische Gesetzmäßigkeiten erzielt. Zum einen stellen die beiden verbleibenden Teile nach der Trennung des Übungsgeschosses durch Zerlegung ballistisch ungünstige, d. h. mit einem höheren Widerstandsbeiwert behaftete Körper dar, deren Fluggeschwindigkeit sich wesentlich schneller abbaut als bei einem Gesamtgeschoß. Ein erneutes Stabilisieren von solchen Geschoßbruchstücken ist darüber hinaus unwahrscheinlich. Zum anderen sind die beiden oder mehreren Geschoßbruchstücke nach Zerlegung des Übungsgeschosses leichter als das Gesamtgeschoß. Dadurch wird die den Geschoßteilen noch innewohnende Restgeschwindigkeit sehr schnell abgebaut.The range reduction is essentially through achieved two physical laws. On the one hand put the two remaining parts after separation of the practice floor by ballistic disassembly unfavorable, d. H. with a higher drag coefficient afflicted bodies whose flight speed is different degrades much faster than a whole floor. A new stabilization of such fragments of floors is also unlikely. To the others are the two or more story fragments after disassembling the practice floor easier than the entire floor. This is the floor parts remaining speed very quickly reduced.

In der Zeichnung ist ein Beispiel der Erfindung dargestellt. Es zeigen:

Figur 1
Ein Übungsgeschoß mit eingesetztem Zerlegeelement im Halbschnitt
Figur 2
Das Zerlegeelement gemäß Figur 1 mit innenliegender Sollbruchstelle
Figur 3
Ein Zerlegeelement anderer Bauart mit innenliegender Sollbruchstelle
Figur 4
Ein Zerlegeelement noch anderer Bauart mit außenliegender Sollbruchstelle
Figur 5
Ein Zerlegeelement für ein Übungsgeschoß mit innen- und außenliegender Sollbruchstelle
Figur 6
Ein Übungsgeschoß mit einem Zerlegeelement nach Figur 3 in Kombination mit Preßkörpern
Figur 7
Ein Übungsgeschoß mit Zerlegeelement nach Figur 3 in Kombination mit Preßkörpern und Zerlege-Formkörpern.
An example of the invention is shown in the drawing. Show it:
Figure 1
A practice floor with an inserted disassembly element in half cut
Figure 2
The disassembly element according to Figure 1 with an internal predetermined breaking point
Figure 3
A disassembly element of another design with an internal predetermined breaking point
Figure 4
A disassembly element of yet another design with an external predetermined breaking point
Figure 5
A disassembly element for a practice floor with an internal and external predetermined breaking point
Figure 6
A practice floor with a disassembling element according to Figure 3 in combination with compacts
Figure 7
A training projectile with disassembly element according to Figure 3 in combination with compacts and disassembly molded bodies.

Das Übungsgeschoß besteht im wesentlichen aus einer Geschoßhaube 2 und einem Geschoßheck 3, welches das Führungsband 4 in einer Ringnut aufnimmt. Die Geschoßhaube 2 und das Geschoßheck 3 sind durch ein Zerlegeelement 5, welches hohlzylindrisch ausgebildet ist und zu beiden Seiten eines Mittelbereiches 6 Gewindeansätze 7 und 8 aufweist, verbunden. Mit dem Gewindeansatz 7 ist das Zerlegeelement 6 in ein entsprechendes Innengewinde einer Sackbohrung 9 der Geschoßhaube 2 eingeschraubt. Das Geschoßheck 3 ist mit einem Innengewinde der Ausnehmung 10 auf den Gewindeansatz 8 aufgeschraubt. In dem Beispiel der Figur 1 hat der Mittelbereich 6 des Zerlegeelementes 5 einen gleichen Außendurchmesser 11 wie die Geschoßhaube 2 und das Geschoßheck 3. Dies bedeutet, daß der Mittelbereich 6 des Zerlegeelementes 5 ringförmig zwischen den einander zugewandten Stirnseiten der Geschoßhaube 2 und des Geschoßhecks 3 liegt.The practice floor essentially consists of a floor hood 2 and a bullet tail 3, which is the guide band 4 accommodates in an annular groove. The storey hood 2 and the tail 3 are by a disassembly element 5, which is hollow cylindrical and to both Sides of a central area 6 thread approaches 7 and 8 has connected. With the threaded approach 7 that is Disassembly element 6 in a corresponding internal thread a blind hole 9 of the projectile hood 2 is screwed in. The tailgate 3 is with an internal thread of the recess 10 screwed onto the threaded attachment 8. In In the example of FIG. 1, the central region 6 of the Disassembly element 5 has the same outer diameter 11 like the hood 2 and the tail 3. This means that the central region 6 of the disassembly element 5 ring-shaped between the facing end faces the floor hood 2 and the rear floor 3 is located.

