EP2221575A2 - Cartridge - Google Patents
Cartridge Download PDFInfo
- Publication number
- EP2221575A2 EP2221575A2 EP09015606A EP09015606A EP2221575A2 EP 2221575 A2 EP2221575 A2 EP 2221575A2 EP 09015606 A EP09015606 A EP 09015606A EP 09015606 A EP09015606 A EP 09015606A EP 2221575 A2 EP2221575 A2 EP 2221575A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- sabot
- projectile
- cartridge
- cartridge according
- flange
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
- F42B14/06—Sub-calibre projectiles having sabots; Sabots therefor
- F42B14/064—Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B14/00—Projectiles or missiles characterised by arrangements for guiding or sealing them inside barrels, or for lubricating or cleaning barrels
-
- 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
-
- 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 a cartridge which consists of a cartridge case and a projectile assembly which is connected via a sleeve cover with the cartridge case.
- Such a cartridge is for example from the DE 27 47 313 C2 known.
- the known projectile arrangement includes a shotgun with a subcaliber projectile body and a rear side of the projectile body cone-tail, wherein between the center of gravity of the projectile body and the projectile nose a segmented with the arrow floor Einflansch-sabot with outwardly extending wall areas rubbing and / or is positively connected.
- the DE 27 47 313 C2 the use of two-flange sabots, as for example from the DE-PS 17 03 507 are known.
- such sabots also have a high weight and are very expensive.
- the invention has for its object to provide a cartridge of the type mentioned, whose bullet assembly is less expensive to produce than comparable arrangements.
- the invention is based essentially on the idea to connect with the sleeve cover on the projectile side a centering of the tail of the arrow centering and detachable during firing of the cartridge from the tail receiving device which comprises an annular rear flange whose outer diameter corresponds to the bullet caliber of each cartridge.
- the receiving device consists of plastic.
- the receiving device has a conical front part which comprises the tail unit, which is arranged in front of the rear flange on the friction cage side and engages in a form-fitting manner at least in a partial area of the tail unit.
- the outer side of the conical front part of the receiving device can be connected to the rear flange via a plurality of rib-shaped struts distributed uniformly over the circumference.
- the one-flange sabot may preferably have as gas pressure-receiving surfaces on the radial wall areas at the rear subsequent conical rear part, the rear-end but is still located in front of the center of gravity of the arrowhead.
- the sabot segments may be made of steel or a light metal.
- the separating joints formed on the rear side between the sabot segments are preferably closed gas-tight by a vulcanizate layer.
- the radial wall portion of the sabot at its end facing away from the arrowhead end is provided at the rear with a sealing lip, preferably made of rubber ,
- the radial wall portions of the sabot are provided on the outside with a recess in which the front side a wedge-shaped segment ring with a segmented sabot
- the guide and sealing strip covers at least the wedge-shaped region of the segment ring facing it, and wherein the segment ring and the guide and sealing strip are selected such that in the rest position of the projectile arrangement of the outer diameter of the guide and sealing strip is smaller than or equal to the bullet caliber and the wedge-shaped portion of the segment ring presses the guide and sealing strip to the outside when firing the bullet assembly.
- the segment ring can be made of metal and the guide and sealing strip can be made of a suitable plastic.
- the radial wall areas of the sabot are provided with pocket-like depressions both on the front and rear sides, so that the sabot segments are radially offset from the projectile body by the front air pressure forces and rear propellant charge gas forces acting on them when the projectile arrangement has passed the corresponding weapon barrel mouth side.
- Tail and projectile body can consist of two parts, but also made of one part become.
- the center of gravity of the projectile must also be taken into account.
- a tail unit made of (light) aluminum reduces the tensile stress in the transmitting cross-section of the projectile body due to its light weight, but pushes the center of gravity of the projectile further forward.
- Fig.1 1 is a cartridge, which consists essentially of a cartridge case 2 and a projectile assembly 3, which is connected via a sleeve cover 4 with the cartridge case 2. It is in Fig.1 only the sleeve cover 4 facing end portion of the cartridge case 2 indicated.
- the projectile arrangement 3 comprises a projectile 5 with a subcaliber projectile body 6 and a rear side arranged on the projectile body 6 sub-caliber cone tail 7.
