EP1338860A2 - Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method - Google Patents
Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method Download PDFInfo
- Publication number
- EP1338860A2 EP1338860A2 EP02027327A EP02027327A EP1338860A2 EP 1338860 A2 EP1338860 A2 EP 1338860A2 EP 02027327 A EP02027327 A EP 02027327A EP 02027327 A EP02027327 A EP 02027327A EP 1338860 A2 EP1338860 A2 EP 1338860A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- explosive
- projectile
- charge
- interior
- plastic
- 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
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/204—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/208—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by a plurality of charges within a single high explosive warhead
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/0214—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by casting
Definitions
- the invention relates to a method for producing a large-caliber explosive projectile with a shell that contains an interior filled with an explosive charge encloses and has a mouth hole closable on the tip, through which the Explosive charge is brought into the interior of the explosive device.
- the invention also relates to an explosive projectile manufactured by this method is.
- insensitive explosive charges In many cases, defense technology uses insensitive explosive charges required. These are usually plastic-bound explosive charges, which have a relatively high insensitivity despite a high active power. Plastic-bound explosive charges, however, have the disadvantage that they are have relatively large coefficients of thermal expansion, which are eight to twelve times larger is like that of a steel shell made of a corresponding one Explosive projectile. In such a storey filled with explosives positive temperatures so that the explosive body in the shell is held while the explosive body is at lower temperatures contracts and then lies loosely in the shell.
- the invention has for its object a method for producing a large-caliber Specify explosive storey, even when using plastic-bound Explosive charges of the explosive bodies even with large temperature fluctuations is always kept under tension in the shell.
- the invention is essentially based on the idea that the explosive charge in one Arrange plastic cover made of an elastic material in the explosive storey, so that the changing volume of the explosive charge due to temperature fluctuations the elastic plastic cover is added. Because with large-caliber spin-stabilized Artillery shells generally only charge the corresponding explosive charge a front small mouth hole (head fuse holder) can be filled, it is not possible, explosive charges already packaged in plastic films in the interior to bring such an explosive device.
- the invention therefore proposes through the mouth hole only a folded or compressed, inserting a bag-shaped plastic cover into the interior of the explosive device, their dimensions in the unfolded state essentially the dimensions corresponds to the interior of the explosive device. Then the Plastic cover e.g.
- the pourable plastic-bound explosive charge also becomes inserted through the mouth hole in the plastic shell.
- the mouth hole is e.g. by screwing in a head detonator closed.
- the explosive body can be held under tension in the shell, it has proven to be Proven to provide additional clamping devices that are compared to the Compensate for the shell volume of the explosive charge.
- the plastic shell with the Inner wall of the interior of the explosive bullet glued at least in some areas become.
- the swirl transmission from the shell to the Explosives are promoted in that the walls of the interior at least in have a polygonal configuration in a partial area on the bottom.
- the plastic cover can be both a smooth film and one Trade roof film with which preformed after detonation of the explosive charge Splinters can be generated.
- annular sections are in the direction of Roof-shaped protrusions extending along the longitudinal axis of the explosive projectile provided, the roof-shaped protuberances of adjacent annular sections are offset from each other by half a roof.
- the igniter is followed by an amplifier charge is that on the side facing the explosive charge the contour of a shaped charge insert and if the shim has an axially extending central recess has, so that the resulting after ignition of the booster charge Hollow charge jet reaches the explosive charge unhindered. It can be the Contour of the shaped charge insert around both a flat and a pointed cone insert act.
- an ignition tube extends axially into the explosive charge, at whose the End of the compensating disc is arranged a lighting set.
- 1 denotes a large-caliber spin-stabilized explosive projectile, as is the case for example, can be fired from a self-propelled howitzer.
- the explosive storey 1 comprises a projectile casing 2 with a base part 3 and a front detonator 4.
- the head igniter 4 is screwed into an adapter part 17, which in turn is screwed into a mouth hole 5 of the shell 2.
- the shell 2 surrounds an interior 6, with the inner walls 7 a bag-shaped trained elastic (rubber-like) plastic sleeve 8 is glued, in which there is a plastic-bound explosive charge 9.
- the plastic shell 8 has thereby a smooth surface.
- the wall thickness of the plastic sleeve 8 is advantageously between 0.3 and 0.6 mm. It has also proven advantageous if a plastic with about 30% rubber content is used as the material for the plastic sleeve 8 becomes.
- the explosive charge 9 is closed off at the front by an elastic shim 11, on the side facing away from the explosive charge 9, the adapter part 17 a exerts predetermined pressure, so that the explosive charge 9 is under tension.
- the igniter 4 protrudes from the rear into the adapter part 17, which has an amplifier charge 12 comprises, on the side facing the explosive charge 9, the contour of a shaped charge insert 13 has.
- the shim 11 has an axially extending recess 14, so that after the ignition of the booster charge 12 resulting shaped charge jet passes through this recess 14 into the explosive charge 9 and ignite this charge.
- the explosive charge 9 into the explosive storey 1, first if necessary Glue applied to the inner walls 7 of the shell 2. Subsequently the plastic sleeve 8 is compressed such that it passes through the mouth hole 5 can slide into the interior 6. In the interior 6, the plastic sleeve 8 is due of the internal tensions again and lies on the inner walls 7 the shell 2. The explosive charge 9 can then be inserted into the plastic casing 8 introduced and the elastic shim 11 arranged on the explosive charge 9 become. Finally, the adapter part 17 is then screwed into the mouth hole 5 and then the head igniter 4 is connected to the adapter part 17.
- the invention is of course not based on the embodiment described above limited.
- the elastic shim marked there with 11 'needs itself do not extend over the entire cross section of the interior 6 'of the shell 2'.
- the adapter part 17 ' is in this case completely inside the shell 2 'and the head igniter 4' is screwed directly into the mouth hole 5 '.
