EP0763705B1 - Secondary projectile for a tandem warhead - Google Patents
Secondary projectile for a tandem warhead Download PDFInfo
- Publication number
- EP0763705B1 EP0763705B1 EP96114074A EP96114074A EP0763705B1 EP 0763705 B1 EP0763705 B1 EP 0763705B1 EP 96114074 A EP96114074 A EP 96114074A EP 96114074 A EP96114074 A EP 96114074A EP 0763705 B1 EP0763705 B1 EP 0763705B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- charge
- explosive
- ignition
- active charge
- poles
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
-
- 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
- F42B12/22—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 with fragmentation-hull construction
- F42B12/32—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 with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge
Definitions
- the invention relates to a secondary floor for a tandem warhead according to the preamble of claim 1.
- This preamble is known from DE-A-3 941 445.
- EP-A1-0 583 642 a warhead with a tandem charge known.
- the warhead has one main charge designed as a hollow charge and a smaller-caliber additional charge on.
- the secondary storey designed as a fragmentary storey, penetrates through this channel into the target and detonates behind the target with a splintering effect.
- the secondary storey is only due to its inertia on impact of the warhead moved through the channel.
- a separate acceleration charge for the secondary floor is not necessary.
- the splintering effect is caused by the explosive charge and the housing of the secondary floor.
- the splintering effect is due to the design of the secondary floor mainly in the weft direction, with the immediate vicinity of the cover only a slight splintering effect occurs.
- an explosive charge and ogive-shaped also in the rear of the floor arranged construction slitter are provided. Ignition of the rear Explosive charge takes place from a centrally located detonator, this detonator being the separates the front explosive charge from the rear explosive charge.
- the front explosive charge is about an explosive consisting of and on the front explosive charge adjacent ignition amplifier ignited while the rear explosive charge a transmission detonator and a downstream ignition transformer are required.
- This ignition transmitter initiates the explosive charge on the rear eccentrically, i.e. on outer edge of the explosive charge.
- This one-sided ignition of the explosive charge designed as a hemisphere has a very different fragment density in the target area.
- the energy of the construction splinters varies corresponding.
- This transfer of the ignition is to be structurally simple and inexpensive be.
- the invention solves this problem according to the characterizing features of claim 1.
- Essential for the invention is the symmetrical and large-area ignition transmission to the rear active charge.
- the effectiveness of the rear active load corresponds to the front active load.
- the large-area ignition of the front active charge is an advantage.
- a functionally reliable transmission of the ignition is present in claim 1.
- a secondary floor 1 is only partially in one drawn pipe section 2 of a housing 3 of a tandem warhead 4th stored and secured via a threaded connection 5.
- a steam protection is included 6 designated.
- the secondary floor 1 consists of two housing parts screwed together at 109 10, 11, an igniter 12, a two-part explosive charge 13, 14 and from fragments 15, 16 with envelopes 17, 18.
- the igniter 12 according to Figures 2 and 4 consists of an electrically controllable Detonator 20 with detonator 21, a thread 42 and one with detonator 20 screw over igniter 25.
- the igniter 25 has a housing 26 with two flanges 22 and a central pin 27 on the ignition side. Recesses are in the housing 26 28 to 31 with an amplifier charge 32 made of explosives.
- the booster charge 32 is disk-shaped in the direction of the front active charge 13 formed and has a diameter 33 which is almost the diameter 34 corresponds to the front active charge 13.
- Two tongue-like are integrally connected to the rear active charge 14 Explosive poles 50.
- Explosive poles 50 After the detonator 12 completely in a cylindrical metal sleeve 52 made of aluminum, that for the explosive poles 50th required space created by corresponding recesses 55 on the housing part 11.
- the metal sleeve 52 completely encapsulates the rear active charge 14.
- a Elastic element between the housing parts 10 is designated 110.
- One the flanges 22 are pinned at 111.
- the ignition area 60 there are two thin-walled wall sections 59 on the housing 26 provided so that the ignition from the booster charge 32 to the explosive poles 50 - that is, in two ways.
