EP2827094B1 - Device for the controlled initiation of the deflagration of an explosive charge - Google Patents

Device for the controlled initiation of the deflagration of an explosive charge Download PDF

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EP2827094B1
EP2827094B1 EP14002294.8A EP14002294A EP2827094B1 EP 2827094 B1 EP2827094 B1 EP 2827094B1 EP 14002294 A EP14002294 A EP 14002294A EP 2827094 B1 EP2827094 B1 EP 2827094B1
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Prior art keywords
explosive charge
core
explosive
charge
deflagration
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German (de)
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EP2827094A1 (en
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Markus Graswald
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TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
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TDW Gesellschaft fuer Verteidigungstechnische Wirksysteme mbH
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    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/02Fuze bodies; Fuze housings

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  • the invention relates to a device for the controlled initiation of the deflagration of an explosive charge, which is arranged in a sheath with non-constant diameter, comprising at least one extending in the region of the longitudinal axis of the explosive charge detonation cord, wherein the detonation cord is designed as an explosive charge core.
  • a dosable explosive charge for a warhead with two different ignition devices has become known. While the first ignition device detonatively initiates the explosive charge, the further, oppositely directed ignition device is designed such that at most a subdetonative initiation can take place. The use of at least one detonating cord for this purpose is also known from this. In practice, some problems have arisen which, in extreme cases, may lead to the termination of initiation or to complete detonation initiation.
  • the US 2012/0227609 A1 describes an ignition system with two different ignition devices.
  • the first ignition device is conventionally designed for the detonative triggering of the explosive charge.
  • the locally opposite second ignition device is dimensioned for a deflagrative initiation of the explosive charge. Since in this ignition system the same construction principle with opposite ignition points is used, from which the detonation waves run against each other, the already known deficiencies occur here as well.
  • the DE 10 2005 031 588 B3 discloses the preamble of independent claim 1 and shows a device for the controlled initiation of the deflagration of an explosive charge, which is arranged in a casing comprising at least one extending in the region of the longitudinal axis of the explosive charge Detonation cord, the detonation cord is designed as an explosive charge core. Other features of the detonation cord are not described.
  • the present invention has the object to develop an ignition device which is able to maintain a deflagrative initiation over the entire length of the explosive charge, without the deflagration reaction in the axial or radial direction passes into a burn, dies or turns into a detonation.
  • the explosive charge core can be fired from both ends as required.
  • the transverse dimension of the explosive charge core is adapted to the course of the envelope in the longitudinal direction of the explosive charge. This can be done in stages or continuously so that the explosive charge core can be matched to any shape of the envelope.
  • Another adaptation option is that the charging of the explosive charge core over the length of the explosive charge core with respect to the type of explosive is homogeneously or locally differently adjustable. It can therefore be combined with each other to an explosive charge core if necessary, also different explosive types.
  • This jacket or tube may for example consist of a plastic layer or a fabric or a combination of the two.
  • a material for a sheath include textile fibers, plastics (polymers) such.
  • polyethylene polyethylene, Kvlar, nylon, polypropylene but also wax into consideration.
  • the deflagrator which is initiated in the smallest action mode alone, triggers a subdetonative reaction called deflagration.
  • deflagration a subdetonative reaction
  • the reaction ultimately leads to an increase in pressure under which the explosive can also mechanically fail and crack and continue to propagate.
  • the speed of the pressure front is in the range of the speed of sound of the explosive.
  • a stable deflagration results from the rate of energy dissipation compared to the rate of energy production, which is controlled by the detonation cord here.
  • Insensitive explosive charges contain at least 10% of the plastic binder.
  • the proportion of the explosive molecule, for which Hexogen, octogen, Fox-7 (1,1-diamino-2,2-dinitroethylene) and others, can be between 90 and 50%.
  • Suitable binders include, inter alia, a two-component casting resin with hydroxyl-terminated polybutadiene (HTPB), but also silicone rubber, polyurethane rubber, polystyrene, Estan or nylon.