- the explosive charge 9 ' can be used for rapid and uniform ignition Ignition tube 15 may be provided, which is located on the recess 14 'of the shim 11 'connects and extends axially into the explosive charge 9'.
- the ignition tube 15 has a firing set from the end facing away from the compensating disk 11 ' 16 on.
- a roof film can be used as a plastic cover instead of a smooth film be used.
- Such roof foils have adjacent ones in the axial direction ring-shaped sections with the direction of the longitudinal axis of the explosive device extending roof-shaped protuberances are provided, the roof-shaped Protrusions of adjacent annular sections each by half a roof to each other are staggered.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Manufacturing & Machinery (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Toys (AREA)
- Artificial Fish Reefs (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Soft Magnetic Materials (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
Description
Die Erfindung betrifft ein Verfahren zur Herstellung eines, großkalibrigen Sprenggeschosses mit einer Geschoßhülle, die einen mit einer Sprengladung gefüllten Innenraum umschließt und ein spitzenseitig verschließbares Mundloch aufweist, über welches die Sprengladung in den Innenraum des Sprenggeschosses eingebracht wird. Die Erfindung bezieht sich ferner auf ein Sprenggeschoß, welches nach diesem Verfahren hergestellt ist.The invention relates to a method for producing a large-caliber explosive projectile with a shell that contains an interior filled with an explosive charge encloses and has a mouth hole closable on the tip, through which the Explosive charge is brought into the interior of the explosive device. The invention also relates to an explosive projectile manufactured by this method is.
In vielen Fällen wird in der Wehrtechnik die Verarbeitung insensitiver Sprengladungen gefordert. Dabei handelt es sich in der Regel um kunststoffgebundene Sprengladungen, die trotz einer hohen Wirkleistung eine relativ hohe Unempfindlichkeit aufweisen. Kunststoffgebundene Sprengladungen weisen allerdings den Nachteil auf, daß sie einen relativ großen Wärmeausdehnungskoeffizienten,besitzen, der acht bis zwölfmal größer ist, wie etwa derjenige einer aus Stahl bestehenden Geschoßhülle eines entsprechenden Sprenggeschosses. In einem derartigen mit Sprengstoff gefüllten Geschoß treten bei positiven Temperaturen Spannungen auf, so daß der Sprengstoffkörper in der Geschoßhülle gehalten wird, während sich der Sprengstoffkörper bei niedrigeren Temperaturen zusammenzieht und dann lose in der Geschoßhülle liegt.In many cases, defense technology uses insensitive explosive charges required. These are usually plastic-bound explosive charges, which have a relatively high insensitivity despite a high active power. Plastic-bound explosive charges, however, have the disadvantage that they are have relatively large coefficients of thermal expansion, which are eight to twelve times larger is like that of a steel shell made of a corresponding one Explosive projectile. In such a storey filled with explosives positive temperatures so that the explosive body in the shell is held while the explosive body is at lower temperatures contracts and then lies loosely in the shell.
Der Erfindung liegt die Aufgabe zugrunde, ein Verfahren zur Herstellung eines großkalibrigen Sprenggeschosses anzugeben, bei dem auch bei Verwendung kunststoffgebundener Sprengladungen der Sprengstoffkörper selbst bei großen Temperaturschwankungen immer unter Vorspannung in der Geschoßhülle gehalten wird.The invention has for its object a method for producing a large-caliber Specify explosive storey, even when using plastic-bound Explosive charges of the explosive bodies even with large temperature fluctuations is always kept under tension in the shell.
Diese Aufgabe wird erfindungsgemäß hinsichtlich des Verfahrens durch die Merkmale
des Anspruchs 1 und hinsichtlich des Sprenggeschosses durch die Merkmale des Anspruchs
9 gelöst. Weitere, besonders vorteilhafte Ausgestaltungen der Erfindung offenbaren
die Unteransprüche.This object is achieved according to the invention by the features
of claim 1 and with regard to the explosive device by the features of the
Die Erfindung beruht im wesentlichen auf dem Gedanken, die Sprengladung in einer Kunststoffhülle aus einem elastischen Material in dem Sprenggeschoß anzuordnen, so daß bei Temperaturschwankungen das sich ändernde Volumen der Sprengladung durch die elastische Kunststoffhülle aufgenommen wird. Da bei großkalibrigen drallstabilisierten Artilleriegeschossen die entsprechende Sprengladung in der Regel lediglich über ein vorderes kleines Mundloch (Kopfzünderaufnahme) eingefüllt werden kann, ist es nicht möglich, bereits in Kunststoff-Folien verpackte Sprengladungen in den Innenraum eines derartigen Sprenggeschosses einzubringen. Die Erfindung schlägt daher vor, durch das Mundloch zunächst nur eine zusammengefaltete oder zusammengepreßte, sackförmig ausgebildete Kunststoffhülle in den Innenraum des Sprenggeschosses einzubringen, deren Abmessungen im entfalteten Zustand im wesentlichen den Abmessungen des Innenraumes des Sprenggeschosses entspricht. Anschließend wird dann die Kunststoffhülle z.B. durch Aufblasen oder aufgrund ihrer elastischen Rückstellkräfte entfaltet, so daß sie an den Innenwänden des Innenraumes des Sprenggeschosses formschlüssig anliegt. Dann wird die gießfähige kunststoffgebundene Sprengladung ebenfalls durch das Mundloch in die Kunststoffhülle eingebracht. Nach dem Auspolymerisieren des kunststoffgebundenen Sprengstoffes wird das Mundloch z.B. durch Einschrauben eines Kopfzünders verschlossen.The invention is essentially based on the idea that the explosive charge in one Arrange plastic cover made of an elastic material in the explosive storey, so that the changing volume of the explosive charge due to temperature fluctuations the elastic plastic cover is added. Because with large-caliber spin-stabilized Artillery shells generally only charge the corresponding explosive charge a front small mouth hole (head fuse holder) can be filled, it is not possible, explosive charges already packaged in plastic films in the interior to bring such an explosive device. The invention therefore proposes through the mouth hole only a folded or compressed, inserting a bag-shaped plastic cover into the interior of the explosive device, their dimensions in the unfolded state essentially the dimensions corresponds to the interior of the explosive device. Then the Plastic cover e.g. by inflation or due to their elastic restoring forces unfolded so that they form-fit on the inner walls of the interior of the explosive device is applied. Then the pourable plastic-bound explosive charge also becomes inserted through the mouth hole in the plastic shell. After polymerizing of the plastic-bound explosives, the mouth hole is e.g. by screwing in a head detonator closed.
