EP0973006B1 - Projectile with controlled destruction, the projectile having a second active charge which is embedded in a first active charge - Google Patents
Projectile with controlled destruction, the projectile having a second active charge which is embedded in a first active charge Download PDFInfo
- Publication number
- EP0973006B1 EP0973006B1 EP99112702A EP99112702A EP0973006B1 EP 0973006 B1 EP0973006 B1 EP 0973006B1 EP 99112702 A EP99112702 A EP 99112702A EP 99112702 A EP99112702 A EP 99112702A EP 0973006 B1 EP0973006 B1 EP 0973006B1
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- European Patent Office
- Prior art keywords
- component
- effective mass
- canister
- camouflage
- projectile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
- F42B12/48—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances smoke-producing, e.g. infrared clouds
Definitions
- the present invention relates to a projectile with a Active mass, especially a rapidly burning, a spontaneous fog producing deceptive component and a slow burning one Permanent fog-producing camouflage component, with a lighter, with an exhaust charge and / or igniter charge and at least an ignition retarder.
- Such a projectile is, for example, from DE 43 37 680 C2 known.
- a two-component smoke missile disclosed, where the deceptive component when firing from the camouflage component separated and accelerated relative to the same and seen in time before it comes into effect.
- the separation of the two Active mass components and the decomposition of the deceptive component leads to the known two-component smoke missile such an impulse and thus to such an uncontrolled Onward flight that a collocation of the spontaneous fog the deceptive component and the permanent fog of the camouflage component is guaranteed.
- DE 195 48 436 C1 is a quick-fog hand grenade for one Known charge, in which a grenade launcher mainly due to this protected from mechanical injuries that massive Particles of the grenade also during and after disassembly of the active charge related by appropriate security elements and cannot fly apart.
- a training warhead is known from DE 297 18 216, in which an electric lighter to initiate a firing charge for the implementation of an active charge essentially without Delay at least partially built into the ignition disassembly charge is.
- the invention has for its object the generic Continuously develop the throwing body so that its functional reliability increases and a risk of injury to a launcher is minimized is, while reducing costs and simplifying the Construction.
- At least an active mass component can only be dismantled radially, the Bottom of at least one active mass can firmly with the lid of this Active mass can is connected, even when the active mass is disassembled, the exhaust charge and / or the igniter charge as well as the at least an ignition retarder is built into the active mass, and the lighter is at least partially built into the active mass.
- the lid of the least an active mass can over a sieve tube with the bottom of this Effective mass socket is connected, and in the sieve tube an ignition disassembly charge is arranged.
- An embodiment according to the invention is characterized in that that the active mass is a deceptive component and a camouflage component comprises, the deceptive component can only be dismantled radially, the deceptive component is arranged in the at least one active-mass can is that a firm connection between its lid and has its bottom, the camouflage component in a further active substance can is arranged, the two active mass doses with each other are connected, and an ignition retarder of the camouflage component and the discharge charge is built into the camouflage component.
- an ignition retarder Deceptive component is built into the camouflage component.
- the, preferably electrical, lighter is built into the camouflage component.
- the lighter at least Part is built into the exhaust charge.
- an ignition tube that is centered in the longitudinal direction extends through the camouflage component and in which the ejection charge and the ignition delay of the deceptive component is arranged are to be provided.
- the weight of the individual, at the active substance particles that are broken down are minimized is.
- the invention also proposes that the at least one Effective mass socket, especially for the fake component, a sleeve has between its bottom and its lid, and the can sleeve thin and can be dismantled into small, light parts.
- the invention provides that the active mass can of the camouflage component is a sleeve has between its bottom and its lid, and the can sleeve melts away when the camouflage component burns off.
- the invention provides that the radius of the Throwing distance adjustable via the at least one ignition retarder is.
