EP0736745B1 - Method and device for carrying out the method of filling projectiles with submunitions - Google Patents

Method and device for carrying out the method of filling projectiles with submunitions Download PDF

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Publication number
EP0736745B1
EP0736745B1 EP95118419A EP95118419A EP0736745B1 EP 0736745 B1 EP0736745 B1 EP 0736745B1 EP 95118419 A EP95118419 A EP 95118419A EP 95118419 A EP95118419 A EP 95118419A EP 0736745 B1 EP0736745 B1 EP 0736745B1
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EP
European Patent Office
Prior art keywords
submunitions
slide
centring
passage
projectile
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.)
Expired - Lifetime
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EP95118419A
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German (de)
French (fr)
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EP0736745A1 (en
Inventor
Peter Ettmüller
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.)
RWM Schweiz AG
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Oerlikon Contraves Pyrotec AG
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Publication of EP0736745A1 publication Critical patent/EP0736745A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/56Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
    • F42B12/58Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65BMACHINES, APPARATUS OR DEVICES FOR, OR METHODS OF, PACKAGING ARTICLES OR MATERIALS; UNPACKING
    • B65B19/00Packaging rod-shaped or tubular articles susceptible to damage by abrasion or pressure, e.g. cigarettes, cigars, macaroni, spaghetti, drinking straws or welding electrodes
    • B65B19/34Packaging other rod-shaped articles, e.g. sausages, macaroni, spaghetti, drinking straws, welding electrodes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F42B33/02Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges

