EP0047384B1 - Cartridge ammunition for firearms - Google Patents

Cartridge ammunition for firearms Download PDF

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Publication number
EP0047384B1
EP0047384B1 EP81105766A EP81105766A EP0047384B1 EP 0047384 B1 EP0047384 B1 EP 0047384B1 EP 81105766 A EP81105766 A EP 81105766A EP 81105766 A EP81105766 A EP 81105766A EP 0047384 B1 EP0047384 B1 EP 0047384B1
Authority
EP
European Patent Office
Prior art keywords
cartridge ammunition
fact
accordance
projectile
propellant charge
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
Application number
EP81105766A
Other languages
German (de)
French (fr)
Other versions
EP0047384A1 (en
Inventor
Udo Sabranski
Eckhard Rahnenführer
Manfred Dr. Lübben
Horst Pinkernelle
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.)
Rheinmetall Industrie AG
Original Assignee
Rheinmetall 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 Rheinmetall GmbH filed Critical Rheinmetall GmbH
Publication of EP0047384A1 publication Critical patent/EP0047384A1/en
Application granted granted Critical
Publication of EP0047384B1 publication Critical patent/EP0047384B1/en
Expired 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
    • F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02—Cartridges, i.e. cases with charge and missile
    • F42B5/067—Mounting or locking missiles in cartridge cases
    • F42B5/073—Mounting or locking missiles in cartridge cases using an auxiliary locking element