- the invention is therefore based on the surprising finding that for the decomposition of an active mass the corresponding decomposition energy only acts radially, so that only the active mass when disassembled is distributed over a large area, while no other parts of the Throwing body received an impulse by the disassembly, in flight leads to leaving the ballistic trajectory, and no parts Throwing or splinter bullets form a potential hazard represent.
- the bottom and the lid of an active mass can firmly together connected, for example by a sieve tube as a tie rod, and the in the longitudinal direction during the dismantling pressure against the Lid and bottom cancel each other out, so that only an effect remains in the radial direction.
- a significant cost reduction is achieved in that all charges, such as an ejection charge, an ignition decomposer charge and ignition retarders, to save space or better enlarge the space for the active component within the worm body, in the active component and, preferably, the lighter at least partially in the exhaust charge are installed.
- a preferred embodiment of the invention results in the case of two-component smoke towers, for the purpose of disassembly a deceptive component and a camouflage component no separation this active mass components takes place, which minimizes the Risk potential, better collocation and a reduction of costs.
- a projectile according to the invention comprises 1 a camouflage component 2 and a deceptive component 3 within a sleeve 10 with an ignition tube 11 in the area of the camouflage component 2 and a sieve tube 12 in the area of the fake component 3.
- the sleeve 10 is through a lid 13 and a contact cup 14 closed.
- Both the camouflage component 2 and the deceptive component 3 are each in a can 15, 16 with a can lid 15a or 16a and a can bottom 15b or 16b housed.
- an electrical igniter 20 Inside the box 15 of the camouflage component 2 is also at least in part an electrical igniter 20, a lighter delay 21 for the camouflage component 2, one Ejection charge 22 and an ignition retarder 31 for the deceptive component 3 installed; while in the sieve tube 12 inside the can 16 of the deceptive component 3 arranged an ignition decomposition charge is.
- FIG. 2a the throwing body 1 according to FIG. 1 is simplified again 1 shown before shooting from a throw cup, not shown.
- the delay of the ignition retarders 21 and 31 is relative chosen to each other such that there is a temporal collocation of spontaneous fog 43 and permanent fog 42 for camouflage of an object, not shown, to be protected.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Refuse Collection And Transfer (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Lighters Containing Fuel (AREA)
Description
Die gegenwärtige Erfindung betrifft einen Wurfkörper mit einer Wirkmasse, insbesondere einer rasch brennenden, einen Spontannebel erzeugenden Täuschkomponente und einer langsam brennenden, einen Dauernebel erzeugenden Tarnkomponente, mit einem Anzünder, mit einer Ausstoßladung und/oder Anzündzerlegerladung und mit zumindest einem Anzündverzögerer.The present invention relates to a projectile with a Active mass, especially a rapidly burning, a spontaneous fog producing deceptive component and a slow burning one Permanent fog-producing camouflage component, with a lighter, with an exhaust charge and / or igniter charge and at least an ignition retarder.
Solch ein Wurfkörper ist, beispielsweise, aus der DE 43 37 680 C2 bekannt. Dort ist ein Zweikomponenten-Nebelwurfkörper offenbart, bei dem die Täuschkomponente beim Abschuß von der Tarnkomponente getrennt und relativ zu derselben beschleunigt sowie zeitlich gesehen vor derselben zur Wirkung kommt. Die Trennung der beiden Wirkmassenkomponenten sowie die Zerlegung der Täuschkomponente führt jedoch bei dem bekannten Zweikomponenten-Nebelwurfkörper zu einer derartigen Impulsaufprägung und somit zu einem derartig unkontrollierten Weiterflug, daß eine Kollokation des Spontannebels der Täuschkomponente und des Dauernebels der Tarnkomponente nicht gewährleistet ist.Such a projectile is, for example, from DE 43 37 680 C2 known. There is a two-component smoke missile disclosed, where the deceptive component when firing from the camouflage component separated and accelerated relative to the same and seen in time before it comes into effect. The separation of the two Active mass components and the decomposition of the deceptive component However, leads to the known two-component smoke missile such an impulse and thus to such an uncontrolled Onward flight that a collocation of the spontaneous fog the deceptive component and the permanent fog of the camouflage component is guaranteed.
