EP4038340B9 - Active element and method for igniting an active element - Google Patents

Active element and method for igniting an active element Download PDF

Info

Publication number
EP4038340B9
EP4038340B9 EP20764989.8A EP20764989A EP4038340B9 EP 4038340 B9 EP4038340 B9 EP 4038340B9 EP 20764989 A EP20764989 A EP 20764989A EP 4038340 B9 EP4038340 B9 EP 4038340B9
Authority
EP
European Patent Office
Prior art keywords
active
active element
ignition means
grooves
active body
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.)
Active
Application number
EP20764989.8A
Other languages
German (de)
French (fr)
Other versions
EP4038340A1 (en
EP4038340B1 (en
Inventor
Vikorn Kadavanich
Florian Huber
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rheinmetall Waffe Munition GmbH filed Critical Rheinmetall Waffe Munition GmbH
Publication of EP4038340A1 publication Critical patent/EP4038340A1/en
Application granted granted Critical
Publication of EP4038340B1 publication Critical patent/EP4038340B1/en
Publication of EP4038340B9 publication Critical patent/EP4038340B9/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/0803Primers; Detonators characterised by the combination of per se known chemical composition in the priming substance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41JTARGETS; TARGET RANGES; BULLET CATCHERS
    • F41J2/00Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic or acoustic waves
    • F41J2/02Active targets transmitting infrared radiation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/0807Primers; Detonators characterised by the particular configuration of the transmission channels from the priming energy source to the charge to be ignited, e.g. multiple channels, nozzles, diaphragms or filters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/0838Primers or igniters for the initiation or the explosive charge in a warhead
    • F42C19/0846Arrangements of a multiplicity of primers or detonators, dispersed within a warhead, for increased efficiency

Definitions

  • the invention relates to an active body, in particular a dummy target active body, comprising at least one active mass and at least two ignition means, each comprising a pyrotechnic set for igniting the active mass.
  • the invention further relates to a method for igniting an active body.
  • Active bodies such as dummy target active bodies, are used in aviation. Since around 1970, such dummy target active bodies have been provided under a protective film or in a container and initiated from one side. This applies in particular to all conventional MTV (Magnesium-Teflon-Viton) dummy target bodies and spectral dummy target bodies.
  • MTV Magnetic-Teflon-Viton
  • the ignition chain is activated for the active body, which is preferably elongated in aircraft, from the firing side, preferably via a safety system, and then ignites the active body after release.
  • active bodies often have a quick-burning coating in order to achieve ignition on all sides in the required time.
  • Dummy target active bodies with certain active masses and geometries are subject to ignition problems due to the design and type of use, which can lead to delayed and reduced power development in the initial phase of initiation.
  • the initiation usually takes place from an ignition side in the base area, which is the so-called front side of the active body and passes through it inside or outside along the surface in the direction of the ejection side in order to finally achieve an all-round reaction of the active body.
  • the ignition problems described above can have a direct impact on effectiveness against the threat during the ignition phase.
  • the document DE 10 2009 030 871 A1 discloses an active body with a combustible active mass container based on plastic film, which can be ignited inductively, by means of a laser or by high temperature.
  • a pyrotechnic active body with a housing, an ignition device and at least one active set is disclosed.
  • the ignition device is arranged, for example, in the bottom of the active body.
  • the patent application DE 10 2010 030 869 A1 discloses an active body with several active masses, which has several individual flares arranged one behind the other, which can be ignited inductively, by means of a laser or by high temperature.
  • the document DE 10 2009 030 872 A1 relates to an active body that is ignited inductively, consisting of individual flares which are packaged in a carrier material such as a steel foil coated with red phosphorus.
  • the document DE 10 2004 047 231 A1 discloses a generic active body which has a plurality of active compounds and igniting agents. How the ignition is carried out and how the ignition means are arranged is not disclosed.
  • An active body is also known, with at least two active masses that are ignited via a detonator.
  • the invention is based on the object of creating an active body which enables rapid and reliable ignition of several active substances.
  • an active body in particular a dummy target active body, comprising at least one active mass, at least two ignition means, each comprising one Pyrotechnic set for igniting at least one active mass.
  • the at least two ignition means are arranged on the at least one active mass and the at least two ignition means are connected to one another via channels in such a way that the at least one active mass can be ignited on multiple sides at the same time.
  • the active body comprises at least one active mass, at least two ignition means, each comprising a pyrotechnic set for igniting the active masses.
  • the at least two ignition means are arranged on the at least one active mass and the at least two ignition means are connected to one another via channels in such a way that the at least one active mass can be ignited on multiple sides at the same time.
  • the active body in such a way that it can be initiated on multiple sides but at least on two sides, for example on the side surfaces as well as the opposite side, i.e. ignited. It is therefore an active body with multiple ignition.
  • the at least one active substance is preferably at least one pyrotechnic active substance, such as those used in flares.
  • the channels are preferably ignition channels which are designed to ignite the ignition means or to conduct ignition up to the ignition means.
  • the channels can be arranged symmetrically and/or asymmetrically to one another.
  • Multi-sided at the same time means that the active body or the at least one active mass can be ignited simultaneously at several points, such as sides, top, bottom or edges. Simultaneous in the sense of the invention means that the at least one active mass can be ignited essentially without any time delay.
  • the igniting means in the sense of the invention are, for example, squibs, smaller ignition-sensitive pyrotechnic sets or other known igniting means.
  • the multi-sided ignition according to the invention ensures that large-area, less sensitive active substances can be ignited quickly and reliably using significantly smaller ignition means.
  • such an active body has an all-round irritation result immediately after being ejected (e.g. from an aircraft) and incoming missiles can be reliably repelled.
  • the active body according to the invention in particular due to the simultaneous ignitability of the at least one active mass on multiple sides, achieves lower scattering behavior and improved reactivity in use. In addition, there is a better development of the effect of the active body.
  • the at least two active masses can be the same size and/or different sizes. By using a large number of different active substances, it is possible to adjust the wavelength of the spectrum emitted by the active body during the burning of the active substances.
  • the active body has at least two active compounds and the ignition means are arranged between the active compounds of the active body in such a way that the at least two active compounds can be ignited on multiple sides at the same time.
  • the ignition means are arranged inside and/or outside of the active body.
  • the pyrotechnic set of ignition means and the at least one active mass are separated from one another by an inert material.
  • the at least one active mass and/or the ignition means are separated from one another by a film, a housing or an air gap.
  • the individual active substances can preferably be separated from one another in this way.
  • Such physical separation can occur, for example, using a film or a housing made of paper, plastic or metal.
  • the active body has grooves, grooves and/or bores.
  • the channels run in the grooves, grooves and/or holes.
  • the individual active compounds are preferably separated by these grooves and/or grooves.
  • the grooves and/or grooves run in such a way that they cross each other at several crossing points and the ignition means are formed in the crossing points.
  • the grooves, grooves and/or bores are arranged inside and/or outside the active body.
  • the active body is protected from environmental influences by a film or a housing. This ensures that the active body can be reliably ignited even at high wind and/or ejection speeds - for example when fired from a fast-flying aircraft or aircraft.
  • the active body does not have a pyrotechnic coating set that covers the entire active body.
  • a coating set is a fast-burning set that contains the active body covers and allows ignition from all sides. This has the advantage that the active body can be approved even if there is no suitable approved coating set.
  • the ignition means are arranged in such a way and the length of the channels is designed such that the ignition means can be ignited at the same time.
  • the ignition means are connected to an ignition initiator via the channels.
  • the active body is essentially cuboid-shaped and has essentially cuboid-shaped active masses.
  • This can in particular be an active body for ammunition in the NATO standard caliber 2x1x8" or 1x1x8".
  • It can also be a cylindrical active body, preferably with a diameter of 36mm or 55mm.
  • Fig. 1 shows a schematic perspective view of an active body 1 according to the invention.
  • the active body 1 comprises a plurality of active compounds 10 1...n and a plurality of igniters 20 1...n .
  • the ignition means 20 1...n each comprises a pyrotechnic set for igniting the active masses 10 1...n .
  • Fig. 2 also shows a schematic perspective view of the active body according to the invention Fig.1 , where channels 30 1...n are hidden.
  • the igniting means 20 1...n are arranged between the individual active masses 10 1...n and the igniting means 20 1...n are connected to one another via channels 30 1...n in such a way that the active body 1 can be ignited on multiple sides at the same time is.
  • the ignition means 20 1...n are connected to an ignition initiator (not shown) via the channels 30 1...n , the ignition means 20 1 ... n being arranged in such a way and the length of the channels 30 1...n is designed such that the ignition means 20 1...n can be ignited at the same time.
  • the active body 1 has grooves and/or grooves 22 1...n , through which the individual active masses 10 1...n are separated from one another.
  • the grooves and/or grooves 25 1...n are according to the first exemplary embodiment Fig. 1 and 2 arranged inside the active body 1 and/or outside, i.e. on the outside.
  • the grooves and/or grooves 22 1...n run in such a way that they intersect at several intersection points 25 1...n and the ignition means 20 1...n are arranged in the intersection points 25 1...n .
  • the channels 30 1...n ie the channels 30 1...n are arranged in the grooves and/or grooves.
  • the individual channels 30 1...n are designed like a bead.
  • the individual active masses 10 1...n of the active body 1 can be ignited on multiple sides at the same time.
  • the ignition means 20 1...n are arranged inside/outside the active body 1 according to the exemplary embodiment. For this purpose, these are provided in the grooves/grooves of the active body 1.
  • the pyrotechnic set of igniting agents 20 1...n and the active masses 10 1...n are separated from one another by an inert material.
  • This can be designed, for example, as a film, a housing or an air gap.
  • Fig. 3 is a schematic perspective view of an active body 1 according to the invention according to a second exemplary embodiment, which is based on the exemplary embodiment according to the Fig.1 based and the differences are shown below.
  • the active body 1 has internal grooves, grooves and/or bores 23 1...n , in which channels 31 1...n are formed.
  • the channels 31 1...n are formed within the individual active masses 10 1...n and have a symmetrical image.
  • Fig. 4 is a schematic perspective view of an active body 1 according to the invention according to a third exemplary embodiment, which is based on the exemplary embodiment according to Fig. 3 based.
  • the internal channels 31 1...n are formed into symmetrical and/or asymmetrical channels 31 1...n within the individual active masses 10 1... n .
  • the embodiment shown is an active body 1, which comprises eight active masses 10 1...8 and six igniters 20 1...6 .
  • the active body 1 is essentially cuboid-shaped and comprises essentially cuboid-shaped active masses 10 1...8 .
  • This can in particular be an active body for ammunition in the NATO standard caliber 2 ⁇ 1 ⁇ 8" or 1 ⁇ 1 ⁇ 8".
  • this embodiment of the above exemplary embodiment only represents an exemplary embodiment.
  • a number other than eight active masses and six igniters are also possible.
  • It can also be a cylindrical active body, preferably with a diameter of 36mm or 55mm. It is also possible that it is a spherical or triangular active body.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Air Bags (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Infusion, Injection, And Reservoir Apparatuses (AREA)