Das Zerlegeelement 5 nach Figur 1 besitzt eine im Mittelteil 6 innen umlaufende Radialnut 12, die als Radialsollbruchstelle dient, wie dies in Figur 2 deutlich herausgestellt ist. The dismantling element 5 according to FIG. 1 has one in the middle part 6 inner circumferential radial groove 12, which as Radial set point serves, as clearly shown in Figure 2 is highlighted.

Das Zerlegeelement 5 ist aus einer hochfesten Aluminium-Knetlegierung hergestellt, welche über eine geringere Temperaturabhängigkeit der Kerbzähigkeit als Stahl verfügt. Die Restwanddicke 13 der Radialsollbruchstelle 12 ist so bemessen, daß sich das Übungsgeschoß bei einem Aufprall auf ein Zielmedium sicher in zumindest zwei Teile zerlegt. Dies ist auch dann gewährleistet, wenn das Übungsgeschoß 1 in einem relativ flachen Auftreffwinkel von beispielsweise 10° Grad auf ein Zielmedium aufprallt.The disassembly element 5 is made of a high-strength wrought aluminum alloy manufactured which has a lower Temperature dependence of the notch toughness as Steel. The remaining wall thickness 13 of the radial breaking point 12 is dimensioned so that the practice floor in the event of a collision with a target medium disassembled at least two parts. This is also guaranteed if the practice floor 1 in a relative flat impact angle of, for example, 10 ° degrees hits a target medium.

Durch eine konstruktiv günstig gewählte Lage der Trennstelle zwischen der Geschoßhaube 2 und dem Geschoßheck 3 kann die in den meisten Fällen günstigere Ballistik der Geschoßhaube 2 durch eine geringere Restmasse ausgeglichen werden, so daß für die beiden zerlegten Teile jeweils ähnliche Restflugbahnen und Entfernungen erreichbar sind.Due to a structurally favorable location of the separation point between the bonnet 2 and the tailgate 3 can be the most cost-effective ballistics in most cases the storey hood 2 compensated for by a lower residual mass be so that for the two disassembled parts Similar remaining trajectories and distances can be reached are.

In Figur 3 ist ein Zerlegeelement 14 in leicht abgewandelter Bauart dargestellt. Dieses Zerlegeelement 14 unterscheidet sich von dem Zerlegeelement 5 nach Figur 2 bzw. nach Figur 1 dadurch, daß der mittlere Bereich radial nicht über die beiden Gewindeansätze 7 und 8 hinausragt. Der mittlere Bereich 15, an dessen Innenseite wiederum eine umlaufende Radialsollbruchstelle 12 eingebracht ist, schließt im Außendurchmesser mit dem Innendurchmesser der Sackbohrung 9 der Geschoßhaube 2 bzw. mit der Ausnehmung 10 im Geschoßheck ab. Dadurch liegt der Mittelbereich 15 des Zerlegeelementes 14 gemäß den Figuren 6 und 7 innerhalb der Geschoßummantelung, wobei die Radialsollbruchstelle 12 direkt unterhalb der Trennlinie 16 zwischen der Geschoßhaube 2 und dem Geschoßheck 3 liegt.In Figure 3 is a disassembling element 14 in a slightly modified Design shown. This disassembling element 14 differs from the disassembly element 5 according to FIG. 2 or according to Figure 1 in that the central region is radial does not protrude beyond the two threaded lugs 7 and 8. The middle area 15, on the inside again a circumferential radial breaking point 12 is introduced is in the outer diameter with the Inner diameter of the blind bore 9 of the projectile hood 2 or with the recess 10 in the tail end. Thereby is the central region 15 of the disassembly element 14 according to FIGS. 6 and 7 within the floor covering, the radial breaking point 12 directly below the dividing line 16 between the floor hood 2 and the tail 3 is located.

Das Zerlegeelement 17 nach Figur 4 ist ähnlich aufgebaut wie das Zerlegeelement 14 in Figur 3. Als einziger Unterschied besitzt dieses Zerlegeelement 17 eine außenumlaufende Radialsollbruchstelle 18.The disassembly element 17 according to FIG. 4 has a similar structure as the disassembly element 14 in Figure 3. As the only one The difference is that this dismantling element 17 has an outer circumferential one Radial set point 18.