Aus der DE 195 48 436 C1 ist eine Schnellnebelhandgranate für eine Wirkladung bekannt, bei der ein Werfer der Granate vor allem dadurch vor mechanischen Verletzungen geschützt wird, daß massivere Teilchen der Granate auch während und nach Zerlegung der Wirkladung durch entsprechende Sicherungselemente zusammenhängen und nicht auseinanderfliegen können.DE 195 48 436 C1 is a quick-fog hand grenade for one Known charge, in which a grenade launcher mainly due to this protected from mechanical injuries that massive Particles of the grenade also during and after disassembly of the active charge related by appropriate security elements and cannot fly apart.
Ferner ist aus der DE 297 18 216 ein Übungsgefechtskopf bekannt, bei dem ein elektrischer Anzünder zum Initiieren einer Anzündzerlegerladung zwecks Umsetzung einer Wirkladung im wesentlichen ohne Verzögerung zumindest zum Teil in die Anzündzerlegerladung eingebaut ist.Furthermore, a training warhead is known from DE 297 18 216, in which an electric lighter to initiate a firing charge for the implementation of an active charge essentially without Delay at least partially built into the ignition disassembly charge is.
Schließlich ist noch aus der DE 28 30 119 bekannt, Anzündzerlegerladungen in eine Wirkmassenkomponente einzubauen.Finally, from DE 28 30 119 it is known to ignite charges to be built into an active mass component.
Der Erfindung liegt die Aufgabe zugrunde, den gattungsgemäßen Wurfkörper derart weiterzuentwickeln, daß seine Funktionszuverlässigkeit erhöht und ein Verletzungsrisiko eines Werfers minimiert ist, bei gleichzeitiger Kostenreduzierung und Vereinfachung des Aufbaus.The invention has for its object the generic Continuously develop the throwing body so that its functional reliability increases and a risk of injury to a launcher is minimized is, while reducing costs and simplifying the Construction.
Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß zumindest eine Wirkmassenkomponente ausschließlich radial zerlegbar ist, der Boden zumindest einer Wirkmassendose fest mit dem Deckel dieser Wirkmassendose verbunden ist, auch bei Zerlegung der Wirkmasse, die Ausstoßladung und/oder die Anzündzerlegerladung sowie der zumindest eine Anzündverzögerer in die Wirkmasse eingebaut sind, und der Anzünder zumindest zum Teil in die Wirkmasse eingebaut ist. This object is achieved in that at least an active mass component can only be dismantled radially, the Bottom of at least one active mass can firmly with the lid of this Active mass can is connected, even when the active mass is disassembled, the exhaust charge and / or the igniter charge as well as the at least an ignition retarder is built into the active mass, and the lighter is at least partially built into the active mass.
Dabei ist gemäß der Erfindung bevorzugt, daß der Deckel der zumindest einen Wirkmassendose über ein Siebrohr mit dem Boden dieser Wirkmassendose verbunden ist, und in dem Siebrohr eine Anzündzerlegerladung angeordnet ist.It is preferred according to the invention that the lid of the least an active mass can over a sieve tube with the bottom of this Effective mass socket is connected, and in the sieve tube an ignition disassembly charge is arranged.
