[go: up one dir, main page]

EP1370825A1 - Igniter with a safety device for a projectile which is shot from a pipe with angular momentum - Google Patents

Igniter with a safety device for a projectile which is shot from a pipe with angular momentum

Info

Publication number
EP1370825A1
EP1370825A1 EP02727213A EP02727213A EP1370825A1 EP 1370825 A1 EP1370825 A1 EP 1370825A1 EP 02727213 A EP02727213 A EP 02727213A EP 02727213 A EP02727213 A EP 02727213A EP 1370825 A1 EP1370825 A1 EP 1370825A1
Authority
EP
European Patent Office
Prior art keywords
projectile
shaped element
detonator according
region
disc
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP02727213A
Other languages
German (de)
French (fr)
Other versions
EP1370825B1 (en
Inventor
Detlef Haeselich
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
Nico-Pyrotechnikhanns-Juergen Diederichs & Co KG GmbH
NICO PYROTECHNIKHANNS JUERGEN
Nico Pyrotechnik Hanns Juergen Diederichs GmbH and Co KG
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 Nico-Pyrotechnikhanns-Juergen Diederichs & Co KG GmbH, NICO PYROTECHNIKHANNS JUERGEN, Nico Pyrotechnik Hanns Juergen Diederichs GmbH and Co KG filed Critical Nico-Pyrotechnikhanns-Juergen Diederichs & Co KG GmbH
Publication of EP1370825A1 publication Critical patent/EP1370825A1/en
Application granted granted Critical
Publication of EP1370825B1 publication Critical patent/EP1370825B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/34Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by a blocking-member in the pyrotechnic or explosive train between primer and main charge

Definitions

  • the invention relates to an igniter for a projectile to be fired from a tube with a swirl according to the preamble of patent claim 1.
  • Such projectiles, the z. B. from several pyrotechnic charges for triggering an irk bin should be equipped with a safety device that interrupts the ignition chain in a first position and when the projectile is shot through its initial acceleration and its swirl passes from this first position into a second position releasing the ignition chain , This prevents the ignition chain from igniting even though the projectile is at rest, e.g. B. is still in the barrel.
  • a detonator for projectiles which has a safety device with disc-shaped elements, for. B. has a plastically deformable plate. This plate is arranged between a body containing the primer and the part of the projectile containing an opening leading to the charge to be ignited. This arrangement is intended to prevent the explosive charge of the projectile from being detonated in the secure position of the body receiving it in the event of an unwanted ignition of the squib.
  • Impact igniter which ignites the effect of the impact. If this detonator does not work, it must be ensured that the effect is triggered at least after a certain time or self-dismantled in order to safely clear the
  • Safety detonator provided with an ignition chain, which consists of at least one igniter ignited when the effect bullet was fired and at least one further charge, in particular a delay charge, via which, after its combustion, the actual active charge z. B. about
  • Detonating cords or booster charges are fired about four seconds after the launch.
  • Such ammunition is usually fired from short-barreled weapons or from short drum magazines.
  • magazine weapons the magazine is usually covered by a disk that only releases the cartridge that is actually to be fired, whereas all other magazine barrels are covered by the disk.
  • the delay charge for the safety fuse is still ignited, for example by a too weak propellant charge or solely by the primer. Since the ammunition now does not leave the barrel of the firearm, be it a normal barrel weapon or a magazine weapon, the effect is triggered after the specified delay time of about 4 seconds. This can be used for bystanders and the shooter himself a high risk of injury, especially if a magazine weapon is used. As soon as the launch is triggered there, the delay charge for the safety fuse is still ignited, for example by a too weak propellant charge or solely by the primer. Since the ammunition now does not leave the barrel of the firearm, be it a normal barrel weapon or a magazine weapon, the effect is triggered after the specified delay time of about 4 seconds. This can be used for bystanders and the shooter himself a high risk of injury, especially if a magazine weapon is used. As soon as the launch is triggered there, the
  • Delay ignition chain is located, is closed at the front.
  • a safety device into the ignition chain to trigger the active effect, which interrupts the ignition chain in a first position and, when the projectile is shot down, by its initial acceleration and its swirl from this first position into a second releasing the ignition chain Position passes.
  • Such safety devices are known for projectile detonators in a large number of variants.
  • the invention has for its object to provide such a safety device for a projectile of the type in question, which is simple in construction, inexpensive to manufacture and reliably ensures that the effective effect is actually only ignited when the projectile has the initial acceleration associated with a launch and experienced the twist.
  • the securing device has a disk-shaped element with a central area and an edge area surrounding it. Only the central area interrupts the ignition chain and is mechanically supported by a holding device and on Held place.
  • the central area and the peripheral area are connected to one another via a predetermined breaking point that tears open during the initial acceleration of the projectile.
  • a collecting space is provided around the holding device, which the at the initial acceleration of the
  • Such a safety device for an igniter is very simple and inexpensive to manufacture, since the safety device z. B. is a correspondingly prepared simple plastic disc.
  • the initial acceleration affects both the central area and the peripheral area. However, since only the central area is supported, this initial acceleration shears off the edge area at the predetermined breaking point from the central area and falls into the catchment area located behind the edge area in the direction of flight of the projectile. This has a thickness which corresponds to at least twice the thickness of the edge area, so that when the edge area lies in the receiving space, it is removed from the plane of the central area. The swirl now acts on this central area, so that this central area is more or less removed from the ignition chain and this is released thereby.
  • the swirl and the swirl acceleration are usually so large that the center area lies eccentrically to the swirl axis of the projectile due to the remnants of the predetermined breaking point alone, so that the centrifugal forces remove the central area from the ignition chain. It is of course possible to deliberately set the center of mass of the central area eccentrically to the swirl axis of the projectile.
  • the predetermined breaking point can, for. B. by reducing the thickness of the material of the disc-shaped element in the boundary region between the central region and the edge region.