Definitions

  • the subprojectiles should, if possible be evenly distributed on circular surfaces, the even distribution in primarily due to the geometrical arrangement of the subprojectiles inside the floor is determined.
  • a projectile or a bomb with subprojectiles in an even distribution is based on the clues about the method by which the subprojectiles are filled into the projectile and about any devices used to carry out such a method. known.
  • the sub-projectile longitudinal axes are arranged parallel to the longitudinal axis of the projectile, and the projectile contains three layers, which are called clusters, and which are arranged one behind the other.
  • US-A-3,093,072 describes the course of the longitudinal and rotational speeds of the subprojectiles after they have left the projectile and the hit image that can be generated depending on these speeds.
  • FR-A-2 606 135 also describes a projectile with sub-projectiles.
  • the subprojectile axes are parallel to the projectile axis, and the subprojectiles are arranged in several layers one behind the other.
  • the subprojectiles are arranged so that their coats touch.
  • Each subprojectile has three guide vanes at its rear end, the radial dimensions of which essentially correspond to the radius of the subprojectile shells.
  • the mutual arrangement of the sun projectiles is such that - in a section perpendicular to the projectile axis, the guide vanes of six subprojectiles meet in the center of a circle in which there is no projectile jacket.
  • the subprojectiles had no vanes and if a subprojectile were also present in this circle, the subprojectiles would be arranged in the closest possible packing. Clearances between the subprojetiles are filled with a powder-like mass to increase the rigidity of the projectile. There is no description of the method and, if necessary, the device with which the subprojectiles are filled into the projectile.
  • the subprojectiles should, if possible be evenly distributed on circular surfaces, the even distribution in primarily due to the geometrical arrangement of the subprojectiles inside the floor is determined.
  • a method and a device for filling elongated objects, namely sausages, into cans are known from EP-A-0 180 002 . It is provided here that the sausages are arranged in the can so that their length extends parallel to the longitudinal axis of the can. The sausages are combined into layers of six sausages before being pushed into the can. Within each shift, the six sausages occupy the position that they take after being pushed into the can.
  • Each filled can contains only a single layer, and the arrangement of the sausages in layers in the manner described can only be carried out with elongated objects such as sausages and only for exactly six sausages, whereas a storey generally contains a significantly larger number of storeys, their Length can also be so short that it can probably not be combined in layers in the same way as the sausages.
  • the invention has for its object a method and an apparatus of the aforementioned Propose a type that does not have the disadvantages mentioned above.
  • the subprojectiles are combined into layers that are so thick before filling how the length of the subprojectiles are and that in planes transverse to the longitudinal axis of the projectile body run.
  • the subprojectiles occupy a position in the layer that is geometrical Arrangement in a cavity of the projectile body corresponds.
  • the scope of the Layers are formed in the combination in such a way that the subprojectiles after the Inserting a layer into the cavity in compliance with the previously formed geometric arrangement are held against rotation.
  • the circumference of the layer has the shape of a regular one Hexagons, the subprojectiles consisting of cylinders with their axes run parallel to the longitudinal axis of the projectile body.
  • 1 and 2 , 1 denotes a vertically arranged mounting cross-section which is U-shaped in cross section and which is screwed to a cover 2 .
  • the assembly centering 1 and the cover 2 form a reservoir 3, which in cross section has the shape of a slit-like rectangle, the width of which corresponds to the length of cylindrical sub-projectiles ( 20, Fig. 3, 4 ) and the length of which depends on the diameter and the number of Subprojectiles and their geometric arrangement results ( Fig. 3, 4 ).
  • a cover plate 4 is fastened, which has a slot 5 which is approximately congruent with the cross section of the reservoir 3 .
  • a slide 7 is guided horizontally and is connected to a handle 8 for the purpose of actuation.
  • the width of the slide 7 corresponds to the length of the rectangular cross section of the reservoir 3.
  • the slide 7 On its upper side, the slide 7 has a v-shaped notch extending in its longitudinal direction, the inclined surfaces ( 7.1, FIG. 5 ) of which in one preferred embodiment Include angles of 120 ° and correspond to the sides of a regular hexagon.
  • the underside of the slide 7 is roof-shaped, the inclined surfaces ( 7.2 , FIG. 5 ) enclosing an angle of 120 ° and, like the inclined surfaces of the v-shaped notch, corresponding to the sides of a regular hexagon.
  • the mounting centering 1 has a breakthrough 9 which runs coaxially with the slide 7 and is connected on the input side to the reservoir 3 , the outline of which in a first part of the mounting centering 1 corresponds approximately to the outline of the slide 7 described above.
  • an attachment 10 is provided for guiding the sub-projectiles to be filled into a projectile body part ( 41, FIG. 14 ).
  • the projectile body part is centered during filling in an extending coaxially with the shoulder 10 secured to the centering fitting retaining ring 1.
  • Recesses 12 are provided on the sides of the mounting centering 1 and are connected to the opening 9 via openings 13 .
  • the recesses 12 have sliding surfaces 14 which are inclined downward from the horizontal by an angle of, for example, 30 ° and which begin approximately at upper corner points 15 of the vertical sides of the regular hexagon formed by the opening 9 .
  • the assembly centering 1 is screwed to a collecting container 16 and a base plate 17 .
  • the collecting container 16 has two inclined feed surfaces 18 arranged on both sides of the assembly centering 1 in the area of the openings 13 for excess sub-projectiles.
  • cylindrical sub-projectiles 20 with a diameter d are combined to form layers ( 40, FIG. 14 ) in the form of regular hexagons which are assigned to projectile bodies with different diameters.
  • the layers are arranged in planes running transversely to the longitudinal axis ( 43, FIG. 14 ) of a projectile body part ( 41, FIG. 14 ), the axes of the subprojectiles 20 being aligned parallel to the longitudinal axis.
  • U denotes the circumference of the regular hexagons, the diameter D of which results from a whole multiple of the subprojectile diameter d.
  • the distance b between two parallel sides of the regular hexagons results, as already mentioned above, from the diameter d and the number of sub-projectiles 20 and their geometric arrangement.
  • the cylindrical sub-projectiles 20 with the diameter d are combined to form layers in the form of irregular hexagons, which are assigned to projectile bodies with different diameters.
  • both the distance b and the diameter D must be determined from the number and the diameter d of the subprojectiles 20 and their geometric arrangement.
  • the excess sub-projectiles that are ejected during filling are designated 20.1 .
  • Openings 31 are provided in the further assembly centerings 30 , which have the same shape in cross section in a first part of the assembly centerings 30 as the opening 9 of the assembly centering 1 (FIG. 1) and which run concentrically to this.
  • Recesses 32 are provided on the sides of the further assembly centering 30 and are connected to the opening 31 via openings 33 .
  • the recesses 32 have sliding surfaces 34 which are inclined downward from the horizontal by an angle of, for example, 30 ° and which begin approximately at the upper corner points of the vertical sides of a regular hexagon formed by the opening 31 .
  • Ejector lugs 35 are arranged in the opening 31 , which protrude into grooves 37 of a further slide 36 which can be displaced through the openings 9, 31 .
  • the cross section of the further slide 36 corresponds to the cross section of the slide 7 of FIG. 1 , but has a length that extends at least over all assembly centers 1, 30 . 1 and 2, the device described above is connected to a collecting container and a base plate, as well as to a retaining ring 11 for the projectile body part 41, a flange for guiding the slide 36 and with a cover 2 provided.
  • a first step the sub-projectiles 20 are fed to the reservoir 3 by means of a vibratory spiral conveyor, not shown, in which they fall vertically downwards onto a first boundary formed by the top of the slide 7 .
  • the desired geometric arrangement is formed in accordance with the shape of the slide 7 and the cross-sectional length of the reservoir 3 , and the circumference of a layer 40 consisting of subprojectiles 20 , which in a preferred embodiment may be a regular hexagon, is partially shaped.
  • a second step FIGS.
  • the slide 7 is withdrawn so that the subprojectiles 20 fall to a second, lower limit by a certain amount, which corresponds to the diameter D of the circumference of the selected regular rectangle. Since the second boundary is formed by the shape of the lower part of the opening 9 or reservoir 3 , the geometric arrangement and the partially shaped circumference of the layer 40 are retained.
  • a third step FIGS. 13a, 13b
  • the subprojectiles 20 located between the first and second delimitation are pushed in the filling direction with the slide 7 from the reservoir 3 into the opening 9 , the final shaping of the circumference of the layer 40 taking place by the surplus subprojectiles 20.1 ( FIG. 5 ) are discharged through the openings 13 and roll down on the sliding surfaces 14 .
  • a following, preformed layer 40 sub-projectiles is held on the top of the slide 7 .
  • a fourth step (Fig. 14) are introduced, the final formed layers into a cavity 42 of the projectile body portion 41, the preceding layers are shifted 40 from the respectively following the last layer 40 upon repeated reciprocating movement of the slide 7, until the cavity is filled.
  • eight layers 40 each consisting of nineteen sub-projectiles 20 , can be placed in the projectile body part 41 .
  • the second embodiment of the device described with reference to FIGS. 7 to 10 works in the same way as described above both in the assembly centering 1 and in the further assembly centers 30 during the first and second step, but the retraction movement of the further slide 36 extends over all assembly centers 1 , 30 extends.
  • the final shaping of the circumference of the layer in the assembly centering 1 also takes place as described above.
  • the fourth step is the same as described above, but the number of lifting movements is reduced according to the number of reservoirs 3 . An optimal result can be achieved if the number of reservoirs 3 is equal to the number of layers required, since then only a single stroke of the slide is required to fill up a projectile body.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Making Paper Articles (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Buffer Packaging (AREA)
  • Containers Having Bodies Formed In One Piece (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)