Um zu erreichen, daß selbst bei großen Temperaturschwankungen der Sprengstoffkörper unter Vorspannung in der Geschoßhülle gehalten werden kann, hat es sich als zweckmäßig erwiesen, zusätzliche Spannmittel vorzusehen, die das sich gegenüber der Geschoßhülle ändernde Volumen der Sprengladung ausgleichen. To achieve that even with large temperature fluctuations, the explosive body can be held under tension in the shell, it has proven to be Proven to provide additional clamping devices that are compared to the Compensate for the shell volume of the explosive charge.
Dabei hat es sich als vorteilhaft erwiesen, wenn vor dem Verschließen des Mundloches eine elastische Ausgleichsscheibe auf der Sprengladung angeordnet wird, die beim Einschrauben des Kopfzünders oder eines mit dem Kopfzünder verbundenen Adapterteiles durch diese Teile etwas zusammengepreßt wird, so daß die Sprengladung ständig unter Vorspannung steht.It has proven to be advantageous if before closing the mouth hole an elastic shim is placed on the explosive charge when screwing in the igniter or an adapter part connected to the igniter something is pressed together by these parts, so that the explosive charge is constantly below Preload is there.
Um bei drallstabilisierten Sprenggeschossen eine gute Drallübertragung zwischen der Geschoßhülle und der Sprengladung sicherzustellen, kann die Kunststoffhülle mit der Innenwand des Innenraumes des Sprenggeschosses mindestens in Teilbereichen verklebt werden. Außerdem kann die Drallübertragung von der Geschoßhülle auf den Sprengstoff dadurch gefördert werden, daß die Wände des Innenraumes mindestens in einem bodenseitigen Teilbereich eine mehreckige Ausgestaltung aufweisen.In order to ensure good swirl transmission between the To ensure the projectile shell and the explosive charge, the plastic shell with the Inner wall of the interior of the explosive bullet glued at least in some areas become. In addition, the swirl transmission from the shell to the Explosives are promoted in that the walls of the interior at least in have a polygonal configuration in a partial area on the bottom.
Allerdings haben Versuche der Anmelderin ergeben, daß beim Abschuß des erfindungsgemäßen Sprenggeschosses auch ohne besondere Maßnahmen eine gute Drallübertragung zwischen der Geschoßhülle und einer kunststoffgebundenen Sprengladung erfolgt, weil die Sprengstoffmasse sich beim Abschuß aufgrund des Kunststoffanteiles verformt und sich zusammen mit der Kunststoffhülle in der Geschoßhülle "festsetzt".However, tests by the applicant have shown that when the inventive Explosive projectile good swirl transmission even without special measures between the shell and a plastic-bound explosive charge takes place because the explosive mass when fired due to the plastic portion deformed and "sticks" together with the plastic casing in the projectile casing.
Bei der Kunststoffhülle kann es sich sowohl um eine glatte Folie als auch um eine Dachfolie handeln, mit welcher nach der Detonation der Sprengladung vorgeformte Splitter erzeugt werden können. Hierzu sind ringförmige Abschnitte mit in Richtung der Längsachse des Sprenggeschosses sich erstreckenden dachförmigen Ausstülpungen vorgesehen, wobei die dachförmigen Ausstülpungen benachbarter ringförmiger Abschnitte jeweils um ein halbes Dach zueinander versetzt angeordnet sind.The plastic cover can be both a smooth film and one Trade roof film with which preformed after detonation of the explosive charge Splinters can be generated. For this purpose, annular sections are in the direction of Roof-shaped protrusions extending along the longitudinal axis of the explosive projectile provided, the roof-shaped protuberances of adjacent annular sections are offset from each other by half a roof.
Um ein schnelles und sicheres Durchzünden der Sprengladung zu gewährleisten, hat es sich als vorteilhaft erwiesen, wenn dem Zünder eine Verstärkerladung nachgeschaltet ist, die auf der der Sprengladung zugewandten Seite die Kontur einer Hohlladungseinlage besitzt, und wenn die Ausgleichsscheibe eine sich axial erstreckende zentrale Ausnehmung aufweist, so daß der nach dem Zünden der Verstärkerladung entstehende Hohlladungsstrahl ungehindert in die Sprengladung gelangt. Dabei kann es sich bei der Kontur der Hohlladungseinlage sowohl um eine Flach- wie um eine Spitzkegeleinlage handeln.It has to ensure a quick and safe detonation of the explosive charge proved to be advantageous if the igniter is followed by an amplifier charge is that on the side facing the explosive charge the contour of a shaped charge insert and if the shim has an axially extending central recess has, so that the resulting after ignition of the booster charge Hollow charge jet reaches the explosive charge unhindered. It can be the Contour of the shaped charge insert around both a flat and a pointed cone insert act.
Um den Durchzündvorgang weiter zu beschleunigen, ist bei einer weiteren Ausführungsform der Erfindung vorgesehen, daß sich an die zentrale Ausnehmung der Ausgleichsscheibe ein Anzündrohr axial in die Sprengladung hinein erstreckt, an dessen der Ausgleichsscheibe abgewandten Ende ein Anfeuerungssatz angeordnet ist.In order to accelerate the ignition process further, is in a further embodiment the invention provided that located on the central recess of the shim an ignition tube extends axially into the explosive charge, at whose the End of the compensating disc is arranged a lighting set.
