EP1717543B1 - Device for testing ammunition - Google Patents

Device for testing ammunition Download PDF

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Publication number
EP1717543B1
EP1717543B1 EP06004572A EP06004572A EP1717543B1 EP 1717543 B1 EP1717543 B1 EP 1717543B1 EP 06004572 A EP06004572 A EP 06004572A EP 06004572 A EP06004572 A EP 06004572A EP 1717543 B1 EP1717543 B1 EP 1717543B1
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EP
European Patent Office
Prior art keywords
test device
munitions
radiation
munitions test
composite material
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.)
Not-in-force
Application number
EP06004572A
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German (de)
French (fr)
Other versions
EP1717543A1 (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
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Rheinmetall Waffe Munition GmbH
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Publication date
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Publication of EP1717543A1 publication Critical patent/EP1717543A1/en
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Publication of EP1717543B1 publication Critical patent/EP1717543B1/en
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Classifications

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

Definitions

  • 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 method for visualizing a firing process in a gun barrel by means of X-rays is known from US 4,329,584 known.
  • a disadvantage of these testers is that the examinations or evaluations are based only on pure measurement results.
  • 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.
  • 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.
  • 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.

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  • 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.

Ein Verfahren zum Sichtbarmachen eines abfeuerablaufes in einem Waffenrohr mittels Röntgenstrahlen ist aus der US 4 329 584 bekannt.A method for visualizing a firing process in a gun barrel by means of X-rays is known from US 4,329,584 known.

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)

  1. Munitions test device (1) with a housing (2) and with a body (3) in the housing (2) to hold a munition (10), which body consists of a fibre composite material (8) with an inner liner (7), with the body (3) having a layer thickness (d) at which it is transparent to rays (x1-4).
  2. Munitions test device according to Claim 1, characterized in that the body (3) simulates a cartridge holder or loading chamber of a weapon.
  3. Munitions test device according to Claim 1 or 2, characterized in that AFK (asbestos fibre reinforced), CFK (carbon fibre reinforced) and/or GFK (glass fibre reinforced) material, that are reverse wound, can be used as the fibre composite material.
  4. Munitions test device according to one of Claims 1 to 3, characterized in that the body (3) has at least one crack arrester layer.
  5. Munitions test device 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 fibre composite material (8) are wound.
  6. Munitions test device according to one of Claims 1 to 5, characterized in that the body (3) has a layer thickness (d) of approximately 30 mm.
  7. Munitions test device according to one of the preceding claims, characterized in that the rays (x1-4) are x-rays.
  8. Munitions test device according to one of the preceding claims, characterized in that to simulate a recoilless machine gun, a nozzle (4) and a tube (5) are incorporated and functionally connected to the body (3).
  9. Test arrangement using the munitions test device (1) according to one of Claims 1 to 7, characterized in that the x-ray sources (11) are arranged in front of the firing device (1) in such a way that the beams (X1-4) pass through the inlet end of the cartridge holder (3) at a defined angle and strike a detector arrangement (12) at the outlet end.
  10. Test arrangement using the munitions test device (1) according to one of Claims 1 to 7, characterized in that radiation is passed through a multiple-anode tube of the cartridge holder (3), behind which a fluorescent screen is located, with the x-radiation being converted into visible light that can be recorded by a high-speed camera and an upstream image amplifier.
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 EP1717543A1 (en) 2006-11-02
EP1717543B1 true EP1717543B1 (en) 2007-08-22

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

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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

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE174968C (en) *
BE625228A (en) * 1961-11-29
US4081988A (en) * 1977-03-18 1978-04-04 Pcb Piezotronics, Inc. Pressure transducer calibration
SE424765B (en) * 1979-03-29 1982-08-09 Volvo Bm VALVE CONNECTION
AT365776B (en) * 1980-09-30 1982-02-10 List Hans AMMUNITION TEST DEVICE
ATE171779T1 (en) * 1995-02-03 1998-10-15 Akzo Nobel Nv DEVICE FOR PROTECTION AGAINST EXPLOSIVE BODY
AU2002345613A1 (en) * 2001-08-13 2003-03-03 Allied Aerospace Industries, Inc. Method and apparatus for testing engines

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EP1717543A1 (en) 2006-11-02
ATE371161T1 (en) 2007-09-15
DE102005020180B3 (en) 2006-07-13
DE502006000066D1 (en) 2007-10-04

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