  • HTPB hydroxyl-terminated polybutadiene
  • the binder encapsulates the explosive crystals.
  • Such a plastic-bound explosive charge basically has microscopically small pores as a result of the manufacturing process. These pores determine the porosity of the explosive charge and provide the necessary for the deflagration reaction free surface available.
  • the porosities are typically in the single-digit percentage range.
  • the explosive charge may additionally have coated or uncoated metal powder with particles such as aluminum, magnesium, titanium carbide or zirconium carbide.
  • particles such as aluminum, magnesium, titanium carbide or zirconium carbide.
  • a share of 15 to 25 mass percent is sought to optimize the blast pressure.
  • a detonation cord or an explosive charge core are relatively high-energy (highly explosive) and / or sensitive explosives such.
  • high-energy highly explosive
  • sensitive explosives such as hexogen- or octogen-based explosives mixtures, and RDX, PETN, HMX, HNS or explosive mixtures thereof.
  • the detonating cord or detonating core should additionally have a fabric or plastic sheath which prevents direct contact with the explosive charge and results in damping of the shockwave upon detonation of the detonating cord or detonating core.
  • the diameter of the explosive charge core can vary with non-constant sheath diameter and be adapted directly to this.
  • the charging of the detonation cord is to be adapted to the size and shape of the explosive charge or cargo envelope.
  • the relevant parameters are the wall thickness, also in comparison to the charge diameter, and the material strength. These are expediently linked together via the static failure pressure. Above a specific limit pressure, more likely undesirable transitions into stronger reactions (Detonation-to-deflagration-transitions, DDTs) expected. Damping at the charge ends can be regulated by the aeration described below so that there is little difference between charges open at the ends (ie, the expansion rate and hence the pressure rate).
  • higher levels of damming especially if there is insufficient ventilation, may favor transitions into stronger reactions (DDTs).
  • the ventilation can be sustainably influenced by cargo cover, shell breakage and drilling, as long as it is a fully dammed explosive charge.
  • the ventilation is especially in the area of initiation, where the deflagration reaction begins and thereby the pressure increases first.
  • a permanent venting leads to a pressure rate with constant initiation over the charge length, which leads to a stable deflagration reaction over the charge radius.
  • This pressure rate can be measured indirectly via the expansion rate of the cargo envelope.
  • Suitable cladding materials are not only metals such as steel, aluminum, titanium or similar alloys, but also plastics or composite materials such as GRP or CFRP, as well as CRC or CFRC. This achieves a lower lethal effect, but a higher pressure wave.
  • FIG. 2 is a section through an active system shown, which is filled within the envelope HÃœ except for a slender cavity in the region of the longitudinal axis LA with explosive SP.
  • This unspecified cavity serves to receive the explosive charge core SK.
  • the explosive charge core extends from a first ignition device Z1 at the tip of the active system to a further ignition device Z2 at the rear of the active system. Both ignition devices can be used to initiate the explosive charge core.
  • the explosive charge core SK is divided into a plurality of sections A1, A2, A3. Depending on the requirements of the active system, the division may also make sense in fewer or more sections. Each of these sections corresponds to charging of the explosive charge core SK adapted to this section. It is also possible to adjust the course of charging according to the course of the envelope HÃœ such that the Charging decreases to a higher value in the middle range towards the end.
  • charging in section A1 can be in the value range 30 to 50 g / m, in the second range A2 in the value range 50 to 70 g / m and finally in the third range A3 in the value range 70 to 100 g / m.
  • cross section of the explosive charge core SK This can be designed, for example, rectangular, round oval, half round, depending on the need for adjustment, as in FIG. 3 is shown.
  • an explosive charge core can be applied to almost any shape and size of warhead and other active system. Another advantage is the significant reduction of

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Description

Die Erfindung betrifft eine Vorrichtung zur gesteuerten Initiierung der Deflagration einer Sprengladung, die in einer Hülle mit nicht konstantem Durchmesser angeordnet ist, umfassend wenigstens eine im Bereich der Längsachse der Sprengladung verlaufende Detonationsschnur, wobei die Detonationsschnur als Sprengladungskern ausgeführt ist..The invention relates to a device for the controlled initiation of the deflagration of an explosive charge, which is arranged in a sheath with non-constant diameter, comprising at least one extending in the region of the longitudinal axis of the explosive charge detonation cord, wherein the detonation cord is designed as an explosive charge core.