- the illustrated arrowhead 5 is a practice projectile, the projectile body 6 made of steel and its tail 7, for example an aluminum alloy.
- the single flange sabot 10 consists of three similar sabot segments 12-14 (FIG. Fig.2 ), each covering an angle of 120 ° in the circumferential direction and preferably made of steel.
- the single flange sabot 10 has an outwardly extending radial wall portion 15 over which the arrowhead 5 is supported on the inner surface of a corresponding weapon barrel (not shown).
- a conical rear part 16 adjoins the rear side, the rear end 17 of which is also arranged in front of the center of gravity 8 of the arrowhead 5.
- the radial wall portion 15 of the sabot 10 at its end facing away from the arrowhead 5 radial end rear side provided with a circumferential sealing lip 22 made of rubber to ensure that when firing the projectile assembly 3 in the corresponding barrel no propellant gases between the inner surface of the gun barrel and the gun tube side end of the radial wall portion 15 of the sabot 10 flow therethrough.
- the radial wall portion 15 of the sabot 10 is also provided on the outside with a recess 23 in which the front side of a metal wedge-shaped segment ring 24 with a segmented sabot 10 corresponding division and the rear side of a plastic existing circumferential guide and sealing tape 25 is inserted, which the wedge-shaped segment ring 24 at least covered on the rear side.
- the segment ring 24 and the guide and sealing strip 25 are selected such that in the in Fig.1 illustrated rest position of the projectile assembly 3, the outer diameter of the guide and sealing strip 25 is less than or equal to the bullet caliber. This ensures that the guide and sealing strip 25 does not hinder the loading or unloading process of the cartridge 1.
- the radial wall portion 15 of the sabot 10 has pocket-like recesses 26, 27 on both the front and the rear sides, so that the sabot segments 12-14 are approximately of the front air ram forces acting upon launch of the cartridge as well as the rear propellant charge gas forces acting on them parallel to the projectile body 6 of this radially lift off when the projectile assembly 3 has passed the mouth of the corresponding barrel.
- the receiving device 28 is preferably made of plastic and comprises an annular rear flange 29 whose outer diameter corresponds to the bullet caliber of the respective cartridge 1.
- the invention is not limited to the embodiment described above.
- the flange sabot and the arrowhead can also be connected to one another via a form-locking connection, for example a groove profile or a thread.
- a corresponding embodiment show the Figure 3 and 4 ,
- a projectile assembly 3 ' can be removed, in which the one-flange sabot 10' is connected via a groove profile 31 with the projectile body 6 'of the arrow projectile 5'.
- the outside of the conical front part 30 'of the receiving device 28' is connected via a plurality of evenly distributed over the circumference arranged rib-shaped struts 32 with the rear flange 29 '.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
Description
Die Erfindung betrifft eine Patrone, die aus einer Patronenhülse und einer Geschossanordnung besteht, welche über einen Hülsendeckel mit der Patronenhülse verbunden ist.The invention relates to a cartridge which consists of a cartridge case and a projectile assembly which is connected via a sleeve cover with the cartridge case.
Eine derartige Patrone ist beispielsweise aus der
Um bei Verwendung eines derartigen Einflansch-Treibkäfigs im Waffenrohr eine gute Zentrierung des gesamten Geschosses zu erhalten, wird in der
Sofern Pfeilgeschosse mit einem unterkalibrigen Leitwerk verwendet werden sollen, schlägt die
Aus der
Der Erfindung liegt die Aufgabe zugrunde, eine Patrone der eingangs erwähnten Art anzugeben, deren Geschossanordnung kostengünstiger herstellbar ist als vergleichbare Anordnungen.The invention has for its object to provide a cartridge of the type mentioned, whose bullet assembly is less expensive to produce than comparable arrangements.
Diese Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst. Weitere, besonders vorteilhafte Ausgestaltungen der Erfindung offenbaren die Unteransprüche.This object is achieved by the features of claim 1. Further, particularly advantageous embodiments of the invention disclose the dependent claims.