Eine erfindungsgemäße Ausführungsform ist dadurch gekennzeichnet, daß die Wirkmasse eine Täuschkomponente und eine Tarnkomponente umfaßt, die Täuschkomponente ausschließlich radial zerlegbar ist, die Täuschkomponente in der zumindest einen Wirkmassendose angeordnet ist, die eine feste Verbindung zwischen ihrem Deckel und ihrem Boden aufweist, die Tarnkomponente in einer weiteren Wirkmassendose angeordnet ist, die beiden Wirkmassendosen miteinander verbunden sind, und ein Anzündverzögerer der Tarnkomponente und die Ausstoßladung in die Tarnkomponente eingebaut sind.An embodiment according to the invention is characterized in that that the active mass is a deceptive component and a camouflage component comprises, the deceptive component can only be dismantled radially, the deceptive component is arranged in the at least one active-mass can is that a firm connection between its lid and has its bottom, the camouflage component in a further active substance can is arranged, the two active mass doses with each other are connected, and an ignition retarder of the camouflage component and the discharge charge is built into the camouflage component.
Dabei kann vorgesehen sein, daß ein Anzündverzögerer der Täuschkomponente in der Tarnkomponente eingebaut ist.It can be provided that an ignition retarder Deceptive component is built into the camouflage component.
Ferner wird erfindungsgemäß vorgeschlagen, daß der, vorzugsweise elektrische, Anzünder in der Tarnkomponente eingebaut ist.It is further proposed according to the invention that the, preferably electrical, lighter is built into the camouflage component.
Dabei kann auch vorgesehen sein, daß der Anzünder zumindest zum Teil in die Ausstoßladung eingebaut ist.It can also be provided that the lighter at least Part is built into the exhaust charge.
Erfindungsgemäß kann ein Zündrohr, das sich mittig in Längsrichtung durch die Tarnkomponente erstreckt und in dem die Ausstoßladung und der Anzündverzögerer der Täuschkomponente angeordnet sind, vorgesehen sein.According to the invention, an ignition tube that is centered in the longitudinal direction extends through the camouflage component and in which the ejection charge and the ignition delay of the deceptive component is arranged are to be provided.
Ebenfalls kann vorgesehen sein, daß das Gewicht der einzelnen, bei der Zerlegung zerteilt werdenden, Wirkmassenpartikel minimiert ist.It can also be provided that the weight of the individual, at the active substance particles that are broken down are minimized is.
Ferner schlägt die Erfindung auch vor, daß die zumindest eine Wirkmassendose, insbesondere für die Täuschkomponente, eine Hülse zwischen ihrem Boden und ihrem Deckel aufweist, und die Dosenhülse dünn sowie in kleine, leichte Teile zerlegbar ist.Furthermore, the invention also proposes that the at least one Effective mass socket, especially for the fake component, a sleeve has between its bottom and its lid, and the can sleeve thin and can be dismantled into small, light parts.
Bei einer bevorzugten Ausführungsform ist erfindungsgemäß vorgesehen, daß die Wirkmassendose der Tarnkomponente eine Hülse zwischen ihrem Boden und ihrem Deckel aufweist, und die Dosenhülse beim Abbrand der Tarnkomponente wegschmilzt.In a preferred embodiment, the invention provides that the active mass can of the camouflage component is a sleeve has between its bottom and its lid, and the can sleeve melts away when the camouflage component burns off.
Schließlich ist erfindungsgemäß vorgesehen, daß der Radius der Zerlegungswurfweite über den zumindest einen Anzündverzögerer einstellbar ist.Finally, the invention provides that the radius of the Throwing distance adjustable via the at least one ignition retarder is.