Aus der DE 100 08 914 C2 ist eine dosierbare Sprengladung für einen Gefechtskopf mit zwei unterschiedlichen Zündeinrichtungen bekannt geworden. Während die erste Zündeinrichtung die Sprengladung detonativ initiiert, ist die weitere, gegenläufig ausgerichtete Zündeinrichtung so ausgelegt, dass höchstens eine subdetonative Initiierung erfolgen kann. Auch die Verwendung von wenigstens einer Detonationsschnur für diesen Zweck ist hieraus bekannt. In der Praxis haben sich einige Probleme ergeben, die im Extremfall zum Erlöschen der Initiierung oder zur komplett detonativen Initiierung führen können.From the DE 100 08 914 C2 a dosable explosive charge for a warhead with two different ignition devices has become known. While the first ignition device detonatively initiates the explosive charge, the further, oppositely directed ignition device is designed such that at most a subdetonative initiation can take place. The use of at least one detonating cord for this purpose is also known from this. In practice, some problems have arisen which, in extreme cases, may lead to the termination of initiation or to complete detonation initiation.

Die US 2012/0227609 A1 beschreibt ein Zündsystem mit zwei unterschiedlichen Zündeinrichtungen. Die erste Zündeinrichtung ist konventionell für die detonative Auslösung der Sprengladung ausgelegt. Die örtlich gegenüber liegende zweite Zündeinrichtung ist für eine deflagrative Initiierung der Sprengladung dimensioniert. Da in diesem Zündsystem das selbe Bauprinzip mit gegenüber liegenden Zündstellen verwendet wird, von denen aus die Detonationswellen gegeneinander laufen, treten auch hier die bereits bekannten Mängel auf.The US 2012/0227609 A1 describes an ignition system with two different ignition devices. The first ignition device is conventionally designed for the detonative triggering of the explosive charge. The locally opposite second ignition device is dimensioned for a deflagrative initiation of the explosive charge. Since in this ignition system the same construction principle with opposite ignition points is used, from which the detonation waves run against each other, the already known deficiencies occur here as well.

Die DE 10 2005 031 588 B3 offenbart den Oberbegriff des unabhängigen Anspruchs 1 und zeigt eine Vorrichtung zur gesteuerten Initiierung der Deflagration einer Sprengladung, die in einer Hülle angeordnet ist, umfassend wenigstens eine im Bereich der Längsachse der Sprengladung verlaufende Detonationsschnur, wobei die Detonationsschnur als Sprengladungskern ausgeführt ist. Weitere Merkmale der Detonationsschnur sind nicht beschrieben.The DE 10 2005 031 588 B3 discloses the preamble of independent claim 1 and shows a device for the controlled initiation of the deflagration of an explosive charge, which is arranged in a casing comprising at least one extending in the region of the longitudinal axis of the explosive charge Detonation cord, the detonation cord is designed as an explosive charge core. Other features of the detonation cord are not described.

Dem gegenüber liegt der vorliegenden Erfindung die Aufgabe zugrunde, eine Zündvorrichtung zu entwickeln, die in der Lage ist, eine deflagrative Initiierung über die gesamte Länge der Sprengladung aufrecht zu erhalten, ohne dass die Deflagrationsreaktion in axialer oder radialer Richtung in einen Abbrand übergeht, ausstirbt oder in eine Detonation umschlägt.On the other hand, the present invention has the object to develop an ignition device which is able to maintain a deflagrative initiation over the entire length of the explosive charge, without the deflagration reaction in the axial or radial direction passes into a burn, dies or turns into a detonation.

Die Aufgabe wird erfindungsgemäß durch die Merkmale des Anspruchs 1 gelöst. Hieraus ergeben sich diverse Gestaltungsmöglichkeiten, die in den weiteren Ansprüchen beschrieben sind und die eine Anpassung dieser Initiierung an die örtlichen Gegebenheiten in der Sprengladung ermöglichen.The object is achieved by the features of claim 1. This results in various design options, which are described in the other claims and allow an adaptation of this initiation to the local conditions in the explosive charge.