Description

Mit Geschossen die Subprojektile enthalten kann wie beispielsweise aus einer Druckschrift OC 2052 d 94 der Firma Oerlikon Contraves, Zürich, bekannt, ein angreifendes Ziel durch mehrfache Treffer zerstört werden, wenn nach Ausstossen der Subprojektile das Erwartungsgebiet des Zieles von einer durch die Subprojektile gebildeten Wolke belegt ist. Das Ausstossen der Subprojektile erfolgt hierbei durch eine im Geschoss untergebrachte Sprengladung, bei deren Zündung der die Subprojektile tragende Teil des Geschosses abgetrennt und an Sollbruchstellen aufgerissen wird. An solche Geschosse werden hohe Anforderungen gestellt, so ist es z.B. wichtig, dass die Subprojektile fest und verdrehungssicher im Geschoss gehalten werden. Auf diese Weise wird die Rotation auf die Subprojektile übertragen, so dass das Geschoss eine stabile Flugbahn beschreibt. Mit der vollständigen Übertragung der Rotation soll ausserdem eine Drallstabilisierung der Subprojektile nach deren Ausstossen erreicht werden. With projectiles that can contain subprojectiles, such as from an OC publication 2052 d 94 of the company Oerlikon Contraves, Zurich, known, an attacking target by multiple Hits will be destroyed if the expected area after the subprojectiles have been ejected of the target is occupied by a cloud formed by the subprojectiles. The ejection of the Subprojectiles are carried out by an explosive charge housed in the storey Ignition the part of the projectile carrying the subprojectile separated and at predetermined breaking points is torn open. High demands are placed on such storeys, e.g. it is important that the subprojectiles are held firmly and securely on the floor. On in this way the rotation is transferred to the subprojectiles so that the projectile is one describes stable trajectory. With the complete transfer of the rotation should also a swirl stabilization of the subprojectiles can be achieved after their ejection.

Um weiterhin eine bessere Treffwahrscheinlichkeit zu erzielen, sollten die Subprojektile möglichst gleichmässig auf Kreisflächen liegend verteilt sein, wobei die gleichmässige Verteilung in erster Linie durch die geometrische Anordnung der Subprojektile im Innern des Geschosses bestimmt wird. In order to continue to achieve a better chance of being hit, the subprojectiles should, if possible be evenly distributed on circular surfaces, the even distribution in primarily due to the geometrical arrangement of the subprojectiles inside the floor is determined.

Ein Projektil bzw. eine Bombe mit Subprojektilen in gleichmässiger Verteilung ist aus der Anhaltspunkte über das Verfahren, nach welchem die Subprojektile in das Projektil eingefüllt werden, und über eventuell benutzte Vorrichtungen zur Durchführung eines solchen Verfahrens. bekannt. Die Subprojektil-Längsachsen sind parallel zur Längsachse des Projektils angeordnet, und das Projektil enthält drei Schichten, die als Cluster bezeichnet werden, und die hintereinander angeordnet sind. Die US-A-3,093,072 beschreibt den Verlauf der Längs- und Rotationsgeschindigkeiten der Subprojektile nachdem sie das Projektil verlassen haben, und das Trefferbild, das in Abhängigkeit von diesen Geschwindigkeiten erzeugt werden kann.A projectile or a bomb with subprojectiles in an even distribution is based on the clues about the method by which the subprojectiles are filled into the projectile and about any devices used to carry out such a method. known. The sub-projectile longitudinal axes are arranged parallel to the longitudinal axis of the projectile, and the projectile contains three layers, which are called clusters, and which are arranged one behind the other. US-A-3,093,072 describes the course of the longitudinal and rotational speeds of the subprojectiles after they have left the projectile and the hit image that can be generated depending on these speeds.

Auch die FR-A-2 606 135 beschreibt ein Projektil mit Subprojektilen. Die Subprojektilachsen sind parallel zur Projektilachse, und die Subprojektile sind in mehreren Schichten hintereinander angeordnet. Die Subprojektile sind so angeordnet, dass sich ihre Mäntel berühren. Jedes Subprojektil weist an seinem hinteren Ende drei Leitflügel auf, deren radiale Abmessung im wesentlichen dem Radius der Subprojektilmäntel entspricht. Die gegenseitige Anordnung der Sunbprojektile ist so, dass sich - in einem Schnitt senkrecht zur Projektilachsejeweils die Leitflügel von sechs Subprojektilen im Zentrum eines Kreises treffen, in welchem kein Projektilmantel vorhanden ist. Hätten die Subprojektile keine Leitflügel und wäre in diesem Kreis auch ein Subprojektil vorhanden, so wären die Subprojektile in dichtesmöglicher Packung angeordnet. Freiräume zwischen den Subprojetilen sind mit einer pulverartigen Masse gefüllt, um die Rigidität des Projektils zu erhöhen. Es wird nicht beschrieben, nach welchem Verfahren und ggfs. mit Hilfe welcher Vorrichtung die Subprojektile in das Projektil eingefüllt werden. FR-A-2 606 135 also describes a projectile with sub-projectiles. The subprojectile axes are parallel to the projectile axis, and the subprojectiles are arranged in several layers one behind the other. The subprojectiles are arranged so that their coats touch. Each subprojectile has three guide vanes at its rear end, the radial dimensions of which essentially correspond to the radius of the subprojectile shells. The mutual arrangement of the sun projectiles is such that - in a section perpendicular to the projectile axis, the guide vanes of six subprojectiles meet in the center of a circle in which there is no projectile jacket. If the subprojectiles had no vanes and if a subprojectile were also present in this circle, the subprojectiles would be arranged in the closest possible packing. Clearances between the subprojetiles are filled with a powder-like mass to increase the rigidity of the projectile. There is no description of the method and, if necessary, the device with which the subprojectiles are filled into the projectile.