Die Erfindung beruht im Wesentlichen auf dem Gedanken, mit dem Hülsendeckel geschossseitig eine das Leitwerk des Pfeilgeschosses zentrierende und beim Abschuss der Patrone von dem Leitwerk abtrennbare Aufnahmeeinrichtung zu verbinden, welche einen ringförmigen Heckflansch umfasst, dessen Außendurchmesser dem Geschosskaliber der jeweiligen Patrone entspricht.The invention is based essentially on the idea to connect with the sleeve cover on the projectile side a centering of the tail of the arrow centering and detachable during firing of the cartridge from the tail receiving device which comprises an annular rear flange whose outer diameter corresponds to the bullet caliber of each cartridge.
Vorzugsweise besteht die Aufnahmeeinrichtung aus Kunststoff.Preferably, the receiving device consists of plastic.
Bei einer bevorzugten Ausführungsform der Erfindung, bei der das Pfeilgeschoss ein Kegelleitwerk besitzt, weist die Aufnahmeeinrichtung ein das Leitwerk umfassendes kegelförmiges Vorderteil auf, welches treibkäfigseitig vor dem Heckflansch angeordnet ist und mindestens in einem Teilbereich des Leitwerkes an diesem formschlüssig anliegt. Dabei kann die Außenseite des kegelförmigen Vorderteiles der Aufnahmeeinrichtung über mehrere, gleichmäßig über den Umfang verteilt angeordnete, rippenförmige Streben mit dem Heckflansch verbunden sein.In a preferred embodiment of the invention, in which the arrowed floor has a conical structure, the receiving device has a conical front part which comprises the tail unit, which is arranged in front of the rear flange on the friction cage side and engages in a form-fitting manner at least in a partial area of the tail unit. In this case, the outer side of the conical front part of the receiving device can be connected to the rear flange via a plurality of rib-shaped struts distributed uniformly over the circumference.
Der Einflansch-Treibkäfig kann vorzugsweise als Gasdruckaufnahmeflächen ein sich an die radialen Wandbereiche heckseitig anschließendes konusförmiges Heckteil aufweisen, dessen heckseitiges Ende aber noch vor dem Schwerpunkt des Pfeilgeschosses angeordnet ist.The one-flange sabot may preferably have as gas pressure-receiving surfaces on the radial wall areas at the rear subsequent conical rear part, the rear-end but is still located in front of the center of gravity of the arrowhead.
Die Treibkäfigsegmente können aus Stahl oder einem Leichtmetall bestehen.The sabot segments may be made of steel or a light metal.
Die zwischen den Treibkäfigsegmenten heckseitig gebildeten Trennfugen sind vorzugsweise durch eine Vulkanisatschicht gasdicht verschlossen.The separating joints formed on the rear side between the sabot segments are preferably closed gas-tight by a vulcanizate layer.
Um bei der Bewegung der Geschossanordnung nach Schussabgabe sicher zu vermeiden, dass Treibladungsgase rohrwandseitig an der Geschossanordnung vorbeiströmen, hat es sich als vorteilhaft erwiesen, wenn der radiale Wandbereich des Treibkäfigs an seinem dem Pfeilgeschoss abgewandten Ende heckseitig mit einer Dichtlippe, vorzugsweise aus Gummi, versehen ist.In order to reliably avoid the propellant charge gases passing tube wall side of the projectile assembly in the movement of the projectile assembly, it has proved to be advantageous if the radial wall portion of the sabot at its end facing away from the arrowhead end is provided at the rear with a sealing lip, preferably made of rubber ,
Um außerdem die Patrone laden zu können, ohne dass das üblicherweise an dem Treibkäfig am äußeren Umfang befestigte Führungs- und Dichtungsband den Ladevorgang behindert, sind die radialen Wandbereiche des Treibkäfigs außenseitig mit einer Ausnehmung versehen, in welcher vorderseitig ein keilförmiger Segmentring mit einer dem segmentierten Treibkäfig entsprechenden Teilung und heckseitig ein sich an den Segmentring anschließendes umlaufendes Führungs- und Dichtungsband eingelegt sind, wobei das Führungs- und Dichtungsband mindestens den ihm zugewandten keilförmigen Bereich des Segmentringes überdeckt, und wobei der Segmentring und das Führungs- und Dichtungsband derart gewählt sind, dass in der Ruheposition der Geschossanordnung der Außendurchmesser des Führungs- und Dichtungsbandes kleiner oder gleich dem Geschosskaliber ist und beim Abschuss der Geschossanordnung der keilförmige Bereich des Segmentringes das Führungs- und Dichtungsband nach außen drückt.In addition, in order to load the cartridge without the usually attached to the sabot at the outer periphery guide and sealing tape obstructs the loading process, the radial wall portions of the sabot are provided on the outside with a recess in which the front side a wedge-shaped segment ring with a segmented sabot The guide and sealing strip covers at least the wedge-shaped region of the segment ring facing it, and wherein the segment ring and the guide and sealing strip are selected such that in the rest position of the projectile arrangement of the outer diameter of the guide and sealing strip is smaller than or equal to the bullet caliber and the wedge-shaped portion of the segment ring presses the guide and sealing strip to the outside when firing the bullet assembly.
