EP1717543A1 - Device for testing ammunition - Google Patents

Device for testing ammunition Download PDF

Info

Publication number
EP1717543A1
EP1717543A1 EP06004572A EP06004572A EP1717543A1 EP 1717543 A1 EP1717543 A1 EP 1717543A1 EP 06004572 A EP06004572 A EP 06004572A EP 06004572 A EP06004572 A EP 06004572A EP 1717543 A1 EP1717543 A1 EP 1717543A1
Authority
EP
European Patent Office
Prior art keywords
ammunition
tester according
munition
tester
radiation
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
EP06004572A
Other languages
German (de)
French (fr)
Other versions
EP1717543B1 (en
Inventor
Christoph Murek
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Waffe Munition GmbH
Original Assignee
Rheinmetall Waffe Munition GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rheinmetall Waffe Munition GmbH filed Critical Rheinmetall Waffe Munition GmbH
Publication of EP1717543A1 publication Critical patent/EP1717543A1/en
Application granted granted Critical
Publication of EP1717543B1 publication Critical patent/EP1717543B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B35/00Testing or checking of ammunition

Definitions

  • the invention relates to a Munitionsprüf réelle especially for medium caliber ammunition.
  • a further ammunition testing device for determining inside ballistic or pipe-specific parameters occurring during the firing of the ammunition in the measuring run describes the DE 31 32 085 C2 .
  • a disadvantage of these testers is that the examinations or evaluations are based only on pure measurement results.
  • the invention takes on the task to show an ammunition tester, which allows optimal investigation.
  • the invention is based on the idea, in particular to be able to photographically examine the firing process of an ammunition, the area in which the ignition takes place To carry out a radiation-permeable material or material.
  • these may be X-rays.
  • the X-ray transparent and a cartridge storage or Ladungsruam forming in the meter range consists of a preferably cylindrical fiber composite body (Hygienwebe), and is mounted in a metal housing. Due to a preferred wall thickness of max. 25 - 30 mm, the cartridge chamber used in the measuring device is sufficiently permeable to X-rays in order to monitor the burn-up process using X-ray technology, eg. B. to document by X-ray cinematography.
  • the cylindrical fiber composite body is therefore made to withstand the high pressures and temperatures introduced as a result of the ignition and, associated therewith, the explosion, ie, including impact pressures up to 4000 bar.
  • the composite body has a corresponding arrangement of different layers (laminate) made of different fiber composites. Furthermore, large tensile stresses occur in the axially supported cylinder in the circumferential direction, with the inner layers in particular experiencing a very great compressive stress. Therefore, in a preferred embodiment, in addition to an inner liner made of polyamide, at least one crack stop layer is provided in the laminate.
  • synthetic fiber composites up to a laminate thickness of about 30 mm have an X-ray permeability acceptable for the examination but also sufficient pressure stability.
  • fiber composites offer AFK (aramid fiber), CFRP (carbon fiber plastic) and / or GRP (fiberglass) to.
  • the laminate should consist of at least two distinctly different fiber orientations.
  • an aramid layer, a glass fiber layer and, again, an aramid layer are wound thereon.
  • the aramid fibers are each wound at an angle between 25 to 35 ° and the glass fibers at an angle of approximately 45 °.
  • the functioning of the firing device or the ammunition tester is primarily characterized by the specific structure of the composite body, such as fiber type, winding angle and lining of the inner surface with plastics and the installation of the body in the Beschuss réellegeophuse, for example, centered with pipe trim caps.
  • seals that prevent gas leakage are important. These seals may be, for example, plastic seals that have a specific shape.
  • the burn-up of the ammunition is preferably photographed, for example with the aid of X-ray technology or primarily.
  • images, in this case X-ray images, of the interior of the cartridge chamber or charge space are taken by a measuring arrangement.
  • a multi-anode tube radiates through the firing device with cartridge chamber, behind which there is a fluorescent screen. This converts the X-radiation into visible light, which can be recorded, for example, with a high-speed camera with an upstream image intensifier.
  • X-ray sources can also be included in the measurement and aligned with the cartridge chamber at different angles, so that measurements in different subareas of the cartridge chamber are possible.
  • an X-ray film is set up behind the cartridge chamber, whereby it is ensured by means of diaphragms that each radiation source illuminates only one area or strip of the film.
  • the radiation sources are activated with a time delay.
  • FIG. 1 shows a bombardment or measuring device 1 with a housing 2 and a cartridge chamber 3 located in the housing 2, as well as additional components, in this case a recoilless automatic cannon, for reconfiguring the ignition behavior of a projectile or ammunition 10.
  • additional components are in this Execution of a nozzle 4 and a pipe 5.
  • the cartridge chamber 3 is a fiber-wound, X-ray transparent, cylindrical body and preferably centered in the firing device 1 or in the housing 2.
  • the cartridge chamber 3 in each case on the front side according to the installation pipe fitting caps 6, which support the centered holder in the housing 2 by réellezentritation.
  • Fig. 2 shows the cartridge chamber 3 of Fig. 1 in a plan view with a Aufsetzkappe 6.
  • thickness d of the bearing 3 is preferably about 25 mm.
  • FIG. 3 shows a possible measuring arrangement 10 with a plurality of x-ray sources 11 arranged on the nozzle side of the firing device 1, here four.
  • a detector assembly 12 for example a film cassette, wherein in a known manner aperture 13 and 14 are used as collimators and can be made of polyethylene.
  • the radiation sources 11 are activated one after the other at defined time intervals.
  • the beam paths X 1-4 enter through the cartridge chamber 3 on the input side at a defined angle and exit again on the output side and impinge on the detector arrangement 12.
  • the ignition process in its entirety or the burning behavior can be evaluated in particular.
  • the measuring or firing device 1 is very well suited for testing the burn-off behavior of caseless telescoped ammunition 10.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
  • Investigating, Analyzing Materials By Fluorescence Or Luminescence (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Polymers With Sulfur, Phosphorus Or Metals In The Main Chain (AREA)