- the cross sections of the explosive poles 50 are dimensioned such that the ignition to the explosives block 19 of the rear active charge 14 is guaranteed.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
Die Erfindung bezieht sich auf ein Sekundärgeschoß für einen Tandemgefechtskopf
nach dem Oberbegriff des Anspruchs 1. Dieser Oberbegriff ist aus DE-A-3 941 445 bekannt.The invention relates to a secondary floor for a tandem warhead
according to the preamble of
Beim Häuserkampf oder gegen sonstige Deckungen feindlicher Kräfte besteht ein Bedarf an kostengünstigen Waffen und Munition. Durch die EP-A1- 0 583 642 ist ein Gefechtskopf mit einer Tandemladung bekannt. Der Gefechtskopf weist eine als Hohlladung ausgebildete Hauptladung und eine kaliberkleinere Nachschußladung auf. Beim Zielaufprall des Gefechtskopfes schlägt die Hohlladung einen Kanal durch das Ziel. Das als Splittergeschoß ausgebildete Sekundärgeschoß dringt durch diesen Kanal in das Ziel ein und detoniert hinter dem Ziel mit Splitterwirkung. Das Sekundärgeschoß wird allein aufgrund seiner Massenträgheit beim Aufschlag des Gefechtskopfes durch den Kanal bewegt. Eine separate Beschleunigungsladung für das Sekundärgeschoß ist nicht erforderlich. Die Splitterwirkung wird durch die Sprengladung und durch das Gehäuse des Sekundärgeschosses bewirkt. Aufgrund der Ausbildung des Sekundärgeschosses liegt die Splitterwirkung hauptsächlich in Schußrichtung, wobei unmittelbar im Nahbereich der Deckung eine nur geringe Splitterwirkung auftritt.In house warfare or against other coverings from hostile forces, there is a Need for inexpensive weapons and ammunition. Through EP-A1-0 583 642 a warhead with a tandem charge known. The warhead has one main charge designed as a hollow charge and a smaller-caliber additional charge on. When the warhead hits the target, the shaped charge strikes a channel through the goal. The secondary storey, designed as a fragmentary storey, penetrates through this channel into the target and detonates behind the target with a splintering effect. The secondary storey is only due to its inertia on impact of the warhead moved through the channel. A separate acceleration charge for the secondary floor is not necessary. The splintering effect is caused by the explosive charge and the housing of the secondary floor. The splintering effect is due to the design of the secondary floor mainly in the weft direction, with the immediate vicinity of the cover only a slight splintering effect occurs.
Zur Verbesserung der Splitterwirkung entgegen der Flugrichtung eines Geschosses ist es nach der DE-A1 39 41 445 vorgesehen, daß neben Splittern in einer Geschoßogive auch im Heck des Geschosses eine Sprengladung und ogivenförmig angeordnete Konstruktionsslpitter vorgesehen sind. Die Zündung der heckseitigen Sprengladung erfolgt von einem mittig gelagerten Zünder, wobei dieser Zünder die vordere Sprengladung von der hinteren Sprengladung trennt. Die vordere Sprengladung wird über einen, aus Sprengstoff bestehenden und an der vorderen Sprengladung anliegenden Zündverstärker gezündet, während die hintere Sprengladung einen Übertragungsdetonator und einen nachgeordneten Zündübertrager benötigt. Dieser Zündübertrager initiert die heckseitige Sprengladung exzentrisch, also am äußeren Rand der Sprengladung. Durch diese einseitige Zündung der etwa als Halbkugel ausgebildeten Sprengladung liegt eine sehr unterschiedliche Splitterdichte im Zielraum vor. Außerdem variiert die Energie der Konstruktionssplitter entsprechend.To improve the splinter effect against the direction of flight of a projectile it is provided according to DE-A1 39 41 445 that in addition to splinters in a floor arch an explosive charge and ogive-shaped also in the rear of the floor arranged construction slitter are provided. Ignition of the rear Explosive charge takes place from a centrally located detonator, this detonator being the separates the front explosive charge from the rear explosive charge. The front explosive charge is about an explosive consisting of and on the front explosive charge adjacent ignition amplifier ignited while the rear explosive charge a transmission detonator and a downstream ignition transformer are required. This ignition transmitter initiates the explosive charge on the rear eccentrically, i.e. on outer edge of the explosive charge. This one-sided ignition of the explosive charge designed as a hemisphere has a very different fragment density in the target area. In addition, the energy of the construction splinters varies corresponding.