Der Sprengladungskern kann je nach den Erfordernissen von beiden Enden her gezündet werden. Erfindungsgemäß ist die Querabmessung des Sprengladungskerns dem Verlauf der Hülle in Längsrichtung der Sprengladung angepasst. Dies kann in Stufen erfolgen oder auch kontinuierlich, so dass damit der Sprengladungskern an jede Form der Hülle angeglichen werden kann.The explosive charge core can be fired from both ends as required. According to the invention, the transverse dimension of the explosive charge core is adapted to the course of the envelope in the longitudinal direction of the explosive charge. This can be done in stages or continuously so that the explosive charge core can be matched to any shape of the envelope.

Eine weitere Anpassungsmöglichkeit besteht darin, dass die Aufladung des Sprengladungskerns über die Länge des Sprengladungskerns hinsichtlich der Art des Sprengstoffes homogen oder örtlich unterschiedlich einstellbar ist. Es können somit bei Bedarf auch unterschiedliche Sprengstoffarten miteinander zu einem Sprengladungskern kombiniert werden.Another adaptation option is that the charging of the explosive charge core over the length of the explosive charge core with respect to the type of explosive is homogeneously or locally differently adjustable. It can therefore be combined with each other to an explosive charge core if necessary, also different explosive types.

Um den Übergang vom detonativ reagierenden Sprengstoffkern zur Sprengladung bewusst zu beeinflussen ist es hilfreich, wenn der Sprengladungskern von einem Mantel oder einem Rohr umgeben ist. Dieser Mantel oder das Rohr kann beispielsweise aus einer Kunststoffschicht oder einem Gewebe oder einer Kombination aus beiden bestehen. Als Material für eine Ummantelung (Mantel oder Rohr) kommen u. a. Textilfasern, Kunststoffe (Polymere) wie z. B. Polyethylen, Kvlar, Nylon, Polypropylen aber auch Wachs in Betracht.In order to consciously influence the transition from the detonating explosive core to the explosive charge, it is helpful if the explosive charge core of one Sheath or tube is surrounded. This jacket or tube may for example consist of a plastic layer or a fabric or a combination of the two. As a material for a sheath (jacket or tube) include textile fibers, plastics (polymers) such. As polyethylene, Kvlar, nylon, polypropylene but also wax into consideration.

Mit dem Deflagrator, der im Modus der kleinsten Wirkung allein initiiert wird, wird eine subdetonative Reaktion ausgelöst, die als Deflagration bezeichnet wird. Dies geschieht beispielsweise durch Detonation einer Detonationsschnur, wodurch die heißen Reaktionsgase noch nicht reagiertes energetisches Material konvektiv erhitzen. Dies setzt sich weiter über in der Sprengladung vorhandene Poren fort. Es bildet sich eine mehrphasige Reaktionszone heraus, bei der die Druck- und Flammfront im Gegensatz zur Detonation räumlich voneinander getrennt sind und sich durchaus mit unterschiedlicher Geschwindigkeit fortpflanzen können. Die Reaktion führt letztlich zu einer Druckerhöhung, unter der der Sprengstoff auch mechanisch versagen kann und sich Risse bilden und weiter fortpflanzen. Die Reaktionsgeschwindigkeiten hängen auch vom Verdämmungszustand der Sprengladung, d.h. Wandstärke und Festigkeit der Hülle, ab. Die Geschwindigkeit der Druckfront liegt dabei im Bereich der Schallgeschwindigkeit des Sprengstoffs.The deflagrator, which is initiated in the smallest action mode alone, triggers a subdetonative reaction called deflagration. This happens, for example, by detonation of a detonation cord, whereby the hot reaction gases heat unreacted energetic material convectively. This continues through pores present in the explosive charge. It forms a multi-phase reaction zone out, in which the pressure and flame front, in contrast to the detonation are spatially separated from each other and can well propagate at different speeds. The reaction ultimately leads to an increase in pressure under which the explosive can also mechanically fail and crack and continue to propagate. The reaction rates also depend on the state of confinement of the explosive charge, i. Wall thickness and strength of the shell, from. The speed of the pressure front is in the range of the speed of sound of the explosive.

Eine stabile Deflagration ergibt sich aus der Rate der Energiedissipation im Vergleich zur Energieerzeugungsrate, die hier durch die Detonationsschnur kontrolliert wird. Nachfolgend werden einige Systemeinflussfaktoren beschrieben und konkrete Zahlen / Zahlenbereiche für einzelne Parameter angegeben, bei denen eine kontrollierte Deflagration abläuft.A stable deflagration results from the rate of energy dissipation compared to the rate of energy production, which is controlled by the detonation cord here. Here are some system influencing factors described and specific numbers / ranges for individual parameters where controlled deflagration occurs.