Der Erfindung liegt somit die überraschende Erkenntnis zugrunde, daß zur Zerlegung einer Wirkmasse die entsprechende Zerlegungsenergie nur radial wirkt, so daß nur die Wirkmasse bei der Zerlegung großflächig verteilt wird, während keine anderen Teile des Wurfkörpers einen Impuls durch die Zerlegung erhalten, der im Flug zu einem Verlassen der ballistischen Bahn führt, und keine Teile Wurf- oder Splittergeschosse bilden, die ein Gefährdungspotential darstellen. Zu diesem Zweck sowie zur Vereinfachung des Wurfkörperaufbaus bei gleichzeitiger Kostenreduktion sind erfindungsgemäß der Boden und der Deckel einer Wirkmassendose fest miteinander verbunden, zum Beispiel durch ein Siebrohr als Zuganker, und der in Längsrichtung bei der Zerlegung auftretende Druck gegen den Deckel und den Boden hebt sich gegenseitig auf, so daß lediglich eine Wirkung in radialer Richtung verbleibt. Eine erhebliche Kostenreduktion wird dabei dadurch erreicht, daß alle Ladungen, wie eine Ausstoßladung, eine Anzündzerlegerladung und Anzündverzögerer, zur Platzeinsparung oder besser Vergrößerung des Raums für die Wirkkomponente innerhalb des Wurkörpers, in der Wirkkomponente und, vorzugsweise, der Anzünder zumindest zum Teil in der Ausstoßladung eingebaut sind. The invention is therefore based on the surprising finding that for the decomposition of an active mass the corresponding decomposition energy only acts radially, so that only the active mass when disassembled is distributed over a large area, while no other parts of the Throwing body received an impulse by the disassembly, in flight leads to leaving the ballistic trajectory, and no parts Throwing or splinter bullets form a potential hazard represent. For this purpose and to simplify the structure of the throwing body with simultaneous cost reduction are according to the invention the bottom and the lid of an active mass can firmly together connected, for example by a sieve tube as a tie rod, and the in the longitudinal direction during the dismantling pressure against the Lid and bottom cancel each other out, so that only an effect remains in the radial direction. A significant cost reduction is achieved in that all charges, such as an ejection charge, an ignition decomposer charge and ignition retarders, to save space or better enlarge the space for the active component within the worm body, in the active component and, preferably, the lighter at least partially in the exhaust charge are installed.
Eine bevorzugte Ausführungsform der Erfindung ergibt sich im Falle von Zweikomponenten-Nebelwurfkörpern, bei denen zwecks Zerlegung einer Täuschkomponente und einer Tarnkomponente keine Trennung dieser Wirkmassenkomponenten erfolgt, was zu einer Minimierung des Gefährdungspotentials, einer besseren Kollokation sowie einer Reduzierung der Kosten führt.A preferred embodiment of the invention results in the case of two-component smoke towers, for the purpose of disassembly a deceptive component and a camouflage component no separation this active mass components takes place, which minimizes the Risk potential, better collocation and a reduction of costs.
Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der nachfolgenden Beschreibung, in der ein Ausführungsbeispiel der Erfindung anhand von schematischen Zeichnungen im einzelnen erläutert ist. Dabei zeigt:
Figur 1- eine Schnittansicht durch einen erfindungsgemäßen Wurfkörper;
- Figuren 2a bis 2d
- Schnittansichten durch einen erfindungsgemäßen Wurfkörper beim Zerlegen desselben.
- Figure 1
- a sectional view through a projectile according to the invention;
- Figures 2a to 2d
- Section views through a projectile according to the invention when disassembling the same.