Um weiterhin eine bessere Treffwahrscheinlichkeit zu erzielen, sollten die Subprojektile möglichst gleichmässig auf Kreisflächen liegend verteilt sein, wobei die gleichmässige Verteilung in erster Linie durch die geometrische Anordnung der Subprojektile im Innern des Geschosses bestimmt wird.In order to continue to achieve a better chance of being hit, the subprojectiles should, if possible be evenly distributed on circular surfaces, the even distribution in primarily due to the geometrical arrangement of the subprojectiles inside the floor is determined.

Jedes Geschoss der vorstehend beschriebenen Art enthält eine relativ grosse Anzahl Subprojektile, die zwecks Erreichen gleichbleibender Eigenschaften sorgfältig in der erforderlichen geometrischen Anordnung eingefüllt werden müssen. Mit den herkömmlichen Auffüllverfahren kann das nur unter grossem Zeitaufwand bewerkstelligt werden. Each projectile of the type described above contains a relatively large number of sub-projectiles, carefully in order to achieve consistent properties geometric arrangement must be filled. With the conventional filling process this can only be done with a great deal of time.

Anhaltspunkte über das Verfahren, nach welchem die Subprojektile in das Projektil eingefüllt werden, und über eventuell benutzte Vorrichtungen zur Durchführung eines solchen Verfahrens sind weder der US-A-3,093,072 noch der FR-A-2 606 135 zu entnehmen. Neither US-A-3,093,072 nor FR-A-2 606 135 give any clues about the method by which the subprojectiles are filled into the projectile and about any devices used to carry out such a method.

Zwar sind aus der EP-A-0 180 002 ein Verfahren und eine Vorrichtung zum Einfüllen von länglichen Gegenständen, nämlich Würstchen, in Dosen bekannt. Hierbei ist vorgesehen, dass die Würstchen in der Dose so angeordnet sind, dass sich ihre Länge parallel zur Längsachse der Dose erstreckt. Die Würstchen werden vor dem Einschieben in die Dose zu Schichten von sechs Würstchen zusammengefasst. Innerhalb jeder Schicht nehmen die sechs Würstchen diejenige Lage ein, die sie nach dem Einschieben in der Dose einnehmen. Jede gefüllte Dose enthält nur eine einzige Schicht, und die Anordnung der Würstchen in Schichten kann in der beschriebenen Weise nur mit länglichen Gegenständen wie Würstchen und nur für genau sechs Würstchen durchgeführt werden, während ein Geschoss im allgemeinen eine bedeutend grössere Anzahl von Teilgeschossen enthält, deren Länge ausserdem so kurz sein kann, dass sie sich vermutlich nicht in gleicher Weise zu Schichten zusammenfassen lassen wie die Würstchen. A method and a device for filling elongated objects, namely sausages, into cans are known from EP-A-0 180 002 . It is provided here that the sausages are arranged in the can so that their length extends parallel to the longitudinal axis of the can. The sausages are combined into layers of six sausages before being pushed into the can. Within each shift, the six sausages occupy the position that they take after being pushed into the can. Each filled can contains only a single layer, and the arrangement of the sausages in layers in the manner described can only be carried out with elongated objects such as sausages and only for exactly six sausages, whereas a storey generally contains a significantly larger number of storeys, their Length can also be so short that it can probably not be combined in layers in the same way as the sausages.

Der Erfindung liegt die Aufgabe zugrunde ein Verfahren und eine Vorrichtung der eingangs genannten Art vorzuschlagen, die vorstehend erwähnte Nachteile nicht aufweist.The invention has for its object a method and an apparatus of the aforementioned Propose a type that does not have the disadvantages mentioned above.

Diese Aufgabe wird durch die in den Patentansprüchen 1 und 7 angegebene Erfindung gelöst. Hierbei werden die Subprojektile vor dem Auffüllen zu Schichten zusammengefasst, die so dick wie die Länge der Subprojektile sind und die in Ebenen quer zur Längsachse des Geschosskörpers verlaufen. Die Subprojektile nehmen in der Schicht eine Lage ein, die ihrer geometrischen Anordnung in einem Hohlraum des Geschosskörpers entspricht. Der Umfang der Schichten wird bei der Zusammenfassung derart geformt, dass die Subprojektile nach dem Einschieben einer Schicht in den Hohlraum in diesem unter Einhaltung der vorher gebildeten geometrischen Anordnung verdrehsicher gehalten werden.This object is achieved by the invention specified in claims 1 and 7. Here, the subprojectiles are combined into layers that are so thick before filling how the length of the subprojectiles are and that in planes transverse to the longitudinal axis of the projectile body run. The subprojectiles occupy a position in the layer that is geometrical Arrangement in a cavity of the projectile body corresponds. The scope of the Layers are formed in the combination in such a way that the subprojectiles after the Inserting a layer into the cavity in compliance with the previously formed geometric arrangement are held against rotation.

Gemäss einer bevorzugten Ausführung weist der Umfang der Schicht die Form eines regelmässigen Sechseckes auf, wobei die aus Zylindern bestehenden Subprojektile mit ihren Achsen parallel zur Längsachse des Geschosskörpers verlaufen.According to a preferred embodiment, the circumference of the layer has the shape of a regular one Hexagons, the subprojectiles consisting of cylinders with their axes run parallel to the longitudinal axis of the projectile body.

Nach einer Weiterbildung der Erfindung werden mehrere Schichten gleichzeitig erzeugt und hintereinander liegend gleichzeitig in den Hohlraum des Geschosskörpers eingeschoben.According to a further development of the invention, several layers are generated and simultaneously inserted one behind the other into the cavity of the projectile body.