Es ist die Aufgabe der Erfindung, eine Übertragung der Zündung von einem Zünder mit nur einem Zünderausgang auf die vordere und die hintere Wirkladung eines Sekundärgeschosses vorzuschlagen, die zu einer gesteigerten Splitterwirkung führt. Diese Übertragung der Zündung soll konstruktiv einfach und kostengünstig sein.It is the object of the invention to transfer the ignition from an igniter with only one detonator output on the front and the rear active charge one Propose secondary floor, which leads to an increased fragmentation effect leads. This transfer of the ignition is to be structurally simple and inexpensive be.
Die Erfindung löst diese Aufgabe entsprechend den kennzeichnenden Merkmalen
des Anspruches 1.The invention solves this problem according to the characterizing features
of
Vorteilhafte Weiterbildungen der Erfindung sind den Unteransprüchen zu entnehmen.Advantageous developments of the invention can be found in the subclaims.
Wesentlich für die Erfindung ist die symmetrische und großflächige Zündübertragung
auf die hintere Wirkladung. Dadurch ist die Effektivität der hinteren Wirkladung
entsprechend der vorderen Wirkladung.
Von Vorteil ist die großflächige Zündung der vorderen Wirkladung.Essential for the invention is the symmetrical and large-area ignition transmission to the rear active charge. As a result, the effectiveness of the rear active load corresponds to the front active load.
The large-area ignition of the front active charge is an advantage.
Ein funktionssichere Übertragung der Zündung liegt durch den Anspruch 1 vor.
Die dünnen Wandabschnitte der Überzündvorrichtung, die die Verstärkerladung
aus Sprengstoff von den zungenartigen Sprengstoffpolen der hinteren Wirkladung
trennen, gewährleisten die gleichzeitige Zündung der letzteren.A functionally reliable transmission of the ignition is present in
Konstruktive Details gehen aus den Ansprüchen 2 bis 7 hervor, wodurch eine kostengünstige
und montagefreundliche Überzündvorrichtung ermöglicht wird.Structural details emerge from
Ein Ausführungsbeispiel der Erfindung ist in der Zeichnung dargestellt. Es zeigt:
- Fig. 1
- Einen Tandemgefechtskopf mit gestrichelt gezeichnetem Sekundärgeschoß in perspektivischer Darstellung,
- Fig. 2
- das Sekundärgeschoß im Längsschnitt mit einem Teil des Gehäuses des Tandemgefechtskopfes entsprechend einem Schnitt II - II nach Fig. 3,
- Fig. 3
- einen Querschnitt durch das Sekundärgeschoß entsprechend einem Schnitt III -III nach Fig. 2,
- Fig. 4
- den vollständigen Zünder nach Fig. 2 in perspektivischer Darstellung und
- Fig. 5
- eine Wirkladung in Perspektive nach Fig. 2.
- Fig. 1
- A tandem warhead with a dashed secondary floor in perspective,
- Fig. 2
- the secondary floor in longitudinal section with part of the housing of the tandem warhead according to a section II - II of FIG. 3,
- Fig. 3
- 3 shows a cross section through the secondary storey in accordance with a section III-III according to FIG. 2,
- Fig. 4
- the complete igniter of FIG. 2 in perspective and
- Fig. 5
- an active charge in perspective according to FIG. 2.
Entsprechend den Figuren 1 und 2 ist ein Sekundärgeschoß 1 in einem nur teilweise
gezeichneten Rohrabschnitt 2 eines Gehäuses 3 eines Tandemgefechtskopfes 4
gelagert und über eine Gewindeverbindung 5 gesichert. Ein Schwadenschutz ist mit
6 bezeichnet.According to Figures 1 and 2, a
Das Sekundärgeschoß 1 besteht aus zwei bei 109 miteinander verschraubten Gehäuseteilen
10, 11, einem Zünder 12, einer zweiteiligen Sprengstoffladung 13, 14
und aus Splitterladungen 15, 16 mit Hüllen 17, 18.The
Der Zünder 12 nach den Figuren 2 und 4 besteht aus einem elektrisch ansteuerbaren
Zünder 20 mit Detonator 21, einem Gewinde 42 und einer mit dem Zünder 20
verschrauben Überzündvorrichtung 25.The
Die Überzündvorrichtung 25 weist ein Gehäuse 26 mit zwei Flanschen 22 und mit
einem zünderseitigen, zentralen Zapfen 27 auf. In dem Gehäuse 26 sind Ausnehmungen
28 bis 31 mit einer Verstärkerladung 32 aus Sprengstoff.The
Die Verstärkerladung 32 ist in Richtung auf die vordere Wirkladung 13 scheibenförmig
ausgebildet und weist einen Durchmesser 33 auf, der nahezu dem Durchmesser
34 der vorderen Wirkladung 13 entspricht.The
Die hintere Wirkladung 14, siehe auch Fig. 5, nimmt den Zünder 20 in einer Bohrung
40 bis auf einen Ringabschnitt 41 auf In diesem Bereich liegt ein Gewindering
42 des Zünders 20, wobei dieser mit dem Gehäuse 26 über eine Gewindeverbindung
43 verschraubt ist. The rear
Einstückig mit der hinteren Wirkladung 14 verbunden sind zwei zungenartige
Sprengstoffpole 50. Nachdem der Zünder 12 komplett in einer zylindrischen Metallhülse
52 aus Aluminium angeordnet ist, wird der für die Sprengstoffpole 50
benötigte Raum durch entsprechende Ausnehmungen 55 am Gehäuseteil 11 geschaffen.