Weitere Einzelheiten und Vorteile der Erfindung ergeben sich aus den folgenden anhand
von Figuren erläuterten Ausführungsbeispielen. Es zeigen:
In Fig.1 ist mit 1 ein großkalibriges drallstabilisiertes Sprenggeschoß bezeichnet, wie es
beispielsweise aus einer Panzerhaubitze verschossen werden kann. Das Sprenggeschoß
1 umfaßt eine Geschoßhülle 2 mit einem Bodenteil 3 und einem vorderseitigen Kopfzünder
4. Der Kopfzünder 4 ist in ein Adapterteil 17 eingeschraubt, welches seinerseits
in ein Mundloch 5 der Geschoßhülle 2 eingeschraubt ist.In FIG. 1, 1 denotes a large-caliber spin-stabilized explosive projectile, as is the case
for example, can be fired from a self-propelled howitzer. The explosive storey
1 comprises a
Die Geschoßhülle 2 umgibt einen Innenraum 6, mit dessen Innenwänden 7 eine sackförmig
ausgebildete elastische (gummiartige) Kunststoffhülle 8 verklebt ist, in welcher
sich eine kunststoffgebundene Sprengladung 9 befindet. Die Kunststoffhülle 8 weist
dabei eine glatte Oberfläche auf. Die Wanddicke der Kunststoffhülle 8 liegt vorteilhafterweise
zwischen 0,3 und 0,6 mm. Außerdem hat es sich als vorteilhaft erwiesen, wenn
als Material für die Kunststoffhülle 8 ein Kunststoff mit ca. 30% Gummianteil verwendet
wird.The
Im bodenteilseitigen Bereich 10 des Sprenggeschosses 1 weisen die Geschoßhülle 2 und
die Kunststoffhülle 8 zur Sicherstellung einer guten Drallübertragung von der Geschoßhülle
2 auf die Sprengladung 9 eine mehreckige Ausgestaltung auf (Fig.2).In the
Vorderseitig ist die Sprengladung 9 durch eine elastische Ausgleichsscheibe 11 abgeschlossen,
auf deren der Sprengladung 9 abgewandten Seite das Adapterteil 17 einen
vorgebbaren Druck ausübt, so daß die Sprengladung 9 unter Vorspannung steht.The
Der Kopfzünder 4 ragt heckseitig in das Adapterteil 17, welches eine Verstärkerladung
12 umfaßt, die auf der der Sprengladung 9 zugewandten Seite die Kontur einer Hohlladungseinlage
13 aufweist. Außerdem besitzt die Ausgleichsscheibe 11 eine sich axial
erstreckende Ausnehmung 14, so daß nach dem Zünden der Verstärkerladung 12 der
entstehende Hohlladungsstrahl durch diese Ausnehmung 14 in die Sprengladung 9 gelangt
und diese Ladung anzündet.The
Zum Einlaborieren der Sprengladung 9 in das Sprenggeschoß 1 wird bei Bedarf zunächst
Kleber auf die Innenwände 7 der Geschoßhülle 2 aufgebracht. Anschließend
wird die Kunststoffhülle 8 derart zusammengedrückt, daß sie sich durch das Mundloch
5 in den Innenraum 6 schieben läßt. In dem Innenraum 6 geht die Kunststoffhülle 8 aufgrund
der inneren Spannungen von selbst wieder auf und legt sich an die Innenwände 7
der Geschoßhülle 2 an. Daraufhin kann die Sprengladung 9 in die Kunststoffhülle 8
eingebracht und die elastische Ausgleichsscheibe 11 auf der Sprengladung 9 angeordnet
werden. Abschließend wird dann zunächst das Adapterteil 17 in das Mundloch 5 eingeschraubt
und anschließend der Kopfzünder 4 mit dem Adapterteil 17 verbunden.To incorporate the
Die Erfindung ist selbstverständlich nicht auf das vorstehend beschriebene Ausführungsbeispiel beschränkt. Wie aus dem in Fig.3 dargestellten Sprenggeschoß 1' entnehmbar ist, braucht die dort mit 11' gekennzeichnete elastische Ausgleichsscheibe sich nicht über den gesamten Querschnitt des Innenraumes 6' der Geschoßhülle 2' erstrekken. Das Adapterteil 17' befindet sich in diesem Fall vollständig innerhalb der Geschoßhülle 2'und der Kopfzünder 4' ist direkt in das Mundloch 5' eingeschraubt.The invention is of course not based on the embodiment described above limited. As can be seen from the explosive projectile 1 'shown in FIG is, the elastic shim marked there with 11 'needs itself do not extend over the entire cross section of the interior 6 'of the shell 2'. The adapter part 17 'is in this case completely inside the shell 2 'and the head igniter 4' is screwed directly into the mouth hole 5 '.
Außerdem kann zur schnellen und gleichmäßigen Anzündung der Sprengladung 9' ein
Anzündrohr 15 vorgesehen sein, welches sich an die Ausnehmung 14' der Ausgleichsscheibe
11' anschließt und sich axial in die Sprengladung 9' hinein erstreckt. An dem
der Ausgleichsscheibe 11' abgewandten Ende weist das Anzündrohr 15 einen Anfeuerungssatz
16 auf.In addition, the explosive charge 9 'can be used for rapid and uniform
Sofern bei der Detonation des Sprenggeschosses auf einfache Weise vorgeformte Splitter erzeugt werden sollen, kann als Kunststoffhülle statt einer glatten Folie eine Dachfolie verwendet werden. Derartige Dachfolien weisen in axialer Richtung benachbarte ringförmige Abschnitte auf, die mit in Richtung der Längsachse des Sprenggeschosses sich erstreckende dachförmige Ausstülpungen versehen sind, wobei die dachförmigen Ausstülpungen benachbarter ringförmiger Abschnitte jeweils um ein halbes Dach zueinander versetzt angeordnet sind. Provided preformed fragments in a simple manner when detonating the explosive device should be generated, a roof film can be used as a plastic cover instead of a smooth film be used. Such roof foils have adjacent ones in the axial direction ring-shaped sections with the direction of the longitudinal axis of the explosive device extending roof-shaped protuberances are provided, the roof-shaped Protrusions of adjacent annular sections each by half a roof to each other are staggered.
