EP1241435A1 - Projectile and manufacturing method therefor - Google Patents
Projectile and manufacturing method therefor Download PDFInfo
- Publication number
- EP1241435A1 EP1241435A1 EP02002216A EP02002216A EP1241435A1 EP 1241435 A1 EP1241435 A1 EP 1241435A1 EP 02002216 A EP02002216 A EP 02002216A EP 02002216 A EP02002216 A EP 02002216A EP 1241435 A1 EP1241435 A1 EP 1241435A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- jacket
- receiving coil
- energy source
- logic module
- 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
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/006—Mounting of sensors, antennas or target trackers on projectiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/02—Fuze bodies; Fuze housings
Definitions
- the project relates to a projectile according to the preamble of claim 1 and a method for its production according to the preamble of claim 15 and 18 respectively .
- Projectiles of this type are intended to disassemble or detonate in flight and are therefore also called 'Air Bursting Munitions', abbreviated ABM, designated.
- Projectiles detonating in flight have timers, revolvers or proximity detonator. The location or the time of the detonation should be selectable or adjustable. With newer projectiles the setting of the The time of the detonation or temperature control is not done manually by manipulation on the projectile before loading, but automatically, either during feeding or in the chamber or by inductive signal transmission at the muzzle at the launch.
- the projectiles have special devices for receiving the signals and via an energy source for operating a Detonator logic and to deliver the electrical energy required in the projectile to Trigger the detonation.
- the effective mass should be as large as possible and the resulting from the detonation Projectile parts should have the highest possible speed; this requires among other things, a high drive pressure on the projectile floor, which runs solidly must be a high axial acceleration and a high muzzle velocity, so that also rotational speeds and rotational accelerations are high.
- the programmable device with the energy source and the logic module must function reliably and precisely.
- the ineffective mass to which the programmable device, especially the receiving coil, the energy source and the logic module belong be as small as possible. Accordingly, the programmable device delicate and vulnerable parts that need to be well protected so that they have the great forces caused by the great accelerations will survive.
- the projectile should be able to be produced efficiently, if possible from individually producible units that are manufactured in parallel and then in simple Can be put together; A modular one is therefore desirable Construction.
- the new projectile has a jacket which is at least in the The rear area of the projectile is made of a plastic. This is the non-effective mass of the projectile less than that of a projectile with one metallic cladding, and surface treatments, as in conventional metallic coats are not required.
- the shape of the plastic can be machined or non-cutting Procedure.
- the plastic for the jacket is preferably shaped by a non-cutting process such as pressing or spraying; such operations are particular for large quantities, as is common in the manufacture of projectiles are rational, since then the cost of the shape is practically insignificant.
- a reception coil is arranged for receiving external signals. Because this before Pressure must be protected, it is advantageous not to the extent of the projectile but arranged inside the projectile. This means that the plastic from which the jacket is made, at least in the area of Receiver coil has no shielding effect against electromagnetic waves or signals.
- an elaborate protective wrapping as for a conventionally arranged on the outside of the jacket Receiving coil is necessary to provide. You avoid - even better than with the protective wrap - that the conductors that make up the receiving coil deform; this will interfere with the signals to be received avoided due to deformation of the conductor and the risk of short circuits reduced. It further increases the risk of moisture ingress practically turned off. It is also essential that because of the smaller distance the receiving coil from the project longitudinal axis the circumferential acceleration and thus the forces acting on the receiving coil are reduced.
- the receiving coil can thereby as a Unit manufactured and then with the energy source and the logic module to be assembled.
- the energy required can be generated externally and transmitted to the projectile: It is advantageous because it is independent of the weapon system, but it is an internal energy source, for example with a shock generator.
- a particularly advantageous projectile according to the invention is designed such that its active mass, in particular explosives and possibly active bodies, in the front Area of the projectile are arranged; so you get a good effect, as explained below: After the detonation, the velocity vectors add up the resulting active body to the speed of Projectile, and the sum of the speeds is the average of all arising Parts larger in projectiles with front active mass; Furthermore can, for example, in house fighting, by detonating the projectiles the goal of enlarging the target area can be achieved in comparison with conventional ammunition or ABM with a detonator is considerable.
- the projectile 10.1 shown in FIG. 1 with the longitudinal axis A of the projectile has a projectile base 12 made of a suitable metal and a jacket 14 , which consists at least in the rear area, but preferably entirely, of a suitable plastic.
- the jacket 14 is produced by a press or injection molding process, but could alternatively also be formed by machining. Simultaneously with the manufacture of the jacket 14, it can be connected to the projectile floor 12 ;
- the projectile base 12 has grooves 12B on the outer surface of its essentially hollow cylindrical base region 12A .
- the grooves 12B are extrusion- coated with the material of the jacket 14 , so that the forwardly projecting bottom region 12A is connected to a laterally projecting jacket region 14A .
- the plastic used to produce the jacket 14 may contain fillers, but at least in the area of the receiving coil it must consist of a material that does not form a shield against electromagnetic waves or signals. Instead of a plastic, other materials that do not have a shielding effect against electromagnetic waves or signals, for example ceramic or glass, can also be used.