  • the central area and the edge area can be connected to one another via webs. Another possibility is to design the central area and the edge area as individual parts and to connect these with a connecting element, e.g. B. to connect a self-adhesive film that forms the predetermined breaking point.
  • FIG. 1 shows a partially cut effect ammunition from the cartridge case and the projectile with a disk-shaped securing device for interrupting the ignition chain for an effective effect
  • FIG. 2 shows a cross section through the rear area of a projectile with a disk-shaped securing device that is slightly modified compared to FIG. 1;
  • FIG. 3 shows a bottom view of the disk-shaped securing device according to FIG. 2;
  • Figure 4 shows another embodiment of a disk-shaped securing device according to the invention.
  • Figure 5 shows another embodiment of a disk-shaped safety device according to the invention.
  • FIG. 1 an effect ammunition with a cartridge case 2 and a projectile 3 inserted therein is shown partially in section.
  • a primer 4 is arranged, with which one in one Cartridge 5 located propellant charge 6 is ignited.
  • Cartridge 5 has overflow openings which open into a pressure chamber 8 between cartridge case 2 and floor 3.
  • the floor 3 has in its bow a cargo space 10 in which an effect charge, for. B. CS tear gas or the like is located, which can be triggered pyrotechnically. This is usually done by an impact detonator 11, which is only indicated here as a switch, and which ignites a pyrotechnic ignition charge 12 when the projectile hits, which in turn triggers the active charge present in the cargo space 10.
  • an effect charge for. B. CS tear gas or the like
  • an impact detonator 11 which is only indicated here as a switch, and which ignites a pyrotechnic ignition charge 12 when the projectile hits, which in turn triggers the active charge present in the cargo space 10.
  • a delay charge 13 is also ignited by its propellant gases, which, however, is divided into two parts 13a and 13b.
  • the partial charges 13a and 13b are separated from one another by an ignition gap 14.
  • a disk 15 is inserted as a safety device for interrupting or releasing the ignition chain between the two delay charges 13a and 13b, which disk consists of a central area 16 and an edge area 17 surrounding it, which are separated from one another by a predetermined breaking point 18.
  • the central area 16 is one of the
  • Retention charge charge 13a surrounding holding device for. B. a base 19 supported.
  • the edge region 17 has a greater thickness than the central region 16, the step between the central region 16 and the edge region 17 being essentially given by the predetermined breaking point 18. With this step, the disk 15 bears against the base 19, as a result of which the disk 15 is held in its radial position.
  • the disc 15 also lies with its top in the direction of flight of the projectile 3 on the ceiling of a Collection space 21 in which the disc 15 is held laterally with little play.
  • This collecting space 21 has one
  • Thickness which, viewed in the direction of flight of the projectile 3, corresponds to at least twice the thickness of the edge region 17.
  • the predetermined breaking point 18 of the pane 15 breaks open, as a result of which the edge region 17 is moved against the bottom of the collecting space 21 and is preferably clamped in this position.
  • the side wall of the collecting space 21 is slightly conical to the inside or has slipped, etc.
  • the central region 16 is then flung outwards from the position that locks the ignition chain and is also collected in the collecting space 21 above the edge region 17.
  • the ignition chain is thus released in the area of the delay charge 13.
  • the delay charge 13a can then ignite the delay charge 13b and this the active charge in the cargo space 10.
  • the delay charge 13a can have a conical recess in a known manner, through which the detonation waves within the delay charge 13a are focused and centered on the delay charge 13b and ignite it.
  • Load space 10 detonated and projectile 3 can be removed from the barrel of the weapon without risk.
  • the delay charge 13a ignites the second delay charge 13b of the delay charge 13. Should then the impact detonator 11 does not function when the projectile 3 is impacted and thus the active charge in the cargo space 10 is not ignited, this is ignited after the delay charge 13b has burned down.
  • the igniter according to FIG. 1 is shown in FIG. 2 with a small modification of the disk 15.
  • the circular disk 15 in turn consists of a central area 16 and an edge area 17 surrounding it, which is separated from the central area 16 by a predetermined breaking point 18 in the form of a notch.
  • the center of mass S of the central area 16 is located outside the longitudinal and swirl axis A of the projectile.
  • the central area 16 is also very quickly removed from the ignition chain due to the eccentric position of the center of mass S, so that the latter is activated via the delay charges 13a and 13b can ignite.
  • a disc 15 is shown with a central area 16 and an edge area 17, which over several Web 24 are connected to each other, the
  • FIG. 5 shows a disk 15, which in turn is constructed from a central area 16 and an edge area 17.
  • the central area 16 and the edge area 17 are individual parts, i. H. in the simplest case, a small circular disk or an annular disk.
  • the annular disk as the edge area 17 in turn has a greater thickness than the central area 16.
  • the two individual parts 16 and 17 are connected to one another by a self-adhesive plastic film 25, which takes over the function of the predetermined breaking point 18.
  • the plastic film 25 is connected to the underside of the central area 16 and a step 26 in the edge area 17, so that when the edge area 17 is separated from the central area 16 during the initial acceleration of the projectile 3, the plastic film 25 also from the central area Area 16 is replaced.
  • the central area 16 again preferably has a center of gravity S eccentric to the swirl axis A of the projectile 3, so that after the edge area 17 has been sheared off, the central area 16 is quickly conveyed into the collecting space 21.
  • the plastic film 25 is designed in such a way that it enables the delay charges 13a and 13b to ignite.
  • the disk 15 should be made of a material with a low specific mass, so that the small disk accommodated in the collecting space 21 only exerts such a small imbalance on the projectile 3 according to the central area 16 that the trajectory of the projectile 3 does not is disturbed.
  • the base does not have to be a compact base 19, but can be z.
  • Support sections can be realized.
  • the predetermined breaking point 18 of the disk 15 breaks open during the initial acceleration of the projectile 3 in the firing run, so that the central region 16, which interrupts the ignition chain, is then also quickly transported out of the ignition chain.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Emergency Lowering Means (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Air Bags (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Toys (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Catching Or Destruction (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Abstract