Description

Die Erfindung betrifft einen Wirkkörper, insbesondere Scheinzielwirkkörper, umfassend zumindest eine Wirkmasse und zumindest zwei Anzündmittel jeweils umfassend einen pyrotechnischen Satz zum Anzünden der Wirkmasse.The invention relates to an active body, in particular a dummy target active body, comprising at least one active mass and at least two ignition means, each comprising a pyrotechnic set for igniting the active mass.

Weiterhin betrifft die Erfindung ein Verfahren zum Zünden eines Wirkkörpers.The invention further relates to a method for igniting an active body.

Wirkkörper, wie Scheinzielwirkkörper, werden in der Luftfahrt verwendet. Seit ca. 1970 werden solche Scheinzielwirkkörper unter einer Schutzfolie oder in einem Behältnis bereitgestellt und von einer Seite initiiert. Dies gilt insbesondere für alle konventionellen MTV (Magnesium-Teflon-Viton) - Scheinzielwirkkörper und spektralen Scheinzielwirkkörper.Active bodies, such as dummy target active bodies, are used in aviation. Since around 1970, such dummy target active bodies have been provided under a protective film or in a container and initiated from one side. This applies in particular to all conventional MTV (Magnesium-Teflon-Viton) dummy target bodies and spectral dummy target bodies.

Die Zündkette wird dabei für die bei Flugzeugen vorzugsweise länglichen Wirkkörper von der Abschussseite, vorzugsweise über ein Sicherungssystem aktiviert und zündet dann nach der Freigabe den Wirkkörper. Diese Wirkkörper besitzen oft einen schnell brennenden Überzugsatz, um eine allseitige Anzündung in der geforderten Zeit zu erreichen.The ignition chain is activated for the active body, which is preferably elongated in aircraft, from the firing side, preferably via a safety system, and then ignites the active body after release. These active bodies often have a quick-burning coating in order to achieve ignition on all sides in the required time.

Scheinzielwirkkörper mit bestimmten Wirkmassen und Geometrien unterliegen Anzündproblemen aufgrund des Designs und der Einsatzart, welche zu einer verzögerten und zu einer geringeren Leistungsentfaltung in der Anfangsphase der Initiierung führen können.Dummy target active bodies with certain active masses and geometries are subject to ignition problems due to the design and type of use, which can lead to delayed and reduced power development in the initial phase of initiation.