Der Segmentring kann dabei aus Metall und das Führungs- und Dichtungsband kann aus einem geeigneten Kunststoff bestehen.The segment ring can be made of metal and the guide and sealing strip can be made of a suitable plastic.
Als vorteilhaft hat es sich erwiesen, wenn die radialen Wandbereiche des Treibkäfigs sowohl vorder- wie heckseitig mit taschenförmigen Vertiefungen versehen sind, so dass die Treibkäfigsegmente durch die auf sie wirkenden vorderseitigen Luft-Staudruckkräfte und heckseitigen Treibladungsgaskräfte sich etwa parallel zu dem Geschosskörper von diesem radial abheben, wenn die Geschossanordnung das entsprechende Waffenrohr mündungsseitig passiert hat.It has proved to be advantageous if the radial wall areas of the sabot are provided with pocket-like depressions both on the front and rear sides, so that the sabot segments are radially offset from the projectile body by the front air pressure forces and rear propellant charge gas forces acting on them when the projectile arrangement has passed the corresponding weapon barrel mouth side.
Mit der vorliegenden Konstruktion wird sichergestellt, dass nach Abschuss eine genaue Führung des Pfeilgeschosses in dem entsprechenden Waffenrohr realisiert wird. Neben dem Kostengesichtspunkt wird auch die Problematik der Gewichtsgesichtspunkte berücksichtig und die Schnittstelle beispielsweise für eine 120 mm Munition beachtet. Leitwerk und Geschosskörper können aus zwei Teilen bestehen, aber auch aus einem Teil hergestellt werden. Für die Werkstoffauswahl gilt dabei, dass neben den Kräften im Abschussfall auch die Schwerpunktslage des Fluggeschosses zu berücksichtigen ist. So reduziert beispielsweise ein Leitwerk aus (leichtem) Aluminium durch sein leichtes Gewicht die Zug- Spannung im übertragenden Querschnitt des Geschosskörpers, schiebt aber den Schwerpunkt des Fluggeschosses weiter nach vorne.With the present construction it is ensured that after firing an accurate guidance of the arrow bullet is realized in the corresponding barrel. In addition to the cost aspect, the problem of weight considerations is taken into account and the interface is considered, for example, for a 120 mm ammunition. Tail and projectile body can consist of two parts, but also made of one part become. For the selection of materials, it applies that in addition to the forces in the event of firing, the center of gravity of the projectile must also be taken into account. For example, a tail unit made of (light) aluminum reduces the tensile stress in the transmitting cross-section of the projectile body due to its light weight, but pushes the center of gravity of the projectile further forward.
Weitere Einzelheiten und Vorteile der Erfindung ergeben sich aus den folgenden, anhand von Figuren erläuterten Ausführungsbeispielen. Es zeigen:
-
Fig.1 den Längsschnitt durch ein erstes Ausführungsbeispiel einer erfindungsgemäßen Patrone im Bereich deren Geschossanordnung; -
Fig.2 einen Querschnitt entlang der inFig.1 mit II-II bezeichneten Schnittlinie; -
Fig.3 den Längsschnitt durch ein zweites Ausführungsbeispiel einer erfindungsgemäßen Patrone im Bereich deren Geschossanordnung und -
Fig.4 eine perspektivische Ansicht der inFig.3 dargestellten Geschossanordnung mit daran befestigtem Hülsendeckel.