The igniter comprises a disk-shaped element ( 15 ) with a central portion ( 16 ) and a boundary portion ( 17 ) surrounding it for interrupting and/or releasing an ignition chain ( 13 a , 13 b) of the igniter. Only the central portion interrupts the chain of ignition and is supported by a holding device ( 19 ). A collecting space is provided around the holding device which, seen in the direction of flight of the projectile, is located below the boundary portion ( 17 ). The central portion ( 16 ) and the boundary portion ( 17 ) are connected with each other by means of a rated breaking point ( 18 ). Upon the initial acceleration of the projectile the boundary portion ( 17 ) is sheared off from the central portion ( 16 ) and received in the collecting space ( 21 ), whereupon the central portion ( 16 ) is also subsequently removed from the ignition chain ( 13 a , 13 b) by the twist of the projectile.

Description

Zünder mit Sicherungsvorrichtung für ein aus einem Rohr mit Drall abzuschießendes GeschossDetonator with safety device for a projectile to be fired from a tube with swirl
Die Erfindung bezieht sich auf einen Zünder für ein aus einem Rohr mit Drall abzuschießendes Geschoss gemäß dem Oberbegriff des Patentanspruches 1.The invention relates to an igniter for a projectile to be fired from a tube with a swirl according to the preamble of patent claim 1.
Derartige Geschosse, die eine Zündkette z. B. aus mehreren pyrotechnischen Ladungen zum Auslösen eines irkeffektes aufweisen, sollten mit einer Sicherungsvorrichtung ausgerüstet sein, die in einer ersten Position die Zündkette unterbricht und beim Abschuss des Geschosses durch dessen Anfangsbeschleunigung und dessen Drall aus dieser ersten Position in eine die Zündkette freigebende zweite Position übergeht. Damit wird ausgeschlossen, dass die Zündkette durchzündet, obwohl das Geschoss sich in Ruhe, z. B. noch im Lauf befindet.Such projectiles, the z. B. from several pyrotechnic charges for triggering an irkeffekt should be equipped with a safety device that interrupts the ignition chain in a first position and when the projectile is shot through its initial acceleration and its swirl passes from this first position into a second position releasing the ignition chain , This prevents the ignition chain from igniting even though the projectile is at rest, e.g. B. is still in the barrel.
Aus der DE-A12037182 ist ein Zünder für Geschosse bekannt, der eine Sicherungsvorrichtung mit scheibenförmigen Elementen, z. B. eine plastisch verformbare Platte aufweist. Diese Platte ist zwischen einem den Zündsatz enthaltenen Körper und dem eine zu der zu entzündenden Ladung führende Öffnung enthaltenden Teil des Geschosses angeordnet. Mit dieser Anordnung soll verhindert werden, dass bei einer ungewollten Entzündung der Zündpille in der Sicherungslage des sie aufnehmenden Körpers die Sprengladung des Geschosses gezündet wird. Bei einer ungewollten Entzündung der Zündpille treten dann die heißen Explosionsgase unter hohem Druck auf die plastisch verformbare Platte, wodurch diese verformt und fest in die Trennfugen zwischen dem Träger für die Zündpille und den in aufnehmende Teile gepresst wird, so dass die heißen Explosionsgase, die zu der Sprengladung führende Öffnung erreichen. Derartige Geschosse werden auch als so genannteFrom DE-A12037182 a detonator for projectiles is known, which has a safety device with disc-shaped elements, for. B. has a plastically deformable plate. This plate is arranged between a body containing the primer and the part of the projectile containing an opening leading to the charge to be ignited. This arrangement is intended to prevent the explosive charge of the projectile from being detonated in the secure position of the body receiving it in the event of an unwanted ignition of the squib. In the event of an unwanted ignition of the squib, the hot explosion gases then come under high pressure onto the plastically deformable plate, as a result of which the latter is deformed and pressed firmly into the joints between the squib support and the receiving parts, so that the hot explosion gases are released of the explosive charge leading opening. Such projectiles are also called so-called
Effektmunition eingesetzt, z. B. bei der Überrumpelung vonEffect ammunition used, e.g. B. in the surprise of
Kriminellen oder bei der Bekämpfung von gewalttätigenCriminals or in the fight against violent
Demonstranten. Diese Effektmunition ist von der scharfenDemonstrators. This effect ammunition is from the sharp
Munition abgeleitet, ist z. B. eine Patronenmunition mit einem Kalliber von 40 mm. Als Wirkeffekte werden z. B. CS,Ammunition derived, for. B. a cartridge ammunition with a caliber of 40 mm. As effects are z. B. CS,
Tränengas, Nebel, sternenerzeugende Ladungen, Blitzladungen etc. angewendet. Diese Effektmunition weist einenTear gas, fog, star-generating charges, lightning charges, etc. applied. This effect ammunition has one
Aufschlagzünder auf, der den Wirkeffekt beim Aufschlag zündet. Sollte dieser Zünder einmal nicht funktionieren, so muß sichergestellt werden, dass der Wirkeffekt trotzdem zumindest nach einer gewissen Zeit ausgelöst oder selbstzerlegt wird, um das gefahrlose Räumen derImpact igniter, which ignites the effect of the impact. If this detonator does not work, it must be ensured that the effect is triggered at least after a certain time or self-dismantled in order to safely clear the
Effektmunition zu ermöglichen. Hierzu ist ein zusätzlicherTo enable effect ammunition. Here is an additional one
Sicherheitszünder mit einer Zündkette vorgesehen, die zumindest aus einem beim Abschuss des Effektgeschosses angezündeten Anzünder und mindestens einer weiteren Ladung, insbesondere einer Verzögerungsladung besteht, über die nach deren Abbrand die eigentliche Wirkladung z. B. überSafety detonator provided with an ignition chain, which consists of at least one igniter ignited when the effect bullet was fired and at least one further charge, in particular a delay charge, via which, after its combustion, the actual active charge z. B. about
Zündschnüre oder Boosterladungen etwa vier Sekunden nach dem Abschuss gezündet wird.Detonating cords or booster charges are fired about four seconds after the launch.
Derartige Effektmunition wird meistens aus Kurzlaufwaffen bzw. aus kurzen Trommelmagazinen verschossen. Bei Magazinwaffen ist das Magazin üblicherweise durch eine Scheibe abgedeckt, die nur die tatsächlich zu verschießende Patrone freigibt, wohingegen alle anderen Magazinläufe durch die Scheibe abgedeckt sind.Such ammunition is usually fired from short-barreled weapons or from short drum magazines. In magazine weapons, the magazine is usually covered by a disk that only releases the cartridge that is actually to be fired, whereas all other magazine barrels are covered by the disk.
Wenn der Treibsatz beim versuchten Abschuss der Effektmunition nicht gezündet wird, kann es nun vorkommen, dass die Verzögerungsladung für den Sicherheitszünder trotzdem angezündet wird, zum Beispiel durch eine zu schwache Treibladung oder allein durch das Anzündhütchen. Da die Effektmunition nunmehr den Lauf der Abschusswaffe, sei es eine normale Rohrwaffe oder eine Magazinwaffe, nicht verlässt, wird der Wirkefefkt nach der vorgegebenen Verzögerungszeit von etwa 4 Sekunden ausgelöst. Dieses kann für umstehende Personen und für den Schützen selbst mit einem hohen Verletzungsrisiko verbunden sein, insbesondere dann, wenn eine Magazinwaffe verwendet wird. Sobald dort nämlich der Abschuß ausgelöst wird, wird dieIf the propellant charge is not fired when attempting to fire the effect ammunition, it may happen that the delay charge for the safety fuse is still ignited, for example by a too weak propellant charge or solely by the primer. Since the ammunition now does not leave the barrel of the firearm, be it a normal barrel weapon or a magazine weapon, the effect is triggered after the specified delay time of about 4 seconds. This can be used for bystanders and the shooter himself a high risk of injury, especially if a magazine weapon is used. As soon as the launch is triggered there, the
Magazintrommel, obwohl das Geschoss das Magazin nicht verlässt, um eine Stelle weitergedreht, sodass nunmehr derMagazine drum, although the projectile does not leave the magazine, turned one place, so that now the