Die Initiierung erfolgt üblicherweise von einer Anzündseite im Bodenbereich, die die sogenannte Stirnseite des Wirkkörpers und durchläuft diesen innen oder außen entlang der Oberfläche in Richtung der Ausstoßseite, um schließlich eine allseitige Reaktion des Wirkkörpers zu erreichen.The initiation usually takes place from an ignition side in the base area, which is the so-called front side of the active body and passes through it inside or outside along the surface in the direction of the ejection side in order to finally achieve an all-round reaction of the active body.

Die oben geschilderten Anzündprobleme können einen unmittelbaren Einfluss auf die Wirksamkeit gegenüber der Bedrohung während der Zündphase bewirken.The ignition problems described above can have a direct impact on effectiveness against the threat during the ignition phase.

Das Dokument DE 10 2009 030 871 A1 offenbart einen Wirkkörper mit einem verbrennbaren Wirkmassencontainer auf Kunststofffolienbasis, der induktiv, mittels Laser oder per Hochtemperatur gezündet werden kann.The document DE 10 2009 030 871 A1 discloses an active body with a combustible active mass container based on plastic film, which can be ignited inductively, by means of a laser or by high temperature.

Aus der DE 102016 122740 A1 ist ein pyrotechnischer Wirkkörper mit einem Gehäuse, einer Zündvorrichtung und mindestens einem Wirksatz offenbart. Die Zündvorrichtung ist beispielsweise im Boden des Wirkkörpers angeordnet.From the DE 102016 122740 A1 a pyrotechnic active body with a housing, an ignition device and at least one active set is disclosed. The ignition device is arranged, for example, in the bottom of the active body.

Die Patentanmeldung DE 10 2010 030 869 A1 offenbart einen Wirkkörper mit mehreren Wirkmassen, der mehrere hintereinander angeordnete Einzelflares aufweist, die induktiv, mittels Laser oder per Hochtemperatur gezündet werden kann.The patent application DE 10 2010 030 869 A1 discloses an active body with several active masses, which has several individual flares arranged one behind the other, which can be ignited inductively, by means of a laser or by high temperature.

Das Dokument DE 10 2009 030 872 A1 betrifft einen Wirkkörper der induktiv gezündet wird, bestehend aus Einzelflares, welche in einem Trägermaterial wie einer mit rotem Phosphor beschichteten Stahlfolie verpackt sind.The document DE 10 2009 030 872 A1 relates to an active body that is ignited inductively, consisting of individual flares which are packaged in a carrier material such as a steel foil coated with red phosphorus.

Aus dem Dokument DE 10 2010 013 110 A1 ist ein gekapselter Wirkkörper mit einer Vielzahl an Einzelkomponenten für ein Infrarot-Scheinziel bekannt, der eine zentrale Längsanzündung vorsiehtFrom the document DE 10 2010 013 110 A1 an encapsulated active body with a large number of individual components for an infrared dummy target is known, which provides a central longitudinal ignition

Das Dokument DE 10 2004 047 231 A1 offenbart einen gattungsgemäßen Wirkkörper, der eine Mehrzahl an Wirkmassen und Anzündmitteln aufweist. Wie die Anzündung vorgenommen wird und wie die Anzündmittel angeordnet sind, ist nicht offenbart.The document DE 10 2004 047 231 A1 discloses a generic active body which has a plurality of active compounds and igniting agents. How the ignition is carried out and how the ignition means are arranged is not disclosed.

Aus der US 2005/0241521 A1 ist ebenfalls ein Wirkkörper bekannt, mit wenigstens zwei Wirkmassen, die über einen Detonator gezündet werden.From the US 2005/0241521 A1 An active body is also known, with at least two active masses that are ignited via a detonator.

Je nach Grundmaterial und Geometrie des Wirkkörpers kann es vorkommen, dass kein geeigneter zugelassener oder zu belastbarer Überzugsatz existiert, welcher für die Einführung als militärischen Wirkkörper verwendet werden kann. Eine Änderung der Wirkmassenkomposition oder Geometrie ist allerdings aufgrund vorhandener Systeme nicht ohne Einschränkung möglich, sodass sich hier ein Zielkonflikt ergibt.Depending on the base material and geometry of the active body, it may happen that there is no suitable approved or resilient cover set that can be used for introduction as a military active body. However, changing the active mass composition or geometry is not possible without restrictions due to existing systems, which results in a conflict of objectives.

Ferner kann ohne Überzugsatz ein all- bzw. mehrseitige Anzündbarkeit nicht gewährleistet werden.Furthermore, without a cover set, ignitability on all or multiple sides cannot be guaranteed.

Ausgehend davon, liegt der Erfindung die Aufgabe zugrunde, einen Wirkkörper zu schaffen, der eine schnelle und zuverlässige Anzündung mehrerer Wirkmassen ermöglicht.Based on this, the invention is based on the object of creating an active body which enables rapid and reliable ignition of several active substances.

Diese Aufgabe wird durch den Wirkkörper des Anspruchs 1 gelöst. Weiterhin wird diese Aufgabe durch das Verfahren des Anspruchs 13 gelöst. Vorteilhafte Ausgestaltungen und Weiterbildungen sind Gegenstand der jeweiligen Unteransprüche.This task is solved by the active body of claim 1. Furthermore, this task is solved by the method of claim 13. Advantageous refinements and further developments are the subject of the respective subclaims.

Erfindungsgemäß wird ein Wirkkörper, insbesondere Scheinzielwirkkörper bereitgestellt, umfassend zumindest eine Wirkmasse, zumindest zwei Anzündmittel jeweils umfassend einen pyrotechnischen Satz zum Anzünden der zumindest einen Wirkmasse. Die zumindest zwei Anzündmittel sind an der zumindest einen Wirkmasse angeordnet und die zumindest zwei Anzündmittel sind derart untereinander über Kanäle miteinander verbunden, dass die zumindest eine Wirkmasse mehrseitig gleichzeitig anzündbar ist.According to the invention, an active body, in particular a dummy target active body, is provided, comprising at least one active mass, at least two ignition means, each comprising one Pyrotechnic set for igniting at least one active mass. The at least two ignition means are arranged on the at least one active mass and the at least two ignition means are connected to one another via channels in such a way that the at least one active mass can be ignited on multiple sides at the same time.