Abstract

In a munition testing device comprising a housing containing a receiver (3) for a munition, the receiver comprises fiber composite material (8) with an inner liner (7) and has a suitable layer thickness (d) to make it transparent to radiation. INDEPENDENT CLAIM are also included for two measuring systems incorporating the above device, in which: (A) X-ray sources are arranged before the shooting (i.e. testing) device such that radiation beams enter through a cartridge store (3) under a defined angle and collide with a detector device at the exit side; or (B) the cartridge store is irradiated through a multi-anode tube, behind which a fluorescence screen is located, so that the X-ray radiation is converted into visible light, which is received by a high-speed camera and an image intensifier in series.

Description

Die Erfindung betrifft ein Munitionsprüfgerät insbesondere für Mittelkaliber-Munition.The invention relates to a Munitionsprüfgerät especially for medium caliber ammunition.

Insbesondere für die Entwicklung von neuartiger Munition ist es wichtig, dass Zündverhalten und den Zündvorgang dieser Munition zu kennen bzw. zu studieren. In der Regel wird für diese Aufgabe ein Beschussgerät verwendet und die Ergebnisse ausgewertet.In particular, for the development of novel ammunition, it is important to know or study the ignition behavior and the ignition process of this ammunition. As a rule, a firing device is used for this task and the results are evaluated.

Bekannt ist ein Munitionsprüfgerät aus der DE 14 28 695 A1 . Die Brauchbarkeit der Munition wird hierbei durch die Messung eines Höchstgasdruckes und die Ermittlung eines Trefferbildes in einer Versuchsreihe bestimmt. Vorgeschlagen wird, alle mit dem Waffenrohr beweglichen Anbauten wie auch den Gasdruckmessapparat so anzubringen, dass der gemeinsame Schwerpunkt in der Seelenachse des Rohres liegt.Is known a Munitionsprüfgerät from the DE 14 28 695 A1 , The usefulness of the ammunition is determined here by the measurement of a maximum gas pressure and the determination of a target image in a series of experiments. It is proposed to mount all attachments movable with the weapon barrel as well as the gas pressure gauge so that the common center of gravity lies in the axis of the tube.

Eine weitere Munitionsprüfvorrichtung für die Ermittlung von beim Anfeuern der Munition im Messlauf auftretenden innenballistischen bzw. rohrspezifischen Kenngrößen beschreibt die DE 31 32 085 C2 .A further ammunition testing device for determining inside ballistic or pipe-specific parameters occurring during the firing of the ammunition in the measuring run describes the DE 31 32 085 C2 ,

Mit der CH 629 891 A5 wird ein Munitionsprüfapparat mit einem piezoelektrischen Druckwandler offenbart.With the CH 629 891 A5 An ammunition testing apparatus with a piezoelectric pressure transducer is disclosed.