- An integral guide band 15 is formed on the outer contour of the jacket 14 ; this eliminates the production and assembly of a separate, for example metallic, guide belt.
- a receiving coil 16 is arranged centrally as part of the programmable device, the winding 18 of which is attached to a coil former 20, preferably made of a plastic, in the center of the projectile longitudinal axis A.
- the receiving coil 16 is conductively connected to an energy source or energy storage unit 22 and a logic module 23 .
- a conductor does not have to be passed through a narrow bore, as in conventional projectiles, but the connection can be made due to the central arrangement of both the receiving coil 16 and the energy source or Energy storage unit 22 and the logic module 23 can be created in a simple manner.
- the conductive connection including the actual contact can be made by soldering.
- an inserted intermediate part can be used, the contacting being produced by means of a conductive adhesive. It is particularly easy to manufacture, but it is less certain to make the contact simply by pressing.
- a plug-in connection is complex to manufacture, but this ensures great security and is easy to assemble.
- the projectile 10.1 described above according to FIG. 1 is produced as follows: the jacket 14 is produced by spraying; the projectile base 12 is extrusion-coated with the plastic of the jacket 12 or the tail.
- the energy source or energy storage unit 22, the logic module 23 and the receiving coil 16 are then introduced from the front.
- FIG. 2 shows a further projectile 10.2 according to the invention.
- the projectile 10.2 differs only slightly from the projectile 10.1, therefore only the details deviating from FIG. 1 are described below, and the same reference numerals are used for the individual structural elements in FIG. 2 and further below in FIG. 3 as in FIG Fig. 1.
- the inner diameter of the jacket region 14A projecting to the rear is larger than the outer diameter of the coil 16.
- the projectile 10.2 is produced as follows: The jacket 14 or the rear is produced by non-cutting or machining, the jacket region 14A projecting to the rear being provided with an internal thread 14B .
- the projecting bottom area 12A of the projectile bottom is not provided with the ribs 12A but with an external thread 12B which is complementary to the internal thread 14B .
- the receiving coil 16, the energy source or energy storage unit 22 and the logic module 23 are manufactured individually, attached to the projectile base 12 and contacted. Finally, the resulting component is introduced into the jacket 14 from behind, the connection of the projectile base 12 and jacket 14 being achieved by screwing the external thread 12B into the internal thread 14B .
- a third projectile 10.3 is shown in FIG. 3 .
- the same material is used for the projectile base 12 for the projectile 10.3 as for the jacket 14; in this case, the projectile base 12 and the jacket 14 are produced integrally in a press or injection molding process as a press or injection part 13 .
- the reception coil 16, the energy source or energy storage unit 22 and the logic module 23 are produced separately, then these three components of the projectile 10.3 are combined into one component in the same way as described with reference to the projectile 10.1 of FIG. 1 , and this component mounted from the front in the pressed or injection molded part 13 .
- the receiving coil 16 the energy source or energy storage unit 22 and the logic module 23 are arranged in the rear projectile area, so that the front projectile area is free to accommodate an active mass, not shown.
Abstract
Description
Die Erfindung betrifft ein Projektil nach dem Oberbegriff des Anspruchs 1 und ein
Verfahren zu dessen Herstellung nach dem Oberbegriff des Anspruchs 15 bzw.
18. The project relates to a projectile according to the preamble of claim 1 and a method for its production according to the preamble of
Projektile dieser Art sind dazu vorgesehen, sich im Flug zu zerlegen bzw. zu detonieren und werden deshalb auch als ,Air Bursting Munition', abgekürzt ABM, bezeichnet. Im Flug detonierende Projektile weisen Zeitzünder, Umdrehungszünder oder Näherungszünder auf. Der Ort bzw. der Zeitpunkt der Detonation soll wählbar bzw. einstellbar sein. Bei neueren Projektilen erfolgt das Einstellen des Zeitpunktes der Detonation bzw. Tempieren nicht manuell durch eine Manipulation am Projektil vor dem Laden, sondern selbsttätig, entweder bei der Zuführung oder im Patronenlager oder durch induktive Signalübertragung an der Waffenmündung beim Abschuss. Die Projektile verfügen über spezielle Vorrichtungen zum Empfangen der Signale und über eine Energiequelle zum Betreiben einer Zünderlogik und zur Abgabe der im Projektil benötigten elektrischen Energie zum Auslösen der Detonation.Projectiles of this type are intended to disassemble or detonate in flight and are therefore also called 'Air Bursting Munitions', abbreviated ABM, designated. Projectiles detonating in flight have timers, revolvers or proximity detonator. The location or the time of the detonation should be selectable or adjustable. With newer projectiles the setting of the The time of the detonation or temperature control is not done manually by manipulation on the projectile before loading, but automatically, either during feeding or in the chamber or by inductive signal transmission at the muzzle at the launch. The projectiles have special devices for receiving the signals and via an energy source for operating a Detonator logic and to deliver the electrical energy required in the projectile to Trigger the detonation.
Die Anforderungen, die an solche Projektile gestellt werden, sind zahlreich.The demands placed on such projectiles are numerous.