Weiterhin wird erfindungsgemäß ein Verfahren zum Zünden eines solchen oder wie nachfolgend beschriebenen Wirkkörpers bereitgestellt. Der Wirkkörper umfasst zumindest eine Wirkmasse, zumindest zwei Anzündmittel jeweils umfassend einen pyrotechnischen Satz zum Anzünden der Wirkmassen. Die zumindest zwei Anzündmittel sind an der zumindest einen Wirkmasse angeordnet und die zumindest zwei Anzündmittel sind derart untereinander über Kanäle miteinander verbunden, dass die zumindest eine Wirkmasse mehrseitig gleichzeitig anzündbar ist.Furthermore, according to the invention, a method for igniting such an active body or as described below is provided. The active body comprises at least one active mass, at least two ignition means, each comprising a pyrotechnic set for igniting the active masses. The at least two ignition means are arranged on the at least one active mass and the at least two ignition means are connected to one another via channels in such a way that the at least one active mass can be ignited on multiple sides at the same time.

Es wird somit erfindungsgemäß vorgeschlagen den Wirkkörper so auszubilden, dass dieser mehrseitig jedoch mindestens an zwei Seiten, zum Beispiel an den Seitenflächen als auch der gegenüberliegenden Seite initiierbar, also anzündbar ist. Es handelt sich somit um einen Wirkkörper mit Mehrfachanzündung.It is therefore proposed according to the invention to design the active body in such a way that it can be initiated on multiple sides but at least on two sides, for example on the side surfaces as well as the opposite side, i.e. ignited. It is therefore an active body with multiple ignition.

Bei der zumindest einen Wirkmasse handelt es sich vorzugsweise um zumindest eine pyrotechnische Wirkmasse, wie diese bei Flares zum Einsatz kommen.The at least one active substance is preferably at least one pyrotechnic active substance, such as those used in flares.

Bei den Kanälen handelt es sich vorzugsweise um Zündkanäle, die dazu ausgebildet sind die Anzündmittel anzuzünden bzw. eine Anzündung bis zu den Anzündmitteln leiten. Die Kanäle können symmetrisch und/oder unsymmetrisch zueinander angeordnet sein.The channels are preferably ignition channels which are designed to ignite the ignition means or to conduct ignition up to the ignition means. The channels can be arranged symmetrically and/or asymmetrically to one another.

Mehrseitig gleichzeitig heißt, dass der Wirkkörper bzw. die zumindest eine Wirkmasse an mehreren Stellen, wie Seiten, Oberseite, Unterseite oder Kanten gleichzeitig zündbar ist. Gleichzeit im Sinne der Erfindung bedeutet, dass die zumindest eine Wirkmassen im Wesentlichen ohne zeitliche Verzögerung anzündbar sind.Multi-sided at the same time means that the active body or the at least one active mass can be ignited simultaneously at several points, such as sides, top, bottom or edges. Simultaneous in the sense of the invention means that the at least one active mass can be ignited essentially without any time delay.

Bei den Anzündmitteln im Sinne der Erfindung handelt es ich beispielsweise um Zündpillen, kleinere zündempfindliche pyrotechnische Sätze oder andere bekannte Anzündmittel.The igniting means in the sense of the invention are, for example, squibs, smaller ignition-sensitive pyrotechnic sets or other known igniting means.

Durch die erfindungsgemäße mehrseitige Anzündung wird erreicht, dass großflächige wenig empfindliche Wirkmassen durch deutlich kleinere Anzündmittel schnell und zuverlässig anzündbar sind.The multi-sided ignition according to the invention ensures that large-area, less sensitive active substances can be ignited quickly and reliably using significantly smaller ignition means.

Da eine Mehrzahl an Anzündmitteln vorgesehen ist, ergibt sich eine Verbesserung der Zuverlässigkeit der Anzündung durch dieses redundante Vorsehen der Anzündmittel.Since a plurality of ignition means is provided, the reliability of the ignition is improved by this redundant provision of the ignition means.

Ferner wird erreicht, dass ein solcher Wirkkörper unmittelbar nach einem Ausstoßen (bspw. aus einem Flugzeug) ein allseitiges Irritationsergebnis hat und anfliegende Flugkörper zuverlässig abgewehrt werden können.Furthermore, it is achieved that such an active body has an all-round irritation result immediately after being ejected (e.g. from an aircraft) and incoming missiles can be reliably repelled.

Zudem wird durch den erfindungsgemäßen Wirkkörper, insbesondere durch die gleichzeitig mehrseitige Anzündbarkeit der zumindest einen Wirkmasse ein geringeres Streuungsverhalten und eine verbesserte Reaktionsfreudigkeit im Einsatz erreicht. Zudem ergibt sich eine bessere Wirkentfaltung des Wirkkörpers.In addition, the active body according to the invention, in particular due to the simultaneous ignitability of the at least one active mass on multiple sides, achieves lower scattering behavior and improved reactivity in use. In addition, there is a better development of the effect of the active body.

In vorteilhafter Weiterbildung der Erfindung kann vorgesehen sein, dass mehrere, vorzugsweise jede, der Wirkmassen des Wirkkörpers mehrseitig gleichzeitig anzündbar sind.In an advantageous development of the invention, it can be provided that several, preferably each, of the active masses of the active body can be ignited on multiple sides at the same time.

Die zumindest zwei Wirkmassen können gleichgroß und/oder unterschiedlich groß sein. Durch eine Vielzahl an unterschiedlichen Wirkmassen ist es möglich eine Wellenlängeneinstellung des von dem Wirkkörper während des Abbrands der Wirkmassen abgestrahlten Spektrum vorzunehmen.The at least two active masses can be the same size and/or different sizes. By using a large number of different active substances, it is possible to adjust the wavelength of the spectrum emitted by the active body during the burning of the active substances.

In vorteilhafter Weiterbildung weist der Wirkkörper zumindest zwei Wirkmassen auf und die Anzündmittel sind derart zwischen den Wirkmassen des Wirkkörpers angeordnet sind, dass die zumindest zwei Wirkmassen mehrseitig gleichzeitig anzündbar sind.In an advantageous development, the active body has at least two active compounds and the ignition means are arranged between the active compounds of the active body in such a way that the at least two active compounds can be ignited on multiple sides at the same time.

Hierdurch wird erreich, dass jede der Wirkmassen des Wirkkörpers zuverlässig und gleichzeitig gezündet wird und sich ein allseitiges gutes Irritationsergebnis durch den Wirkkörper ergibt.This ensures that each of the active masses of the active body is ignited reliably and simultaneously and that an all-round good irritation result is achieved by the active body.

Ferner kann vorteilhafterweise vorgesehen sein, dass die Anzündmittel innerhalb und/oder außerhalb des Wirkkörpers angeordnet sind.Furthermore, it can advantageously be provided that the ignition means are arranged inside and/or outside of the active body.

Weiterhin kann vorgesehen sein, dass der pyrotechnische Satz der Anzündmittel und die zumindest eine Wirkmasse durch ein inertes Material voneinander getrennt sind.Furthermore, it can be provided that the pyrotechnic set of ignition means and the at least one active mass are separated from one another by an inert material.