-
Fig.1 the longitudinal section through a first embodiment of a cartridge according to the invention in the region of the projectile arrangement; -
Fig.2 a cross section along inFig.1 II-II section line; -
Figure 3 the longitudinal section through a second embodiment of a cartridge according to the invention in the region of the projectile assembly and -
Figure 4 a perspective view of inFigure 3 shown bullet assembly with attached sleeve cover.
In
Die Geschossanordnung 3 umfasst ein Pfeilgeschoss 5 mit einem unterkalibrigen Geschosskörper 6 und einem heckseitig an dem Geschosskörper 6 angeordneten unterkalibrigen Kegel-Leitwerk 7. Bei dem dargestellten Pfeilgeschoss 5 handelt es sich um ein Übungsgeschoss, dessen Geschosskörper 6 aus Stahl und dessen Leitwerk 7 zum Beispiel aus einer Aluminiumlegierung besteht.The
Zwischen dem mit 8 bezeichneten Schwerpunkt des Geschosskörpers 6 und der Geschossspitze 9 des Pfeilgeschosses 5 ist ein durch Längsteilung segmentierter Einflansch-Treibkäfig 10 befestigt, wobei die Kraftübertragung zwischen dem Treibkäfig 10 und dem Geschosskörper 6 reibschlüssig mittels eines Kegelsitzes 11 erfolgt.Between the 8 designated center of gravity of the
Der Einflansch-Treibkäfig 10 besteht aus drei gleichartigen Treibkäfigsegmenten 12-14 (
Der Einflansch-Treibkäfig 10 weist einen sich nach außen erstreckenden radialen Wandbereich 15 auf, über den sich das Pfeilgeschoss 5 an der inneren Oberfläche eines entsprechenden Waffenrohres (nicht dargestellt) abstützt. An den radialen Wandbereich 15 schließt sich heckseitig ein konusförmiges Heckteil 16 an, dessen heckseitige Ende 17 ebenfalls noch vor dem Schwerpunkt 8 des Pfeilgeschosses 5 angeordnet ist.The
Die zwischen den Treibkäfigsegmenten 12-14 heckseitig gebildeten Trennfugen 18-20 (
Außerdem ist der radiale Wandbereich 15 des Treibkäfigs 10 an seinem dem Pfeilgeschoss 5 abgewandten radialen Ende heckseitig mit einer umlaufenden Dichtlippe 22 aus Gummi versehen, um sicherzustellen, dass beim Abschuss der Geschossanordnung 3 in dem entsprechenden Waffenrohr keine Treibladungsgase zwischen der inneren Oberfläche des Waffenrohres und dem waffenrohrseitigen Ende des radialen Wandbereiches 15 des Treibkäfigs 10 hindurchströmen.In addition, the
Der radiale Wandbereich 15 des Treibkäfigs 10 ist außerdem außenseitig mit einer Ausnehmung 23 versehen, in welcher vorderseitig ein aus Metall bestehender keilförmiger Segmentring 24 mit einer dem segmentierten Treibkäfig 10 entsprechenden Teilung und heckseitig ein aus Kunststoff bestehendes umlaufendes Führungs- und Dichtungsband 25 eingelegt ist, welches den keilförmigen Segmentring 24 mindestens heckseitig überdeckt. Dabei sind der Segmentring 24 und das Führungs- und Dichtungsband 25 derart gewählt, dass in der in
Hingegen werden beim Abschuss der Patrone 1 die Segmente des Segmentringes 24 mit ihren dem Führungs- und Dichtungsband 25 zugewandten keilförmigen Enden axial in Richtung zum Leitwerk 7 hin beschleunigt, und das Führungs- und Dichtungsband 25 weitet sich auf, so dass zusätzlich zu der durch die Dichtlippe 22 gewährleisteten Anfangsliderung eine weitere Dichtung gegen an der inneren Oberfläche des entsprechenden Waffenrohres entlang strömende Treibladungsgase erfolgt.By contrast, when the cartridge 1 is launched, the segments of the
Der radiale Wandbereich 15 des Treibkäfigs 10 weist sowohl vorder- wie heckseitig taschenförmige Vertiefungen 26, 27 auf, so dass die Treibkäfigsegmente 12-14 durch die beim Abschuss der Patrone auf sie wirkenden vorderseitigen Luft-Staudruckkräfte als auch durch die auf sie wirkenden heckseitigen Treibladungsgaskräfte etwa parallel zu dem Geschosskörper 6 von diesem radial abheben, wenn die Geschossanordnung 3 die Mündung des entsprechenden Waffenrohres passiert hat.The