Unempfindliche Sprengladungen enthalten einen Anteil des Kunststoffbinders von mindestens 10%. Der Anteil des Sprengstoffmoleküls, für das sich Hexogen, Oktogen, Fox-7 (1,1-Diamino-2,2-Dinitroethylen) u.a. anbieten, kann dabei zwischen 90 und 50% liegen. Als Binder eignet sich hierfür u. a. ein Zweikomponenten-Gießharz mit Hydroxyl-terminiertem Polybutadien (HTPB), aber auch Silikongummi, Polyurethangummi, Polystyren, Estan oder Nylon. Der Binder kapselt die Sprengstoffkristalle ein. Eine solche kunststoffgebundene Sprengladung verfügt grundsätzlich infolge des Herstellungsprozesses über mikroskopisch kleine Poren. Diese Poren bestimmen die Porosität der Sprengladung und stellen die für die Deflagrationsreaktion notwendige freie Oberfläche zu Verfügung. Die Porositäten liegen hierbei typischerweise im einstelligen Prozentbereich. Zur Steigerung der Blastdruckwirkung kann die Sprengladung zusätzlich über gecoatete oder nicht gecoatete Metallpulver mit Partikeln z.B. aus Aluminium, Magnesium, Titankarbid oder Zirkonkarbid verfügen. Hierbei wird ein Anteil von 15 bis 25 Masse-Prozenten angestrebt um den Blastdruck zu optimieren.Insensitive explosive charges contain at least 10% of the plastic binder. The proportion of the explosive molecule, for which Hexogen, octogen, Fox-7 (1,1-diamino-2,2-dinitroethylene) and others, can be between 90 and 50%. Suitable binders include, inter alia, a two-component casting resin with hydroxyl-terminated polybutadiene (HTPB), but also silicone rubber, polyurethane rubber, polystyrene, Estan or nylon. The binder encapsulates the explosive crystals. Such a plastic-bound explosive charge basically has microscopically small pores as a result of the manufacturing process. These pores determine the porosity of the explosive charge and provide the necessary for the deflagration reaction free surface available. The porosities are typically in the single-digit percentage range. To increase the Blastdruckwirkung the explosive charge may additionally have coated or uncoated metal powder with particles such as aluminum, magnesium, titanium carbide or zirconium carbide. Here, a share of 15 to 25 mass percent is sought to optimize the blast pressure.

Für eine Detonationsschnur oder einen Sprengladungskern eignen sich vergleichsweise energiereiche (hochbrisante) und/oder sensitive Sprengstoffe wie z. B. hexogen- oder oktogenbasierte Sprengstoffmischungen, sowie RDX, PETN, HMX, HNS oder Sprengstoffmischungen hieraus.For a detonation cord or an explosive charge core are relatively high-energy (highly explosive) and / or sensitive explosives such. As hexogen- or octogen-based explosives mixtures, and RDX, PETN, HMX, HNS or explosive mixtures thereof.

Die Detonationsschnur oder der Sprengladungskern sollte zusätzlich über eine Gewebe- oder Kunststoffummantelung verfügen, die einen direkten Kontakt mit der Sprengladung unterbindet und zu einer Dämpfung der Schockwelle bei der Detonation der Detonationsschnur oder des Sprengladungskerns führt. Zudem kann der Durchmesser des Sprengladungskerns bei nicht konstantem Hüllendurchmesser variieren und direkt an diesen angepasst werden. Die Aufladung der Detonationsschnur ist dabei an Größe und Form der Sprengladung bzw. Ladungshülle anzupassen.The detonating cord or detonating core should additionally have a fabric or plastic sheath which prevents direct contact with the explosive charge and results in damping of the shockwave upon detonation of the detonating cord or detonating core. In addition, the diameter of the explosive charge core can vary with non-constant sheath diameter and be adapted directly to this. The charging of the detonation cord is to be adapted to the size and shape of the explosive charge or cargo envelope.