Die mit der Erfindung erzielten Vorteile sind darin zu sehen, dass die Auffüllzeit wesentlich verkürzt wird und Kosten gespart werden können. Ausserdem werden Fehler, die z.B. durch Umlagerung von Subprojektilen entstehen könnten weitgehend vermieden, so dass der Ausschuss auf ein Minimum reduziert werden kann.The advantages achieved with the invention can be seen in the fact that the filling time is significantly reduced and costs can be saved. In addition, errors that e.g. by rearrangement of sub-projectiles could be largely avoided, so the committee can be reduced to a minimum.

Mit der vorgeschlagenen Weiterbildung der Erfindung, mehrere Reservoire für die gleichzeitige Bildung mehrerer Schichten von Subprojektilen zu verwenden, kann die Auffüllzeit nochmals reduziert werden. Durch die besondere Ausgestaltung der erfindungsgemässen Vorrichtung, die Subprojektile zu Schichten in Form eines regelmässigen Sechseckes zusammenzufassen und in dieser Form im Geschoss zu plazieren, wird nach deren Ausstossen eine optimale gleichmässige, auf Kreisflächen liegende Verteilung der Subprojektile und damit eine bessere Treffwahrscheinlichkeit erzielt.With the proposed development of the invention, several reservoirs for the simultaneous Using multiple sub-projectile layers can add refill time be reduced. Due to the special design of the device according to the invention, Combine the subprojectiles into layers in the form of a regular hexagon and placing it in this form on the floor will be an optimal one after it has been ejected uniform distribution of the subprojectiles lying on circular areas and thus a better one Hit probability achieved.

Im folgenden wird die Erfindung anhand mehrerer Ausführungsbeispiele im Zusammenhang mit der Zeichnung näher erläutert. Es zeigen:

  • Fig. 1 einen Längsschnitt der erfindungsgemässen Vorrichtung gemäss der I-I in der Fig. 2,
  • Fig. 2 eine teilweise geschnittene Ansicht der Vorrichtung in Pfeilrichtung A der Fig. 1,
  • Fig. 3a 3b 3c Geometrische Anordnungen von Subprojektilen in quer zur Längsachse eines Geschosskörpers verlaufenden Ebenen,
  • Fig. 4a 4b 4c Weitere Ausführungen geometrischer Anordnungen von Subprojektilen in quer zur Längsachse des Geschosskörpers verlaufenden Ebenen,
  • Fig. 5a 5b 5c Querschnittsformen eines Schiebers der Vorrichtung für Anwendung bei Anordnungen gemäss Fig. 3a bis 3c,
  • Fig. 6a 6b 6c Querschnittsformen des Schiebers der Vorrichtung für Anwendung bei Anordnungen gemäss Fig. 4a bis 4c,
  • Fig. 7 einen Längsschnitt durch Reservoire einer zweiten Ausführung der Vorrichtung gemäss der Linie VII-VII in der Fig. 8,
  • Fig. 8 eine teilweise geschnittene Ansicht des ersten Reservoirs in Pfeilrichtung B der Fig. 7,
  • Fig. 9 einen Querschnitt durch zwei Reservoire der zweiten Ausführung gemäss der Linie IX-IX in Fig. 8,
  • Fig. 10 einen Querschnitt eines Schiebers der zweiten Ausführung der Vorrichtung,
  • Fig. 11a 11b die Vorrichtung gemäss Fig. 1 und 2 während eines ersten Verfahrensschrittes,
  • Fig. 12a 12b die Vorrichtung gemäss Fig. 1 und 2 während eines zweiten Verfahrensschrittes,
  • Fig. 13a 13b die Vorrichtung gemäss Fig. 1 und 2 während eines dritten Verfahrensschrittes, und
  • Fig. 14 die Vorrichtung gemäss Fig. 1 und 2 während eines vierten Verfahrensschrittes.
  • The invention is explained in more detail below with the aid of several exemplary embodiments in connection with the drawing. Show it:
  • 1 shows a longitudinal section of the device according to the invention according to the II in FIG. 2,
  • 2 is a partially sectioned view of the device in the direction of arrow A of FIG. 1,
  • 3a 3b 3c geometric arrangements of sub-projectiles in planes running transversely to the longitudinal axis of a projectile body,
  • 4a 4b 4c further designs of geometrical arrangements of sub-projectiles in planes running transversely to the longitudinal axis of the projectile body,
  • 5a 5b 5c cross-sectional shapes of a slide of the device for use in arrangements according to FIGS. 3a to 3c,
  • 6a 6b 6c cross-sectional shapes of the slide of the device for use in arrangements according to FIGS. 4a to 4c,
  • 7 shows a longitudinal section through reservoirs of a second embodiment of the device according to line VII-VII in FIG. 8,
  • 8 is a partially sectioned view of the first reservoir in the direction of arrow B of FIG. 7,
  • 9 shows a cross section through two reservoirs of the second embodiment along the line IX-IX in FIG. 8,
  • 10 shows a cross section of a slide of the second embodiment of the device,
  • 11a 11b the device according to FIGS. 1 and 2 during a first method step,
  • 12a, 12b the device according to FIGS. 1 and 2 during a second method step,
  • 13a, 13b the device according to FIGS. 1 and 2 during a third method step, and
  • 14 shows the device according to FIGS. 1 and 2 during a fourth method step.
  • In den Fig. 1 und 2 ist mit 1 eine senkrecht angeordnete, im Querschnitt u-förmige Montagezentrierung bezeichnet, die mit einer Abdeckung 2 verschraubt ist. Die Montagezentrierung 1 und die Abdeckung 2 bilden ein Reservoir 3, das im Querschnitt die Form eines schlitzartigen Rechteckes aufweist, dessen Breite der Länge von zylindrischen Subprojektilen (20, Fig. 3, 4) entspricht und dessen Länge sich aus dem Durchmesser und der Anzahl der Subprojektile sowie deren geometrischer Anordnung ergibt (Fig. 3, 4). Am oberen Ende der Montagezentrierung 1 ist eine Deckplatte 4 befestigt, die einen Schlitz 5 aufweist, der annähernd deckungsgleich mit dem Querschnitt des Reservoirs 3 ist. In einem im unteren Bereich des Reservoirs 3 mit der Montagezentrierung 1 verschraubten Flansch 6 wird ein Schieber 7 horizontal geführt, der zwecks Betätigung mit einem Griff 8 verbunden ist. Im Querschnitt entspricht die Breite des Schiebers 7 der Länge des rechteckigen Querschnittes des Reservoirs 3. An seiner Oberseite weist der Schieber 7 eine sich in seiner Längsrichtung erstreckende v-förmige Einkerbung auf, deren Schrägflächen (7.1, Fig. 5) in einer bevorzugten Ausführungsform einen Winkel von 120 DEG einschliessen und die den Seiten eines regelmässigen Sechseckes entsprechen. 1 and 2 , 1 denotes a vertically arranged mounting cross-section which is U-shaped in cross section and which is screwed to a cover 2 . The assembly centering 1 and the cover 2 form a reservoir 3, which in cross section has the shape of a slit-like rectangle, the width of which corresponds to the length of cylindrical sub-projectiles ( 20, Fig. 3, 4 ) and the length of which depends on the diameter and the number of Subprojectiles and their geometric arrangement results ( Fig. 3, 4 ). At the upper end of the assembly centering 1 , a cover plate 4 is fastened, which has a slot 5 which is approximately congruent with the cross section of the reservoir 3 . In a flange 6 screwed to the mounting centering 1 in the lower region of the reservoir 3 , a slide 7 is guided horizontally and is connected to a handle 8 for the purpose of actuation. In cross section, the width of the slide 7 corresponds to the length of the rectangular cross section of the reservoir 3. On its upper side, the slide 7 has a v-shaped notch extending in its longitudinal direction, the inclined surfaces ( 7.1, FIG. 5 ) of which in one preferred embodiment Include angles of 120 ° and correspond to the sides of a regular hexagon.