- 1, 1'1, 1 '
- Sprenggeschoßexplosive projectile
- 2,2'2,2 '
- Geschoßhülleprojectile casing
- 33
- Bodenteilthe bottom part
- 4,4'4,4 '
- Kopfzündernose fuse
- 5,5'5.5 '
- MundlochMundloch
- 6,6'6.6 '
- Innenrauminner space
- 77
- Innenwändeinterior walls
- 88th
- KunststoffhüllePlastic sheath
- 9,9'9.9 '
- Sprengladungexplosive charge
- 1010
- BereichArea
- 11,11'11.11 '
- Ausgleichsscheibe, SpannmittelShim, clamping device
- 1212
- Verstärkerladungbooster charge
- 1313
- HohlladungseinlageShaped charge liner
- 14,14'14.14 '
- Ausnehmungrecess
- 1515
- Anzündrohrignition tube
- 1616
- AnfeuerungssatzAnfeuerungssatz
- 17,17'17.17 '
- Adapterteil, SpannmittelAdapter part, clamping device
Claims (15)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10207209 | 2002-02-21 | ||
DE10207209A DE10207209A1 (en) | 2002-02-21 | 2002-02-21 | Process for producing a large-caliber explosive projectile and an explosive projectile produced by this process |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1338860A2 true EP1338860A2 (en) | 2003-08-27 |
EP1338860A3 EP1338860A3 (en) | 2004-03-17 |
EP1338860B1 EP1338860B1 (en) | 2005-08-24 |
Family
ID=7713877
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02027327A Expired - Lifetime EP1338860B1 (en) | 2002-02-21 | 2002-12-07 | Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method |
Country Status (7)
Country | Link |
---|---|
US (2) | US6860185B2 (en) |
EP (1) | EP1338860B1 (en) |
AT (1) | ATE302934T1 (en) |
DE (2) | DE10207209A1 (en) |
ES (1) | ES2247254T3 (en) |
IL (1) | IL154424A0 (en) |
NO (1) | NO325786B1 (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1363102A2 (en) * | 2002-05-16 | 2003-11-19 | Diehl Munitionssysteme GmbH & Co. KG | Warhead |
FR2862378A1 (en) * | 2003-11-17 | 2005-05-20 | Giat Ind Sa | Explosive shell, has washer with outer diameter lower than inner diameter of opening of envelope and allowing friction of connecting unit, where washer and unit constitute compression unit for ring |
WO2008011969A1 (en) * | 2006-07-25 | 2008-01-31 | Rheinmetall Waffe Munition Gmbh | Liner |
WO2009103408A1 (en) * | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile |
WO2009103409A1 (en) * | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile and method for the production thereof |
EP1485669B1 (en) * | 2002-03-11 | 2011-06-15 | BAE Systems PLC | Ordnance with explosives liner and method of manufacture of the ordnance |
RU2450235C2 (en) * | 2010-07-12 | 2012-05-10 | Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" - ФГУП "РФЯЦ-ВНИИЭФ" | Explosive assembly with plastisol explosive |
US8601950B2 (en) | 2009-05-25 | 2013-12-10 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile, and an explosive projectile produced using this method |
EP3091329A1 (en) | 2015-05-08 | 2016-11-09 | Diehl BGT Defence GmbH & Co. Kg | Method for producing a load for an explosive projectile |
EP3267143A1 (en) * | 2016-07-09 | 2018-01-10 | Diehl Defence GmbH & Co. KG | Bullet |
DE102018108766A1 (en) | 2018-04-12 | 2019-10-17 | Rheinmetall Waffe Munition Gmbh | explosive projectile |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10312717B4 (en) * | 2003-03-21 | 2008-04-30 | Rheinmetall Waffe Munition Gmbh | Wing-stabilized full-caliber explosive projectile |
EP2054695A4 (en) * | 2006-08-25 | 2013-01-23 | Blake K Thomas | Reduced collateral damage bomb (rcdb) and system and method of making same |
WO2008118235A2 (en) * | 2006-12-20 | 2008-10-02 | Ruhlman James D | Reduced collateral damage bomb (rcdb) including fuse system with shaped charges and a system and method of making same |
US7886667B1 (en) * | 2008-10-15 | 2011-02-15 | The United States Of America As Represented By The Secretary Of The Army | More safe insensitive munition for producing a controlled fragmentation pattern |
DE102012000011A1 (en) | 2012-01-02 | 2013-07-04 | Rheinmetall Waffe Munition Gmbh | Spin-stabilized explosive projectile |
CN102865780A (en) * | 2012-10-15 | 2013-01-09 | 北京吉保中试工程技术研究所有限公司 | Bottom-concave shrapnel of howitzer |
RU2531643C1 (en) * | 2013-05-29 | 2014-10-27 | Открытое акционерное общество "Федеральный научно-производственный центр "Научно-исследовательский институт прикладной химии" | Artillery cartridge |
AU2014310465B2 (en) * | 2013-08-20 | 2017-12-14 | Bae Systems Plc | Common carrier munition |
EP3036498B1 (en) | 2013-08-20 | 2017-06-07 | BAE Systems PLC | Smoke payload apparatus |
US9784544B2 (en) * | 2013-08-20 | 2017-10-10 | Bae Systems Plc | Frangible munition |
WO2015025145A1 (en) | 2013-08-20 | 2015-02-26 | Bae Systems Plc | Illumination munition |
DE102013014665B3 (en) * | 2013-08-29 | 2014-04-30 | Bundesrepublik Deutschland, vertreten durch das BMVg, vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr | Explosive projectile has auger that is inserted into the explosive charge in the direction of the projectile axis, and head igniter that is fixed with auger |
DE102014103105B3 (en) * | 2014-03-07 | 2014-12-04 | Rheinmetall Waffe Munition Gmbh | Method and production of a large caliber warhead and warhead produced by this method |
US9759533B2 (en) | 2015-03-02 | 2017-09-12 | Nostromo Holdings, Llc | Low collateral damage bi-modal warhead assembly |
WO2019083819A1 (en) * | 2017-10-26 | 2019-05-02 | Spectra Technologies Llc | Explosive ordnance cold assembly process |
US9946159B2 (en) | 2016-03-29 | 2018-04-17 | The United States Of America As Represented By The Secretary Of The Army | Lithographic fragmentation technology |
FR3089621B1 (en) * | 2018-12-07 | 2022-04-01 | Nexter Munitions | PIERCING MILITARY HEAD |