Nachteilig bei diesen Prüfgeräten ist, dass die Untersuchungen bzw. Auswertungen nur auf reinen Messergebnissen basieren.A disadvantage of these testers is that the examinations or evaluations are based only on pure measurement results.

Hier greift die Erfindung die Aufgabe auf, ein Munitionsprüfgerät aufzuzeigen, welches eine optimale Untersuchung ermöglicht.Here, the invention takes on the task to show an ammunition tester, which allows optimal investigation.

Gelöst wird die Aufgabe durch die Merkmale des Patentanspruchs 1. Eine Messanordnung wird in den Ansprüchen 9 und 10 beansprucht.The problem is solved by the features of claim 1. A measuring arrangement is claimed in claims 9 and 10.

Der Erfindung liegt die Idee zugrunde, um insbesondere den Zündungsvorgang einer Munition fotographisch untersuchen zu können, den Bereich, in welchem die Zündung erfolgt, aus einem Strahlen durchlässigen Material bzw. Werkstoff auszuführen. Bevorzugt kann es sich dabei um Röntgenstrahlen handeln.The invention is based on the idea, in particular to be able to photographically examine the firing process of an ammunition, the area in which the ignition takes place To carry out a radiation-permeable material or material. Preferably, these may be X-rays.

Der Röntgenstrahlen transparente und ein Patronenlager bzw. Ladungsruam im Messgerät bildende Bereich besteht dabei aus einem vorzugsweise zylindrischen Faserverbundkörper (Hybridgewebe), und ist in einem Metallgehäuse angebracht. Das im Messgerät verwendete Patronenlager ist aufgrund einer bevorzugten Wanddicke von maximal 25 - 30 mm für Röntgenstrahlen ausreichend durchlässig, um den Abbrandvorgang röntgentechnisch, z. B. mittels Röntgenkinematographie zu dokumentieren.The X-ray transparent and a cartridge storage or Ladungsruam forming in the meter range consists of a preferably cylindrical fiber composite body (Hygienwebe), and is mounted in a metal housing. Due to a preferred wall thickness of max. 25 - 30 mm, the cartridge chamber used in the measuring device is sufficiently permeable to X-rays in order to monitor the burn-up process using X-ray technology, eg. B. to document by X-ray cinematography.

Insbesondere bei der Prüfung von teleskopierter hülsenloser Munition treten hohe Drücke im Patronenlager auf. Der zylindrische Faserverbundkörper ist deshalb so gefertigt, dass dieser den hohen Drücken und Temperaturen, die infolge der Zündung und damit verbunden der Explosion eingeleitet werden, standhält, d.h., u. a. Beschussdrücke bis zu 4000 bar. Der Verbundkörper weist dazu eine entsprechende Anordnung verschiedener Schichten (Laminat) aus unterschiedlichen Faserverbundwerkstoffen auf.
Im axial abgestützten Zylinder treten des Weiteren in Umfangsrichtung große Zugspannungen auf, wobei insbesondere die inneren Schichten eine sehr große Druckbeanspruchung erfahren. Daher ist in einer bevorzugten Ausführung neben einem inneren Liner aus Polyamid wenigstens eine Rissstoppschicht im Laminat vorgesehen.
Especially in the examination of telescoped caseless ammunition occur high pressures in the chamber. The cylindrical fiber composite body is therefore made to withstand the high pressures and temperatures introduced as a result of the ignition and, associated therewith, the explosion, ie, including impact pressures up to 4000 bar. The composite body has a corresponding arrangement of different layers (laminate) made of different fiber composites.
Furthermore, large tensile stresses occur in the axially supported cylinder in the circumferential direction, with the inner layers in particular experiencing a very great compressive stress. Therefore, in a preferred embodiment, in addition to an inner liner made of polyamide, at least one crack stop layer is provided in the laminate.