    Die Unterseite des Schiebers 7 ist dachförmig ausgebildet, wobei die Schrägflächen (7.2, Fig. 5) einen Winkel von 120 DEG einschliessen und wie die Schrägflächen der v-förmigen Einkerbung den Seiten eines regelmässigen Sechseckes entsprechen. Die Montagezentrierung 1 weist einen koaxial zum Schieber 7 verlaufenden eingangsseitig mit dem Reservoir 3 verbundenen Durchbruch 9 auf, dessen Umriss in einem ersten Teil der Montagezentrierung 1 annähernd mit dem vorstehend beschriebenen Umriss des Schiebers 7 übereinstimmt. Am Ausgang des Durchbruches 9 ist ein Ansatz 10 für die Führung der in einen Geschosskörperteil (41, Fig. 14) zu füllenden Subprojektile vorgesehen. Das Geschosskörperteil wird während des Auffüllvorganges in einem koaxial zum Ansatz 10 verlaufenden an der Montagezentrierung 1 befestigten Haltering 11 zentriert.The underside of the slide 7 is roof-shaped, the inclined surfaces ( 7.2 , FIG. 5 ) enclosing an angle of 120 ° and, like the inclined surfaces of the v-shaped notch, corresponding to the sides of a regular hexagon. The mounting centering 1 has a breakthrough 9 which runs coaxially with the slide 7 and is connected on the input side to the reservoir 3 , the outline of which in a first part of the mounting centering 1 corresponds approximately to the outline of the slide 7 described above. At the exit of the breakthrough 9 , an attachment 10 is provided for guiding the sub-projectiles to be filled into a projectile body part ( 41, FIG. 14 ). The projectile body part is centered during filling in an extending coaxially with the shoulder 10 secured to the centering fitting retaining ring 1. 11

    An den Seiten der Montagezentrierung 1 sind Aussparungen 12 vorgesehen, die über Öffnungen 13 mit dem Durchbruch 9 in Verbindung stehen. Die Aussparungen 12 weisen Gleitflächen 14 auf, die um einen Winkel von z.B. 30 DEG aus der Horizontalen nach unten geneigt sind und die ihren Anfang annähernd an oberen Eckpunkten 15 der vom Durchbruch 9 gebildeten vertikalen Seiten des regelmässigen Sechseckes nehmen.Recesses 12 are provided on the sides of the mounting centering 1 and are connected to the opening 9 via openings 13 . The recesses 12 have sliding surfaces 14 which are inclined downward from the horizontal by an angle of, for example, 30 ° and which begin approximately at upper corner points 15 of the vertical sides of the regular hexagon formed by the opening 9 .

    Die Montagezentrierung 1 ist mit einem Auffangbehälter 16 und einer Grundplatte 17 verschraubt. Der Auffangbehälter 16 weist zwei zu beiden Seiten der Montagezentrierung 1 im Bereich der Öffnungen 13 angeordnete geneigte Zuführflächen 18 für überzählige Subprojektile auf.The assembly centering 1 is screwed to a collecting container 16 and a base plate 17 . The collecting container 16 has two inclined feed surfaces 18 arranged on both sides of the assembly centering 1 in the area of the openings 13 for excess sub-projectiles.