Bei Vorhandensein einer Ladungshülle sind die relevanten Parameter die Wandstärke, auch im Vergleich zum Ladungsdurchmesser, und die Materialfestigkeit. Diese werden über den statischen Versagensdruck zweckmäßig miteinander verknüpft. Oberhalb eines spezifischen Grenzdrucks werden mit höherer Wahrscheinlichkeit unerwünschte Übergänge in stärkere Reaktionen (Detonation-to-Deflagration-Transitions, DDTs) erwartet. Eine Verdämmung an den Ladungsenden kann durch die nachfolgend beschriebene Belüftung so reguliert werden, dass sich kaum Unterschiede zu an den Enden offenen Ladungen zeigen (d.h. durch die Aufweitungsgeschwindigkeit und damit der Druckrate).In the presence of a charge envelope, the relevant parameters are the wall thickness, also in comparison to the charge diameter, and the material strength. These are expediently linked together via the static failure pressure. Above a specific limit pressure, more likely undesirable transitions into stronger reactions (Detonation-to-deflagration-transitions, DDTs) expected. Damping at the charge ends can be regulated by the aeration described below so that there is little difference between charges open at the ends (ie, the expansion rate and hence the pressure rate).

Der Versagensdruck einer Verdämmung unter statischer Belastung wird berechnet anhand p max = σ max 1 − k 2 1 + k 2

Figure imgb0001
mit k = di /da , di als Innendurchmesser, da als Außendurchmesser und σmax als Maximalspannung. Eine Verdämmung mit einem statischen Versagendruck kleiner als 2,6 kBar, typischerweise kleiner als 2,0 kBar, wird dabei, sofern die Initiierung optimal an die Ladungsabmessungen angepasst ist, als günstig angesehen, um eine kontrolliert ablaufende Deflagration zu gewährleisten. Im Gegensatz dazu können höhere Verdämmungswerte, insbesondere wenn keine ausreichende Belüftung vorhanden ist, Übergänge in stärkere Reaktionen (DDTs) begünstigen. Grundsätzlich kann die Belüftung durch Ladungsdeckel, Sollbruchstellen der Hülle und Bohrungen nachhaltig beeinflusst werden, sofern es sich um eine vollständig verdämmte Sprengladung handelt. Vorteilhaft ist die Belüftung insbesondere im Bereich der Initiierung, wo die Deflagrationsreaktion beginnt und hierdurch der Druck zuerst ansteigt. Eine permanente Entlüftung führt bei konstanter Initiierung über die Ladungslänge zu einer Druckrate, die zu einer stabilen Deflagrationsreaktion über den Ladungsradius führt. Diese Druckrate lässt sich indirekt über die Aufweitungsgeschwindigkeit der Ladungshülle messen. Als Hüllenmaterial eignen sich nicht nur Metalle wie Stahl, Aluminium, Titan oder entsprechende Legierungen, sondern auch Kunststoffe oder Komposit-Werkstoffe wie GFK oder CFK, sowie CRC oder CFRC. Damit wird eine geringere letale Wirkung erreicht, dagegen aber eine höhere Druckwelle.The failure pressure of a static load suspension is calculated by p Max = σ Max 1 - k 2 1 + k 2
Figure imgb0001
with k = d i / d a , di as inner diameter, as outer diameter and σ max as maximum stress. A stagnation with a static failure pressure of less than 2.6 kbar, typically less than 2.0 kbar, is considered favorable, provided the initiation is optimally adapted to the charge dimensions, in order to ensure controlled deflagration. In contrast, higher levels of damming, especially if there is insufficient ventilation, may favor transitions into stronger reactions (DDTs). Basically, the ventilation can be sustainably influenced by cargo cover, shell breakage and drilling, as long as it is a fully dammed explosive charge. Advantageously, the ventilation is especially in the area of initiation, where the deflagration reaction begins and thereby the pressure increases first. A permanent venting leads to a pressure rate with constant initiation over the charge length, which leads to a stable deflagration reaction over the charge radius. This pressure rate can be measured indirectly via the expansion rate of the cargo envelope. Suitable cladding materials are not only metals such as steel, aluminum, titanium or similar alloys, but also plastics or composite materials such as GRP or CFRP, as well as CRC or CFRC. This achieves a lower lethal effect, but a higher pressure wave.