Hierdurch wird eine definierte Trennung der zumindest einen Wirkmasse von dem pyrotechnischen Satz des Anzündmittels erreicht. Dies verhindert eine chemische Beeinflussung von Wirkmasse und pyrotechnischem Satz untereinander bei der Lagerung des Wirkkörpers. Weiterhin wird hierdurch eine ungewollte Zündung vermieden. Zudem wird hierdurch erreicht, dass eine definierte Zündenergie nötig ist, um den Körper zu zünden.This achieves a defined separation of the at least one active mass from the pyrotechnic composition of the igniter. This prevents chemical influences between the active substance and the pyrotechnic composition when storing the active body. Furthermore, this prevents unwanted ignition. This also ensures that a defined ignition energy is required to ignite the body.

In Ausgestaltung kann ferner vorgesehen sein, dass die zumindest eine Wirkmasse und/oder die Anzündmittel durch eine Folie, ein Gehäuse oder einen Luftspalt voneinander getrennt sind. Vorzugsweise können die einzelnen Wirkmassen derart voneinander getrennt sein.In an embodiment it can further be provided that the at least one active mass and/or the ignition means are separated from one another by a film, a housing or an air gap. The individual active substances can preferably be separated from one another in this way.

Eine solche physische Trennung kann beispielsweise durch eine Folie oder ein Gehäuse aus Papier, Kunststoff oder Metall geschehen.Such physical separation can occur, for example, using a film or a housing made of paper, plastic or metal.

Zudem kann vorgesehen sein, dass der Wirkkörper Rillen, Nuten und/oder Bohrungen aufweist. In den Rillen, Nuten und/oder Bohrungen verlaufen die Kanäle. Vorzugsweise sind durch diese Rillen und/oder Nuten die einzelnen Wirkmassen getrennt. Es ist aber auch möglich, dass sich die Rillen, Nuten und/oder Bohrungen innerhalb einer Wirkmasse erstrecken.In addition, it can be provided that the active body has grooves, grooves and/or bores. The channels run in the grooves, grooves and/or holes. The individual active compounds are preferably separated by these grooves and/or grooves. However, it is also possible for the grooves, grooves and/or holes to extend within an active mass.

Durch das Vorsehen von Rillen, Nuten und/oder Bohrungen wird einerseits die Positionierung der Kanäle vorgegeben und andererseits erreicht, dass die Kanäle nicht oder nur geringfügig über die Kontur des Wirkkörpers hervorstehen.By providing grooves, grooves and/or bores, on the one hand the positioning of the channels is specified and on the other hand it is ensured that the channels do not protrude or only protrude slightly beyond the contour of the active body.

In Weiterbildung kann vorgesehen sein, dass die Rillen und/oder Nuten derart verlaufen, dass diese sich an mehreren Kreuzungspunkten kreuzen und die Anzündmittel in den Kreuzungspunkten ausgebildet sind.In a further development, it can be provided that the grooves and/or grooves run in such a way that they cross each other at several crossing points and the ignition means are formed in the crossing points.

Durch das vorsehen von solchen Kreuzungspunkten wird erreicht, dass mehrere Wirkmassen, beispielsweise vier oder acht an einem Kreuzungspunkt voneinander beabstandet vorgesehen sind und somit eine Mehrzahl an Wirkmassen an einem Punkt durch ein Anzündmittel gezündet werden können.By providing such crossing points, it is achieved that several active masses, for example four or eight, are provided at a distance from one another at a crossing point and thus a plurality of active masses can be ignited at one point by an igniter.

Ferner kann vorgesehen sein, dass die Rillen, Nuten und/oder Bohrungen innerhalb und/oder außerhalb des Wirkkörpers angeordnet sind.Furthermore, it can be provided that the grooves, grooves and/or bores are arranged inside and/or outside the active body.

Zudem kann vorgesehen sein, dass der Wirkkörper durch eine Folie oder ein Gehäuse vor Umwelteinflüssen geschützt ist. Hierdurch wird erreich, dass der Wirkkörper auch bei hohen Wind- und/oder Ausstoßgeschwindigkeiten - also zum Beispiel beim Verschuss aus einem schnellfliegenden Fluggerät oder Luftfahrzeug - zuverlässig angezündet werden kann.In addition, it can be provided that the active body is protected from environmental influences by a film or a housing. This ensures that the active body can be reliably ignited even at high wind and/or ejection speeds - for example when fired from a fast-flying aircraft or aircraft.

Weiterhin kann gemäß der Erfindung vorgesehen sein, dass der Wirkkörper keinen pyrotechnischen Überzugsatz aufweist, der den gesamten Wirkkörper überzieht. Bei einem solchen Überzugsatz handelt es sich um einen schnell brennenden Satz, der den Wirkkörper überzieht und eine allseitige Anzündung erlaubt. Dies hat den Vorteil, dass auch, wenn kein geeigneter zugelassener Überzugssatz existiert, der Wirkkörper zugelassen werden kann.Furthermore, according to the invention it can be provided that the active body does not have a pyrotechnic coating set that covers the entire active body. Such a coating set is a fast-burning set that contains the active body covers and allows ignition from all sides. This has the advantage that the active body can be approved even if there is no suitable approved coating set.

Es kann vorgesehen sein, dass die Anzündmittel derart angeordnet sind und die Länge der Kanäle derart ausgebildet ist, dass die Anzündmittel gleichzeitig anzündbar sind.It can be provided that the ignition means are arranged in such a way and the length of the channels is designed such that the ignition means can be ignited at the same time.

Ferner kann vorgesehen sein, dass die Anzündmittel über die Kanäle mit einem Zündinitiator verbunden sind.Furthermore, it can be provided that the ignition means are connected to an ignition initiator via the channels.

In Ausgestaltung des Verfahrens kann ferner vorgesehen sein, dass mehrere Wirkmassen des Wirkkörpers mehrseitig gleichzeitig angezündet werden.In an embodiment of the method, it can also be provided that several active masses of the active body are ignited on multiple sides at the same time.

In vorteilhafter Weiterbildung kann ferner vorgesehen sein, dass der Wirkkörper im Wesentlichen quaderförmig ausgebildet ist und im Wesentlichen quaderförmige Wirkmassen aufweist. Hierbei kann es sich insbesondere um einen Wirkkörper für Munition im NATO Standardkaliber 2x1x8" oder 1x1x8" handeln.In an advantageous further development, it can further be provided that the active body is essentially cuboid-shaped and has essentially cuboid-shaped active masses. This can in particular be an active body for ammunition in the NATO standard caliber 2x1x8" or 1x1x8".

Ebenso kann es sich aber auch um eine zylinderförmigen Wirkkörper handeln, vorzugsweise mit einem Durchmesser von 36mm oder 55mm.It can also be a cylindrical active body, preferably with a diameter of 36mm or 55mm.