Die Metallhülse 52 kapselt die hintere Wirkladung 14 vollständig ab. Ein
eleastisches Element zwischen den Gehäuseteilen 10 ist mit 110 bezeichnet. Einer
der Flansche 22 ist bei 111 verstiftet.Two tongue-like are integrally connected to the rear
Im Überzündbereich 60 sind am Gehäuse 26 zwei dünnwandige Wandabschnitte 59
vorgesehen, so daß die Überzündung von der Verstärkerladung 32 zu den Sprengstoffpolen
50 - also auf zwei Wegen - erfolgen kann.In the
Die Querschnitte der Sprengstoffpole 50 sind so bemessen, daß die Durchzündung
zum Sprengstoffblock 19 der hinteren Wirkladung 14 gewährleistet ist.The cross sections of the
Bei Aufschlag des Tandemgefechtskopfes 4 auf eine nicht dargestellte Deckung
wird durch die ebenfalls nicht dargestellte Hohlladung ein Durchschußkanal in der
Deckung erzeugt. Durch diesen Durchschußkanal dringt das vom Gehäuse 3 abgelöste
Sekundärgeschoß. Aufgrund einer entsprechend eingestellten Zeitverzögerung
zündet der Detonator 21 des Zünders 20 die Verstärkerladung 32. Ausgehend
von der Verstärkerladung 32 wird die vordere Wirkladung 13 und gleichzeitig
werden die Sprengstoffpole 50 gezündet, in dem in den Überzündbereichen 60 das
Gehäuse 26 durchschlagen wird. Die einander gegenüberliegenden Sprengstoffpole
50 leiten dem Sprengimpuls symmetrisch über einen Halsbereich 61 zum Sprengstoffblock
19. Die gleichzeitige Detonation der vorderen und der hinteren Wirkladung
13, 14 führt sowohl zu einer vorderen Splitterverteilung als auch zu einer
hinteren Splitterverteilung. Die Splitterverteilung aufgrund der hinteren Wirkladung
14 ist gerade in Richtung auf den Durchschußkanal und dessen Umgebungsfeld
groß.When the tandem warhead 4 strikes a cover, not shown
is a bullet channel in the
Cover generated. The detached from the housing 3 penetrates through this penetration channel
Secondary floor. Due to a time delay set accordingly
detonator 21 of
Claims (5)
- Secondary projectile (1) for a tandem warhead (4), having a front active charge (13), a rear active charge (14) and a fuse (12, 20) located between them, its direction of ignition being oriented towards the front active charge (13), whereby ignition is induced forward by way of a booster charge (32) and backward by a flashover-ignition device (25), whereby the booster charge (32) which can be initiated by the fuse (12, 20) consists of explosive and rests directly against the front active charge (13),
characterized in that
the booster charge (32) is separated by thin, ignitable wall sections (59) of a casing (26) of the flashover-ignition device (25) from at least two tongue-like explosive poles (50) of the rear active charge (14). - Secondary projectile according to Claim 1,
characterized in thatthe explosive poles (50) are formed in one piece with the rear active charge (14) and,together with the booster charge (32), form flashover-ignition areas (50). - Secondary projectile according to Claim 1,
characterized in that
the explosive poles (50) rest extensively against a metal sleeve encasing the fuse (12, 20), i.e. over a large surface in the region of the casing (26) of the flashover-ignition device, and are limited in radial direction by the casing section (11) of the rear active charge (14). - Secondary projectile according to Claim 3,
characterized in that
the casing section (11) has recesses (55) corresponding with the explosive poles (50). - Secondary projectile according to Claim 1,
characterized in that
the booster charge (32) takes the form of a disk and has a diameter (33) which almost corresponds with the diameter (33) of the front active charge (13).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19534211A DE19534211A1 (en) | 1995-09-15 | 1995-09-15 | Secondary storey for a tandem warhead |
DE19534211 | 1995-09-15 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0763705A2 EP0763705A2 (en) | 1997-03-19 |
EP0763705A3 EP0763705A3 (en) | 1997-03-26 |
EP0763705B1 true EP0763705B1 (en) | 1998-12-02 |