Magazinlauf, in dem sich Patronenmunition mit abbrennenderMagazine barrel in which cartridge ammunition with burning
Verzögerungszündkette befindet, vorne verschlossen ist.Delay ignition chain is located, is closed at the front.
Wird dann nach der vorgegebenen Verzögerungszeit derIs then after the predetermined delay time
Wirkeffekt ausgelöst , so z. B. ein Tränengas freigegeben, so kann dieser praktisch nur nach hinten in Richtung auf den Schützen austreten, so dass für diesen ein hohesEffect triggered, such. B. released a tear gas, it can practically only escape towards the back of the shooter, so that a high one
Verletzungsrisiko gegeben ist.There is a risk of injury.
Es wäre daher wünschenswert, in die Zündkette zur Auslösung des Wirkeffektes in an sich bekannter Weise eine Sicherungsvorrichtung einzufügen, die in einer ersten Position die Zündkette unterbricht und beim Abschuss des Geschosses durch dessen Anfangsbeschleunigung und dessen Drall aus dieser ersten Position in eine die Zündkette freigebende zweite Position übergeht. Derartige Sicherungsvorrichtungen sind für Geschosszünder in einer Vielzahl von Varianten bekannt.It would therefore be desirable to insert, in a manner known per se, a safety device into the ignition chain to trigger the active effect, which interrupts the ignition chain in a first position and, when the projectile is shot down, by its initial acceleration and its swirl from this first position into a second releasing the ignition chain Position passes. Such safety devices are known for projectile detonators in a large number of variants.
Der Erfindung liegt die Aufgabe zugrunde, für ein Geschoss der in Rede stehenden Art eine derartige Sicherungsvorrichtung anzugeben, die einfach konstruiert ist, billig herzustellen ist und zuverlässig gewährleistet, dass der Wirkeffekt tatsächlich nur dann gezündet wird, wenn das Geschoss die mit einem Abschuß verbundene Anfangsbeschleunigung und den Drall erfahren hat.The invention has for its object to provide such a safety device for a projectile of the type in question, which is simple in construction, inexpensive to manufacture and reliably ensures that the effective effect is actually only ignited when the projectile has the initial acceleration associated with a launch and experienced the twist.
Diese Aufgabe ist gemäß der Erfindung durch die kennzeichnenden Merkmale des Patentanspruchs 1 gelöst .This object is achieved according to the invention by the characterizing features of patent claim 1.
Demgemäß weist die Sicherungsvorrichtung ein scheibenförmiges Element mit einem zentralen Bereich und einem diesen umgebenden Randbereich auf. Lediglich der zentrale Bereich unterbricht hierbei die Zündkette und wird durch eine Haltevorrichtung mechanisch abgestützt und am Platz gehalten. Der zentrale Bereich und der Randbereich sind über eine bei der Anfangsbeschleunigung des Geschosses aufreißende Sollbruchstelle miteinander verbunden. Zudem ist um die Haltevorrichtung herum ein Auffangraum vorgesehen, der den bei der Anfangsbeschleunigung desAccordingly, the securing device has a disk-shaped element with a central area and an edge area surrounding it. Only the central area interrupts the ignition chain and is mechanically supported by a holding device and on Held place. The central area and the peripheral area are connected to one another via a predetermined breaking point that tears open during the initial acceleration of the projectile. In addition, a collecting space is provided around the holding device, which the at the initial acceleration of the
Geschosses von dem zentralen Bereich an der Sollbruchstelle abgetrennten Randbereich und den anschließend durch denBullet separated from the central area at the predetermined breaking point and then by the
Drall des Geschosses aus der Zündkette entfernten zentralenSwirl of the projectile removed from the central chain
Bereich aufnimmt .Area.
Eine derartige Sicherungsvorrichtung für einen Zünder ist sehr einfach und auch billig herzustellen, da die Sicherungsvorrichtung z. B. eine entsprechend präparierte einfache KunststoffScheibe ist.Such a safety device for an igniter is very simple and inexpensive to manufacture, since the safety device z. B. is a correspondingly prepared simple plastic disc.
Bei einem Abschuss des Geschosses wirkt die Anfangsbeschleunigung sowohl auf den zentralen Bereich als auch auf den Randbereich. Da allerdings nur der zentrale Bereich abgestützt ist, wird durch diese Anfangsbeschleunigung der Randbereich bei der Sollbruchstelle von dem zentralen Bereich abgeschert und fällt in den in Flugrichtung des Geschosses hinter dem Randbereich gelegenen Auffangraum. Dieser hat eine Dicke, die mindestens der doppelten Dicke des Randbereiches entspricht, sodass dann, wenn der Randbereich in dem Aufnahmeraum liegt, er aus der Ebene des zentralen Bereiches entfernt ist. Auf diesen zentralen Bereich wirkt nun der Drall, sodass dieser zentrale Bereich mehr oder minder bald aus der Zündkette entfernt und diese dadurch freigegeben wird.When the projectile is fired, the initial acceleration affects both the central area and the peripheral area. However, since only the central area is supported, this initial acceleration shears off the edge area at the predetermined breaking point from the central area and falls into the catchment area located behind the edge area in the direction of flight of the projectile. This has a thickness which corresponds to at least twice the thickness of the edge area, so that when the edge area lies in the receiving space, it is removed from the plane of the central area. The swirl now acts on this central area, so that this central area is more or less removed from the ignition chain and this is released thereby.
Der Drall und die Drallbeschleunigung sind in der Regel so groß, dass der zentrale Bereich allein durch die Reste der Sollbruchstelle mit seinem Massenschwerpunkt exzentrisch zur Drallachse des Geschosses liegt, sodass die Zentrifugalkräfte den zentralen Bereich aus der Zündkette entfernen. Es ist natürlich möglich, den Massenschwerpunkt des zentralen Bereiches bewusst exzentrisch zur Drallachse des Geschosses zu legen. Die Sollbruchstelle kann z. B. durch eine Verringerung der Dicke des Materials des scheibenförmigen Elementes in dem Grenzbereich zwischen zentralem Bereich und Randbereich gebildet werden. Ferner können zentraler Bereich und Randbereich über Stege miteinander verbunden werden. Eine weitere Möglichkeit ist, zentralen Bereich und Randbereich jeweils als Einzelteile auszubilden und diese durch ein Verbindungselement, z. B. eine selbstklebende Folie miteinander zu verbinden, die die Sollbruchstelle bildet.The swirl and the swirl acceleration are usually so large that the center area lies eccentrically to the swirl axis of the projectile due to the remnants of the predetermined breaking point alone, so that the centrifugal forces remove the central area from the ignition chain. It is of course possible to deliberately set the center of mass of the central area eccentrically to the swirl axis of the projectile. The predetermined breaking point can, for. B. by reducing the thickness of the material of the disc-shaped element in the boundary region between the central region and the edge region. Furthermore, the central area and the edge area can be connected to one another via webs. Another possibility is to design the central area and the edge area as individual parts and to connect these with a connecting element, e.g. B. to connect a self-adhesive film that forms the predetermined breaking point.
Weitere Ausgestaltungen der Erfindung gehen aus den Unteransprüchen hervor.Further embodiments of the invention emerge from the subclaims.
Die Erfindung ist in Ausführungsbeispielen anhand der Zeichnung näher erläutert. In dieser stellen dar:The invention is explained in more detail in exemplary embodiments with reference to the drawing. In this represent:
Figur 1 eine teilweise geschnittene Effektmunition aus Patronenhülse und Geschoss mit einer scheibenförmigen Sicherungsvorrichtung zur Unterbrechung der Zündkette für einen Wirkeffekt;1 shows a partially cut effect ammunition from the cartridge case and the projectile with a disk-shaped securing device for interrupting the ignition chain for an effective effect;