Mit dem Hülsendeckel 4 der Patrone 1 ist geschossseitig eine das Leitwerk 7 des Pfeilgeschosses 5 zentrierende und beim Abschuss der Patrone 1 von dem Leitwerk 7 abtrennbare Aufnahmeeinrichtung 28 verbunden. Die Aufnahmeeinrichtung 28 besteht vorzugsweise aus Kunststoff und umfasst einen ringförmigen Heckflansch 29, dessen Außendurchmesser dem Geschosskaliber der jeweiligen Patrone 1 entspricht. An den Heckflansch 29 schließt sich treibkäfigseitig ein das Kegel-Leitwerk 7 des Pfeilgeschosses 5 umfassendes kegelförmiges Vorderteil 30 an, welches in einem Teilbereich des Leitwerkes 7 an diesem formschlüssig anliegt.With the
Die Erfindung ist selbstverständlich nicht auf das vorstehend beschriebene Ausführungsbeispiel beschränkt. So können der Einflansch-Treibkäfig und das Pfeilgeschoss beispielsweise auch über eine Formschlussverbindung, etwa einem Rillenprofil oder einem Gewinde, miteinander verbunden sein. Ein entsprechendes Ausführungsbeispiel zeigen die
Dabei ist den
- 11
- Patronecartridge
- 22
- Patronenhülsecartridge case
- 3,3'3,3 '
- Geschossanordnungenfloor arrangements
- 44
- Hülsendeckelcasing cover
- 5,5'5.5 '
- Pfeilgeschosseflechettes
- 6,6'6.6 '
- Geschosskörperprojectile body
- 77
- Leitwerk, Kegel-LeitwerkTail, cone tail
- 8,8'8,8 '
- Schwerpunktmain emphasis
- 99
- Geschossspitzebullet tip
- 10,10'10.10 '
- Treibkäfige, Einflansch-TreibkäfigeSower cages, one-flange sabots
- 1111
- Kegelsitzconical seat
- 12-1412-14
- TreibkäfigsegmenteSabot segments
- 1515
- radialer Wandbereichradial wall area
- 1616
- Heckteiltail section
- 1717
- heckseitiges Enderear end
- 18-2018-20
- Trennfugenjoints
- 2121
- VulkanisatschichtVulkanisatschicht
- 2222
- Dichtlippesealing lip
- 2323
- Ausnehmungrecess
- 2424
- Segmentringsegment ring
- 2525
- Führungs- und DichtungsbandGuide and sealing tape
- 26, 2726, 27
- taschenförmige Vertiefungenpocket-shaped depressions
- 28,28'28.28 '
- Aufnahmeeinrichtungenreception facilities
- 29,29'29.29 '
- HeckflanscheHeckflansche
- 30,30'30.30 '
- Vorderteilefronts
- 3131
- Rillenprofilgroove profile
- 3232
- Strebenpursuit
Claims (13)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009009776A DE102009009776A1 (en) | 2009-02-20 | 2009-02-20 | cartridge |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2221575A2 true EP2221575A2 (en) | 2010-08-25 |
EP2221575A3 EP2221575A3 (en) | 2013-07-24 |
EP2221575B1 EP2221575B1 (en) | 2014-03-05 |
Family
ID=41809084
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09015606.8A Not-in-force EP2221575B1 (en) | 2009-02-20 | 2009-12-17 | Cartridge |
Country Status (5)
Country | Link |
---|---|
US (1) | US8171854B2 (en) |
EP (1) | EP2221575B1 (en) |
KR (1) | KR20100095365A (en) |
DE (1) | DE102009009776A1 (en) |
ES (1) | ES2455199T3 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108654040A (en) * | 2018-05-21 | 2018-10-16 | 哈尔滨工业大学 | A kind of adaptive archery auxiliary training system |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10996037B2 (en) * | 2018-09-04 | 2021-05-04 | The United States Of America As Represented By The Secretary Of The Army | Obturator for robust and uniform discard |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1703507A1 (en) | 1968-05-31 | 1972-03-09 | Rheinmetall Gmbh | Propulsion cage for wing stabilized sub-caliber projectiles |
DE2747313C2 (en) | 1977-10-21 | 1983-01-20 | Rheinmetall GmbH, 4000 Düsseldorf | Sub-caliber arrow projectile with a resistance-stabilizing conical tail section |
DE3937665A1 (en) | 1989-11-11 | 1991-05-16 | Rheinmetall Gmbh | FLOOR ARRANGEMENT |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3978792A (en) * | 1975-04-25 | 1976-09-07 | The United States Of America As Represented By The Secretary Of The Army | Projectile-to-cartridge case attachment |
US4140061A (en) | 1977-06-06 | 1979-02-20 | The United States Of America As Represented By The Secretary Of The Army | Short-range discarding-sabot training practice round and self-destruct subprojectile therefor |