Es hat sich gezeigt, dass Kunstfaserverbundstoffe bis zu einer Laminatdicke von ca. 30 mm eine für die Untersuchung akzeptable Durchlässigkeit für die Röntgenstrahlen aber auch eine ausreichende Druckstabilität aufweisen. Als Faserverbundstoffe bieten sich AFK (Aramidfaserkunststoff), CFK (Kohlenstofffaserkunststoff) und / oder GFK (Glasfaserkunststoff) an. Dabei sollte das Laminat aus wenigstens zwei deutlich unterschiedlichen Faserorientierungen bestehen. Gewickelt werden dazu abwechselnd beispielsweise eine Aramidschicht, eine Glasfaserlage und darauf erneut eine Aramidschicht. Die Aramidfasern werden dabei beispielsweise jeweils in einem Winkel zwischen 25 bis 35 ° und die Glasfasern in einem Winkel von ca. 45° gewickelt.It has been shown that synthetic fiber composites up to a laminate thickness of about 30 mm have an X-ray permeability acceptable for the examination but also sufficient pressure stability. As fiber composites offer AFK (aramid fiber), CFRP (carbon fiber plastic) and / or GRP (fiberglass) to. The laminate should consist of at least two distinctly different fiber orientations. Alternately, for example, an aramid layer, a glass fiber layer and, again, an aramid layer are wound thereon. For example, the aramid fibers are each wound at an angle between 25 to 35 ° and the glass fibers at an angle of approximately 45 °.

Die Funktionsweise des Beschussgerätes bzw. des Munitionsprüfgerätes wird vorrangig durch den spezifischen Aufbau des Verbundkörpers, wie Faserart, Wickelwinkel und Auskleidung der Innenoberfläche mit Kunststoffen sowie dem Einbau des Körpers in das Beschussgerätgehäuse, beispielsweise innenzentriert mit Rohraufsatzkappen geprägt. In einigen Fällen sind Dichtungen, die einen Gasaustritt verhindern, wichtig. Diese Dichtungen können beispielsweise Kunststoffdichtungen sein, die eine spezifische Form aufweisen.The functioning of the firing device or the ammunition tester is primarily characterized by the specific structure of the composite body, such as fiber type, winding angle and lining of the inner surface with plastics and the installation of the body in the Beschussgerätgehäuse, for example, centered with pipe trim caps. In some cases, seals that prevent gas leakage are important. These seals may be, for example, plastic seals that have a specific shape.

Im Verbundkörper wird beispielsweise mit Hilfe der Röntgentechnik vorzugsweise oder auch vorrangig der Abbrand der Munition fotografiert. Dazu werden während des Schusses zu definierten Zeiten Bilder, hier Röntgenbilder, vom Innenleben des Patronenlagers bzw. Ladungsraums durch eine Messanordnung aufgenommen.In the composite body, the burn-up of the ammunition is preferably photographed, for example with the aid of X-ray technology or primarily. For this purpose, during the shot at defined times, images, in this case X-ray images, of the interior of the cartridge chamber or charge space are taken by a measuring arrangement.

In einer ersten Variante einer möglichen Messanordnung durchstrahlt eine Mehrfachanodenröhre das Beschussgerät mit Patronenlager, hinter dem sich ein Fluoreszenzschirm befindet. Dieser wandelt die Röntgenstrahlung in sichtbares Licht um, welches beispielsweise mit einer Hochgeschwindigkeitskamera mit einem vorgeschalteten Bildverstärker aufgenommen werden kann.In a first variant of a possible measuring arrangement, a multi-anode tube radiates through the firing device with cartridge chamber, behind which there is a fluorescent screen. This converts the X-radiation into visible light, which can be recorded, for example, with a high-speed camera with an upstream image intensifier.

Bei der bevorzugten weiteren Variante können auch mehrere (beispielsweise vier) Röntgenstrahlenquellen in die Messung eingebunden und zum Patronenlager in unterschiedlichen Winkeln ausgerichtet werden, so dass Messungen in verschiedenen Teilbereichen des Patronenlagers möglich sind. Hinter dem Patronenlager wird beispielsweise ein Röntgenfilm aufgestellt, wobei mittels Blenden sichergestellt wird, dass jede Strahlenquelle nur einen Bereich bzw. Streifen des Films belichtet. Für die Messung werden die Strahlenquellen zeitversetzt aktiviert.In the preferred further variant, several (for example four) X-ray sources can also be included in the measurement and aligned with the cartridge chamber at different angles, so that measurements in different subareas of the cartridge chamber are possible. For example, an X-ray film is set up behind the cartridge chamber, whereby it is ensured by means of diaphragms that each radiation source illuminates only one area or strip of the film. For the measurement, the radiation sources are activated with a time delay.