    Gemäss den Fig. 3a bis 3c sind zylindrische Subprojektile 20 mit einem Durchmesser d zu Schichten (40, Fig. 14) in Form von regelmässigen Sechsecken zusammengefasst, die Geschosskörpern mit verschiedenen Durchmessern zugeordnet sind. Die Schichten sind in quer zur Längsachse (43, Fig. 14) eines Geschosskörperteiles (41, Fig. 14) verlaufenden Ebenen angeordnet, wobei die Achsen der Subprojektile 20 parallel zur Längsachse ausgerichtet sind. Mit U ist der Umkreis der regelmässigen Sechsecke bezeichnet, dessen Durchmesser D sich aus einem ganzen Vielfachen des Subprojektildurchmessers d ergibt. Der Abstand b zwischen zwei parallel verlaufenden Seiten der regelmässigen Sechsecke ergibt sich, wie vorstehend bereits erwähnt, aus dem Durchmesser d und der Anzahl der Subprojektile 20 sowie deren geometrischer Anordnung.According to FIGS. 3a to 3c , cylindrical sub-projectiles 20 with a diameter d are combined to form layers ( 40, FIG. 14 ) in the form of regular hexagons which are assigned to projectile bodies with different diameters. The layers are arranged in planes running transversely to the longitudinal axis ( 43, FIG. 14 ) of a projectile body part ( 41, FIG. 14 ), the axes of the subprojectiles 20 being aligned parallel to the longitudinal axis. U denotes the circumference of the regular hexagons, the diameter D of which results from a whole multiple of the subprojectile diameter d. The distance b between two parallel sides of the regular hexagons results, as already mentioned above, from the diameter d and the number of sub-projectiles 20 and their geometric arrangement.

    Wie in den Fig. 4a bis 4c dargestellt, sind die zylindrischen Subprojektile 20 mit dem Durchmesser d zu Schichten in Form von unregelmässigen Sechsecken zusammengefasst, die Geschosskörpern mit verschiedenen Durchmessern zugeordnet sind. Hierbei müssen sowohl der Abstand b als auch der Durchmesser D aus der Anzahl und dem Durchmesser d der Subprojektile 20 sowie deren geometrischer Anordnung bestimmt werden.As shown in FIGS. 4a to 4c , the cylindrical sub-projectiles 20 with the diameter d are combined to form layers in the form of irregular hexagons, which are assigned to projectile bodies with different diameters. Here, both the distance b and the diameter D must be determined from the number and the diameter d of the subprojectiles 20 and their geometric arrangement.

    Gemäss den Fig. 5a bis 5c und 6a bis 6c sind die überzähligen Subprojektile, die beim Auffüllen ausgeworfen werden, mit 20.1 bezeichnet.According to FIGS. 5a to 5c and 6a to 6c , the excess sub-projectiles that are ejected during filling are designated 20.1 .

    In den Fig. 7 bis 10 sind mit 30 weitere u-förmige Montagezentrierungen bezeichnet, die mit der Montagezentrierung 1 verschraubt sind, wobei entsprechend der Anzahl Montagezentrierungen 1, 30 gleich viele Reservoire 3 gebildet werden. In den weiteren Montagezentrierungen 30 sind Durchbrüche 31 vorgesehen, die in einem ersten Teil der Montagezentrierungen 30 im Querschnitt die gleiche Form aufweisen wie der Durchbruch 9 der Montagezentrierung 1 (Fig.1) und die konzentrisch zu diesem verlaufen. An den Seiten der weiteren Montagezentrierung 30 sind Aussparungen 32 vorgesehen, die über Öffnungen 33 mit dem Durchbruch 31 in Verbindung stehen. Die Aussparungen 32 weisen Gleitflächen 34 auf, die um einen Winkel von z.B. 30 DEG aus der Horizontalen nach unten geneigt sind und die ihren Anfang annähernd an oberen Eckpunkten der vom Durchbruch 31 gebildeten vertikalen Seiten eines regelmässigen Sechseckes nehmen. Im Durchbruch 31 sind Auswerfernasen 35 angeordnet, die in Nuten 37 eines durch die Durchbrüche 9, 31 verschiebbaren weiteren Schiebers 36 hineinragen. Der Querschnitt des weiteren Schiebers 36 stimmt bis auf die Nuten 37 mit dem Querschnitt des Schiebers 7 der Fig. 1 überein, weist jedoch eine Länge auf, die sich mindestens über alle Montagezentrierungen 1, 30 erstreckt. Wie nicht weiter dargestellt, ist die vorstehend beschriebene Vorrichtung ähnlich wie die Vorrichtung gemäss Fig. 1 und 2 mit einem Auffangbehälter und einer Grundplatte verbunden, sowie mit einem Haltering 11 für das Geschosskörperteil 41, einem Flansch für die Führung des Schiebers 36 und mit einer Abdeckung 2 versehen. 7 to 10 refer to 30 further U-shaped mounting centers, which are screwed to the mounting center 1 , with the same number of reservoirs 3 being formed in accordance with the number of mounting centers 1, 30 . Openings 31 are provided in the further assembly centerings 30 , which have the same shape in cross section in a first part of the assembly centerings 30 as the opening 9 of the assembly centering 1 (FIG. 1) and which run concentrically to this. Recesses 32 are provided on the sides of the further assembly centering 30 and are connected to the opening 31 via openings 33 . The recesses 32 have sliding surfaces 34 which are inclined downward from the horizontal by an angle of, for example, 30 ° and which begin approximately at the upper corner points of the vertical sides of a regular hexagon formed by the opening 31 . Ejector lugs 35 are arranged in the opening 31 , which protrude into grooves 37 of a further slide 36 which can be displaced through the openings 9, 31 . Except for the grooves 37 , the cross section of the further slide 36 corresponds to the cross section of the slide 7 of FIG. 1 , but has a length that extends at least over all assembly centers 1, 30 . 1 and 2, the device described above is connected to a collecting container and a base plate, as well as to a retaining ring 11 for the projectile body part 41, a flange for guiding the slide 36 and with a cover 2 provided.