Zum Einen soll zwecks Erzielen einer guten Wirkung die zum Detonationsort gebrachte Wirkmasse möglichst gross sein und die bei die Detonation entstehenden Geschossteile sollen eine möglichst hohe Geschwindigkeit haben; dies bedingt unter Anderem eine hohen Antriebsdruck auf den Projektilboden, der solid ausgeführt sein muss, eine hohe Achsialbeschleunigung und eine hohe Mündungsgeschwindigkeit, so dass auch Rotationsgeschwindigkeiten und Rotationsbeschleunigungen hoch sind. Die programmierbare Einrichtung mit der Energiequelle und dem Logikmodul muss zuverlässig und präzis funktionieren.On the one hand, in order to achieve a good effect, the one brought to the detonation site The effective mass should be as large as possible and the resulting from the detonation Projectile parts should have the highest possible speed; this requires among other things, a high drive pressure on the projectile floor, which runs solidly must be a high axial acceleration and a high muzzle velocity, so that also rotational speeds and rotational accelerations are high. The programmable device with the energy source and the logic module must function reliably and precisely.
Zum Anderen soll die nicht-wirksame Masse, zu der die programmierbare Einrichtung, insbesondere die Empfangsspule, die Energiequelle und das Logikmodul gehören, möglichst gering sein. Demzufolge weist die programmierbare Einrichtung heikle und leicht verletzliche Teile auf, die gut geschützt werden müssen, damit sie die grossen Kräfte, die durch die grossen Beschleunigungen verursacht werden, überstehen.Secondly, the ineffective mass to which the programmable device, especially the receiving coil, the energy source and the logic module belong, be as small as possible. Accordingly, the programmable device delicate and vulnerable parts that need to be well protected so that they have the great forces caused by the great accelerations will survive.
Schliesslich sollte das Projektil rationell hergestellt werden können, möglichst aus einzeln anfertigbaren Einheiten, die parallel hergestellt und anschliessend in einfacher Weise zusammensetzbar sind; erwünscht ist demzufolge ein modularer Aufbau.Finally, the projectile should be able to be produced efficiently, if possible from individually producible units that are manufactured in parallel and then in simple Can be put together; A modular one is therefore desirable Construction.
Bisher sind keine Projektile der eingangs genannten Art bekannt, die allen diesen Anforderungen genügen.So far, no projectiles of the type mentioned at the outset are known to all of them Requirements met.
Die Aufgabe der Erfindung wird somit darin gesehen,
- ein Projektil der eingangs genannten Art so zu verbessern, dass die Nachteile der bekannten Projektile entfallen, und
- ein Verfahren zur Herstellung dieses Projektils vorzuschlagen.
- to improve a projectile of the type mentioned at the outset so that the disadvantages of the known projectiles are eliminated, and
- to propose a method for producing this projectile.
Die Lösung dieser Aufgabe erfolgt erfindungsgemäss
- für das Projektil durch die Merkmale des kennzeichnenden Teils des Anspruchs 1, und
- für das Verfahren durch die Merkmale des kennzeichnenden Teils des
Anspruchs 15 bzw. 18.
- for the projectile by the features of the characterizing part of claim 1, and
- for the method by the features of the characterizing part of
15 and 18 respectively .claims
Vorteilhafte Weiterbildungen des erfindungsgemässen Projektils sind durch die
Ansprüche sind durch die Ansprüche 2 bis 14 definiert, und vorteilhafte Weiterbildungen
des erfindungsgemässen Verfahrens sind durch die Ansprüche 16 und
17 definiert.Advantageous developments of the projectile according to the invention are defined by the claims are defined by claims 2 to 14 , and advantageous developments of the method according to the invention are defined by
Das neue Projektil weist erfindungsgemäss einen Mantel auf, der mindestens im Heckbereich des Projektils aus einem Kunststoff hergestellt ist. Dadurch ist die nicht-wirksame Masse des Projektils geringer als die eines Projektils mit einem metallischen Mantel, und Oberflächenbehandlungen, wie sie bei herkömmlichen metallischen Mänteln erforderlich sind, entfallen.According to the invention, the new projectile has a jacket which is at least in the The rear area of the projectile is made of a plastic. This is the non-effective mass of the projectile less than that of a projectile with one metallic cladding, and surface treatments, as in conventional metallic coats are not required.
Die Formgebung des Kunststoffes kann durch ein spanabhebendes oder spanloses Verfahren erfolgen.The shape of the plastic can be machined or non-cutting Procedure.
Vorzugsweise erfolgt die Formgebung des Kunststoffes für den Mantel durch einen spanlosen Vorgang wie Pressen bzw. Spritzen; solche Vorgänge sind insbesondere bei hohen Stückzahlen, wie sie bei der Fertigung von Projektilen üblich sind, rationell, da dann die Kosten für die Form praktisch nicht ins Gewicht fallen.The plastic for the jacket is preferably shaped by a non-cutting process such as pressing or spraying; such operations are particular for large quantities, as is common in the manufacture of projectiles are rational, since then the cost of the shape is practically insignificant.