Ein Ausführungsbeispiel ist in der Zeichnung dargestellt und wird im Folgenden näher beschrieben. Es zeigen:

Fig.1:
die Radiallänge einer Sprengladung in Relation zur Aufladung eines Sprengladungskerns;
Fig.2:
ein Ausführungsbeispiel einer erfindungsgemäßen Vorrichtung bei der Verwendung in einem bekannten Wirksystem;
Fig.3:
Beispiele möglicher Querschnitte von Sprengladungskernen.
An embodiment is shown in the drawing and will be described in more detail below. Show it:
Fig.1:
the radial length of an explosive charge in relation to the charging of an explosive charge core;
Figure 2:
an embodiment of a device according to the invention when used in a known active system;
Figure 3:
Examples of possible cross sections of explosive charge cores.

In der Figur 1 ist vertikal der Innenradius (Radiallänge) von der Mittelachse bis zur Innenwand der Hülle aufgetragen und horizontal die hierfür geeignete Aufladung eines Sprengstoffkerns. Innerhalb der gestrichelten Linien wird eine kontrolliert ablaufende Deflagration erreicht. Oberhalb der gestrichelten Linien erstirbt die Deflagration und unterhalb sie geht unkontrolliert in eine Detonation über.In the FIG. 1 vertically the inner radius (radial length) is applied from the central axis to the inner wall of the shell and horizontally the appropriate charge of an explosive core for this purpose. Within the dashed lines a controlled deflagration is achieved. Above the dashed lines the deflagration dies and below it goes uncontrolled into a detonation.

In der Figur 2 ist ein Schnitt durch ein Wirksystem dargestellt, das innerhalb der Hülle HÜ bis auf einen schlanken Hohlraum im Bereich der Längsachse LA mit Sprengstoff SP gefüllt ist. Dieser nicht näher bezeichnete Hohlraum dient der Aufnahme des Sprengladungskerns SK. Der Sprengladungskern erstreckt sich von einer ersten Zündeinrichtung Z1 an der Spitze des Wirksystems bis zu einer weiteren Zündeinrichtung Z2 am Heck des Wirksystems. Beide Zündeinrichtungen können zur Initiierung des Sprengladungskerns herangezogen werden.In the FIG. 2 is a section through an active system shown, which is filled within the envelope HÜ except for a slender cavity in the region of the longitudinal axis LA with explosive SP. This unspecified cavity serves to receive the explosive charge core SK. The explosive charge core extends from a first ignition device Z1 at the tip of the active system to a further ignition device Z2 at the rear of the active system. Both ignition devices can be used to initiate the explosive charge core.

Erfindungsgemäß ist der Sprengladungskern SK in mehrere Abschnitte A1, A2, A3 aufgeteilt. Dabei kann die Aufteilung je nach den Erfordernissen des Wirksystems auch in weniger oder mehr Abschnitte sinnvoll sein. Diese Abschnitte entsprechen jeweils einer genau für diesen Abschnitt angepassten Aufladung des Sprengladungskerns SK. Es ist auch möglich den Verlauf der Aufladung entsprechend dem Verlauf der Hülle HÜ derart anzupassen, dass die Aufladung nach einem höheren Wert im mittleren Bereich zum Ende hin wieder abnimmt.According to the invention, the explosive charge core SK is divided into a plurality of sections A1, A2, A3. Depending on the requirements of the active system, the division may also make sense in fewer or more sections. Each of these sections corresponds to charging of the explosive charge core SK adapted to this section. It is also possible to adjust the course of charging according to the course of the envelope HÜ such that the Charging decreases to a higher value in the middle range towards the end.

Es wurden bereits typische Werte für Aufladungen in den unterschiedlichen Bereichen ermittelt, die Erfolg versprechend sind. So kann eine Aufladung im Abschnitt A1 im Wertebereich 30 bis 50 g/m liegen, im zweiten Bereich A2 im Wertebereich 50 bis 70 g/m und schließlich im dritten Bereich A3 im Wertebereich 70 bis 100 g/m.Typical values have already been determined for charges in the different ranges, which are promising. Thus, charging in section A1 can be in the value range 30 to 50 g / m, in the second range A2 in the value range 50 to 70 g / m and finally in the third range A3 in the value range 70 to 100 g / m.