Figur 2 einen Querschnitt durch den Heckbereich eines Geschosses mit einer gegenüber Figur 1 leicht modifizierten scheibenförmigen Sicherungsvorrichtung;FIG. 2 shows a cross section through the rear area of a projectile with a disk-shaped securing device that is slightly modified compared to FIG. 1;
Figur 3 eine Untersicht der scheibenförmigen Sicherungsvorrichtung gemäß Figur 2 ;FIG. 3 shows a bottom view of the disk-shaped securing device according to FIG. 2;
Figur 4 eine andere Ausgestaltung einer scheibenförmigen Sicherungsvorrichtung gemäß der Erfindung; undFigure 4 shows another embodiment of a disk-shaped securing device according to the invention; and
Figur 5 eine weitere Ausfuhrungsform einer scheibenförmigen Sicherungsvorrichtung gemäß der Erfindung.Figure 5 shows another embodiment of a disk-shaped safety device according to the invention.
In Figur 1 ist eine Effektmunition mit einer Patronenhülse 2 und einem darin eingesetzten Geschoss 3 teilweise geschnitten dargestellt. Am Boden der Patronenhülse 2 ist ein Anzündhütchen 4 angeordnet, mit dem eine in einer Kartusche 5 gelegene Treibladung 6 angezündet wird. DieIn Figure 1, an effect ammunition with a cartridge case 2 and a projectile 3 inserted therein is shown partially in section. At the bottom of the cartridge case 2, a primer 4 is arranged, with which one in one Cartridge 5 located propellant charge 6 is ignited. The
Kartusche 5 weist hierbei Überströmöffnungen auf, die in einen Druckraum 8 zwischen Patronenhülse 2 und Geschoss 3 münden .Cartridge 5 has overflow openings which open into a pressure chamber 8 between cartridge case 2 and floor 3.
Das Geschoss 3 weist in seinem Bug einen Ladungsraum 10 auf, in dem eine Effektladung, z. B. CS-Tränengas oder dergleichen gelegen ist, die pyrotechnisch ausgelöst werden kann. Dies erfolgt üblicherweise durch einen hier nur als Schalter angedeuteten Aufschlagzünder 11, der eine pyrotechnische Zündladung 12 beim Aufschlag des Geschosses zündet, die ihrerseits die im Ladungsraum 10 vorhandene Wirkladung auslöst .The floor 3 has in its bow a cargo space 10 in which an effect charge, for. B. CS tear gas or the like is located, which can be triggered pyrotechnically. This is usually done by an impact detonator 11, which is only indicated here as a switch, and which ignites a pyrotechnic ignition charge 12 when the projectile hits, which in turn triggers the active charge present in the cargo space 10.
Mit der Anzündung der Treibladung 6 wird durch deren Treibgase auch eine Verzögerungsladung 13 angezündet, die jedoch in zwei Teile 13a und 13b aufgeteilt ist. Die Teilladungen 13a und 13b sind durch einen Überzündspalt 14 voneinander getrennt.When the propellant charge 6 is ignited, a delay charge 13 is also ignited by its propellant gases, which, however, is divided into two parts 13a and 13b. The partial charges 13a and 13b are separated from one another by an ignition gap 14.
In diesem Überzündspalt 14 ist als Sicherungsvorrichtung zum Unterbrechen bzw. Freigeben der Zündkette zwischen den beiden Verzögerungsladungen 13a und 13b eine Scheibe 15 eingefügt, die aus einem zentralen Bereich 16 und einem diesen umgebenden Randbereich 17 besteht, die voneinander durch eine Sollbruchstelle 18 getrennt sind.In this overfire gap 14, a disk 15 is inserted as a safety device for interrupting or releasing the ignition chain between the two delay charges 13a and 13b, which disk consists of a central area 16 and an edge area 17 surrounding it, which are separated from one another by a predetermined breaking point 18.
Der zentrale Bereich 16 ist von einer dieThe central area 16 is one of the
Verzögerungsladungladung 13a umgebenden Haltevorrichtung, z. B. einem Sockel 19 abgestützt. Der Randbereich 17 hat eine größere Dicke als der zentrale Bereich 16, wobei die Stufe zwischen dem zentralen Bereich 16 und dem Randbereich 17 im wesentlichen durch die Sollbruchstelle 18 gegeben ist. Die Scheibe 15 liegt mit dieser Stufe an den Sockel 19 an, wodurch die Scheibe 15 in ihrer radialen Position gehalten wird.Retention charge charge 13a surrounding holding device, for. B. a base 19 supported. The edge region 17 has a greater thickness than the central region 16, the step between the central region 16 and the edge region 17 being essentially given by the predetermined breaking point 18. With this step, the disk 15 bears against the base 19, as a result of which the disk 15 is held in its radial position.
Die Scheibe 15 liegt ferner mit ihrer in Flugrichtung des Geschosses 3 gesehenen Oberseite an der Decke eines Auffangraumes 21 an, in dem die Scheibe 15 seitlich mit geringem Spiel gehalten ist. Dieser Auffangraum 21 hat eineThe disc 15 also lies with its top in the direction of flight of the projectile 3 on the ceiling of a Collection space 21 in which the disc 15 is held laterally with little play. This collecting space 21 has one
Dicke, die in Flugrichtung des Geschosses 3 gesehen mindestens der doppelten Dicke des Randbereiches 17 entspricht .Thickness, which, viewed in the direction of flight of the projectile 3, corresponds to at least twice the thickness of the edge region 17.
Wenn das Geschoss 3 abgeschossen wird und die Treibladung 6 vorschriftsmäßig zündet, baut sich in dem Druckraum 8 ein Druck auf, wobei der Druck schließlich so weit ansteigt, dass die Verbindung zwischen Patronenhülse 2 und Geschoss 3 getrennt und das Geschoss 3 aus der Patronenhülse 2 ausgetrieben wird. Hierbei erfährt das Geschoss 3 eine Beschleunigung, zudem wird dem Geschoss über Drallbänder 22 und die Drallzüge des Abschusslaufes ein Drall aufgeprägt.When the projectile 3 is fired and the propellant charge 6 ignites in accordance with regulations, a pressure builds up in the pressure chamber 8, the pressure finally increasing to such an extent that the connection between the cartridge case 2 and the projectile 3 is separated and the projectile 3 is expelled from the cartridge case 2 becomes. The projectile 3 is accelerated, and a swirl is imparted to the projectile by means of swirl bands 22 and the swirl trains of the launch run.
Durch die Anfangsbeschleunigung des Geschosses 3 bricht die Sollbruchstelle 18 der Scheibe 15 auf, wodurch der Randbereich 17 gegen den Boden des Auffangraumes 21 bewegt und vorzugsweise in dieser Position geklemmt wird. Hierzu kann z. B. die Seitenwand des Auffangraumes 21 leicht konisch nach innen verlaufen oder angerut sein, etc.. Durch die Drallbeschleunigung wird anschließend auch der zentrale Bereich 16 aus der die Zündkette sperrenden Position nach außen geschleudert und ebenfalls in dem Auffangraum 21 oberhalb des Randbereiches 17 aufgefangen. Damit ist die Zündkette im Bereich der Verzögerungsladung 13 freigebeben. Die Verzögerungsladung 13a kann dann die Verzögerungsladung 13b und diese die Wirkladung im Ladungsraum 10 zünden. Für die Überzündung zwischen den Verzögerungsladungen 13a und 13b kann die Verzögerungsladung 13a in bekannter Weise eine kegelförmige Ausnehmung aufweisen, durch die die Detonationswellen innerhalb der Verzögerungsladung 13a gebündelt und zentriert auf die Verzögerungsladung 13b gerichtet werden und diese anzünden.Due to the initial acceleration of the projectile 3, the predetermined breaking point 18 of the pane 15 breaks open, as a result of which the edge region 17 is moved against the bottom of the collecting space 21 and is preferably clamped in this position. For this, e.g. B. the side wall of the collecting space 21 is slightly conical to the inside or has slipped, etc. Due to the swirl acceleration, the central region 16 is then flung outwards from the position that locks the ignition chain and is also collected in the collecting space 21 above the edge region 17. The ignition chain is thus released in the area of the delay charge 13. The delay charge 13a can then ignite the delay charge 13b and this the active charge in the cargo space 10. For the over-ignition between the delay charges 13a and 13b, the delay charge 13a can have a conical recess in a known manner, through which the detonation waves within the delay charge 13a are focused and centered on the delay charge 13b and ignite it.