Definitions

  • the invention relates to cartridge ammunition for barrel weapons according to the preamble of claim 1.
  • a generic ammunition is known from DE-B-1 013 202.
  • a propellant charge sleeve made of metal extends from a rear floor to its front case mouth, in the area of which it is connected to the latter in the vicinity of an essentially tubular caliber rear face of the projectile.
  • an additional element in the form of an ignition tube is arranged in such a way that it positively connects the projectile tail projecting into the propellant charge sleeve to the bottom of the propellant charge sleeve.
  • a caseless propellant charge for projectiles is known from DE-A-1 962 386, but this known arrangement does not meet the requirements in connection with a wing-stabilized projectile.
  • the propellant charge is measured longitudinally axially by a rod-shaped or tubular propellant charge holder, a front end of the propellant charge holder being connected to the projectile tail via a frictional connection.
  • the invention has for its object to provide a cartridge ammunition of the type mentioned, which is characterized by the greatest possible elimination of empties by a type of additional attachment for the floor, which avoids dimensional tolerance problems in a simple manner.
  • a projectile rear part 10 which forms a first region 42, has a stabilizing tail unit 12 and a trailing tracer mount 36 with a tracer set 37.
  • a screw 15 is fastened in a wall 11 and forms a first holder H.1.
  • one end 2 of a wire-shaped support element 1.1 is fixed on the rear part 10 of the projectile.
  • a central bore 28 of the bottom 30, which is only shown in part, of a bottom bore, which is not shown for reasons of clarity and which is partially combustible propellant charge sleeve, is aligned with the rear part 10 of the bullet.
  • the arrangement shown in Fig. 1 is made.
  • a screw-in cup 38 is arranged in an essentially circular-cylindrical projection 32 encompassing the central bore 28.
  • a bore 40 is located in the upward-pointing bottom part 39 thereof.
  • the location of a second holder H.2 is essentially given.
  • an end 3 of the support element 1.1 facing away from the projectile is introduced into the bore 40.
  • the end 3 has a part 4 to be explained as a continuation.
  • the end 3 can be “threaded” into the bore 40 by means of the part 4. Then the part 4 is pulled out in the direction of an arrow 50.
  • the end 3 can be provided with a thread as a form-locking member 5.
  • the support element 1.1 With a nut as a corresponding form-locking member 21, brought over the part 4 and screwed onto the thread 5, the support element 1.1 can be prestressed. After the screwing of FIGS. 5 and 21, the latter form-fitting member lies closely against the underside of the base part 39 forming an abutment 41. An end of the support element 1. 1 projecting in particular with the part 4 downward is now advantageously separated in the immediate vicinity of the form-locking member 21. Then, as shown in FIG. 2, a propellant charge lighter 34 is inserted into the receptacle provided for it and fastened there. The projectile is now positively connected to the bottom of the propellant charge sleeve in the direction of the longitudinal axis A of the train. In order to ensure a minimum propellant gas pressure that should not be undercut when developing the shot for internal ballistic reasons, a predetermined breaking point 46, not shown and described, is advantageously provided in the area of the first holder H.1.
  • two retaining pins 14 are arranged in the wall 11, aligned with one another over a diameter. They serve the two unspecified ends of a bracket 16 - it essentially forms the first holder H.1 in the area 42 for fastening to the rear part 10 of the projectile. With its end 2 on the projectile side, the support element 1.1 is not closer shown manner attached to the bracket 16. While the support element 1.1 in the first exemplary embodiment according to FIG. 1 was formed by a wire, it is now designed, for example, as a sufficiently strong thread, for example made of nylon, or as a band. The end 3 of the support element 1.1 facing away from the projectile is fastened by means of a cross member 19 in a tubular, radially resilient pull-in part 22.
  • the pull-in part 22 has an outside saw profile, which forms a ratchet lock with the inside saw profile 20 of a screw-in part 18 for positive locking under tension against the arrow 50.
  • the screw-in part 18 is screwed into the receiving insert 32, the two corresponding threads being designated 26.1 and 26.2.
  • a detachable cord of sufficient tensile strength, for example, is suitable as part 4 going beyond an attachment point 6. 3, the screw-in part 18 is only partially screwed into the receiving projection 32.
  • the pull-in part 22 has already been introduced to such an extent that there is a form fit between 18 and 22 in the event of a tensile stress against the arrow 50.
  • the two retaining pins 14 can, for example, be broken off at a predefinable load.
  • An equivalent effect can be achieved by a targeted combustibility, ie with a burning rate adapted to the relevant circumstances, for example of the material from which the holding pins 14 are made. This advantageously leaves no remainder protruding beyond the aerodynamic contour of the projectile.
  • the support element 1.2 is made of a tubular film and is provided with openings 7, which are intended to help prevent the ignition process from developing the shot.
  • the film is connected to the inner surface 23 of the pull-in part 22 in a manner not shown and described.
  • a cross member 19 'for fastening the part 4 can be arranged removably in the lower region of the pull-in part 22 in a manner not shown.
  • the hose 1.2 can also be made of a woven fabric, whereby there is obviously no need to make openings. Non-combustible parts of the support element arrangement, provided that they impair the flight properties of the projectile, are removed from the tube on the closure side with the bottom of the propellant charge sleeve. In this way, disability is avoided with certainty.
  • Reference symbol list

Description

Die Erfindung betrifft patronierte Munition für Rohrwaffen nach dem Oberbegriff des Patentanspruchs 1.The invention relates to cartridge ammunition for barrel weapons according to the preamble of claim 1.

Eine gattungsgleiche Munition ist bekannt aus der DE-B-1 013 202. Eine Treibladungshülse aus Metall erstreckt sich von einem rückseitigen Boden zu ihrem vorderseitigen Hülsenmund, in dessen Bereich sie in der Nachbarschaft einer im wesentlichen rohrkalibergleichen Rückseitenfläche eines Geschosses mit letzterem verbunden ist. Als zusätzliche Befestigung ist ein Zusatzelement in Form eines Zündrohres derart angeordnet, daß sie das in die Treibladungshülse hineinragende Geschoßheck formschlüssig mit dem Boden derTreibladungshülse verbinden.A generic ammunition is known from DE-B-1 013 202. A propellant charge sleeve made of metal extends from a rear floor to its front case mouth, in the area of which it is connected to the latter in the vicinity of an essentially tubular caliber rear face of the projectile. As an additional attachment, an additional element in the form of an ignition tube is arranged in such a way that it positively connects the projectile tail projecting into the propellant charge sleeve to the bottom of the propellant charge sleeve.