DE2844870C2 (en) * | 1978-10-14 | 1984-10-18 | Rheinmetall GmbH, 4000 Düsseldorf | Sub-caliber training projectile |
US4450770A (en) | 1980-09-22 | 1984-05-29 | The United States Of America As Represented By The Secretary Of The Army | Pivot ring for a discarding sabot |
US4444113A (en) | 1981-04-06 | 1984-04-24 | The United States Of America As Represented By The Secretary Of The Army | High-pressure self-sealing obturator in sabot discard projectile |
USH403H (en) * | 1987-05-07 | 1988-01-05 | The United States Of America As Represented By The Secretary Of The Army | Gun launched kinetic energy penetrator |
US7594472B1 (en) * | 1990-06-13 | 2009-09-29 | Qinetiq Limited | Sabot |
DE19748829C2 (en) * | 1997-11-05 | 2000-04-27 | Rheinmetall W & M Gmbh | Packaging container for large-caliber ammunition |
US6655293B1 (en) * | 2000-06-29 | 2003-12-02 | General Dynamics Ordnance And Tactical Systems, Inc. | Fin-stabilized ammunition |
FR2842896B1 (en) * | 2002-07-26 | 2004-10-22 | Giat Ind Sa | SEALING BELT FOR A PROJECTILE, PROJECTILE UNDER CALIBER AND AMMUNITION PROVIDED WITH SUCH A BELT |
FR2851038B1 (en) * | 2003-02-10 | 2005-03-18 | Giat Ind Sa | SABOT FOR PROJECTILE UNDER SIZE |
FR2854687B1 (en) * | 2003-05-09 | 2006-06-16 | Giat Ind Sa | SUB-CALIBER PROJECTILE, BAR AND SHAFT CONSTITUTING SUCH A PROJECTILE |
DE102007037738A1 (en) * | 2007-08-09 | 2009-02-12 | Rheinmetall Waffe Munition Gmbh | Projectile with a guide cage and pusher plate with acceleration-optimized opening |
US7934456B1 (en) * | 2008-11-20 | 2011-05-03 | Rheinmetall Waffe Munition Gmbh | Sabot projectile |
-
2009
- 2009-02-20 DE DE102009009776A patent/DE102009009776A1/en not_active Withdrawn
- 2009-12-17 EP EP09015606.8A patent/EP2221575B1/en not_active Not-in-force
- 2009-12-17 ES ES09015606.8T patent/ES2455199T3/en active Active
-
2010
- 2010-01-06 KR KR1020100000882A patent/KR20100095365A/en not_active Application Discontinuation
- 2010-02-19 US US12/709,411 patent/US8171854B2/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1703507A1 (en) | 1968-05-31 | 1972-03-09 | Rheinmetall Gmbh | Propulsion cage for wing stabilized sub-caliber projectiles |
DE2747313C2 (en) | 1977-10-21 | 1983-01-20 | Rheinmetall GmbH, 4000 Düsseldorf | Sub-caliber arrow projectile with a resistance-stabilizing conical tail section |
DE3937665A1 (en) | 1989-11-11 | 1991-05-16 | Rheinmetall Gmbh | FLOOR ARRANGEMENT |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108654040A (en) * | 2018-05-21 | 2018-10-16 | 哈尔滨工业大学 | A kind of adaptive archery auxiliary training system |
Also Published As
Publication number | Publication date |
---|---|
US8171854B2 (en) | 2012-05-08 |
DE102009009776A1 (en) | 2010-08-26 |
US20100236441A1 (en) | 2010-09-23 |
EP2221575B1 (en) | 2014-03-05 |
EP2221575A3 (en) | 2013-07-24 |
KR20100095365A (en) | 2010-08-30 |
ES2455199T3 (en) | 2014-04-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2221575B1 (en) | Cartridge | |
EP1475600B1 (en) | Discarding sabot | |
DE102012006892B3 (en) | Tail unit-stabilized full caliber-training projectile, has recesses formed between guiding elements for axial passage of propellant gases produced during firing of projectile, and sealing system arranged in solid head part | |
DE10157668B4 (en) | bullet | |
EP3317607B1 (en) | Fin-stabilized sub-calibre projectile which can be fired from a rifled barrel and method for the production thereof | |
EP2828609B1 (en) | Fin-stabilized full-calibre practice projectile | |
EP2834589B1 (en) | Fin-stabilized full-caliber training projectile, and method for producing same | |
EP2828607B1 (en) | Fin-stabilized full-calibre practice projectile | |
DE102013006498A1 (en) | Sabot projectile | |
DE19704489A1 (en) | Sub-caliber sabot bullet | |
EP2828606B1 (en) | Fin-stabilized full-calibre practice projectile | |
DE3934043C2 (en) | ||
DE3827830A1 (en) | Kinetic energy projectile | |