RU2720141C1 (en) * | 2019-02-26 | 2020-04-24 | Акционерное общество "Федеральный научно-производственный центр "Научно-исследовательский институт прикладной химии" | Ammunition of reinforced high-explosive fragmentation or high-explosive action |
CN114440724A (en) * | 2022-01-12 | 2022-05-06 | 南京理工大学 | Bullet detonator connects spiral shell structure that is favorable to detonator after-misfire explosive safety processing |
GB2620736A (en) * | 2022-07-18 | 2024-01-24 | Bae Systems Plc | Common carrier munition |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2373883A (en) * | 1942-10-30 | 1945-04-17 | Clyde B Ferrel | Shell structure |
GB1212116A (en) * | 1968-01-25 | 1970-11-11 | Oerlikon Buehrle Ag | Fragmentation shell |
GB1439450A (en) * | 1974-02-08 | 1976-06-16 | Hesselgren K E | Method and device for filling a casing with particulate matter |
US4365556A (en) * | 1980-10-06 | 1982-12-28 | The United States Of America As Represented By The Secretary Of The Army | Method and system for preventing base separation of cast explosives in projectiles |
DE3929020A1 (en) * | 1989-09-01 | 1991-03-21 | Diehl Gmbh & Co | Detonator for shell - which hollow charge booster and plastic shock absorber ring |
DE19648355A1 (en) * | 1996-11-22 | 1999-07-15 | Diehl Stiftung & Co | Artillery shell for shrapnel production |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2279416A (en) * | 1939-03-18 | 1942-04-14 | Trojan Powder Co | Exudate trap for shells |
US2276110A (en) * | 1939-03-18 | 1942-03-10 | Trojan Powder Co | Explosive missile |
US3000309A (en) * | 1943-01-30 | 1961-09-19 | Zapf Louis | Fragmentation projectile |
US4112849A (en) * | 1949-02-11 | 1978-09-12 | California Institute Research Foundation | Smokeless slow burning cast propellant |
US3218975A (en) * | 1950-06-28 | 1965-11-23 | Mark F Massey | Shaped charge liner |
US3491694A (en) * | 1954-06-08 | 1970-01-27 | Us Navy | Plastic liners for controlled fragmentation |
US3599570A (en) * | 1969-08-28 | 1971-08-17 | Thiokol Chemical Corp | Ammunition antidefuzing device |
FR2240427B1 (en) * | 1973-08-09 | 1976-11-19 | Thomson Brandt | |
US3967527A (en) * | 1975-07-11 | 1976-07-06 | The United States Of America As Represented By The Secretary Of The Army | Method of producing a cavity in the bursting charge of a high explosive projectile |
NO138610C (en) * | 1976-08-24 | 1978-10-04 | Raufoss Ammunisjonsfabrikker | PROJECTIL FOR DISTRIBUTION OF PRODUCED LOAD AND PROCEDURE IN MANUFACTURING THE PROJECTILE |
US4152987A (en) * | 1977-02-18 | 1979-05-08 | The United States Of America As Represented By The Secretary Of The Navy | Impermeable polymer bomb liner for use with TNT containing explosives |
US4395934A (en) * | 1980-04-21 | 1983-08-02 | The United States Of America As Represented By The Secretary Of The Army | Wear reducer |
US4369711A (en) * | 1980-11-24 | 1983-01-25 | Harold Leader | Bag for explosives with lower reinforcing sleeves |
US4461214A (en) * | 1982-06-24 | 1984-07-24 | The United States Of America As Represented By The Secretary Of The Navy | Cartridge loaded hybrid propellant |
US4438700A (en) * | 1982-07-19 | 1984-03-27 | The United States Of America As Represented By The Secretary Of The Army | White smoke spotting composition for training ammunition |
FR2534369B1 (en) * | 1982-10-08 | 1987-03-20 | Brandt Francois | PERFORATING EXPLOSIVE PROJECTILE IN CARTRIDGE |
IT1177199B (en) * | 1984-11-14 | 1987-08-26 | Simmel Spa | SUPPORTING BODY FOR ARTILLERY PROJECTS WITH INTERNAL DISCHARGE AND FILLING SECTORS |
AU602870B2 (en) * | 1985-10-22 | 1990-11-01 | Bae Systems Plc | Explosive projectiles |
IN169266B (en) * | 1985-10-22 | 1991-09-21 | Royal Ordnance Plc | |
NO158898C (en) * | 1986-05-29 | 1988-11-09 | Raufoss Ammunisjonsfabrikker | Projectile. |
US4833994A (en) * | 1988-01-14 | 1989-05-30 | Honeywell, Inc. | Dual purpose explosive lead for a projectile having a shaped charge warhead |
US5054399A (en) * | 1988-07-05 | 1991-10-08 | The United States Of America As Represented By The Secretary Of The Air Force | Bomb or ordnance with internal shock attenuation barrier |
US5133259A (en) * | 1990-05-23 | 1992-07-28 | Olin Corporation | Seal ring for pyrotechnically initiated projectile |
US5313890A (en) * | 1991-04-29 | 1994-05-24 | Hughes Missile Systems Company | Fragmentation warhead device |
DE4123649C2 (en) * | 1991-07-17 | 1993-11-11 | Rheinmetall Gmbh | Ejection device |
FR2683310B1 (en) * | 1991-11-06 | 1993-12-31 | Giat Industries | DEVICE FOR EJECTING USEFUL LOAD ELEMENTS OUTSIDE THE SHELL OF A CARGO SHELL. |
US5337673A (en) * | 1993-12-17 | 1994-08-16 | The United States Of America As Represented By The Secretary Of The Navy | Controlled fragmentation warhead case |
US5939662A (en) * | 1997-12-03 | 1999-08-17 | Raytheon Company | Missile warhead design |
US6283037B1 (en) * | 1999-12-20 | 2001-09-04 | Procopio J. Sclafani | Non-lethal shot-gun round |
US6655294B1 (en) * | 2002-01-21 | 2003-12-02 | James T. Kerr | Ammunition for a less-lethal projectile |
-
2002
- 2002-02-21 DE DE10207209A patent/DE10207209A1/en not_active Withdrawn
- 2002-12-07 EP EP02027327A patent/EP1338860B1/en not_active Expired - Lifetime
- 2002-12-07 ES ES02027327T patent/ES2247254T3/en not_active Expired - Lifetime
- 2002-12-07 AT AT02027327T patent/ATE302934T1/en active
- 2002-12-07 DE DE50204016T patent/DE50204016D1/en not_active Expired - Lifetime
- 2002-12-10 NO NO20025914A patent/NO325786B1/en not_active IP Right Cessation
-
2003