Besonders vorteilhaft ist es hierbei, gleichzeitig mit der spanlosen Formung des Mantels die gegenseitige Verbindung des Mantels mit dem aus Festigkeitsgründen im allgemeinen metallischen Projektilboden durchzuführen, wobei der Projektilboden als Einlegeteil in die zur Herstellung des Kunststoffteiles benutzte Spritzform eingebracht und mit dem Kunststoff umspritzt wird. It is particularly advantageous here, at the same time as the chipless shaping of the Jacket the mutual connection of the jacket with the for strength reasons to perform in general metallic projectile floor, the projectile floor used as an insert in the for the manufacture of the plastic part Injection mold introduced and the plastic is encapsulated.
Durch eine optimale Gestaltung des Mantels kann anstelle eines separaten Führungsbandes im Heckbereich des Mantels eine Führungsbandpartie bzw. ein integrales angeformtes Führungsband erzeugt werden.By optimally designing the jacket, instead of a separate guide belt in the rear area of the jacket a guide belt section or an integral one molded guide band are generated.
Zum Empfang externer Signale ist eine Empfangsspule angeordnet. Da diese vor Druckeinwirkungen geschützt werden muss, wird sie vorteilhaft nicht am Umfang des Projektils sondern in Inneren des Projektils angeordnet. Dies bedingt, dass der Kunststoff, aus dem der Mantel hergestellt ist, mindestens im Bereich der Empfangsspule keine abschirmende Wirkung gegen elektromagnetische Wellen bzw. Signale ausübt. Durch die Anordnung der Empfangsspule im Inneren statt am Äusseren des Mantels wird es überflüssig, eine aufwändige Schutzumwicklung, wie sie für eine in herkömmlicher Weise am Äusseren des Mantels angeordnete Empfangsspule notwendig ist, vorzusehen. Man vermeidet - sogar besser als mit der Schutzumwicklung - dass die Leiter, welche die Empfangsspule bilden, sich deformieren; damit werden Störungen der zu empfangenden Signale infolge von Deformationen der Leiter vermieden und das Risiko von Kurzschlüssen vermindert. Im weiteren wird das Risiko des Eindringens von Feuchtigkeit praktisch ausgeschaltet. Wesentlich ist ferner, dass wegen des geringeren Abstandes der Empfangsspule von der Projektillängsachse die Umfangsbeschleunigung und damit die auf die Empfangsspule wirkenden Kräfte verringert werden.A reception coil is arranged for receiving external signals. Because this before Pressure must be protected, it is advantageous not to the extent of the projectile but arranged inside the projectile. This means that the plastic from which the jacket is made, at least in the area of Receiver coil has no shielding effect against electromagnetic waves or signals. By arranging the receiving coil inside instead on the outside of the jacket it becomes superfluous, an elaborate protective wrapping, as for a conventionally arranged on the outside of the jacket Receiving coil is necessary to provide. You avoid - even better than with the protective wrap - that the conductors that make up the receiving coil deform; this will interfere with the signals to be received avoided due to deformation of the conductor and the risk of short circuits reduced. It further increases the risk of moisture ingress practically turned off. It is also essential that because of the smaller distance the receiving coil from the project longitudinal axis the circumferential acceleration and thus the forces acting on the receiving coil are reduced.
Es hat sich als günstig erwiesen, die Wicklung der Empfangsspule auf einen separaten Spulenkörper aufzubringen. Die Empfangsspule kann dadurch für sich als Einheit hergestellt und anschliessend mit der Energiequelle und dem Logikmodul montiert werden.It has proven beneficial to wind the receiving coil on a separate one Apply bobbin. The receiving coil can thereby as a Unit manufactured and then with the energy source and the logic module to be assembled.
Die benötigte Energie kann extern erzeugt und dem Projektil übermittelt werden: Vorteilhaft, da vom Waffensystem unabhängig, ist es aber, eine interne Energiequelle, beispielsweise mit einem Stossgenerator, vorzusehen.The energy required can be generated externally and transmitted to the projectile: It is advantageous because it is independent of the weapon system, but it is an internal energy source, for example with a shock generator.
Um die Erstellung der Leiterverbindung zwischen Energiequelle, Logikmodul und Empfangsspule in einfacher Weise herzustellen, ist es günstig, die Empfangsspule benachbart zur Energiequelle und zum Logikmodul anzuordnen. To create the conductor connection between the energy source, logic module and To produce the receiving coil in a simple manner, it is favorable to use the receiving coil to be arranged adjacent to the energy source and to the logic module.
Eine solche Gestaltung des neuen Projektils, gemäss welcher die Energiequelle und das Logikmodul angrenzend an die Empfangsspule angeordnet sind, erlaubt es, die Leiterverbindung zwischen Empfangsspule, Energiequelle und Logikmodul in einfacher Weise zu erstellen; nicht-automatisierbare und daher kostenintensive Arbeitsschritte wie das Einbringen der Leiterverbindung in eine enge Durchführung, wie sie bei aussenliegenden Empfangsspulen notwendig sind, entfallen.Such a design of the new projectile, according to which the energy source and the logic module are arranged adjacent to the receiving coil es, the conductor connection between the receiving coil, energy source and logic module easy to create; non-automatable and therefore expensive Steps such as placing the conductor connection in a narrow implementation, as they are necessary with external receiving coils, are not necessary.