Sollte die Anzündung der Treibladung 6 nur unvollständig sein und trotzdem die Verzögerungsladung 13 gezündet werden, d. h. dass das Geschoss nicht aus dem Lauf der Waffe austritt, dann tritt auch keine Anfangsbeschleunigung oder eine Drallbeschleunigung auf, sodass die Scheibe 15 an ihrem Platz verbleibt und am Ende des Abbrandes derIf the ignition of the propellant charge 6 is only incomplete and the delay charge 13 is still ignited, ie that the projectile does not emerge from the barrel of the weapon, then no initial acceleration occurs or a spin acceleration, so that the disc 15 remains in place and at the end of the burn
Verzögerungsladung 13a eine Zündung der VerzögerungsladungDelay charge 13a ignition of the delay charge
13b verhindert. Damit wird auch nicht die Wirkladung in dem13b prevented. This does not mean that the active charge in the
Ladungsraum 10 gezündet und das Geschoss 3 kann ohne Risiko aus dem Lauf der Waffe entfernt werden.Load space 10 detonated and projectile 3 can be removed from the barrel of the weapon without risk.
Nach einem ordnungsgemäßen Abschuß des Geschosses 3, bei dem der Randbereich 17 und anschließend der zentrale Bereich 16 der Scheibe 15 durch die Anfangsbeschleunigung bzw. den Drall in dem Auffangraum 21 aufgefangen werden, zündet die Verzögerungsladung 13a die zweite Verzögerungsladung 13b der Verzögerungsladung 13. Sollte dann der Aufschlagzünder 11 bei dem Aufschlag des Geschosses 3 nicht funktionieren und damit auch die Wirkladung in dem Ladungsraum 10 nicht gezündet werden, wird diese nach dem Abbrand der Verzögerungsladung 13b gezündet .After the projectile 3 has been properly fired, in which the edge region 17 and then the central region 16 of the pane 15 are caught by the initial acceleration or the swirl in the collecting space 21, the delay charge 13a ignites the second delay charge 13b of the delay charge 13. Should then the impact detonator 11 does not function when the projectile 3 is impacted and thus the active charge in the cargo space 10 is not ignited, this is ignited after the delay charge 13b has burned down.
In Figur 2 ist der Zünder gemäß Figur 1 mit einer kleiner Modifizierung der Scheibe 15 dargestellt. Die kreisförmige Scheibe 15 besteht wiederum aus einem zentralen Bereich 16 und einem diesen umgebenden Randbereich 17, der von dem zentralen Bereich 16 durch eine Sollbruchstelle 18 in Form einer Einkerbung getrennt ist. Wie aus Figur 3 ersichtlich, ist der Massenschwerpunkt S des zentralen Bereiches 16 außerhalb der Längs- und Drallachse A des Geschosses gelegen.The igniter according to FIG. 1 is shown in FIG. 2 with a small modification of the disk 15. The circular disk 15 in turn consists of a central area 16 and an edge area 17 surrounding it, which is separated from the central area 16 by a predetermined breaking point 18 in the form of a notch. As can be seen from FIG. 3, the center of mass S of the central area 16 is located outside the longitudinal and swirl axis A of the projectile.
Wenn durch die Anfangsbeschleunigung der Randbereich 17 von dem zentralen Bereich 16 abgeschert wird und in dem Auffangraum 21 aufgenommen wird, wird durch die exzentrische Lage des Massenschwerpunktes S auch der zentrale Bereich 16 sehr rasch aus der Zündkette entfernt, sodass diese über die Verzögerungsladungen 13a und 13b durchzünden kann.If, due to the initial acceleration, the edge area 17 is sheared off from the central area 16 and is received in the collecting space 21, the central area 16 is also very quickly removed from the ignition chain due to the eccentric position of the center of mass S, so that the latter is activated via the delay charges 13a and 13b can ignite.
In Figur 4 ist eine Scheibe 15 mit einem zentralen Bereich 16 und einen Randbereich 17 dargestellt, die über mehrere Stege 24 miteinander verbunden sind, die dieIn Figure 4, a disc 15 is shown with a central area 16 and an edge area 17, which over several Web 24 are connected to each other, the
Sollbruchstelle 18 bilden.Form predetermined breaking point 18.
In Figur 5 ist eine Scheibe 15 gezeigt, die wiederum aus einem zentralen Bereich 16 und einem Randbereich 17 aufgebaut ist. Der zentrale Bereich 16 und der Randbereich 17 sind Einzelteile, d. h. im einfachsten Fall eine kleine kreisförmige Scheibe bzw. eine Ringscheibe. Die Ringscheibe als Randbereich 17 weist wiederum eine größere Dicke als der zentrale Bereich 16 auf. Die beiden Einzelteile 16 und 17 sind miteinander durch eine selbstklebende Kunststofffolie 25 verbunden, die die Funktion der Sollbruchstelle 18 übernimmt. Im dargestellten Falle der Figur 5 ist die Kunststofffolie 25 mit der Unterseite des zentralen Bereiches 16 und einer Stufe 26 im Randbereich 17 verbunden, sodass beim Trennen des Randbereiches 17 von dem zentralen Bereich 16 bei der Anfangsbeschleunigung des Geschosses 3 die Kunststofffolie 25 auch von dem zentralen Bereich 16 abgelöst wird. Der zentrale Bereich 16 hat vorzugsweise wiederum einen Massenschwerpunkt S exzentrisch zu der Drallachse A des Geschosses 3, sodass nach dem Abscheren des Randbereiches 17 der zentrale Bereich 16 schnell in den Auffangraum 21 befördert wird.FIG. 5 shows a disk 15, which in turn is constructed from a central area 16 and an edge area 17. The central area 16 and the edge area 17 are individual parts, i. H. in the simplest case, a small circular disk or an annular disk. The annular disk as the edge area 17 in turn has a greater thickness than the central area 16. The two individual parts 16 and 17 are connected to one another by a self-adhesive plastic film 25, which takes over the function of the predetermined breaking point 18. In the case shown in FIG. 5, the plastic film 25 is connected to the underside of the central area 16 and a step 26 in the edge area 17, so that when the edge area 17 is separated from the central area 16 during the initial acceleration of the projectile 3, the plastic film 25 also from the central area Area 16 is replaced. The central area 16 again preferably has a center of gravity S eccentric to the swirl axis A of the projectile 3, so that after the edge area 17 has been sheared off, the central area 16 is quickly conveyed into the collecting space 21.
Es ist natürlich möglich, die Kunststofffolie 25 auch auf der oberen Seite der Scheibe 15 zu befestigen. In jedem Falle ist die Kunststofffolie 25 so ausgebildet, dass sie ein Durchzünden zwischen den Verzögerungsladungen 13a und 13b ermöglicht.It is of course possible to also attach the plastic film 25 to the upper side of the pane 15. In any case, the plastic film 25 is designed in such a way that it enables the delay charges 13a and 13b to ignite.
In allen Fällen sollte die Scheibe 15 aus einem Material mit geringer spezifischer Masse bestehen, damit durch die in dem Auffangsraum 21 aufgenommene kleine Scheibe entsprechend dem zentralen Bereich 16 nur eine so geringfügige Unwucht auf das Geschoss 3 ausgeübt wird, dass die Flugbahn des Geschosses 3 nicht gestört wird.In all cases, the disk 15 should be made of a material with a low specific mass, so that the small disk accommodated in the collecting space 21 only exerts such a small imbalance on the projectile 3 according to the central area 16 that the trajectory of the projectile 3 does not is disturbed.
Selbstverständlich sind andere Ausgestaltungen der Erfindung, insbesondere der Form der Scheibe 15 möglich, z. B. längliche, rechteckige oder quadratische Scheiben.Of course, other embodiments of the invention, in particular the shape of the disc 15 are possible, for. B. elongated, rectangular or square discs.
Ebenso muß der Sockel kein kompakter Sockel 19 sein, sondern kann durch z. B. mehrere Abstützpunkte oderLikewise, the base does not have to be a compact base 19, but can be z. B. several support points or
Abstützabschnitte realisiert werden.Support sections can be realized.
Wesentlich ist, dass die Sollbruchstelle 18 der Scheibe 15 noch während der Anfangsbeschleunigung des Geschosses 3 in dem Abschusslauf aufbricht, sodass danach der zentrale Bereich 16, der die Zündkette unterbricht, rasch ebenfalls aus der Zündkette transportiert wird. It is essential that the predetermined breaking point 18 of the disk 15 breaks open during the initial acceleration of the projectile 3 in the firing run, so that the central region 16, which interrupts the ignition chain, is then also quickly transported out of the ignition chain.