Nachteilig ist an dieser bekannten Munition der große Anfall von Leergut, der sich besonders in engen Kampfräumen störend auswirkt. Ferner sind Toleranzprobleme möglich.The disadvantage of this known ammunition is the large amount of empties, which is particularly disruptive in narrow combat areas. Tolerance problems are also possible.

Zwar ist aus der DE-A-1 962 386 eine hülsenlose Treibladung für Geschosse bekannt, aber diese bekannte Anordnung trägt nicht den Forderungen im Zusammenhang mit einem flügelstabilisierten Geschoß Rechnung. Die Treibladung wird von einer stab- oder rohrförmigen Treibladungshalterung längsaxial durchmessen, wobei ein vorderes Ende der Treibladungshalterung über Reibschluß mit dem Geschoßheck verbunden ist.A caseless propellant charge for projectiles is known from DE-A-1 962 386, but this known arrangement does not meet the requirements in connection with a wing-stabilized projectile. The propellant charge is measured longitudinally axially by a rod-shaped or tubular propellant charge holder, a front end of the propellant charge holder being connected to the projectile tail via a frictional connection.

Der Erfindung liegt die Aufgabe zugrunde, eine patronierte Munition der eingangs genannten Gattung zu schaffen, die sich bei möglichst weitgehendem Entfall von Leergut durch eine Art der zusätzlichen Befestigung für das Geschoß auszeichnet, welche auf einfache Weise Maßtoleranzprobleme vermeidet.The invention has for its object to provide a cartridge ammunition of the type mentioned, which is characterized by the greatest possible elimination of empties by a type of additional attachment for the floor, which avoids dimensional tolerance problems in a simple manner.

Gelöst wird diese Aufgabe durch die im Kennzeichen des Patentanspruchs 1 angegebene Erfindung.This object is achieved by the invention specified in the characterizing part of patent claim 1.

Dabei sind vorteilhafterweise nicht nur die erforderlichen Mittel einfach, sondern auch die Maßnahmen zu deren Anordnung. So verlieren beispielsweise unter anderem die Toleranzen im Abstand der beiden Bereiche voneinander an Bedeutung.Advantageously, not only the necessary means are simple, but also the measures for their arrangement. For example, the tolerances in the distance between the two areas lose importance.

Die Erfindung wird nachstehend anhand dreier in der Zeichnung im wesentlichen schematisch dargestellter Ausführungsbeispiele des näheren erläutert.The invention is explained below with reference to three exemplary embodiments of the closer, which are shown essentially schematically in the drawing.

Es zeigt - jeweils im Schnitt entlang einer zentralen Patronenlängsachse -

  • Fig. 1 ein erstes Ausführungsbeispiel mit einer ersten Festlegeanordnung vor dem Festlegen,
  • Fig. 2 in einem Ausschnitt aus Fig. 1 die betreffende Festlegeanordnung nach dem Festlegen und nach dem Einsetzen eines Treibladungszünders,
  • Fig. 3 ein zweites Ausführungsbeispiel mit einerzweiten Festlegeanordnung und
  • Fig. 4 ein drittes Ausführungsbeispiel mit der Festlegeanordnung nach Fig. 3 in einer ausschnittsweisen Darstellung des hülsenbodenseitigen Bereichs.
It shows - each in section along a central longitudinal axis of the cartridge -
  • 1 shows a first embodiment with a first fixing arrangement before fixing,
  • 2 in a detail from FIG. 1, the fixing arrangement in question after the fixing and after the insertion of a propellant charge igniter,
  • Fig. 3 shows a second embodiment with a second fixing arrangement and
  • Fig. 4 shows a third embodiment with the fixing arrangement according to Fig. 3 in a fragmentary representation of the sleeve bottom area.