Ein besonders vorteilhaftes Projektil nach der Erfindung ist so ausgebildet, dass seine Wirkmasse, insbesondere Sprengstoff und ggfs. Wirkkörper, im vorderen Bereich des Projektils angeordnet sind; dadurch erzielt man eine gute Wirkung, wie im Folgenden dargelegt wird: Nach der Detonation addieren sich die Geschwindigkeitsvektoren der entstehenden Wirkkörper zur Geschwindigkeit des Projektils, und die Summe der Geschwindigkeiten ist im Mittel aller entstehenden Teile grösser bei Projektilen mit vorne angeordneter Wirkmasse; ausserdem kann, beispielsweise im Häuserkampf, durch das Detonieren der Projektile vor dem Ziel eine Vergrösserung der Trefferfläche erreicht werden, die im Vergleich mit herkömmlicher Munition oder ABM mit Kopfzünder beträchtlich ist.A particularly advantageous projectile according to the invention is designed such that its active mass, in particular explosives and possibly active bodies, in the front Area of the projectile are arranged; so you get a good effect, as explained below: After the detonation, the velocity vectors add up the resulting active body to the speed of Projectile, and the sum of the speeds is the average of all arising Parts larger in projectiles with front active mass; Furthermore can, for example, in house fighting, by detonating the projectiles the goal of enlarging the target area can be achieved in comparison with conventional ammunition or ABM with a detonator is considerable.
Bei der Herstellung des neuen Projektils werden mehrere Komponenten separat hergestellt und erst anschliessend zusammengefügt. Dies hat drei wesentliche Vorteile: Erstens ist die Lagerhaltung und Herstellung flexibler, zweitens sind bei der Herstellung insgesamt kürzere Durchlaufzeiten möglich, da parallel an den einzelnen Komponenten gearbeitet werden kann; drittens werden keine heiklen Komponenten durch nachfolgende Herstellungsoperationen bereits vor Gebrauch vorbelastet oder sogar beschädigt.When manufacturing the new projectile, several components are separated manufactured and then assembled. This has three essentials Advantages: Firstly, warehousing and manufacturing are more flexible, secondly, at shorter throughput times possible, since parallel to the individual components can be worked; third, no sensitive Components through subsequent manufacturing operations before use preloaded or even damaged.
Im folgenden werden Einzelheiten und Vorteile der Erfindung anhand eines Ausführungsbeispiels und mit Bezug auf die Zeichnung ausführlich beschrieben. Es zeigen:
- Fig. 1
- ein erstes Ausführungsbeispiel des Projektils nach der Erfindung, in Einem die Projektilängsachse enthaltenden Schnitt;
- Fig. 2
- ein zweites Ausführungsbeispiel des Projektils nach der Erfindung, in gleicher Darstellung wie Fig. 1; und
- Fig. 3
- ein drittes Ausführungsbeispiel eines Projektils nach der Erfindung, in gleicher Darstellung wie die Fig.1 und 2.
- Fig. 1
- a first embodiment of the projectile according to the invention, in a section containing the longitudinal axis of the projectile;
- Fig. 2
- a second embodiment of the projectile according to the invention, in the same representation as Fig. 1; and
- Fig. 3
- a third embodiment of a projectile according to the invention, in the same representation as the Fig.1 and 2.
Das in Fig. 1 dargestellte Projektil 10.1 mit der Profjektilängsachse A weist einen
Projektilboden 12 aus einem geeigneten Metall und einen Mantel 14 auf, der
mindestens im Heckbereich, aber vorzugsweise gesamthaft aus einem geeigneten
Kunststoff besteht. Der Mantel 14 ist durch ein Press- oder Spritzgiessverfahren
hergestellt, könnte alternativ aber auch durch spanabhebende Bearbeitung
geformt werden. Gleichzeitig mit der Herstellung des Mantels 14 kann seine
Verbindung mit dem Projektilboden 12 erfolgen; um eine sichere Verbindung
zwischen Projektilboden und Mantel 14 zu erhalten, weist der Projektilboden 12
an der Aussenfläche seines nach vorne ragenden im Wesentlichen hohlzylindrischen
Bodenbereiches 12A Rillen 12B auf. Die Rillen 12B sind mit dem Material
des Mantels 14 umspritzt, so dass der nach vorne ragende Bodenbereich 12A
mit einem nach hinten ragenden Mantelbereich 14A verbunden ist.The projectile 10.1 shown in FIG. 1 with the longitudinal axis A of the projectile has a
Es ist auch möglich, den Projektilboden 12 und den Mantel 14 durch eine andere
geeignete Verbindung wie zum Beispiel eine Verschraubung, Schweissung, Klebung
oder eine Steckverbindung aneinander zu befestigen, wie dies weiter unten
mit Bezug auf Fig. 2 beschrieben wird.It is also possible to fasten the
Der zur Herstellung des Mantels 14 verwendete Kunststoff kann zwar Füllstoffe
enthalten, muss aber mindestens im Bereich der Empfangsspule aus einem Material
bestehen, das keine Abschirmung gegen elektromagnetische Wellen bzw.