Claims

Patentansprüche claims
1. Zünder für ein aus einem Rohr mit Drall abzuschießendes Geschoss (3) , mit einer einen Wirkeffekt auslösenden Zündkette, wobei eine Sicherungsvorrichtung (15, 19, 21) vorgesehen ist, die in einer ersten Position die Zündkette unterbricht und beim Abschuß des Geschosses (3) durch dessen Anfangsbeschleunigung und dessen Drall in eine die Zündkette freigebende zweite Position übergeht, wobei die Sicherungsvorrichtung (15, 19, 21) ein scheibenförmiges Element (15) mit einem zentralen Bereich (16) und einem diesen umgebenden Randbereich1. Detonator for a projectile (3) to be fired from a tube with a twist, with an ignition chain that triggers an effect, a safety device (15, 19, 21) is provided which interrupts the ignition chain in a first position and when the projectile is fired ( 3) by its initial acceleration and its swirl into a second position releasing the ignition chain, the securing device (15, 19, 21) being a disk-shaped element (15) with a central region (16) and an edge region surrounding it
(17) aufweist, dadurch gekennzeichnet, dass lediglich der zentrale Bereich (16) die Zündkette unterbricht, dass der zentrale Bereich (16) des Scheibenförmigen Elements (15) nicht jedoch der Randbereich (17) durch eine Haltevorrichtung (19) abgestützt und am Platz gehalten ist, dass der zentrale Bereich (16) und der Randbereich (17) über eine bei der(17), characterized in that only the central area (16) interrupts the ignition chain, that the central area (16) of the disk-shaped element (15) but not the edge area (17) is supported by a holding device (19) and in place is held that the central region (16) and the edge region (17) over one at the
Anfangsbeschleunigung des Geschosses (3) aufreißende Sollbruchstelle (18) miteinander verbunden sind und dass um die Haltevorrichtung (19) ein Auffangraum (21) vorgesehen ist, der den bei der Anfangsbeschleunigung des Geschosses (3) von dem zentralen Bereich (16) abgetrennten Randbereich (17) und den anschließend durch den Drall des Geschosses (3) aus der Zündkette entfernten zentralen Bereich (16) aufnimmt.The predetermined breaking point (18) which tears open the initial acceleration of the projectile (3) are connected to one another and that a collecting space (21) is provided around the holding device (19), which serves to separate the peripheral region (16) separated from the central region (16) during the initial acceleration of the projectile (3). 17) and the central region (16) which is subsequently removed from the ignition chain by the swirl of the projectile (3).
2. Zünder nach Anspruch 1, dadurch gekennzeichnet, dass die Haltevorrichtung (19) eine die Zündkette umgebende Auflage für den zentralen Bereich (16) ist, und dass der Randbereich (17) eine Stufe aufweist, die an der Auflage anliegt und damit das scheibenförmige Element2. Detonator according to claim 1, characterized in that the holding device (19) is a support surrounding the ignition chain for the central region (16), and that the edge region (17) has a step which rests on the support and thus the disk-shaped element
(15) in seiner ersten, die Zündkette unterbrechenden Position sichert.(15) in its first position, which disconnects the ignition chain.
3. Zünder nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass der Randbereich (17) eine größere Dicke als der zentrale Bereich (16) aufweist.3. Detonator according to claim 1 or 2, characterized in that the edge region (17) has a greater thickness than that Central area (16).
4. Zünder nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass der Auffangraum (21) in Flugrichtung des Geschosses (3) gesehen hinter dem Randbereich (17) liegt und eine Tiefe aufweist, die mindestens der doppelten Dicke des Randbereiches (17) entspricht .4. Detonator according to one of claims 1 to 3, characterized in that the collecting space (21) in the flight direction of the projectile (3) lies behind the edge region (17) and has a depth which is at least twice the thickness of the edge region (17) corresponds.
5. Zünder nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass der Rand des scheibenförmigen Elementes (15) in der ersten Position an den Seitenwänden des Auffangraumes (21) mit Spiel anliegt.5. Detonator according to one of claims 1 to 4, characterized in that the edge of the disc-shaped element (15) in the first position lies against the side walls of the collecting space (21) with play.
6. Zünder nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass für das scheibenförmige Element6. Igniter according to one of claims 1 to 5, characterized in that for the disc-shaped element
(15) in der zweiten Position, in der es an dem Boden des Auffangraumes (21) aufliegt, eine Halte-, vorzugsweise Klemmeinrichtung vorgesehen ist.(15) in the second position, in which it rests on the bottom of the collecting space (21), a holding, preferably clamping device is provided.
7. Zünder nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass der Massenschwerpunkt (S) des zentralen Bereiches (16) exzentrisch zur Drallachse (A) des Geschosses (3) gelegen ist.7. Detonator according to one of claims 1 to 6, characterized in that the center of mass (S) of the central region (16) is located eccentrically to the swirl axis (A) of the projectile (3).
8. Zünder nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass das scheibenförmige Element (15) kreisförmig oder rechteckig ist.8. Detonator according to one of claims 1 to 7, characterized in that the disc-shaped element (15) is circular or rectangular.
9. Zünder nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass das scheibenförmige Element (15) aus Kunststoff ist.9. Detonator according to one of claims 1 to 8, characterized in that the disc-shaped element (15) is made of plastic.
10. Zünder nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass die Sollbruchstelle (18) durch eine Verringerung der Dicke des Materiales des scheibenförmigen Elementes (15) gebildet ist. 10. Detonator according to one of claims 1 to 9, characterized in that the predetermined breaking point (18) is formed by reducing the thickness of the material of the disc-shaped element (15).
11. Zünder nach einem der Ansprüche 1 bis 10, dadurch gekennzeichnet, dass der zentrale Bereich (16) und der Randbereich (17) des scheibenförmigen Elementes (15) über Stege (24) als Sollbruchstelle (18) miteinander verbunden sind.11. Detonator according to one of claims 1 to 10, characterized in that the central region (16) and the edge region (17) of the disc-shaped element (15) are connected to one another via webs (24) as a predetermined breaking point (18).
12. Zünder nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass der zentrale Bereich (16) und der Randbereich (17) jeweils Einzelteile sind, die durch ein die Sollbruchstelle (18) bildendes Verbindungselement miteinander verbunden sind.12. Detonator according to one of claims 1 to 9, characterized in that the central region (16) and the edge region (17) are each individual parts which are connected to one another by a connecting element which forms the predetermined breaking point (18).
13. Zünder nach Anspruch 12, dadurch gekennzeichnet, dass das Verbindungselement eine selbstklebende Folie (25) ist . 13. Detonator according to claim 12, characterized in that the connecting element is a self-adhesive film (25).
EP02727213A 2001-03-12 2002-03-12 Igniter with a safety device for a projectile which is shot from a pipe with angular momentum Expired - Lifetime EP1370825B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10111714 2001-03-12
DE10111714A DE10111714C1 (en) 2001-03-12 2001-03-12 Detonator for a projectile to be fired from a tube with swirl
PCT/DE2002/000864 WO2002073119A1 (en) 2001-03-12 2002-03-12 Igniter with a safety device for a projectile which is shot from a pipe with angular momentum

Publications (2)

Publication Number Publication Date
EP1370825A1 true EP1370825A1 (en) 2003-12-17
EP1370825B1 EP1370825B1 (en) 2009-02-11