Anhand eines Ausführungsbeispieles mit Zeichnung wird die Erfindung näher erläutert. Es zeigt:

Fig. 1
eine Darstellung des Beschussgerätes mit einem fasergewickelten Patronenlager,
Fig. 2
eine Darstellung des gewickelten Patronenlagers in einer Draufsicht,
Fig.3
eine Messanordnung mit dem Patronenlager und dem Beschussgerätes aus Fig. 1.
Reference to an embodiment with drawing, the invention is explained in detail. It shows:
Fig. 1
a representation of the firing device with a fiber-wound cartridge chamber,
Fig. 2
a representation of the wound cartridge chamber in a plan view,
Figure 3
a measuring arrangement with the cartridge chamber and the firing device of FIG. 1.

Fig. 1 zeigt ein Beschuss- bzw. Messgerät 1 mit einem Gehäuse 2 und einem im Gehäuse 2 befindlichen Patronenlager 3, sowie zusätzlichen Komponenten, hier einer rückstoßfreien Maschinenkanone, zur Nachgestaltung des Zündungsverhaltens eines Projektils oder einer Munition 10. Diese zusätzlichen Komponenten sind in dieser Ausführung eine Düse 4 sowie ein Rohr 5.1 shows a bombardment or measuring device 1 with a housing 2 and a cartridge chamber 3 located in the housing 2, as well as additional components, in this case a recoilless automatic cannon, for reconfiguring the ignition behavior of a projectile or ammunition 10. These additional components are in this Execution of a nozzle 4 and a pipe 5.

Das Patronenlager 3 ist ein fasergewickelter, Röntgenstrahlen transparenter, zylindrischer Körper und im Beschussgerät 1 bzw. im Gehäuse 2 bevorzugt zentriert gelagert. Dazu weist das Patronenlager 3 jeweils stirnseitig dem Einbau entsprechend Rohraufsatzkappen 6 auf, welche durch Innenzentrierung die zentrierte Halterung im Gehäuse 2 unterstützen. Als Innenliner 7 bietet sich insbesondere eine Ausführung ein Kunststoff, beispielsweise Polyamid an, auf den der Faserverbundstoff 8 bzw. die Lagen aufgewickelt werden. Die Herstellung bzw. Wicklung ist herkömmlich.The cartridge chamber 3 is a fiber-wound, X-ray transparent, cylindrical body and preferably centered in the firing device 1 or in the housing 2. For this purpose, the cartridge chamber 3 in each case on the front side according to the installation pipe fitting caps 6, which support the centered holder in the housing 2 by Innenzentrierung. As an inner liner 7, in particular, a design offers a plastic, such as polyamide on which the fiber composite 8 or the layers are wound. The production or winding is conventional.

Fig. 2 zeigt das Patronenlager 3 aus Fig. 1 in einer Draufsicht mit einer Aufsetzkappe 6. Dicke d des Lagers 3 beträgt vorzugsweise ca. 25 mm.Fig. 2 shows the cartridge chamber 3 of Fig. 1 in a plan view with a Aufsetzkappe 6. thickness d of the bearing 3 is preferably about 25 mm.

In Fig. 3 ist eine mögliche Messanordnung 10 mit mehreren, hier vier, um das Beschussgerät 1 düsenseitig angeordneten Röntgenstrahlenquellen 11 aufgezeigt. Am Ausgang des Beschussgerätes 1, rohrseitig, befindet sich eine Detektoranordnung 12, beispielsweise eine Filmkassette, wobei in bekannter Art und Weise Blenden 13 und 14 als Kollimatoren eingesetzt werden und aus Polyethylen bestehen können.FIG. 3 shows a possible measuring arrangement 10 with a plurality of x-ray sources 11 arranged on the nozzle side of the firing device 1, here four. At the output of the firing device 1, tube side, there is a detector assembly 12, for example a film cassette, wherein in a known manner aperture 13 and 14 are used as collimators and can be made of polyethylene.