Signale bildet. Anstelle eines Kunststoffes kommen auch andere Materialien in
Frage, die keine Abschirmwirkung gegen elektromagnetische Wellen bzw. Signale
ausüben, beispielsweise Keramik oder Glas. The plastic used to produce the
An der Aussenkontur des Mantels 14 ist ein integrales Führungsband 15 angeformt;
dadurch entfallen die Herstellung und die Montage eines separaten, beispielsweise
metallischen, Führungsbandes.An
Zentrisch im Bereich der Projektillängsachse A ist als Bestandteil der programmierbaren
Einrichtung eine Empfangsspule 16 angeordnet, deren Wicklung 18
auf einem Spulenkörper 20, vorzugsweise aus einem Kunststoff, angebracht ist. A receiving
Die Empfangsspule 16 ist leitend mit einer Energiequelle beziehungsweise Energiespeichereinheit
22 und einem Logikmodul 23 verbunden. Zur Herstellung der
leitenden Verbindung zwischen Empfangsspule 16, Energiequelle bzw. Energiespeichereinheit
22 und Logikmodul 23 muss nicht wie bei herkömmlichen Projektilen
ein Leiter durch eine enge Bohrung hindurch geführt werden, sondern die
Verbindung kann infolge der zentrischen Anordnung sowohl der Empfangsspule
16 wie auch der Energiequelle bzw. Energiespeichereinheit 22 wie auch des Logikmoduls
23 in einfacher Weise erstellt werden. Beispielsweise kann die leitende
Verbindung einschliesslich der eigentlichen Kontaktierung durch eine Lötung erfolgen.
In einer anderen Variante kann ein eingelegtes Zwischenteil verwendet
werden, wobei die Kontaktierung mittels eines leitenden Klebstoffes hergestellt
wird. Besonders einfach in der Herstellung, aber weniger sicher ist es, die Kontaktierung
lediglich durch eine Pressung herbeizuführen. Aufwändig in der Herstellung
der Einzelteile ist eine Steckverbindung, welche aber grosse Sicherheit
gewährleistet und einfach zu montieren ist.The receiving
Das oben beschriebene Projektil 10.1 gemäss Fig. 1 wird wie folgt hergestellt:
Der Mantel 14 wird durch Spritzen erzeugt; hierbei wird der Projektilboden 12
mit dem Kunststoff des Mantels 12 bzw. des Hecks umspritzt. Die Energiequelle
bzw. Energiespeichereinheit 22, das Logikmodul 23 und die Empfangsspule 16
werden anschliessend von vorne eingebracht.The projectile 10.1 described above according to FIG. 1 is produced as follows: the
Fig. 2 zeigt ein weiteres Projektil 10.2 nach der Erfindung. Das Projektil 10.2
unterscheidet sich vom Projektil 10.1 nur unwesentlich, daher werden im Folgenden
nur die von Fig. 1 abweichenden Einzelheiten beschrieben, und für die
einzelnen konstruktiven Elemente werden in Fig. 2 und weiter unten auch in Fig. 3 die gleichen Bezugszeichen verwendet wie in Fig. 1. Im Unterschied zum Projektil
10.1 ist beim Projektil 10.2 der Innendurchmesser des nach hinten ragenden
Mantelbereiches 14A grösser als der Aussendurchmesser der Spule 16. 2 shows a further projectile 10.2 according to the invention. The projectile 10.2 differs only slightly from the projectile 10.1, therefore only the details deviating from FIG. 1 are described below, and the same reference numerals are used for the individual structural elements in FIG. 2 and further below in FIG. 3 as in FIG Fig. 1. In contrast to the projectile 10.1 in the projectile 10.2, the inner diameter of the
Bei der Herstellung des Projektils 10.2 wird wie folgt vorgegangen: Der Mantel
14 bzw. das Heck wird durch spanlose oder durch spanabhebende Formgebung
hergestellt, wobei der nach hinten ragende Mantelbereich 14A mit einem Innengewinde
14B versehen wird. Der nach vorne ragende Bodenbereich 12A des
Projektilbodens wird nicht mit den Rippen 12A sondern mit einem zum Innengewinde
14B komplementären Aussengewinde 12B versehen. Die Empfangsspule
16, die Energiequelle bzw. Energiespeichereinheit 22 und das Logikmodul 23
werden einzeln hergestellt, am Projektilboden 12 befestigt und kontaktiert.