Family
ID=7772239
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96114074A Expired - Lifetime EP0763705B1 (en) | 1995-09-15 | 1996-09-03 | Secondary projectile for a tandem warhead |
Country Status (4)
Country | Link |
---|---|
US (1) | US5594197A (en) |
EP (1) | EP0763705B1 (en) |
DE (2) | DE19534211A1 (en) |
ES (1) | ES2127596T3 (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5686692A (en) * | 1996-09-30 | 1997-11-11 | The United States Of America As Represented By The Secretary Of The Navy | Single fuse follow-through grenade |
DE19651170A1 (en) * | 1996-12-10 | 1998-06-18 | Diehl Gmbh & Co | Detonatorless, ballistic explosive device |
SG82583A1 (en) * | 1997-04-23 | 2001-08-21 | Diehl Stiftung & Co | Fragmentation body for a fragmentation projectile |
US6105505A (en) | 1998-06-17 | 2000-08-22 | Lockheed Martin Corporation | Hard target incendiary projectile |
SE519542C2 (en) * | 2000-07-03 | 2003-03-11 | Bofors Weapon Sys Ab | Ammunition unit with one or more action shells |
US6966265B2 (en) * | 2000-07-03 | 2005-11-22 | Bofors Defence Ab | Unit of ammunition with one or more warhead casings |
US6962202B2 (en) * | 2003-01-09 | 2005-11-08 | Shell Oil Company | Casing conveyed well perforating apparatus and method |
US7363862B2 (en) * | 2005-05-27 | 2008-04-29 | United States Of America As Represented By The Secretary Of The Army | Multi-purpose single initiated tandem warhead |
US20070006768A1 (en) * | 2005-07-06 | 2007-01-11 | Rafael-Armament Development Authority Ltd. | Mushroom warhead |
US7930978B1 (en) * | 2008-05-19 | 2011-04-26 | Raytheon Company | Forward firing fragmentation warhead |
US8196513B1 (en) * | 2009-12-04 | 2012-06-12 | The United States Of America As Represented By The Secretary Of The Navy | Stand-off disrupter apparatus |
KR101259734B1 (en) | 2012-01-20 | 2013-04-30 | 주식회사 한화 | Projectile with submunition |
SE541548C2 (en) * | 2015-06-17 | 2019-10-29 | Bae Systems Bofors Ab | Procedure for pre-fragmentation of a combat part and pre-fragmented combat part |
DE102019101762A1 (en) * | 2019-01-24 | 2020-07-30 | Rheinmetall Denel Munition (Pty) Ltd. | Explosive charge arrangement of a rocket with two different explosives |
RU192887U1 (en) * | 2019-06-19 | 2019-10-04 | Федеральное Государственное Бюджетное Образовательное Учреждение Высшего Образования "Новосибирский Государственный Технический Университет" | High-explosive fragmentation warhead |
SE2000234A1 (en) * | 2020-12-14 | 2022-06-15 | Saab Ab | A fragmentation warhead a method of manufacturing of a fragmentation warhead |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US94647A (en) * | 1869-09-07 | John d | ||
DE317581C (en) * | ||||
DE2648137C2 (en) * | 1976-10-23 | 1984-04-12 | Dynamit Nobel Ag, 5210 Troisdorf | Propellant charge lighter for ammunition |
DE3133634A1 (en) * | 1980-09-05 | 1982-06-24 | General Electric Co., Schenectady, N.Y. | "BLAST CAPS ARRANGEMENT AND APPLICATION THEREOF IN AN EXPLOSIVE BULLET" |
US4803928A (en) * | 1986-08-02 | 1989-02-14 | Stefan Kramer | Tandem charge projectile |
DE3703773A1 (en) * | 1987-02-07 | 1988-08-18 | Diehl Gmbh & Co | Projectile, especially a mortar round |
DE3941445A1 (en) * | 1989-12-15 | 1991-06-20 | Diehl Gmbh & Co | Infantry projectile propels shot forward and backward - from similar hemispherical charges sepd. by transverse detonator assembly |
DE4225704A1 (en) * | 1992-08-04 | 1994-02-10 | Diehl Gmbh & Co | Warhead with a tandem charge |
-
1995
- 1995-09-15 DE DE19534211A patent/DE19534211A1/en not_active Withdrawn
- 1995-10-11 US US08/540,935 patent/US5594197A/en not_active Expired - Fee Related
-
1996
- 1996-09-03 DE DE59600895T patent/DE59600895D1/en not_active Expired - Fee Related
- 1996-09-03 ES ES96114074T patent/ES2127596T3/en not_active Expired - Lifetime
- 1996-09-03 EP EP96114074A patent/EP0763705B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE59600895D1 (en) | 1999-01-14 |
EP0763705A3 (en) | 1997-03-26 |
DE19534211A1 (en) | 1997-03-20 |