Wie Figur 1 zu entnehmen ist, umfaßt ein erfindungsgemäßer Wurfkörper
1 eine Tarnkomponente 2 sowie eine Täuschkomponente 3 innerhalb
einer Hülse 10 mit einem Zündrohr 11 im Bereich der Tarnkomponente
2 und einem Siebrohr 12 im Bereich der Täuschkomponente
3. Die Hülse 10 ist durch einen Deckel 13 und einen Kontaktbecher
14 verschlossen. Sowohl die Tarnkomponente 2 als auch die Täuschkomponente
3 sind jeweils in einer Dose 15, 16 mit einem Dosendeckel
15a beziehungsweise 16a und einem Dosenboden 15b beziehungsweise
16b untergebracht. Innerhalb der Dose 15 der Tarnkomponente
2 ist außerdem zumindest zum Teil ein elektrischer Anzünder
20, ein Anzünderverzögerer 21 für die Tarnkomponente 2, eine
Ausstoßladung 22 und ein Anzündverzögerer 31 für die Täuschkomponente
3 eingebaut; während in dem Siebrohr 12 innerhalb der Dose
16 der Täuschkomponente 3 eine Anzündzerlegerladung angeordnet
ist. As can be seen in FIG. 1, a projectile according to the invention comprises
1 a
Eine Zerlegung des erfindungsgemäßen Wurfkörpers 1 wird im Anschluß
mit Bezug auf die Figuren 2a bis 2d im Detail erläutert:A disassembly of the
In Figur 2a ist vereinfacht nochmals der Wurfkörper 1 gemäß Figur
1 vor Abschuß aus einem nicht dargestellten Wurfbecher gezeigt.In FIG. 2a, the
Durch Initiieren des elektrischen Anzünders 20 kommt es zu einem
Zünden der Ausstoßladung 22, wodurch die Dosen 15, 16 aus der
Hülse 10 und somit dem Wurfbecher herausgeschossen werden, während
die Hülse 10 samt dem Kontaktbecher 14 in dem Wurfbecher verbleibt.
Somit fliegen nunmehr lediglich die Dosen 15, 16, die fest
miteinander verbunden sind, auf einer ausgewählten ballistischen
Bahn, wie in Figur 2b angedeutet.By initiating the
Nach einer vorherbestimmten Zeitdauer kommt es über den Anzündverzögerer
31, der ebenso wie die Ausstoßladung 22 in dem Zündrohr 11
angeordnet ist, zu einer Zerlegung der Täuschkomponente 2 zwecks
Erzeugung eines Spontannebels 43, wie in Figur 2c dargestellt.After a predetermined period of time it comes through the
Nach einer weiteren vorherbestimmten Zeitdauer kommt es über den
Anzündverzögerer 21 zu einem Abbrand Zerlegung der Tarnkomponente
2 zwecks Erzeugung eines Dauernebels 42, wie in Figur 2d angedeutet.
Dabei ist die Verzögerung der Anzündverzögerer 21 und 31 relativ
zueinander derart gewählt, daß es zu einer zeitlichen Kollokation
von Spontannebel 43 und Dauernebel 42 zwecks Tarnung
eines nicht gezeigten, zu schützenden Objekts kommt.After another predetermined period of time, it comes over the
Die in der vorstehenden Beschreibung, in den Zeichnungen sowie in den Ansprüchen offenbarten Merkmale der Erfindung können sowohl einzeln als auch in jeder beliebigen Kombination für die Verwirklung der Erfindung in ihren verschieden Ausführungen wesentlich sein. The in the above description, in the drawings and in Features of the invention disclosed in the claims can both individually as well as in any combination for the realization the invention in its various versions essential his.