Gemäß Fig. 1 weist ein Geschoßheckteil 10, welcher einen ersten Bereich 42 bildet, ein Stabilisierungsleitwerk 12 und eine rückendige Leuchtspuraufnahme 36 mit einem Leuchtspursatz 37 auf. Eine Schraube 15 ist in einer Wandung 11 befestigt und bildet eine erste Halterung H.1. Dort ist ein Ende 2 eines drahtförmigen Stützelements 1.1 am Geschoßheckteil 10 festgelegt. Entlang einer Patronenachse A fluchtet mit dem Geschoßheckteil 10 eine zentrale Bohrung 28 des nur ausschnittsweise dargestellten Bodens 30 einer aus Gründen der Übersichtlichkeit nicht abgebildeten, wengistens teilverbrennbaren Treibladungshülse. Zum Zwecke der gegenseitigen Verbindung ist die in Fig. 1 dargestellte Anordnung getroffen.1, a projectile rear part 10, which forms a first region 42, has a stabilizing tail unit 12 and a trailing tracer mount 36 with a tracer set 37. A screw 15 is fastened in a wall 11 and forms a first holder H.1. There, one end 2 of a wire-shaped support element 1.1 is fixed on the rear part 10 of the projectile. Along a cartridge axis A, a central bore 28 of the bottom 30, which is only shown in part, of a bottom bore, which is not shown for reasons of clarity and which is partially combustible propellant charge sleeve, is aligned with the rear part 10 of the bullet. For the purpose of mutual connection, the arrangement shown in Fig. 1 is made.

In einem die zentrale Bohrung 28 umgreifenden, im wesentlichen kreiszylindrischen Ansatz 32 ist ein Einschraubnapf 38 angeordnet. In dessen nach oben weisendem Bodenteil 39 befindet sich eine Bohrung 40. Mit ihr ist der Ort einer zweiten Halterung H.2 im wesentlichen gegeben. Zum Festlegen des Stützelements 1.1 im hülsenseitigen Bereich 44 wird ein dem Geschoß abgewandtes Ende 3 des Stützelements 1.1 in die Bohrung 40 eingebracht. Vorteilhafterweise weist das Ende 3 einen noch zu erläuternden Teil 4 als Fortsetzung auf. Mittels des Teils 4 kann das Ende 3 in die Bohrung 40 »eingefädelt« werden. Dann wird der Teil 4 in Richtung eines Pfeils 50 ausgezogen. Das Ende 3 kann mit einem Gewinde als Formschlußglied 5 versehen sein. Mit einer Mutter als korrespondierendes Formschlußglied 21, über den Teil 4 hinweggebracht und auf das Gewinde 5 aufgeschraubt, kann das Stützelement 1.1 vorgespannt werden. Nach dem Verschrauben von 5 und 21 liegt letzteres Formschlußglied eng an der ein Widerlager 41 bildenden Unterseite des Bodenteils 39 an. Ein insbesondere mit dem Teil 4 nach unten überstehendes Ende des Stützelements 1.1 wird nun vorteilhafterweise in unmittelbarer Nachbarschaft des Formschlußglieds 21 abgetrennt. Anschließend wird, wie in Fig. 2 dargestellt, ein Treibladungsanzünder 34 in die für ihn vorgesehene Aufnahme eingebracht und dort befestigt. Das Geschoß ist nun in Richtung der Patronenlängsachse A auf Zug formschlüssig mit dem Boden der Treibladungshülse verbunden. Zum Gewährleisten eines aus innerballistischen Gründen bei der Schußentwicklung nicht zu unterschreitenden Mindesttreibgasdrucks ist, vorteilhafterweise im Bereich der ersten Halterung H.1 eine nicht näher dargestellte und beschriebene Sollbruchstelle 46 vorgesehen.A screw-in cup 38 is arranged in an essentially circular-cylindrical projection 32 encompassing the central bore 28. A bore 40 is located in the upward-pointing bottom part 39 thereof. The location of a second holder H.2 is essentially given. To fix the support element 1.1 in the sleeve-side area 44, an end 3 of the support element 1.1 facing away from the projectile is introduced into the bore 40. Advantageously, the end 3 has a part 4 to be explained as a continuation. The end 3 can be “threaded” into the bore 40 by means of the part 4. Then the part 4 is pulled out in the direction of an arrow 50. The end 3 can be provided with a thread as a form-locking member 5. With a nut as a corresponding form-locking member 21, brought over the part 4 and screwed onto the thread 5, the support element 1.1 can be prestressed. After the screwing of FIGS. 5 and 21, the latter form-fitting member lies closely against the underside of the base part 39 forming an abutment 41. An end of the support element 1. 1 projecting in particular with the part 4 downward is now advantageously separated in the immediate vicinity of the form-locking member 21. Then, as shown in FIG. 2, a propellant charge lighter 34 is inserted into the receptacle provided for it and fastened there. The projectile is now positively connected to the bottom of the propellant charge sleeve in the direction of the longitudinal axis A of the train. In order to ensure a minimum propellant gas pressure that should not be undercut when developing the shot for internal ballistic reasons, a predetermined breaking point 46, not shown and described, is advantageously provided in the area of the first holder H.1.