- 2003-02-12 IL IL15442403A patent/IL154424A0/en unknown
- 2003-02-21 US US10/369,774 patent/US6860185B2/en not_active Expired - Lifetime
-
2004
- 2004-09-30 US US10/953,190 patent/US7114449B2/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2373883A (en) * | 1942-10-30 | 1945-04-17 | Clyde B Ferrel | Shell structure |
GB1212116A (en) * | 1968-01-25 | 1970-11-11 | Oerlikon Buehrle Ag | Fragmentation shell |
GB1439450A (en) * | 1974-02-08 | 1976-06-16 | Hesselgren K E | Method and device for filling a casing with particulate matter |
US4365556A (en) * | 1980-10-06 | 1982-12-28 | The United States Of America As Represented By The Secretary Of The Army | Method and system for preventing base separation of cast explosives in projectiles |
DE3929020A1 (en) * | 1989-09-01 | 1991-03-21 | Diehl Gmbh & Co | Detonator for shell - which hollow charge booster and plastic shock absorber ring |
DE19648355A1 (en) * | 1996-11-22 | 1999-07-15 | Diehl Stiftung & Co | Artillery shell for shrapnel production |
Cited By (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1485669B1 (en) * | 2002-03-11 | 2011-06-15 | BAE Systems PLC | Ordnance with explosives liner and method of manufacture of the ordnance |
EP1363102A3 (en) * | 2002-05-16 | 2004-10-20 | Diehl Munitionssysteme GmbH & Co. KG | Warhead |
EP1363102A2 (en) * | 2002-05-16 | 2003-11-19 | Diehl Munitionssysteme GmbH & Co. KG | Warhead |
AU2004226912B2 (en) * | 2003-11-17 | 2010-01-14 | Giat Industries | Explosive shells |
FR2862378A1 (en) * | 2003-11-17 | 2005-05-20 | Giat Ind Sa | Explosive shell, has washer with outer diameter lower than inner diameter of opening of envelope and allowing friction of connecting unit, where washer and unit constitute compression unit for ring |
EP1533590A1 (en) * | 2003-11-17 | 2005-05-25 | Giat Industries | Explosive ammuniton with increased resistance against shocks |
US7174834B2 (en) | 2003-11-17 | 2007-02-13 | Giat Industries | Explosive shell having improved resistance to shocks |
NO338258B1 (en) * | 2003-11-17 | 2016-08-08 | Nexter Munitions | Explosive grenade with good support tolerance |
AU2004226912B8 (en) * | 2003-11-17 | 2010-05-06 | Giat Industries | Explosive shells |
WO2008011969A1 (en) * | 2006-07-25 | 2008-01-31 | Rheinmetall Waffe Munition Gmbh | Liner |
US8408138B2 (en) | 2006-07-25 | 2013-04-02 | Rheinmetall Waffe Munition Gmbh | Liner |
WO2009103408A1 (en) * | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile |
WO2009103409A1 (en) * | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile and method for the production thereof |
DE102008010706A1 (en) | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | explosive projectile |
DE102008010707A1 (en) | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile and method for its production |
US8601950B2 (en) | 2009-05-25 | 2013-12-10 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile, and an explosive projectile produced using this method |
US8739671B2 (en) | 2009-05-25 | 2014-06-03 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile |
RU2450235C2 (en) * | 2010-07-12 | 2012-05-10 | Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" - ФГУП "РФЯЦ-ВНИИЭФ" | Explosive assembly with plastisol explosive |
EP3091329A1 (en) | 2015-05-08 | 2016-11-09 | Diehl BGT Defence GmbH & Co. Kg | Method for producing a load for an explosive projectile |
EP3267143A1 (en) * | 2016-07-09 | 2018-01-10 | Diehl Defence GmbH & Co. KG | Bullet |
EP3267143B1 (en) | 2016-07-09 | 2019-03-06 | Diehl Defence GmbH & Co. KG | Bullet |
DE102018108766A1 (en) | 2018-04-12 | 2019-10-17 | Rheinmetall Waffe Munition Gmbh | explosive projectile |
WO2019197095A1 (en) | 2018-04-12 | 2019-10-17 | Rheinmetall Waffe Munition Gmbh | Explosive projectile |
Also Published As
Publication number | Publication date |
---|---|
DE10207209A1 (en) | 2003-09-11 |
EP1338860A3 (en) | 2004-03-17 |
ES2247254T3 (en) | 2006-03-01 |
NO20025914L (en) | 2003-08-22 |
EP1338860B1 (en) | 2005-08-24 |
US7114449B2 (en) | 2006-10-03 |
NO325786B1 (en) | 2008-07-14 |
US20060011053A1 (en) | 2006-01-19 |
US20040031380A1 (en) | 2004-02-19 |
US6860185B2 (en) | 2005-03-01 |
NO20025914D0 (en) | 2002-12-10 |
IL154424A0 (en) | 2003-09-17 |
DE50204016D1 (en) | 2005-09-29 |
ATE302934T1 (en) | 2005-09-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1338860A2 (en) | Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method | |
EP0215042B1 (en) | Cartridged ammunition | |
DE2265398B1 (en) | cartridge | |
DE69915427T2 (en) | Ammo cartridge with its propellant charge configuration | |
WO2010145734A1 (en) | Method for producing a large-calibre explosive projectile, and an explosive projectile produced using this method | |
DE3048617A1 (en) | COMBAT HEAD WITH SECONDARY BODIES AS A PAYLOAD | |
DE2105295C1 (en) | Powder body for caseless ammunition | |
DE2826497A1 (en) | DRIVING MIRROR FLOOR WITH PYROTECHNICAL SET | |
EP0158121A2 (en) | Cartridge ammunition for barrel weapons | |
DE60022509T2 (en) | DEVICE FOR SHOOTING SHOTS FROM A ROCKET | |
DE60104950T2 (en) | LIGHT TUBE FOR ARTILLERIEMUNITION | |
EP2245419B1 (en) | Explosive projectile and method for the production thereof | |
DE3918005C2 (en) | ||
EP0600385B1 (en) | Igniter for propulsive charge | |
EP0345420A1 (en) | Missile with a propulsive charge | |
DE3048595A1 (en) | Warhead for screening or radar deception - has internal bursting tube, surrounded by smoke sections with outer strip packing | |
DE102018008106B4 (en) | Bullet with a leader band arrangement | |