- 11
- Wurfkörperprojectile
- 22
- Tarnkomponentecamouflage component
- 33
- Täuschkomponentedecoy
- 1010
- Hülseshell
- 1111
- Zündrohrignition tube
- 1212
- Siebrohrperforated pipe
- 1313
- Deckelcover
- 1414
- KontaktbecherContact Mug
- 1515
- Dosecan
- 15a15a
- Dosendeckelcan end
- 15b15b
- Dosenbodencan bottom
- 1616
- Dosecan
- 16a16a
- Dosendeckelcan end
- 16b16b
- Dosenbodencan bottom
- 2020
- elektrischer Anzünderelectric lighter
- 2121
- Anzündverzögererignition delay
- 2222
- Ausstoßladungejection charge
- 3131
- Anzündverzögererignition delay
- 3232
- Anzündzerlegerladungigniter-
- 4242
- Dauernebelcontinuous output
- 4343
- SpontarmebelSpontarmebel
Claims (11)
- A projectile having an effective mass, in particular a quick-burning decoy component generating spontaneous smoke and a slow-burning camouflage component generating persistent smoke, having an igniter, having an ejection charge and/or ignition decomposition charge and having at least one ignition delay device, characterised in that decomposition of at least one effective mass component (3) may only be effected in a radial direction,
the base (16b) of at least one effective mass canister (16) is fixedly connected to the cover (16a) of this effective mass canister (16), even upon decomposition of the effective mass (3),
the ejection charge (22) and/or the ignition decomposition charge (32) and also the at least one ignition delay device (21, 31) are incorporated in the effective mass (2, 3), and
the igniter (20) is at least partially incorporated in the effective mass (2). - A projectile according to Claim 1, characterised in that the cover (16a) of the at least one effective mass canister (16) is connected to the base (16b) of this effective mass canister (16) by way of a perforated tube (12), and
an ignition decomposition charge (32) is arranged in the perforated tube (12). - A projectile according to Claim 1 or 2, characterised in that the effective mass comprises a decoy component (3) and a camouflage component (2),
decomposition of the decoy component (3) may only be effected in a radial direction, and the decoy component (3) is arranged in the at least one effective mass canister (16), which has a fixed connection between its cover (16a) and its base (16b),
the camouflage component (2) is arranged in a further effective mass canister (15),
the two effective mass canisters (15, 16) are connected to one another,
and an ignition delay device (21) of the camouflage component (2) and the ejection charge (22) are incorporated in the camouflage component (2). - A projectile according to Claim 3, characterised in that an ignition delay device (31) of the decoy component (3) is incorporated in the camouflage component (2).
- A projectile according to Claim 3 or 4, characterised in that the preferably electric igniter (20) is incorporated in the camouflage component (2).
- A projectile according to Claim 5, characterised in that the igniter (20) is at least partially incorporated in the ejection charge (22).
- A projectile according to one of Claims 3 to 6, characterised by an ignition tube (11), which extends centrally through the camouflage component (2) in the longitudinal direction and in which the ejection charge (22) and the ignition delay device (31) of the decoy component (3) are arranged.
- A projectile according to one of the preceding claims, characterised in that the weight of the individual effective mass particles which are dispersed upon decomposition is minimised.
- A projectile according to one of the preceding claims, characterised in that the at least one effective mass canister (16), in particular for the decoy component (3), has a sleeve between its base (16b) and its cover (16a), and the canister sleeve can decompose finely and into small, light parts.
- A projectile according to one of Claims 3 to 9, characterised in that the effective mass canister (15) of the camouflage component (2) has a sleeve between its base (15b) and its cover (15a), and the canister sleeve melts away as the camouflage component burns up.