Gemäß Fig. 3 sind in die Wandung 11, auf einem Durchmesser miteinander fluchtend, zwei Haltestifte 14 angeordnet. Sie dienen den beiden nicht näher bezeichneten Enden eines Bügels 16 - er bildet im Bereich 42 im wesentlichen die erste Halterung H.1- zum Befestigen am Geschoßheckteil 10. Mit seinem geschoßseitigen Ende 2 ist das Stützelement 1.1 auf nicht näher dargestellte Weise am Bügel 16 befestigt. Während das Stützelement 1.1 beim ersten Ausführungsbeispiel nach Fig. 1 durch einen Draht gebildet wurde, ist es nun beispielsweise als ausreichend starker Faden, beispielsweise aus Nylon, oder als Band ausgeführt. Das dem Geschoß abgewandte Ende 3 des Stützelements 1.1 ist mittels einer Traverse 19 in einem rohrförmigen, radial federnden Einziehteil 22 befestigt. Das Einziehteil 22 weist ein außenseitiges Sägeprofil auf, welches mit dem innenseitigen Sägeprofil 20 eines Einschraubteils 18 zum Formschluß unter Zugbeanspruchung entgegen dem Pfeil 50 einen Ratschenverschluß bildet. Das Einschraubteil 18 ist in den Aufnahmeeinsatz 32 eingeschraubt, wobei die beiden korrespondierenden Gewinde mit 26.1 und 26.2 bezeichnet sind. Als über einen Befestigungspunkt 6 hinausgehender Teil 4 eignet sich beispielsweise eine abtrennbare Schnur ausreichender Zugfestigkeit. In Fig. 3 ist das Einschraubteil 18 erst teilweise in den Aufnahmeansatz 32 eingeschraubt. Das Einziehteil 22 ist bereits soweit eingebracht, daß bei einer Zugbeanspruchung entgegen dem Pfeil 50 Formschluß zwischen 18 und 22 besteht. Nach dem völligen Einschrauben des Einschraubteils 18 wird durch Ziehen an dem abtrennbaren Teil 4 in Richtung des Pfeils 50 das Stützelement 1.1 zum endgültigen Festlegen im Bereich 44 auf vorgebbare Weise vorgespannt. Anschließend wird das Teil4 abgetrennt, so daß ein nicht näher bezeichneter Innenraum zur Aufnahme des Treibladungsanzünders 34 frei ist. Anstelle der im Zusammenhang mit dem ersten Ausführungsbeispiel erwähnten Sollbruchstelle 46 können beispielsweise die beiden Haltestifte 14 bei einer vorgebbaren Belastung abbrechbar sein. Ein gleichwertiger Effekt läßt sich erzielen durch eine gezielte Verbrennbarkeit, d. h. mit einer den relevanten Umständen angepaßten Abbrandgeschwindigkeit, beispielsweise des Werkstoffs, aus welchem die Haltestifte 14 gefertigt sind. Hierdurch verbleibt vorteilhafterweise kein über die aerodynamische Kontur des Geschosses überstehender Rest.According to FIG. 3, two retaining pins 14 are arranged in the wall 11, aligned with one another over a diameter. They serve the two unspecified ends of a bracket 16 - it essentially forms the first holder H.1 in the area 42 for fastening to the rear part 10 of the projectile. With its end 2 on the projectile side, the support element 1.1 is not closer shown manner attached to the bracket 16. While the support element 1.1 in the first exemplary embodiment according to FIG. 1 was formed by a wire, it is now designed, for example, as a sufficiently strong thread, for example made of nylon, or as a band. The end 3 of the support element 1.1 facing away from the projectile is fastened by means of a cross member 19 in a tubular, radially resilient pull-in part 22. The pull-in part 22 has an outside saw profile, which forms a ratchet lock with the inside saw profile 20 of a screw-in part 18 for positive locking under tension against the arrow 50. The screw-in part 18 is screwed into the receiving insert 32, the two corresponding threads being designated 26.1 and 26.2. A detachable cord of sufficient tensile strength, for example, is suitable as part 4 going beyond an attachment point 6. 3, the screw-in part 18 is only partially screwed into the receiving projection 32. The pull-in part 22 has already been introduced to such an extent that there is a form fit between 18 and 22 in the event of a tensile stress against the arrow 50. After the screw-in part 18 has been screwed in completely, pulling on the detachable part 4 in the direction of arrow 50 prestresses the support element 1.1 for final fixing in the region 44 in a predeterminable manner. The part 4 is then separated off, so that an interior space (not specified in more detail) for receiving the propellant charge lighter 34 is free. Instead of the predetermined breaking point 46 mentioned in connection with the first exemplary embodiment, the two retaining pins 14 can, for example, be broken off at a predefinable load. An equivalent effect can be achieved by a targeted combustibility, ie with a burning rate adapted to the relevant circumstances, for example of the material from which the holding pins 14 are made. This advantageously leaves no remainder protruding beyond the aerodynamic contour of the projectile.