Für die Messung werden die Strahlenquellen 11 nacheinander in definierten Zeitabständen aktiviert. Die Strahlengänge X1-4 treten dabei durch das Patronenlager 3 eingangsseitig unter einem definierten Winkel ein und ausgangsseitig wieder aus und treffen auf die Detektoranordnung 12 auf. Mit Hilfe der dabei abgebildeten Röntgenbilder (nicht näher dargestellt) kann dann der Zündvorgang in seiner Gesamtheit bzw. das Abbrandverhalten im speziellen ausgewertet werden.For the measurement, the radiation sources 11 are activated one after the other at defined time intervals. In this case, the beam paths X 1-4 enter through the cartridge chamber 3 on the input side at a defined angle and exit again on the output side and impinge on the detector arrangement 12. With the help of the X-ray images shown here (not shown in detail), the ignition process in its entirety or the burning behavior can be evaluated in particular.

Das Mess- bzw. Beschussgerät 1 eignet sich sehr gut für die Prüfung des Abbrandverhaltens hülsenloser teleskopierter Munition 10.The measuring or firing device 1 is very well suited for testing the burn-off behavior of caseless telescoped ammunition 10.

Claims (10)

Munitionsprüfgerät (1) mit einem Gehäuse (2) und einem im Gehäuse (2) eine Munition (10) aufnehmenden Körper (3), welcher aus einem Faserverbundwerkstoff (8) mit einem Innenliner (7) besteht, wobei der Körper (3) eine Schichtdicke (d) aufweist, bei der dieser Strahlen (X1-4) transparent ist.Ammunition tester (1) comprising a housing (2) and a body (3) accommodating an ammunition (10) in the housing (2), which consists of a fiber composite material (8) with an inner liner (7), wherein the body (3) has a Layer thickness (d) at which these rays (X 1-4 ) is transparent. Munitionsprüfgerät nach Anspruch 1, dadurch gekennzeichnet, dass der Körper (3) ein Patronelager bzw. Ladungsraum einer Waffe nachbildet.Ammunition tester according to claim 1, characterized in that the body (3) simulates a cartridge storage or cargo space of a weapon. Munitionsprüfgerät nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass als Faserverbundstoffe AFK, CFK und / oder GFK eingesetzt werden können, die abwechselnd gewickelt werden.Munition tester according to claim 1 or 2, characterized in that AFK, CFK and / or GRP can be used as fiber composites, which are wound alternately. Munitionsprüfgerät nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass der Körper (3) wenigstens eine Rissstoppschicht aufweist.Ammunition tester according to one of claims 1 to 3, characterized in that the body (3) has at least one crack stop layer. Munitionsprüfgerät nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass der Innenliner (7) des Körpers (3) aus Polyamid besteht, auf dem die Lagen des Faserverbundstoffes (8) aufgewickelt sind.Ammunition tester according to one of claims 1 to 4, characterized in that the inner liner (7) of the body (3) consists of polyamide, on which the layers of the fiber composite material (8) are wound. Munitionsprüfgerät nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass der Körper (3) eine Schichtdicke (d) von ca. 30mm aufweist.Munition tester according to one of claims 1 to 5, characterized in that the body (3) has a layer thickness (d) of about 30mm. Munitionsprüfgerät nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass die Strahlen (X1-4) Röntgenstrahlen sind.Ammunition tester according to one of the preceding claims, characterized in that the beams (X 1-4 ) are X-rays. Munitionsprüfgerät nach einem der vorgenannten Ansprüche, dadurch gekennzeichnet, dass zur Simulation einer rückstoßfreien Maschinenkanone eine Düse (4) sowie ein Rohr (5) eingebunden und mit dem Körper (3) funktional verbunden sind.Ammunition tester according to one of the preceding claims, characterized in that for simulation of a recoilless machine gun a nozzle (4) and a pipe (5) are integrated and connected to the body (3) functionally. Messanordnung unter Nutzung des Munitionsprüfgerätes (1) nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass Röntgenstrahlenquellen (11) so vor dem Beschussgerät (1) angeordnet werden, dass die Strahlengänge (X1-4) durch das Patronenlager (3) eingangsseitig unter einem definierten Winkel ein und ausgangsseitig auf eine Detektoranordnung (12) auftreffen.Measuring arrangement using the ammunition testing device (1) according to one of claims 1 to 7, characterized in that X-ray sources (11) are arranged in front of the firing device (1) that the beam paths (X 1-4 ) through the chamber (3) on the input side at a defined angle and on the output side impinge on a detector arrangement (12). Messanordnung unter Nutzung des Munitionsprüfgerätes (1) nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass durch eine Mehrfachanodenröhre das Patronenlager (3) durchstrahlt wird, hinter dem sich ein Fluoreszenzschirm befindet, wobei die Röntgenstrahlung in sichtbares Licht umgewandelt wird, welches mit einer Hochgeschwindigkeitskamera und einem vorgeschalteten Bildverstärker aufgenommen wird.Measuring arrangement using the ammunition testing device (1) according to one of claims 1 to 7, characterized in that through a multi-anode tube, the chamber (3) is irradiated behind which a fluorescent screen is, wherein the X-radiation is converted into visible light, which with a High-speed camera and an upstream image intensifier is recorded.
EP06004572A 2005-04-28 2006-03-07 Device for testing ammunition Not-in-force EP1717543B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005020180A DE102005020180B3 (en) 2005-04-28 2005-04-28 Munition testing device, especially for investigating priming behaviour, comprises radiation-transparent munition receiver of fiber composite material with inner liner, allowing photographic monitoring