- A projectile according to one of the preceding claims, characterised in that the radius of the range of the projectile upon decomposition may be set by way of the at least one ignition delay device (31, 32).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE29812623U DE29812623U1 (en) | 1998-07-15 | 1998-07-15 | Throwing body with controlled disassembly and charge integrated in the active mass area |
| DE29812623U | 1998-07-15 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0973006A2 EP0973006A2 (en) | 2000-01-19 |
| EP0973006A3 EP0973006A3 (en) | 2001-04-04 |
| EP0973006B1 true EP0973006B1 (en) | 2003-02-19 |
Family
ID=8059913
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP99112702A Expired - Lifetime EP0973006B1 (en) | 1998-07-15 | 1999-06-30 | Projectile with controlled destruction, the projectile having a second active charge which is embedded in a first active charge |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6283032B1 (en) |
| EP (1) | EP0973006B1 (en) |
| DE (2) | DE29812623U1 (en) |
| ES (1) | ES2190155T3 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6895865B2 (en) * | 2003-03-20 | 2005-05-24 | Hornady Manufacturing Company | Sabot for muzzleloading firearm |
| DE102008028292B4 (en) | 2008-06-13 | 2021-10-14 | Diehl Defence Gmbh & Co. Kg | Smoke missile |
| FR2937123B1 (en) * | 2008-10-13 | 2016-09-16 | Nexter Munitions | MUNITION FOR CONTROLLING CROWDS WITH NON-LETTER EFFECT |
| US20110226492A1 (en) * | 2010-03-18 | 2011-09-22 | Tagliareni Russell V | Fire Suppression System Including an Integral Time Delay and Output Starter with Attach and Detach Firing Pin Assesmbly |
| ES2392984A1 (en) * | 2010-05-10 | 2012-12-17 | Falken, S.A. | Multi-pectral hidden artificial (Machine-translation by Google Translate, not legally binding) |
| US8776691B2 (en) * | 2012-06-04 | 2014-07-15 | Csi-Penn Arms, Llc | Launched smoke grenade |
| JP6563773B2 (en) * | 2015-10-20 | 2019-08-21 | 株式会社ダイセル | Smoke screen generator |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1382750A (en) * | 1917-07-24 | 1921-06-28 | Sprague Frank Desmond | Projectile |
| US1367464A (en) * | 1918-05-16 | 1921-02-01 | Robert N Cook | Explosive shell |
| US2419371A (en) * | 1939-02-02 | 1947-04-22 | Schlumberger Marcel | Cartridge |
| US3358600A (en) * | 1966-01-13 | 1967-12-19 | Trojan Powder Co | Self-destroying explosive cartridge for underwater seismic exploration |
| US3517616A (en) * | 1967-12-19 | 1970-06-30 | Atlas Chem Ind | Axially expandable and contractable container |
| NO142929C (en) * | 1978-03-08 | 1980-11-12 | Raufoss Ammunisjonsfabrikker | ROEYKBOKS. |
| DE2830119C2 (en) | 1978-07-08 | 1985-09-19 | Nico-Pyrotechnik Hans-Jürgen Diederichs KG, 2077 Trittau | Smoke charge for missiles and projectiles |
| DE3238455C2 (en) * | 1982-10-16 | 1987-03-05 | Pyrotechnische Fabrik F. Feistel GmbH + Co KG, 6719 Göllheim | Smoke grenades |
| DE3334464A1 (en) * | 1983-09-23 | 1985-04-11 | Dynamit Nobel Ag, 5210 Troisdorf | INDUSTRIAL CARTRIDGE |
| FR2612287B1 (en) * | 1987-03-12 | 1993-09-10 | France Etat Armement | SMOKE PROJECTILE AND AMMUNITION THUS EQUIPPED |
| US5092245A (en) * | 1990-07-18 | 1992-03-03 | The United States Of America As Represented By The Secretary Of The Army | Explosive stemming device |
| DE4337680C2 (en) * | 1993-11-04 | 1995-08-24 | Buck Chem Tech Werke | Two-component smoke projectors |
| DE19548436C1 (en) | 1995-12-22 | 1997-06-26 | Buck Chem Tech Werke | Rapid smoke grenade |
| DE29718216U1 (en) | 1997-10-14 | 1997-12-11 | Buck Werke GmbH & Co., 73337 Bad Überkingen | Practice warhead |
-
1998
- 1998-07-15 DE DE29812623U patent/DE29812623U1/en not_active Expired - Lifetime
-
1999
- 1999-06-30 EP EP99112702A patent/EP0973006B1/en not_active Expired - Lifetime
- 1999-06-30 ES ES99112702T patent/ES2190155T3/en not_active Expired - Lifetime
- 1999-06-30 DE DE59904310T patent/DE59904310D1/en not_active Expired - Lifetime
- 1999-07-15 US US09/353,642 patent/US6283032B1/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP0973006A3 (en) | 2001-04-04 |
| DE29812623U1 (en) | 1998-12-10 |
| EP0973006A2 (en) | 2000-01-19 |
| DE59904310D1 (en) | 2003-03-27 |
| ES2190155T3 (en) | 2003-07-16 |
| US6283032B1 (en) | 2001-09-04 |
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