Bei dem dritten Ausführungsbeispiel nach Fig. 4 ist das Stützelement 1.2 aus einer Folie schlauchförmig ausgebildet und mit Öffnungen 7 versehen, welche dazu beitragen sollen, den Anzündvorgang zur Schußentwicklung nicht zu behindern. Die Folie ist auf nicht näher dargestellte und beschriebene Weise mit der Innenfläche 23 des Einziehteils 22 verbunden. Eine Traverse 19' zum Befestigen des Teils 4 kann im unteren Bereich des Einziehteils 22 auf nicht dargestellte Weise entfernbar angeordnet sein.In the third exemplary embodiment according to FIG. 4, the support element 1.2 is made of a tubular film and is provided with openings 7, which are intended to help prevent the ignition process from developing the shot. The film is connected to the inner surface 23 of the pull-in part 22 in a manner not shown and described. A cross member 19 'for fastening the part 4 can be arranged removably in the lower region of the pull-in part 22 in a manner not shown.

Der Schlauch 1.2 kann auch aus einem Gewebe hergestellt sein, wobei sich das Einbringen von Öffnungen naheliegenderweise erübrigt. Nicht verbrennbare Teile der Stützelementanordnung werden, sofern sie die Flugeigenschaften des Geschosses beeinträchtigten, mit dem Boden der Treibladungshülse verschlußseitig aus dem Rohr entfernt. Auf diese Weise wird eine Behinderung mit Sicherheit vermieden. BezugszeichenlisteThe hose 1.2 can also be made of a woven fabric, whereby there is obviously no need to make openings. Non-combustible parts of the support element arrangement, provided that they impair the flight properties of the projectile, are removed from the tube on the closure side with the bottom of the propellant charge sleeve. In this way, disability is avoided with certainty. Reference symbol list

Figure imgb0001
Figure imgb0001

Claims (6)