Ferner ist es möglich, dass es sich um eine kugelförmigen oder dreieckförmigen Wirkkörper handelt.It is also possible that it is a spherical or triangular active body.

Nachfolgend soll die Erfindung anhand von einem Ausführungsbeispiel mit Bezug auf die Zeichnungen erläutert werden.The invention will be explained below using an exemplary embodiment with reference to the drawings.

Es zeigen:

Fig. 1
eine schematische perspektivische Ansicht eines erfindungsgemäßen Wirkkörpers mit Kanälen gemäß einem ersten Ausführungsbeispiel;
Fig. 2
eine schematische perspektivische Ansicht des erfindungsgemäßen Wirkkörpers gemäß den ersten Ausführungsbeispiel aus Fig. 1, wobei die Kanäle ausgeblendet sind;
Fig. 3
eine schematische perspektivische Ansicht eines erfindungsgemäßen Wirkkörpers gemäß einem zweiten Ausführungsbeispiel, wobei der Wirkkörper innenliegende Kanäle ausweist;
Fig. 4
eine schematische perspektivische Ansicht eines erfindungsgemäßen Wirkkörpers gemäß einem dritten Ausführungsbeispiel, wobei der Wirkkörper innenliegende symmetrische und unsymmetrische Kanäle ausweist.
Show it:
Fig. 1
a schematic perspective view of an active body according to the invention with channels according to a first exemplary embodiment;
Fig. 2
a schematic perspective view of the active body according to the invention according to the first exemplary embodiment Fig. 1 , with the channels hidden;
Fig. 3
a schematic perspective view of an active body according to the invention according to a second exemplary embodiment, wherein the active body has internal channels;
Fig. 4
a schematic perspective view of an active body according to the invention according to a third exemplary embodiment, wherein the active body has internal symmetrical and asymmetrical channels.

Fig. 1 zeigt eine schematische perspektivische Ansicht eines erfindungsgemäßen Wirkkörpers 1. Der Wirkkörper 1 umfasst eine Mehrzahl an Wirkmassen 101...n und eine Mehrzahl an Anzündmittel 201...n. Die Anzündmittels 201...n umfassend jeweils einen pyrotechnischen Satz zum Anzünden der Wirkmassen 101...n. Fig. 1 shows a schematic perspective view of an active body 1 according to the invention. The active body 1 comprises a plurality of active compounds 10 1...n and a plurality of igniters 20 1...n . The ignition means 20 1...n each comprises a pyrotechnic set for igniting the active masses 10 1...n .

Fig. 2 zeigt ebenso eine schematische perspektivische Ansicht des erfindungsgemäßen Wirkkörpers nach Fig.1, wobei die Kanäle 301...n ausgeblendet sind. Fig. 2 also shows a schematic perspective view of the active body according to the invention Fig.1 , where channels 30 1...n are hidden.

Die Anzündmittel 201...n sind zwischen den einzelnen Wirkmassen 101...n angeordnet und die Anzündmittel 201...n sind derart untereinander über Kanäle 301...n miteinander verbunden, dass der Wirkkörper 1 mehrseitig gleichzeitig anzündbar ist.The igniting means 20 1...n are arranged between the individual active masses 10 1...n and the igniting means 20 1...n are connected to one another via channels 30 1...n in such a way that the active body 1 can be ignited on multiple sides at the same time is.

Die Anzündmittel 201...n sind über die Kanäle 301...n mit einem Zündinitiator (nicht dargestellt) verbunden sind, wobei die Anzündmittel 201...n derart angeordnet und die Länge der Kanäle 301...n derart ausgebildet ist, dass die Anzündmittel 201...n gleichzeitig anzündbar sind.The ignition means 20 1...n are connected to an ignition initiator (not shown) via the channels 30 1...n , the ignition means 20 1 ... n being arranged in such a way and the length of the channels 30 1...n is designed such that the ignition means 20 1...n can be ignited at the same time.

Wie aus Fig. 2 ersichtlich, weist der Wirkkörper 1 Rillen und/oder Nuten 221...n auf, durch welche die einzelnen Wirkmassen 101...n voneinander getrennt sind. Die Rillen und/oder Nuten 251...n sind gemäß dem ersten Ausführungsbeispiel der Fig. 1 und 2 innerhalb des Wirkkörpers 1 und/oder außerhalb, also außenliegend, angeordnet.How out Fig. 2 As can be seen, the active body 1 has grooves and/or grooves 22 1...n , through which the individual active masses 10 1...n are separated from one another. The grooves and/or grooves 25 1...n are according to the first exemplary embodiment Fig. 1 and 2 arranged inside the active body 1 and/or outside, i.e. on the outside.

Die Rillen und/oder Nuten 221...n verlaufen derart, dass diese sich an mehreren Kreuzungspunkten 251...n kreuzen und die Anzündmittel 201...n in den Kreuzungspunkten 251...n angeordnet sind.The grooves and/or grooves 22 1...n run in such a way that they intersect at several intersection points 25 1...n and the ignition means 20 1...n are arranged in the intersection points 25 1...n .

Die Rillen und/oder Nuten 221...n nehmen, wie in Fig. 1 dargestellt, die Kanäle 301...n auf, d.h. die Kanäle 301...n sind in den Rillen und/oder Nuten angeordnet.Take the grooves and/or grooves 22 1...n , as in Fig. 1 shown, the channels 30 1...n , ie the channels 30 1...n are arranged in the grooves and/or grooves.

Die einzelnen Kanäle 301...n sind wulstartig ausgebildet.The individual channels 30 1...n are designed like a bead.

Die einzelnen Wirkmassen 101...n des Wirkkörpers 1 sind mehrseitig gleichzeitig anzündbar.The individual active masses 10 1...n of the active body 1 can be ignited on multiple sides at the same time.

Die Anzündmittel 201...n sind gemäß Ausführungsbespiel innerhalb/außerhalb des Wirkkörpers 1 angeordnet. Hierzu sind diese in den Nuten/Rillen des Wirkkörpers 1 vorgesehen.The ignition means 20 1...n are arranged inside/outside the active body 1 according to the exemplary embodiment. For this purpose, these are provided in the grooves/grooves of the active body 1.

Der pyrotechnische Satz der Anzündmittel 201...n und die Wirkmassen 101...n sind durch ein inertes Material voneinander getrennt. Dies kann beispielsweise als eine Folie, ein Gehäuse oder ein Luftspalt ausgebildet sein.The pyrotechnic set of igniting agents 20 1...n and the active masses 10 1...n are separated from one another by an inert material. This can be designed, for example, as a film, a housing or an air gap.