Schliesslich wird die hierbei entstandene Komponente wird von hinten in den
Mantel 14 eingebracht, wobei die Verbindung von Projektilboden 12 und Mantel
14 durch Einschrauben des Aussengewindes 12B in das Innengewinde 14B zu
Stande kommt.The projectile 10.2 is produced as follows: The
Ein drittes Projektil 10.3 ist in Fig. 3 dargestellt. Beim Projektil 10.3 wird für
den Projektilboden 12 dasselbe Material verwendet wie für den Mantel 14; hierbei
werden der Projektilboden 12 und der Mantel 14 integral in einem Pressoder
Spritzgiessvorgang als Press- bzw. Spritzteil 13 erzeugt. Die Herstellung
der Empfangsspule 16, der Energiequelle bzw. Energiespeichereinheit 22 und
des Logikmoduls 23 erfolgt separat, anschliessend werden diese drei Bestandteile
des Projektils 10.3 in gleicher Weise wie mit Bezug auf das Projektil 10.1
der Fig. 1 beschrieben, zu einer Komponente zusammengefügt und diese Komponente
von vorne im Press- bzw. Spritzteil 13 montiert.A third projectile 10.3 is shown in FIG. 3 . The same material is used for the
Bei allen drei Projektilen 10.1, 10.2, 10.3 sind die Empfangsspule 16, die Energiequelle
bzw. Energiespeichereinheit 22 und das Logikmodul 23 im hinteren
Projektilbereich angeordnet, so dass der vordere Projektilbereich zur Aufnahme
einer nicht dargestellten Wirkmasse frei ist.In all three projectiles 10.1, 10.2, 10.3 , the receiving
Claims (18)
dadurch gekennzeichnet, dass der Mantel (14) vollständig aus einem Kunststoff hergestellt ist.Projectile (10.1, 10.2, 10.3) according to claim 1,
characterized in that the jacket (14) is made entirely of a plastic.
dadurch gekennzeichnet, dass der Mantel (14) durch spanabhebende Formgebung erzeugt ist.Projectile (10.2) according to one of Claims 1 to 2,
characterized in that the jacket (14) is produced by machining.
dadurch gekennzeichnet, dass der Mantel (14) durch spanlose Formgebung erzeugt ist. Projectile (10.1) according to one of claims 1 to 2,
characterized in that the jacket (14) is produced by non-cutting shaping.
dadurch gekennzeichnet, dass die Verbindung des Projektilbodens (12) mit dem Mantel (14) durch das spanlos verformte Material des Mantels (14) erzeugt ist.Projectile (10.1) according to claim 4,
characterized in that the connection of the projectile bottom (12) to the jacket (14) is produced by the material of the jacket (14) deformed without cutting.
dadurch gekennzeichnet, dass die Verbindung des Projektilbodens (12) mit dem Mantel (14) eine Schraub-, Steck- Kleb- , Schweiss- oder Lötverbindung ist.Projectile (10.2) according to one of claims 1 to 5,
characterized in that the connection of the projectile base (12) to the jacket (14) is a screw, plug-in, adhesive, welded or soldered connection.
dadurch gekennzeichnet, dass der Projektilboden (12) aus demselben Kunststoff wie der Mantel (14) hergestellt ist.Projectile (10.3) according to claim 4,
characterized in that the projectile base (12) is made of the same plastic as the jacket (14) .
dadurch gekennzeichnet, dass der Projektilboden (12) und der Mantel (14) als integrales Pressbzw. Spritzteil (13) hergestellt sind.Projectile (10.3) according to claim 7,
characterized in that the projectile bottom (12) and the jacket (14) as an integral press or. Injection molded part (13) are made.
dadurch gekennzeichnet, dass am Mantel (14) ein integrales Führungsband (15) angeformt ist.Projectile (10.1, 10.2, 10.3) according to one of claims 1 to 8,
characterized in that an integral guide band (15) is formed on the jacket (14) .
dadurch gekennzeichnet,
characterized,
dadurch gekennzeichnet, dass die Empfangsspule (16) eine Wicklung (18) aufweist, die auf einem Spulenkörper (20) angebracht ist.Projectile (10.1, 10.2, 10.3) according to one of claims 1 to 10,
characterized in that the receiving coil (16) has a winding (18 ) which is attached to a coil former (20) .
dadurch gekennzeichnet, dass die Energiequelle (22) und das Logikmodul (23) im Inneren des Mantels (14) angeordnet und der Empfangsspule (16) benachbart sind.Projectile (10.1, 10.2, 10.3) according to one of claims 1 to 11,
characterized in that the energy source (22) and the logic module (23 ) are arranged inside the jacket (14) and are adjacent to the receiving coil (16) .
dadurch gekennzeichnet, dass die Kontaktierung der Wicklung (18) der Empfangsspule (16) mit der Energiequelle (22) durch Lötung, Klebung mit einem leitenden Klebstoff, Pressung oder mittels einer Steckverbindung hergestellt ist.Projectile (10.1, 10.2, 10.3) according to one of claims 1 to 12,
characterized in that the contacting of the winding (18) of the receiving coil (16) with the energy source (22) is produced by soldering, gluing with a conductive adhesive, pressing or by means of a plug connection.
dadurch gekennzeichnet, dass die Empfangsspule (16), die Energiequelle und das Logikmodul (23) im hinteren Bereich des Projektils (10) angeordnet sind.Projectile (10.1, 10.2, 10.3) according to one of claims 1 to 13,
characterized in that the receiving coil (16), the energy source and the logic module (23) are arranged in the rear region of the projectile (10) .
dadurch gekennzeichnet, dass der Mantel (14) durch spanlose Formgebung hergestellt und hierbei mit dem Projektilboden (12) verbunden wird.A method according to claim 15,
characterized in that the jacket (14) is produced by non-cutting shaping and is thereby connected to the projectile base (12) .
dadurch gekennzeichnet, dass der Mantel (14) und der Projektilboden (12) aus dem gleichen Material als integrales Press- bzw. Spritzteil (13) hergestellt werden.A method according to claim 16,
characterized in that the jacket (14) and the projectile base (12) are produced from the same material as an integral pressed or injection-molded part (13) .
