EP1717543A1 - Device for testing ammunition - Google Patents
Device for testing ammunition Download PDFInfo
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing 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.
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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
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
Eine weitere Munitionsprüfvorrichtung für die Ermittlung von beim Anfeuern der Munition im Messlauf auftretenden innenballistischen bzw. rohrspezifischen Kenngrößen beschreibt die
Mit der
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
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.
- 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
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
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
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
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
Das Mess- bzw. Beschussgerät 1 eignet sich sehr gut für die Prüfung des Abbrandverhaltens hülsenloser teleskopierter Munition 10.The measuring or
Claims (10)
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)
| 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)
| 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 |
-
2005
- 2005-04-28 DE DE102005020180A patent/DE102005020180B3/en not_active Expired - Fee Related
-
2006
- 2006-03-07 DE DE502006000066T patent/DE502006000066D1/en active Active
- 2006-03-07 AT AT06004572T patent/ATE371161T1/en not_active IP Right Cessation
- 2006-03-07 EP EP06004572A patent/EP1717543B1/en not_active Not-in-force
Patent Citations (8)
| 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 |
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