Family

ID=7677088

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02727213A Expired - Lifetime EP1370825B1 (en) 2001-03-12 2002-03-12 Igniter with a safety device for a projectile which is shot from a pipe with angular momentum

Country Status (11)

Country Link
US (1) US6880464B2 (en)
EP (1) EP1370825B1 (en)
JP (1) JP4053428B2 (en)
KR (1) KR20030090667A (en)
AT (1) ATE422657T1 (en)
AU (1) AU2002257524B2 (en)
CA (1) CA2440731C (en)
DE (2) DE10111714C1 (en)
ES (1) ES2324096T3 (en)
NO (1) NO327470B1 (en)
WO (1) WO2002073119A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005020177A1 (en) 2005-04-28 2006-11-02 Rheinmetall Waffe Munition Gmbh Launch system
DE102007054777B3 (en) * 2007-11-16 2009-08-13 Junghans Microtec Gmbh Safety device for an igniter
FI120708B (en) * 2008-01-31 2010-01-29 Patria Weapon Systems Oy Arrangement to support the projectile into the barrel of the weapon, support element and method
US8424456B2 (en) 2009-10-05 2013-04-23 Amtec Corporation Non-dud signature training cartridge and projectile
SG181192A1 (en) 2010-11-25 2012-06-28 Advanced Material Engineering Pte Ltd A cartridged projectile
US10495425B1 (en) * 2018-10-04 2019-12-03 United States Of America, As Represented By The Secretary Of The Navy Thermoformed projectile cartridge

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB100046A (en) * 1914-04-29 1917-01-04 John Bonner Semple Improvements in Projectiles.
BE423814A (en) * 1937-09-28
LU31364A1 (en) * 1946-11-02 Energa
US3640225A (en) * 1969-06-20 1972-02-08 Honeywell Inc Fuze apparatus
US3750589A (en) * 1971-12-13 1973-08-07 Honeywell Inc Centrifugally driven spin device
SE407286B (en) * 1975-11-07 1979-03-19 Bofors Ab FUSE DEVICE
FR2349817A1 (en) * 1976-04-29 1977-11-25 Europ Propulsion Solid fuelled rocket charge ignition device - has arming charge to remove end of sleeve housing primary ignition charge
NO153441C (en) * 1980-12-11 1986-03-19 Junghans Gmbh Geb PROJECT INSURANCE FOR ROTATING PROJECTILES.
GB2169691B (en) * 1984-12-10 1988-08-03 British Aerospace Projectiles
DE3660940D1 (en) * 1985-04-04 1988-11-17 Oerlikon Buehrle Ag Safety device for a fuze activated by the rotation of a projectile
US4744298A (en) * 1986-05-09 1988-05-17 Dragolyoub Popovitch Safing and arming device and method
US4699058A (en) * 1986-05-09 1987-10-13 Interdyne Service Corporation Safing and arming device and method
US5033382A (en) * 1987-03-25 1991-07-23 Magnavox Government And Industrial Electronics Company Piezoelectric fuse for projectile with safe and arm mechanism
US4938138A (en) * 1989-08-07 1990-07-03 Honeywell Inc. Safing and arming mechanism with creep ribbon arming delay
USH1603H (en) * 1995-11-07 1996-11-05 The United States Of America As Represented By The Secretary Of The Navy Flare with safe-and-arm ignition system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO02073119A1 *

Also Published As

Publication number Publication date
NO20033952D0 (en) 2003-09-08
CA2440731C (en) 2010-05-25
JP4053428B2 (en) 2008-02-27
KR20030090667A (en) 2003-11-28
WO2002073119A1 (en) 2002-09-19
US6880464B2 (en) 2005-04-19
ATE422657T1 (en) 2009-02-15
NO20033952L (en) 2003-09-08
JP2004521309A (en) 2004-07-15
ES2324096T3 (en) 2009-07-30
AU2002257524B2 (en) 2006-05-18
EP1370825B1 (en) 2009-02-11
US20040074411A1 (en) 2004-04-22
DE50213267D1 (en) 2009-03-26
DE10111714C1 (en) 2002-10-10
NO327470B1 (en) 2009-07-13
CA2440731A1 (en) 2002-09-19

Similar Documents

Publication Publication Date Title
EP0600388B1 (en) Tandem warhead having piezo-electric igniters
EP0364670B1 (en) Grenade
EP0764826B1 (en) Carrier projectile with a single penetrator as the submunition
DE69225973T2 (en) Practice floor
EP0411243B1 (en) Fuse for a bomblet
DE2907308C2 (en) Floor with at least one pushable daughter floor
DE19651170A1 (en) Detonatorless, ballistic explosive device
DE3416787A1 (en) ARMORING BULLET
DE2556075C2 (en) Cartridge for shooting target objects used as bait
DE19831807B4 (en) Ignition device for submunition with a self-destruction device
EP1370825B1 (en) Igniter with a safety device for a projectile which is shot from a pipe with angular momentum
DE3740967A1 (en) PYROTECHNICAL IGNITION FOR BULLETS
EP1001244A1 (en) Artillery projectile
DE102004016356A1 (en) Igniter for grenade comprises housing, threaded ignition pin coaxially orientated to grenade and threaded hole for weighted insert
EP1166033B1 (en) Electronically and mechanically-operated ignition delay for cartridge-type pyrotechnic decoy flare ammunition
EP0387675A2 (en) Bottom fuze for a grenade
EP0236325B1 (en) Self-destroying igniter
DE3153378C2 (en)
EP0913663B1 (en) Pyrotechnic impact igniter
EP0227919B1 (en) Impact fuze for a projectile
CH656001A5 (en) IGNITION AND BULLET WITH ONE IGNITION.
DE3703774A1 (en) Projectile, especially a full-calibre explosive projectile
DE44298C (en) Detonator for grenades charged with wet wool or similar, difficult-to-detonate explosives
DE3544529C1 (en) Munition for attacking actively armoured targets
DE2453267A1 (en) EXPLOSIVE FLOOR

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20031010

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: RHEINMETALL WAFFE MUNITION GMBH

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REF Corresponds to:

Ref document number: 50213267

Country of ref document: DE

Date of ref document: 20090326

Kind code of ref document: P

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: FREI PATENTANWALTSBUERO AG

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2324096

Country of ref document: ES

Kind code of ref document: T3

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

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090211

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: 20090211

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 20090429

Year of fee payment: 8

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

BERE Be: lapsed

Owner name: RHEINMETALL WAFFE MUNITION G.M.B.H.

Effective date: 20090331

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

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090211

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090211

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: 20090713

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20090427

Year of fee payment: 8

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20091130

26N No opposition filed

Effective date: 20091112

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

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090331

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

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20091123

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: 20090512

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100312

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

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100331

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20100331

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

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090211

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

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20090312

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

Ref country code: TR

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: 20090211

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

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090211

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20150326

Year of fee payment: 14

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20150319

Year of fee payment: 14

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

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

Ref country code: SE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160313

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

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20160313

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20181205

REG Reference to a national code

Ref country code: DE

Ref legal event code: R084

Ref document number: 50213267

Country of ref document: DE

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20210319

Year of fee payment: 20

Ref country code: GB

Payment date: 20210324

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 50213267

Country of ref document: DE

Representative=s name: DREISS PATENTANWAELTE PARTG MBB, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 50213267

Country of ref document: DE

Representative=s name: DREISS PATENTANWAELTE PARTG MBB, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 50213267

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20220311

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

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20220311