In Figur 5 ist wiederum ein Zerlegelement 19 im Halbschnitt gezeigt, welches vom Baukörper her dem Zerlegeelement 14 entspricht. Jedoch sind in dem Zerlegeelement 19 nun eine innenumlaufende und eine außenumlaufende Radialsollbruchstelle 20 bzw. 21 eingebracht.In Figure 5 is again a disassembling element 19 in half section shown which the disassembling element from the building 14 corresponds. However, are in the disassembly element 19 now an inner circumferential and an outer circumferential Radial set point 20 or 21 introduced.

Alle vorgenannten Zerlegeelemente 5,14,17 und 19 erfüllen die gestellten Anforderungen optimal. In allen Fällen wurde in Versuchsreihen an einem Übungsgeschoß aus Stahl die einwandfreie Zerlegung des Übungsgeschosses 1 in zumindest zwei Teile nachgewiesen.All of the aforementioned disassembly elements 5, 14, 17 and 19 are met the requirements set optimally. In all cases was used in test series on a practice floor Steel the perfect disassembly of the practice floor 1 proven in at least two parts.

Die Figur 6 zeigt wiederum ein Übungsgeschoß 22 mit einer Geschoßhaube 2 und einem Geschoßheck 3 mit Führungsband 4. Die Geschoßhaube 2 und das Geschoßheck 3 sind wiederum durch ein Zerlegeelement 23 miteinander verbunden, wobei lediglich die Gewindeansätze 7 und 8 unterschiedliche Durchmesser aufweisen. Die Radialsollbruchstelle 12 liegt direkt unterhalb der Trennfuge 16 zwischen der Geschoßhaube 2 und dem Geschoßheck 3. Im vorderen Bereich des Übungsgeschosses 2 befinden sind ein oder mehrere Preßkörper 24,25 und 26 aus einem Eisenpulver.FIG. 6 again shows a practice floor 22 with a Missile hood 2 and a missile tail 3 with a guide band 4. The projectile hood 2 and the projectile tail 3 are in turn by a disassembly element 23 connected, only the threaded lugs 7 and 8 have different diameters. The radial breaking point 12 is located directly below the parting line 16 between the hood 2 and the tail 3. In the front area of exercise floor 2 are located one or more compacts 24, 25 and 26 made of an iron powder.

Das Übungsgeschoß 22 nach Figur 7 ist wiederum mit einem Zerlegeelement 23 versehen, als einziger Unterschied zur Figur 6 sind in diesem Fall nach Figur 7 zwischen dem Zerlegeelement 23 und dem Preßkörper 24 kugelförmige Formkörper 27 und 28 von unterschiedlichen Durchmessern eingesetzt. Durch den Einsatz von Preßkörpern 24,25 und 26 sowie Formkörpern 27 und 28 wird die Zerlegung des Übungsgeschosses 1 bzw. 22 weiter optimiert. Durch Zurückverlegen der Trennstelle 16 am Übungsgeschoß 22,1 wird dann noch eine relativ schwere, ballistisch optimierte Geschoßhaube 2 im mehrere unkritische Teile bei Zielaufschlag zerlegt. Für das Geschoßheck 3 verbleibt dadurch nur noch ein relativ leichter, ballistisch ungünstig fliegender zylinderähnlicher Restkörper.The exercise floor 22 according to FIG. 7 is again with a Disassembly element 23 provided as the only difference 6 are in this case according to FIG. 7 between the disassembling element 23 and the pressing body 24 spherical shaped bodies 27 and 28 of different Diameters used. Through the use of compacts 24, 25 and 26 and shaped bodies 27 and 28 is the Disassembly of practice levels 1 and 22 further optimized. By moving the separation point 16 am Practice floor 22.1 will then be a relatively difficult Ballistic-optimized storey hood 2 in several uncritical ones Parts disassembled on target impact. For the tailgate 3 remains only a relative lighter, ballistically unfavorable cylinder-like flying Residual body.