Gemäß Fig. 3 ist eine schematische perspektivische Ansicht eines erfindungsgemäßen Wirkkörpers 1 gemäß einem zweiten Ausführungsbeispiel gezeigt, das auf dem Ausführungsbeispiel gemäß der Fig.1 basiert und nachfolgend ergänzend die Unterschiede dargestellt sind. Der Wirkkörper 1 weist innenliegende Nuten, Rillen und/oder Bohrungen 231...n auf, in denen Kanäle 311...n ausgebildet sind. Die Kanäle 311...n sind innerhalb der einzelnen Wirkmassen 101...n ausgebildet und haben ein symmetrisches Bild.According to Fig. 3 is a schematic perspective view of an active body 1 according to the invention according to a second exemplary embodiment, which is based on the exemplary embodiment according to the Fig.1 based and the differences are shown below. The active body 1 has internal grooves, grooves and/or bores 23 1...n , in which channels 31 1...n are formed. The channels 31 1...n are formed within the individual active masses 10 1...n and have a symmetrical image.

Gemäß Fig. 4 ist eine schematische perspektivische Ansicht eines erfindungsgemäßen Wirkkörpers 1 gemäß einem dritten Ausführungsbeispiel gezeigt, das auf dem Ausführungsbeispiel gemäß Fig. 3 basiert. Im Gegensatz zu dem Ausführungsbeispiel nach Fig. 3 sind die innenliegenden Kanäle 311...n in innerhalb der einzelnen Wirkmassen 101...n symmetrisch und/oder unsymmetrisch Kanäle 311...n ausgebildet.According to Fig. 4 is a schematic perspective view of an active body 1 according to the invention according to a third exemplary embodiment, which is based on the exemplary embodiment according to Fig. 3 based. In contrast to the exemplary embodiment Fig. 3 the internal channels 31 1...n are formed into symmetrical and/or asymmetrical channels 31 1...n within the individual active masses 10 1... n .

Gemäß der in den Fig. 1 bis 4 dargestellten Ausführungsform handelt es sich um einen Wirkkörper 1, der acht Wirkmassen 101...8 und sechs Anzündmittel 201...6 umfasst. Der Wirkkörper 1 ist im Wesentlichen quaderförmig und umfasst im Wesentlichen quaderförmige Wirkmassen 101...8. Hierbei kann es sich insbesondere um einen Wirkkörper für Munition im NATO Standardkaliber 2×1×8" oder 1×1×8" handeln. Diese Ausgestaltung des vorstehenden Ausführungsbeispiel stellt jedoch lediglich ein exemplarisches Ausführungsbeispiel dar. Es sind aber auch eine andere Anzahl als acht Wirkmassen und sechs Anzündmittel möglich. Ebenso kann es sich aber auch um eine zylinderförmigen Wirkkörper handeln, vorzugsweise mit einem Durchmesser von 36mm oder 55mm. Ferner ist es möglich, dass es sich um eine kugelförmigen oder dreieckförmigen Wirkkörper handelt.According to the in the Fig. 1 to 4 The embodiment shown is an active body 1, which comprises eight active masses 10 1...8 and six igniters 20 1...6 . The active body 1 is essentially cuboid-shaped and comprises essentially cuboid-shaped active masses 10 1...8 . This can in particular be an active body for ammunition in the NATO standard caliber 2×1×8" or 1×1×8". However, this embodiment of the above exemplary embodiment only represents an exemplary embodiment. However, a number other than eight active masses and six igniters are also possible. It can also be a cylindrical active body, preferably with a diameter of 36mm or 55mm. It is also possible that it is a spherical or triangular active body.

BezugszeichenlisteReference symbol list

11
Wirkkörperactive body
101...n101...n
WirkmassenActive masses
201...n201...n
Anzündmitteligniters
221...n221...n
Nuten, Rillen und/oder Bohrungen (innenliegend)Grooves, grooves and/or holes (internal)
231...n231...n
Nuten, Rillen und/oder Bohrungen (außenliegend)Grooves, grooves and/or holes (external)
251...n251...n
Kreuzungspunkte (innenliegend)Crossing points (internal)
261...n261...n
Kreuzungspunkte (außenliegend)Crossing points (external)
301...n301...n
Kanäle (innenliegend)Channels (internal)
311...n311...n
Kanäle (außenliegend)Channels (external)

Claims (14)

  1. Active element (1), in particular a decoy active element, comprising
    at least one active substance (101...n),
    at least two ignition means (201...n), each comprising a pyrotechnic composition for igniting the active substances (101...n),
    characterized in that
    the at least two ignition means (201...n) are arranged on the at least one active substance (101...n) and the at least two ignition means (201...n) are connected to one another via channels (301...n, 311...n) in such a way that the at least one active substance (101...n) can be ignited simultaneously from a plurality of sides.
  2. Active element (1) according to claim 1, characterized in that the active element (1) comprises at least two active substances (101...n) and the ignition means (201...n) are arranged between the active substances (101...n) of the active element (1) in such a way that the at least two active substances (101...n) can be ignited simultaneously from a plurality of sides.
  3. Active element (1) according to claim 1 or claim 2, characterized in that the at least two ignition means (201...n) are arranged inside and/or outside the active element (1).
  4. Active element (1) according to any of the preceding claims, characterized in that the pyrotechnic composition of each ignition means (201...n) and the at least one active substance (10) are separated from one another by an inert material.
  5. Active element (1) according to claim 4, characterized in that the at least one active substance and/or the ignition means (201...n) are separated from one another by a film, a housing and/or an air gap.
  6. Active element (1) according to any of the preceding claims, characterized in that the active element (1) has grooves, slots and/or bores (221...n, 231...n) by means of which the individual active substances (101...n) are separated and in which the channels (301...n, 311...n) extend.
  7. Active element (1) according to any of the preceding claims, characterized in that the at least one active substance (101...n) has grooves, slots and/or bores (221...n, 231...n) in which the channels (301...n, 31...n) extend.
  8. Active element (1) according to claim 6, characterized in that the grooves, slots and/or bores (221...n, 231...n) extend in such a way that they intersect at a plurality of intersection points (251...n, 261...n) and the ignition means (201...n) are formed at the intersection points (251...n, 261...n).
  9. Active element (1) according to any of the preceding claims, characterized in that the grooves, slots and/or bores (221...n, 231...n) are arranged inside and/or outside the active element (1).
  10. Active element (1) according to any of the preceding claims, characterized in that the active element (1) is protected from environmental influences by an inert film or a housing.
  11. Active element (1) according to any of the preceding claims, characterized in that the active element (1) does not have a pyrotechnic coating composition which coats the entire active element (1).
  12. Active element (1) according to any of the preceding claims, characterized in that the length of the channels (301...n, 311...n) is formed in such a way that the ignition means (201...n) can be ignited simultaneously.
  13. Method for igniting an active element (1), in particular according to any of claims 1 to 12, comprising
    at least one active substance (101...n),
    at least two ignition means (201...n), each comprising a pyrotechnic composition for igniting the active substances (101...n),
    characterized in that
    the at least two ignition means (201...n) are arranged on the at least one active substance (101...n) and the at least two ignition means (201...n) are connected to one another via channels (301...n, 311...n) in such a way that the at least one active substance (101...n) can be ignited simultaneously from a plurality of sides.
  14. Method for igniting an active element (1) according to claim 13, characterized in that a plurality of active substances (101...n) of the active element (1) are ignited simultaneously from a plurality of sides.
EP20764989.8A 2019-10-01 2020-09-01 Active element and method for igniting an active element Active EP4038340B9 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102019126466.9A DE102019126466A1 (en) 2019-10-01 2019-10-01 Active body and method for igniting an active body
PCT/EP2020/074306 WO2021063615A1 (en) 2019-10-01 2020-09-01 Active element and method for igniting an active element