1. Cartridge ammunition for barrel weapons with the following characteristics:
(a) a sub-calibre rear part (10) is connected with a stabilizing fin guide arrangement (12) by means of a rear side surface of the projectile which surface is generally of the same calibre as the gun barrel,
b) a propellant charge casing is secured to the projectile at the casing mouth, in the vicinity of the rear side surface,
(c) an additional element (1 ...) between the rear part (10) and a zone (44) near the base (30) of the propellant charge casing forming an additional securing means for the projectile,
(d) the additional securing means being constructed to form a mechanical lock an the rear part (10) and in the zone (44) near the base, in order to absorb a predeterminable axial tension force,
(e) the propellant charge casing being at least partly combustible,
(f) the additional element (1 ...) being solely subjected to tractive stress, and
(g) the additional elements (1 ...) being pres- tressable in the zone (44) near the base,

features (a) to (d) being generic and features (e) to (g) being characteristic.
2. Cartridge ammunition in accordance with Claim 1, characterised by the fact that the additional element (1 ...) ist at least partially combustible.
3. Cartridge ammunition in accordance with Claim 1 or 2, characterised by the fact that the additional element (1 ...) is in the form of a band or wire (1.1).
4. Cartridge ammunition in accordance with Claim 1 or 2, characterised by the fact that the additional element (1 ...) is in the form of a tube (1.2) and is provided with openings (7) in the wall.
5. Cartridge ammunition in accordance with Claim 4, characterised by the fact that the tubing (1.2) is of a foil material.
6. Cartridge ammunition in accordance with Claim 4, characterised by the fact that the tubing (1.2) consists of a woven fabric.
EP81105766A 1980-09-10 1981-07-22 Cartridge ammunition for firearms Expired EP0047384B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3033923 1980-09-10
DE19803033923 DE3033923A1 (en) 1980-09-10 1980-09-10 CARTRIDGED AMMUNITION FOR TUBE ARMS WITH AT LEAST PARTLY COMBUSTIBLE DRIVE CHARGE

Publications (2)

Publication Number Publication Date
EP0047384A1 EP0047384A1 (en) 1982-03-17
EP0047384B1 true EP0047384B1 (en) 1985-05-29

Family

ID=6111498

Family Applications (1)

Application Number Title Priority Date Filing Date
EP81105766A Expired EP0047384B1 (en) 1980-09-10 1981-07-22 Cartridge ammunition for firearms

Country Status (3)

Country Link
EP (1) EP0047384B1 (en)
JP (1) JPS5787597A (en)
DE (2) DE3033923A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11248884B2 (en) * 2019-03-27 2022-02-15 Nexter Munitions Cartridge with igniter cords

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3009342A1 (en) * 1980-03-12 1986-06-26 Rheinmetall GmbH, 4000 Düsseldorf CARTRIDGED AMMUNITION WITH AT LEAST PARTLY COMBUSTIBLE DRIVE CHARGE
DE3409017A1 (en) * 1984-03-13 1985-09-26 Rheinmetall GmbH, 4000 Düsseldorf CARTRIDGED AMMUNITION FOR TUBE ARMS
JPH0442100U (en) * 1990-08-06 1992-04-09

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE536577A (en) * 1954-03-22
DE1578171A1 (en) * 1966-12-15 1971-05-27 Erhard Lutz Caseless ammunition
DE1962386A1 (en) * 1969-12-12 1971-06-16 Eta Corp Cartridgeless projectile propellant charge
US4016796A (en) * 1976-03-29 1977-04-12 The United States Of America As Represented By The Secretary Of The Navy Weapon retention device
DE2853527C2 (en) * 1978-12-12 1982-05-06 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Launching device for projectiles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11248884B2 (en) * 2019-03-27 2022-02-15 Nexter Munitions Cartridge with igniter cords

Also Published As

Publication number Publication date
EP0047384A1 (en) 1982-03-17
JPS5787597A (en) 1982-06-01
DE3170709D1 (en) 1985-07-04
JPS6146760B2 (en) 1986-10-15
DE3033923A1 (en) 1982-04-15

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