Publications (2)

Publication Number Publication Date
EP1717543A1 true EP1717543A1 (en) 2006-11-02
EP1717543B1 EP1717543B1 (en) 2007-08-22

Family

ID=36599644

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06004572A Not-in-force EP1717543B1 (en) 2005-04-28 2006-03-07 Device for testing ammunition

Country Status (3)

Country Link
EP (1) EP1717543B1 (en)
AT (1) ATE371161T1 (en)
DE (2) DE102005020180B3 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006016352A1 (en) * 2006-04-05 2007-10-11 Rheinmetall Waffe Munition Gmbh Munitions
RU2413917C1 (en) * 2009-12-28 2011-03-10 Государственное Образовательное Учреждение Высшего Профессионального Образования "Московский Государственный Технический Университет Имени Н.Э. Баумана" Device and method of wire electric connection for recording of operation parametres of thrown body in complete ballistic cycle
DE102010016963A1 (en) 2010-05-17 2011-11-17 Krauss-Maffei Wegmann Gmbh & Co. Kg Weapon system, method for firing and detecting ammunition bodies
CN103335566B (en) * 2013-07-09 2015-01-21 中国工程物理研究院总体工程研究所 Grid mesh target shell penetration depth testing device

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE174968C (en) *
DE1428695A1 (en) 1961-11-29 1969-01-23 Mauser Werke Ag Ammunition testing device
DE3132085A1 (en) * 1980-09-30 1982-04-15 List, Hans, Prof. Dipl.-Ing. Dr.Dr.h.c., 8010 Graz Ammunition testing device
US4329584A (en) * 1979-03-27 1982-05-11 Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag Apparatus for rendering visible moved objects
CH629891A5 (en) 1977-03-18 1982-05-14 Pcb Piezotronics Inc AMMUNITION CONTROLLER.
EP0725260A1 (en) * 1995-02-03 1996-08-07 Akzo Nobel N.V. Protection device against explosive objects
WO2003016849A2 (en) * 2001-08-13 2003-02-27 Allied Aerospace Industries, Inc. Method and apparatus for testing engines

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE174968C (en) *
DE1428695A1 (en) 1961-11-29 1969-01-23 Mauser Werke Ag Ammunition testing device
CH629891A5 (en) 1977-03-18 1982-05-14 Pcb Piezotronics Inc AMMUNITION CONTROLLER.
US4329584A (en) * 1979-03-27 1982-05-11 Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag Apparatus for rendering visible moved objects
DE3132085A1 (en) * 1980-09-30 1982-04-15 List, Hans, Prof. Dipl.-Ing. Dr.Dr.h.c., 8010 Graz Ammunition testing device
DE3132085C2 (en) 1980-09-30 1983-06-01 List, Hans, Prof. Dipl.-Ing. Dr.Dr.h.c., 8010 Graz Ammunition testing device
EP0725260A1 (en) * 1995-02-03 1996-08-07 Akzo Nobel N.V. Protection device against explosive objects
WO2003016849A2 (en) * 2001-08-13 2003-02-27 Allied Aerospace Industries, Inc. Method and apparatus for testing engines

Also Published As

Publication number Publication date
ATE371161T1 (en) 2007-09-15
DE102005020180B3 (en) 2006-07-13
DE502006000066D1 (en) 2007-10-04
EP1717543B1 (en) 2007-08-22