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH4722001 | 2001-03-14 | ||
CH4722001 | 2001-03-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1241435A1 true EP1241435A1 (en) | 2002-09-18 |
EP1241435B1 EP1241435B1 (en) | 2007-01-17 |
Family
ID=4516032
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02002216A Expired - Lifetime EP1241435B1 (en) | 2001-03-14 | 2002-01-30 | Projectile and manufacturing method therefor |
Country Status (10)
Country | Link |
---|---|
US (2) | US6874402B2 (en) |
EP (1) | EP1241435B1 (en) |
JP (1) | JP4028741B2 (en) |
AT (1) | ATE352023T1 (en) |
CA (1) | CA2369708C (en) |
DE (1) | DE50209260D1 (en) |
ES (1) | ES2280440T3 (en) |
NO (1) | NO327204B1 (en) |
SG (1) | SG118113A1 (en) |
ZA (1) | ZA200200942B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010053607A3 (en) * | 2008-09-08 | 2010-07-01 | Raytheon Company | Smart fuze guidance system with replaceable fuze module |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7059234B2 (en) * | 2003-05-29 | 2006-06-13 | Natec, Inc. | Ammunition articles and method of making ammunition articles |
US7640359B1 (en) * | 2003-09-19 | 2009-12-29 | At&T Intellectual Property, I, L.P. | Method, system and computer program product for facilitating the design and assignment of ethernet VLANs |
US7624187B1 (en) | 2003-09-19 | 2009-11-24 | At&T Intellectual Property, I, L.P. | Method, system and computer program product for providing Ethernet VLAN capacity requirement estimation |
US20160231095A1 (en) * | 2014-12-04 | 2016-08-11 | John M. Storm | Limited range lethal ammunition |
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DE29817728U1 (en) * | 1998-10-05 | 1999-02-04 | Honeywell Ag | Missile detonator structure |
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- 2002-01-30 DE DE50209260T patent/DE50209260D1/en not_active Expired - Lifetime
- 2002-01-30 ES ES02002216T patent/ES2280440T3/en not_active Expired - Lifetime
- 2002-01-30 EP EP02002216A patent/EP1241435B1/en not_active Expired - Lifetime
- 2002-01-30 CA CA002369708A patent/CA2369708C/en not_active Expired - Lifetime
- 2002-01-30 AT AT02002216T patent/ATE352023T1/en not_active IP Right Cessation
- 2002-02-01 NO NO20020520A patent/NO327204B1/en not_active IP Right Cessation
- 2002-02-01 ZA ZA200200942A patent/ZA200200942B/en unknown
- 2002-02-04 SG SG200200663A patent/SG118113A1/en unknown
- 2002-03-06 US US10/093,262 patent/US6874402B2/en not_active Expired - Lifetime
- 2002-03-14 JP JP2002070029A patent/JP4028741B2/en not_active Expired - Lifetime
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US2872865A (en) * | 1955-09-29 | 1959-02-10 | Karsten S Skaar | High strength fiber glass-metal construction and process for its manufacture |
DE3345618A1 (en) * | 1983-12-16 | 1985-06-20 | Diehl GmbH & Co, 8500 Nürnberg | Carrier projectile |
US4750424A (en) * | 1986-03-06 | 1988-06-14 | Honeywell Regelsysteme Gmbh | Running time display for a projectile time fuze |
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Publication number | Priority date | Publication date | Assignee | Title |
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WO2010053607A3 (en) * | 2008-09-08 | 2010-07-01 | Raytheon Company | Smart fuze guidance system with replaceable fuze module |
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Also Published As
Publication number | Publication date |
---|---|
US7197981B2 (en) | 2007-04-03 |
NO20020520D0 (en) | 2002-02-01 |
JP4028741B2 (en) | 2007-12-26 |
CA2369708A1 (en) | 2002-09-14 |
DE50209260D1 (en) | 2007-03-08 |
EP1241435B1 (en) | 2007-01-17 |
US20070017404A1 (en) | 2007-01-25 |
ZA200200942B (en) | 2002-08-14 |
SG118113A1 (en) | 2006-01-27 |
ATE352023T1 (en) | 2007-02-15 |
NO327204B1 (en) | 2009-05-11 |
NO20020520L (en) | 2002-09-16 |
US20020129727A1 (en) | 2002-09-19 |
US6874402B2 (en) | 2005-04-05 |
JP2002318099A (en) | 2002-10-31 |
ES2280440T3 (en) | 2007-09-16 |
CA2369708C (en) | 2006-03-21 |
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