US5594197A (en) | 1997-01-14 |
EP0763705A2 (en) | 1997-03-19 |
ES2127596T3 (en) | 1999-04-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE19617221C2 (en) | Steerable projectile that can be used as a mortar | |
EP0763705B1 (en) | Secondary projectile for a tandem warhead | |
DE19535218C1 (en) | Ballistic projectile | |
EP0583642B1 (en) | Warhead with tandem charge | |
EP0600388B1 (en) | Tandem warhead having piezo-electric igniters | |
DE2900802C1 (en) | Warhead against fortified or armored targets, especially for damaging runways, pavement ceilings, bunker walls or the like | |
DE2919807C2 (en) | Twist-stabilized sabot projectile to overcome a heterogeneous resistance | |
EP0848228B1 (en) | Ballistic high-explosive type projectile without a fuze | |
DE1240760B (en) | Tank incendiary bullet | |
DE3416787A1 (en) | ARMORING BULLET | |
EP0763704A2 (en) | Fragmentation casing for a secondary projectile of a tandem projectile | |
DE977946C (en) | Process for generating a secondary effect in connection with the known effect of a shaped charge | |
EP1001244B1 (en) | Artillery projectile | |
DE69506024T2 (en) | Projectile for attacking hard targets | |
DE60202419T2 (en) | explosive projectile | |
EP0236325B1 (en) | Self-destroying igniter | |
DE69907791T2 (en) | Kit for converting an explosive projectile to a projectile breaking a benton structure, as well as a projectile converted in this way | |
DE3522008C2 (en) | ||
DE19612890C2 (en) | mortar round | |
DE4331236C1 (en) | Active armour-piercing warhead | |
DE19638295B3 (en) | Warhead, for attacking and penetrating buildings, barricades and armored vehicles, comprises bore charge and bullet charge embedded in main charge | |
DE19651169A1 (en) | Lock for pyrotechnic impact igniter of ballistic explosive round | |
DE69705670T2 (en) | Splinter floor with equatorial ejection symmetry | |
EP0801287B1 (en) | Fragmentation projectile with base fuze and cartridge case | |
DE3737231A1 (en) | Projectile |
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 |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): CH DE ES GB LI SE |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): CH DE ES GB LI SE |
|
17P | Request for examination filed |
Effective date: 19970226 |
|
17Q | First examination report despatched |
Effective date: 19970530 |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: DIEHL STIFTUNG & CO. |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): CH DE ES GB LI SE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REF | Corresponds to: |
Ref document number: 59600895 Country of ref document: DE Date of ref document: 19990114 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: A. BRAUN, BRAUN, HERITIER, ESCHMANN AG PATENTANWAE |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19990212 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2127596 Country of ref document: ES Kind code of ref document: T3 |
|
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 | ||
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20050920 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20060927 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20061114 Year of fee payment: 11 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20070910 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20060927 Year of fee payment: 11 |
|
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: 20070904 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
EUG | Se: european patent has lapsed | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20070930 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080401 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20070930 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20070904 |
|
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: 20070904 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20080903 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20080903 |