Publications (3)

Publication Number Publication Date
EP4038340A1 EP4038340A1 (en) 2022-08-10
EP4038340B1 EP4038340B1 (en) 2023-11-15
EP4038340B9 true EP4038340B9 (en) 2024-02-14

Family

ID=72322452

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20764989.8A Active EP4038340B9 (en) 2019-10-01 2020-09-01 Active element and method for igniting an active element

Country Status (9)

Country Link
EP (1) EP4038340B9 (en)
JP (1) JP2022550429A (en)
KR (1) KR20220071964A (en)
AU (1) AU2020358276A1 (en)
CA (1) CA3156363A1 (en)
DE (1) DE102019126466A1 (en)
ES (1) ES2969340T3 (en)
IL (1) IL291705A (en)
WO (1) WO2021063615A1 (en)

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2619597A1 (en) * 1976-05-04 1977-11-17 Dynamit Nobel Ag IGNITION DEVICE FOR INFRARED RADIATOR
DE2830119C2 (en) * 1978-07-08 1985-09-19 Nico-Pyrotechnik Hans-Jürgen Diederichs KG, 2077 Trittau Smoke charge for missiles and projectiles
GB9612655D0 (en) * 1996-06-17 2003-05-28 Secr Defence Infra-red emitting decoy flare
EP1342047B1 (en) * 2000-12-13 2006-02-22 The Secretary of State for Defence Infra-red emitting decoy flare
FR2867848B1 (en) * 2004-03-18 2006-04-28 Giat Ind Sa DEVICE FOR INITIATION OF TWO EXPLOSIVE LOADS AND MILITARY HEAD USING SUCH AN INITIATION DEVICE
DE102004047231B4 (en) 2004-09-28 2008-08-21 Rheinmetall Waffe Munition Gmbh submunitions
US7546806B1 (en) * 2006-03-24 2009-06-16 The United States Of America As Represented By The Secretary Of The Army Selectable output well perforator and method for producing variable hole profiles
DE102009030871B4 (en) 2009-06-26 2013-05-29 Rheinmetall Waffe Munition Gmbh Combustible mass container
DE102009030872A1 (en) 2009-06-26 2010-12-30 Rheinmetall Waffe Munition Gmbh submunitions
DE102010013110A1 (en) 2010-03-26 2011-09-29 Rheinmetall Waffe Munition Gmbh Encapsulated active body for an IR deception or decoy
DE102010030869A1 (en) 2010-07-02 2012-01-05 Ifm Electronic Gmbh Method for evaluating measurement signal of capacitive limit switch, involves modifying deviations of measurement values, determining maximum value of deviations, and evaluating measurement signal on basis of maximum value
DE102016122740A1 (en) 2016-11-24 2018-05-24 Rheinmetall Waffe Munition Gmbh Pyrotechnic active body

Also Published As

Publication number Publication date
DE102019126466A1 (en) 2021-04-01
WO2021063615A1 (en) 2021-04-08
EP4038340A1 (en) 2022-08-10
IL291705A (en) 2022-05-01
AU2020358276A1 (en) 2022-04-21
CA3156363A1 (en) 2021-04-08
ES2969340T3 (en) 2024-05-17
KR20220071964A (en) 2022-05-31
JP2022550429A (en) 2022-12-01
EP4038340B1 (en) 2023-11-15

Similar Documents

Publication Publication Date Title
EP0164732B1 (en) Apparatus for generating decoy clouds, in particular those emitting ir radiation
DE4139372C1 (en) Fragmentation warhead
EP1002213B1 (en) System for protecting objects against shaped charges
DE2738031C2 (en) Device for ejecting and separating bodies from or from a projectile or the like.
DE19524726B4 (en) warhead
EP0806623A1 (en) Spin stabilised carrier projectile
EP1794537B1 (en) Active charge
DE2107102A1 (en) Warhead with detonation-dependent control of the direction of the explosive effect
DE3934042C2 (en)
DE2907308C2 (en) Floor with at least one pushable daughter floor
DE2845414A1 (en) FLOOR TAKES EFFECT WHEN FLYING OVER THE TARGET
DE2556075C2 (en) Cartridge for shooting target objects used as bait
DE19917144B4 (en) Combination action system
EP0435083B1 (en) Adjustable stand-off member on a warhead with a hollow charge switchable between penetration and side operation
EP4038340B1 (en) Active element and method for igniting an active element
DE19830134B4 (en) Lighting torch for a helicopter and method for generating a bait trace
DE1578077C2 (en) Warhead for an anti-tank projectile
DE102007054382A1 (en) Ammunition, with a self-destruction facility, carries a small explosive charge to fracture the casing on a remote command
DE4139371C1 (en) Airborne target missile head has main charge enclosed by cylindrical sleeves incorporating charges detonated for ejection of sleeve on side facing towards target before detonation of main charge
DE2502456C1 (en) Missile to deploy a cloud of missiles
DE19629389C1 (en) Warhead for destruction of aerial targets
DE10230028A1 (en) System for protecting an object, especially an armored vehicle, against the effects of a fast projectile
DE19531287A1 (en) Warhead
DE4108633C2 (en) Use of the active part of a search fuse submunition as a practice ammunition with reduced range
EP2133653B1 (en) Smoke-producing projectile

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

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

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20220427

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL 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 RS SE SI SK SM TR

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20230531

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL 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 RS SE SI SK SM TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502020006067

Country of ref document: DE

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: CH

Ref legal event code: PK

Free format text: BERICHTIGUNG B9

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20231115

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: 20240216

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20240315

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

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: 20231115

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231115

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231115

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: 20231115

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: 20240315

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: 20240216

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: 20240215

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: 20240315

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2969340

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20240517

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231115

Ref country code: RS

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: 20231115

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: 20231115

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: 20240215

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: 20231115

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: 20231115