DE102020127053A1 (en) | Cartridge case for centerfire ammunition and centerfire ammunition | |
DE102007037699B4 (en) | Method for connecting the sleeve cover arranged on a projectile to the sleeve jacket of a cartridge | |
EP3137845A1 (en) | Cartridge with safety fuse in the drive system, and method for producing it | |
DE4336808C2 (en) | Test projectile for displaying the ignition function of a projectile | |
DE2920135A1 (en) | Fuse, delay charge or detonator igniter - with airtight encapsulated large calibre primer of reduced charge wt. ensuring ignition with simple construction | |
DE58322C (en) | Process for hurling projectiles which are filled with liquefied gases to be detonated, as well as cartridge cases and projectiles produced according to this process | |
DE19944379A1 (en) | Cartridge, comprises a sleeve with a front guide and a rear guide, rigidly fixed fins, a cover and at least one base opening. | |
DE3521184A1 (en) | Ejected smoke generator |
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 |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK RO |
|
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 IE IT LI LU MC NL PT SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK RO |
|
17P | Request for examination filed |
Effective date: 20040203 |
|
17Q | First examination report despatched |
Effective date: 20040524 |
|
AKX | Designation fees paid |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SI SK TR |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: RHEINMETALL WAFFE MUNITION GMBH |
|
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 IE IT LI LU MC NL PT SE SI SK TR |
|
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: 20050824 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: 20050824 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: 20050824 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: 20050824 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: 20050824 Ref country code: IE 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: 20050824 |
|
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: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20050824 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REF | Corresponds to: |
Ref document number: 50204016 Country of ref document: DE Date of ref document: 20050929 Kind code of ref document: P |
|
REG | Reference to a national code |
Ref country code: GR Ref legal event code: EP Ref document number: 20050402968 Country of ref document: GR |
|
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: 20051124 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: 20051124 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: OK PAT AG PATENTE MARKEN LIZENZEN |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20051207 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20051231 Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20051231 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20051231 |
|
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: 20060124 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2247254 Country of ref document: ES Kind code of ref document: T3 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
ET | Fr: translation filed | ||
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 |
|
26N | No opposition filed |
Effective date: 20060526 |
|
BERE | Be: lapsed |
Owner name: RHEINMETALL WAFFE MUNITION G.M.B.H. Effective date: 20051231 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20141219 Year of fee payment: 13 Ref country code: CH Payment date: 20141219 Year of fee payment: 13 Ref country code: ES Payment date: 20141226 Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151208 |
|
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: 20151231 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151231 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20170303 |
|
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: 20151208 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 16 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R084 Ref document number: 50204016 Country of ref document: DE |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: TR Payment date: 20191205 Year of fee payment: 18 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20201211 Year of fee payment: 19 Ref country code: FR Payment date: 20201223 Year of fee payment: 19 Ref country code: AT Payment date: 20201222 Year of fee payment: 19 Ref country code: GR Payment date: 20201222 Year of fee payment: 19 Ref country code: GB Payment date: 20201223 Year of fee payment: 19 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20201221 Year of fee payment: 19 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20201224 Year of fee payment: 19 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50204016 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MM Effective date: 20220101 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 302934 Country of ref document: AT Kind code of ref document: T Effective date: 20211207 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20211207 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220101 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20220706 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211207 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220701 Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20211207 |
|
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: 20211231 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20211207 |