Wie die Figuren 6 und 7 verdeutlichen, dient das Zerlegeelement 23 nicht nur der Verbindung und Trennung von Geschoßhaube 2 und Geschoßheck 3, sondern erlaubt gleichzeitig auch eine spielfreie und zum Geschoßheck 3 längentoleranzunabhängige Fixierung von Füllkörpern 24,25,26,27 und 28 in der Geschoßhaube 2. Eine Bauweise nach Figur 6 bzw. 7 ist technisch aufwendiger als die Bauweise des Übungsgeschosses 1 nach Figur 1. Hier bleibt es dem Fachmann überlassen, unter Berücksichtigung der an ihn gestellten Forderungen die richtige Konstruktionsvariante für ein Übungsgeschoß 1 bzw. 22 zu wählen, welches bei Zielaufprall sich in zumindest zwei Teile zerlegt.As shown in FIGS. 6 and 7, the disassembly element serves 23 not just connecting and disconnecting Bullet hood 2 and tailgate 3, but allowed at the same time also a backlash free and to the tailgate 3 fixation of packing elements independent of length tolerance 24, 25, 26, 27 and 28 in the floor hood 2. One construction 6 or 7 is technically more complex than that Construction of practice level 1 according to Figure 1. Here it is left to the specialist, taking into account the right demands on him Construction variant for a practice floor 1 or 22 to choose which one at least in the event of a target impact disassembled two parts.

Claims (6)

  1. Training projectile for barrel weapons, which in form and mass largely corresponds to a training projectile or to a combat projectile, with a projectile cap (2) and a projectile tail (3) and slide ring (4), characterised by the fact that between the projectile cap (2) and the projectile tail (3) a dismountable element (5,14,17,19,23) is located which interconnects both parts and which is provided with at least one radial pre-set rupturing point (12,18,20,21) situated internally or extemally.
  2. Training projectile in accordance with Claim 1, characterised by the fact that the radial pre-set rupturing point (12,18,20,21) is provided in a central zone (6,15) of the dismountable element (5,14,17,19,23), radially spaced from the separating point between the projectile tail (3) and the projectile cap (2).
  3. Training projectile in accordance with Claim 1 or 2, characterised by the fact that the radial pre-set rupturing point (12,18,20,21) is mounted annularly around the dismountable element (5,14,17,19,23).
  4. Training projectile in accordance with Claims 1 to 3, characterised by the fact that the dismountable element (5,14,17,19,23) has a central zone (6,15) of which the external diameter is equal to or smaller than the external diameter of the projectile tail (3) and/or the projectile cap (2).
  5. Training projectile in accordance with any one of Claims 1 to 4, characterised by the fact that the dismountable element (5,14,17,19,23) is made of a high-strength ductile aluminium alloy.
  6. Training projectile in accordance with any one of Claims 1 to 5, characterised by the fact that the dismountable element (5,14,17,19,23) secures with tolerance dependent relationship shaped bodies (24,25,26,27,28) located in the projectile cap (2).
EP95113344A 1994-11-11 1995-08-25 Training projectile for gun barrel Expired - Lifetime EP0716285B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4440263 1994-11-11
DE4440263A DE4440263A1 (en) 1994-11-11 1994-11-11 Practice bullet for barrel weapons

Publications (2)

Publication Number Publication Date
EP0716285A1 EP0716285A1 (en) 1996-06-12
EP0716285B1 true EP0716285B1 (en) 1998-10-21

Family

ID=6533031

Family Applications (1)

Application Number Title Priority Date Filing Date
EP95113344A Expired - Lifetime EP0716285B1 (en) 1994-11-11 1995-08-25 Training projectile for gun barrel

Country Status (3)

Country Link
EP (1) EP0716285B1 (en)
DE (2) DE4440263A1 (en)
NO (1) NO305773B1 (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL291072A (en) * 1962-04-16 Energa
US4108074A (en) * 1977-04-27 1978-08-22 Avco Corporation Frangible target practice projectile
DE3048206C2 (en) * 1980-12-20 1985-06-13 Diehl GmbH & Co, 8500 Nürnberg Practice floor
DE3642414A1 (en) * 1986-12-11 1988-06-23 Feistel Pyrotech Fab EXERCISE CARTRIDGE FOR SHOCK ABSORBED ARMS
DE3902112C1 (en) * 1989-01-25 1990-05-10 Nico Pyrotechnik Hanns-Juergen Diederichs Gmbh & Co Kg, 2077 Trittau, De
AT393735B (en) * 1989-10-13 1991-12-10 Intertechnik Tech Prod BULLET FOR A LIMITED FLIGHT RANGE
CH684804A5 (en) * 1993-06-15 1994-12-30 Contraves Pyrotec Ag Sub-calibre projectile

Also Published As

Publication number Publication date
NO953375D0 (en) 1995-08-29
NO953375L (en) 1996-05-13
EP0716285A1 (en) 1996-06-12
DE59503984D1 (en) 1998-11-26
NO305773B1 (en) 1999-07-19
DE4440263A1 (en) 1996-05-15

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