Eine weitere Anpassungsmöglichkeit besteht in der Wahl des Querschnitts des Sprengladungskerns SK. Dieser kann je nach Anpassungsbedarf beispielsweise eckig, rund oval, halbrund ausgeführt sein, wie dies in Figur 3 dargestellt ist.Another option is the choice of the cross section of the explosive charge core SK. This can be designed, for example, rectangular, round oval, half round, depending on the need for adjustment, as in FIG. 3 is shown.

Aufgrund der Anpassungsmöglichkeiten kann ein Sprengladungskern bei nahezu beliebigen Formen und Größen von Gefechtsköpfen und anderen Wirksystemen Anwendung finden. Ein weiterer Vorteil ist die signifikante Reduktion derDue to the customization options, an explosive charge core can be applied to almost any shape and size of warhead and other active system. Another advantage is the significant reduction of

Anfangsgeschwindigkeit der aus der Hülle abgegebenen Splitter. Ebenso von Vorteil ist die erhebliche Verringerung des maximalen Blastdruckes.Initial speed of the splitter discharged from the shell. Another advantage is the significant reduction of the maximum blast pressure.

Claims (9)

  1. Device for the controller initiation of the deflagration of an explosive charge, which is arranged in a casing of a diameter that is not constant, comprising at least one detonating cord running in the region of the longitudinal axis of the explosive charge, the detonating cord being configured as a core of the explosive charge, characterized in that the transverse dimension of the core of the explosive charge is adapted to the shape of the casing in the longitudinal direction of the explosive charge.
  2. Device according to Claim 1, characterized in that the core of the explosive charge can be initiated at each end as a matter of choice.
  3. Device according to Claim 1, characterized in that the charge of the core of the explosive charge is adapted with respect to its form to the shape of the casing in the longitudinal direction of the explosive charge.
  4. Device according to Claim 1, characterised in that the charge of the core of the explosive charge is set to be homogeneous or to differ locally with respect to the type of explosive over the length of the core of the explosive charge.
  5. Device according to Claim 4, characterized in that the explosive is arranged in the core of the explosive charge in particular with its density and/or its composition in percentage terms taken into consideration.
  6. Device according to Claim 1, characterized in that the core of the explosive charge is surrounded by a sheath.
  7. Device according to Claim 6, characterized in that the sheath consists of a woven fabric and/or of plastic.
  8. Device according to Claim 1, characterized in that the core of the explosive charge is surrounded by a tube.
  9. Device according to Claim 8, characterized in that the tube consists of a woven fabric and/or of plastic.
EP14002294.8A 2013-07-15 2014-07-04 Device for the controlled initiation of the deflagration of an explosive charge Active EP2827094B1 (en)

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DE102014014332B3 (en) 2014-10-01 2016-03-17 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Apparatus and method for the controlled fragmentation by means of temperature-activated Kerbladungen
DE102014018218B4 (en) * 2014-12-06 2023-05-17 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Device for the controlled initiation of the deflagration of an explosive charge

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DE10008914C2 (en) * 2000-02-25 2003-06-26 Tdw Verteidigungstech Wirksys Explosive charge for a warhead
DE10020019A1 (en) * 2000-04-22 2001-10-25 Tzn Forschung & Entwicklung Electrothermal igniter and process for its manufacture
DE10222184B4 (en) * 2002-05-18 2005-06-09 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH warhead
DE102005031588B3 (en) * 2005-07-06 2007-01-11 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Controllable charge of a warhead
DE102009017160B3 (en) * 2009-04-09 2010-08-19 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Disassembling device for the explosive charge of a warhead
US8931415B2 (en) 2010-07-29 2015-01-13 Alliant Techsystems Inc. Initiation systems for explosive devices, scalable output explosive devices including initiation systems, and related methods
DE102012006044B3 (en) * 2012-03-27 2013-03-21 TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH Method and device for measuring the course of a deflagration front in a cylindrical warhead with at least two ignition devices

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DE102013011786A1 (en) 2015-01-15
NO3044088T3 (en) 2018-02-24
EP2827094A1 (en) 2015-01-21
ES2655432T3 (en) 2018-02-20

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