Similar Documents

Publication Publication Date Title
DE2055805A1 (en) Launching device for projectiles
EP1717543B1 (en) Device for testing ammunition
DE3438971A1 (en) SPECIAL ENDOSCOPE FOR OPTICAL TISSUE INSPECTION
Charles et al. Primer composition and memory effect of weapons—Some trends from a systematic approach in casework
DE102011116059A1 (en) Muffler for a handgun
DE102017104088A1 (en) Integral muffler for a rifle barrel
DE3716883A1 (en) Electronic measuring and test system for analyzing weapons and their ammunition
DE102017000486B4 (en) System and method for ballistic testing of projectiles
DE102018106220A1 (en) Optical system of a stereo video endoscope and method of making the same
DE102012103524A1 (en) Method for recording image of scene and/or object, involves widening laser beam to produce unscattered light beam, illuminating and/or screening scene with unscattered light beam to produce shadow image of scene, and recording shadow image
DE2700600C2 (en) Device for testing weapon barrels
Thoma et al. Real time-resolved flash X-ray cinematographic investigation of interface defeat and numerical simulation validation
Werner et al. Influence of pellet seating on the external ballistic parameters of spring-piston air guns
DE102007056500B3 (en) tester
DE2040225A1 (en) Method and device for determining the exit error angle of a projectile when leaving the barrel
DE4336808C2 (en) Test projectile for displaying the ignition function of a projectile
DE202017101110U1 (en) Integral muffler for a rifle barrel
DE102004018529B4 (en) laser measurement system
EP1843121B1 (en) Munition test device
DE102023135978A1 (en) Gun and method for adjusting an aiming device of such a gun
Walker Stress Strain Relationships In Ultra High Molecular Weight Polyethylene Fibers Under Ballistic Loading
Meredith et al. The Novel “Fracture” Gun at the DEVCOM Army Research Laboratory for Precise, Highly Instrumented Impact Experiments
DE19811659C1 (en) Cartridge for use in different weapons systems with aiming device setting independent of target distance
DE102018113136A1 (en) Camera module and camera system with a camera module
Sinclair 3D PRINTING SUPPRESSORFOR SMALL ARMSUSING FUSEDDEPOSITIONMODELING

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

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA HR MK YU

17P Request for examination filed

Effective date: 20061011

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

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK 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

Ref country code: CH

Ref legal event code: NV

Representative=s name: OK PAT AG PATENTE MARKEN LIZENZEN

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20070906

REF Corresponds to:

Ref document number: 502006000066

Country of ref document: DE

Date of ref document: 20071004

Kind code of ref document: P

ET Fr: translation filed
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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20071203

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: 20070822

Ref country code: BG

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

Effective date: 20071122

Ref country code: IS

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

Effective date: 20071222

Ref country code: LT

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

Effective date: 20070822

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: 20070822

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

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

Effective date: 20070822

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

Ref country code: LV

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

Effective date: 20070822

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

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

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: 20070822

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: 20071123

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

Ref country code: SK

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: 20070822

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: 20080122

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: 20070822

Ref country code: CZ

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: 20070822

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

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

Ref country code: RO

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: 20070822

Ref country code: SE

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

Effective date: 20071122

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

Ref country code: AT

Payment date: 20080314

Year of fee payment: 3

26N No opposition filed

Effective date: 20080526

BERE Be: lapsed

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

Effective date: 20080331

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

Ref country code: MC

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

Effective date: 20080331

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

Ref country code: EE

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: 20070822

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: 20080331

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

Ref country code: SI

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: 20070822

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: 20070822

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: 20090307

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

Ref country code: FR

Payment date: 20100402

Year of fee payment: 5

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

Ref country code: GB

Payment date: 20100322

Year of fee payment: 5

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

Ref country code: HU

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: 20080223

Ref country code: LU

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

Effective date: 20080307

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: 20070822

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

Ref country code: DE

Payment date: 20100324

Year of fee payment: 5

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: CH

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

Effective date: 20100331

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: 20070822

Ref country code: LI

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

Effective date: 20100331

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20110307

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20111130

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: 20110331

Ref country code: DE

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

Effective date: 20111001

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502006000066

Country of ref document: DE

Effective date: 20111001

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

Ref country code: GB

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

Effective date: 20110307