DE19933184C2 (en) | Sub-caliber floor | |
EP2191222B1 (en) | Gun barrel for launching spin-stabilized projectiles | |
DE10157667B4 (en) | Full-caliber bullet fired from a gun | |
DE102012006895B3 (en) | Control surface-stabilized full caliber-practice projectile has solid head portion and annular control surface body that is adjoined to rear side of head part, where practice projectile is circumferentially provided with sealing system | |
EP2828608A1 (en) | Fin-stabilized full-calibre practice projectile | |
DE10161726A1 (en) | Ammunition cartridge, especially for artillery or tanks, has sleeve shaped cover connecting combustible propellant charge case to rear side of shell inside case | |
DE10034345A1 (en) | Projectile for tube weapon comprises body, rear section, detonator area and guide bands | |
DE4023220A1 (en) | Sub-calibre projectile with sliding fin assembly - has guide sleeve between penetrator and thrust ring |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: AL BA RS |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: AL BA RS |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F42B 5/067 20060101ALN20130618BHEP Ipc: F42B 5/073 20060101AFI20130618BHEP Ipc: F42B 14/06 20060101ALN20130618BHEP |
|
17P | Request for examination filed |
Effective date: 20130809 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F42B 5/073 20060101AFI20130923BHEP Ipc: F42B 14/06 20060101ALN20130923BHEP Ipc: F42B 5/067 20060101ALN20130923BHEP |
|
INTG | Intention to grant announced |
Effective date: 20131011 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 655174 Country of ref document: AT Kind code of ref document: T Effective date: 20140315 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502009008909 Country of ref document: DE Effective date: 20140410 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2455199 Country of ref document: ES Kind code of ref document: T3 Effective date: 20140414 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: VDEP Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140605 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140705 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140605 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502009008909 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140707 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20141211 Year of fee payment: 6 Ref country code: ES Payment date: 20141226 Year of fee payment: 6 Ref country code: GB Payment date: 20141219 Year of fee payment: 6 |
|
26N | No opposition filed |
Effective date: 20141208 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20141219 Year of fee payment: 6 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502009008909 Country of ref document: DE Effective date: 20141208 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20141231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20141217 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20141231 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20141231 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20141217 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 655174 Country of ref document: AT Kind code of ref document: T Effective date: 20141217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20141217 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140606 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 502009008909 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20091217 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20151217 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20160831 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160701 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151231 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20170126 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151218 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20140305 |