    Die anhand der Fig. 1 und 2 beschriebene Vorrichtung arbeitet wie folgt:The device described with reference to FIGS. 1 and 2 operates as follows:

    Die Subprojektile 20 werden in einem ersten Schritt (Fig. 11a, 11b) mittels eines nicht dargestellten Vibrationswendelförderers dem Reservoir 3 zugeführt, in welchem sie auf eine erste, durch die Oberseite des Schiebers 7 gebildete Begrenzung senkrecht nach unten fallen. Hierbei wird entsprechend der Form des Schiebers 7 und der Querschnittslänge des Reservoirs 3 die gewünschte geometrische Anordnung gebildet und der Umfang einer aus Subprojektilen 20 bestehenden Schicht 40, der in einer bevorzugten Ausführung ein regelmässiges Sechseck sein möge, teilweise geformt. In einem zweiten Schritt (Fig. 12a, 12b) wird der Schieber 7 zurückgezogen, so dass die Subprojektile 20 um einen bestimmten Betrag, der dem Durchmesser D des Umkreises des gewählten regelmässigen Rechteckes entspricht, auf eine zweite, tiefere Begrenzung fallen. Da die zweite Begrenzung durch die Form des unteren Teiles des Durchbruches 9 bzw. Reservoirs 3 gebildet wird, bleibt hierbei die geometrische Anordnung und der teilweise geformte Umfang der Schicht 40 erhalten. In einem dritten Schritt (Fig. 13a, 13b) werden die zwischen der ersten und zweiten Begrenzung befindlichen Subprojektile 20 in Auffüllrichtung mit dem Schieber 7 vom Reservoir 3 in den Durchbruch 9 geschoben, wobei die endgültige Formung des Umfanges der Schicht 40 erfolgt, indem die überzähligen Subprojektile 20.1 (Fig. 5) durch die Öffnungen 13 abgeführt werden und an den Gleitflächen 14 herunterrollen. Dabei fallen sie auf die Zuführflächen 18, von wo aus sie in den Auffangbehälter 16 gelangen. Von dort können sie entnommen und dem Vibrationswendelförderer zwecks Weiterverarbeitung wieder zugeführt werden. Gleichzeitig mit dem dritten Schritt wird eine folgende, vorgeformte Schicht 40 Subprojektile auf der Oberseite des Schiebers 7 gehalten. In einem vierten Schritt (Fig. 14) werden die endgültig geformten Schichten in einen Hohlraum 42 des Geschosskörperteiles 41 eingeführt, wobei bei wiederholter Hin- und Herbewegung des Schiebers 7 die vorhergehenden Schichten 40 von der jeweils nachfolgenden letzten Schicht 40 verschoben werden, bis der Hohlraum gefüllt ist. Hierbei können gemäss Ausführungsbeispiel unter Anwendung der Anordnung nach Fig. 3c acht, aus je neunzehn Subprojektilen 20 bestehende Schichten 40 im Geschosskörperteil 41 plaziert werden.In a first step ( FIGS. 11a, 11b ), the sub-projectiles 20 are fed to the reservoir 3 by means of a vibratory spiral conveyor, not shown, in which they fall vertically downwards onto a first boundary formed by the top of the slide 7 . Here, the desired geometric arrangement is formed in accordance with the shape of the slide 7 and the cross-sectional length of the reservoir 3 , and the circumference of a layer 40 consisting of subprojectiles 20 , which in a preferred embodiment may be a regular hexagon, is partially shaped. In a second step ( FIGS. 12a, 12b ), the slide 7 is withdrawn so that the subprojectiles 20 fall to a second, lower limit by a certain amount, which corresponds to the diameter D of the circumference of the selected regular rectangle. Since the second boundary is formed by the shape of the lower part of the opening 9 or reservoir 3 , the geometric arrangement and the partially shaped circumference of the layer 40 are retained. In a third step ( FIGS. 13a, 13b ), the subprojectiles 20 located between the first and second delimitation are pushed in the filling direction with the slide 7 from the reservoir 3 into the opening 9 , the final shaping of the circumference of the layer 40 taking place by the surplus subprojectiles 20.1 ( FIG. 5 ) are discharged through the openings 13 and roll down on the sliding surfaces 14 . They fall onto the feed surfaces 18, from where they reach the collecting container 16 . From there they can be removed and fed back to the vibratory bowl feeder for further processing. Simultaneously with the third step, a following, preformed layer 40 sub-projectiles is held on the top of the slide 7 . In a fourth step (Fig. 14) are introduced, the final formed layers into a cavity 42 of the projectile body portion 41, the preceding layers are shifted 40 from the respectively following the last layer 40 upon repeated reciprocating movement of the slide 7, until the cavity is filled. According to the exemplary embodiment, using the arrangement according to FIG. 3c, eight layers 40 , each consisting of nineteen sub-projectiles 20 , can be placed in the projectile body part 41 .

    Die anhand der Fig. 7 bis 10 beschriebene zweite Ausführung der Vorrichtung arbeitet während des ersten und zweiten Schrittes sowohl in der Montagezentrierung 1 als auch in den weiteren Montagezentrierungen 30 gleich wie vorstehend beschrieben, wobei sich jedoch die Rückzugsbewegung des weiteren Schiebers 36 über alle Montagezentrierungen 1, 30 erstreckt. Beim dritten Schritt erfolgt die endgültige Formung des Umfanges der Schicht in der Montagezentrierung 1 ebenfalls wie weiter oben beschrieben.The second embodiment of the device described with reference to FIGS. 7 to 10 works in the same way as described above both in the assembly centering 1 and in the further assembly centers 30 during the first and second step, but the retraction movement of the further slide 36 extends over all assembly centers 1 , 30 extends. In the third step, the final shaping of the circumference of the layer in the assembly centering 1 also takes place as described above.

    In den weiteren Montagezentrierungen 30 stossen bei der Hubbewegung des Schiebers 36 die untersten der überzähligen Subprojektile 20.1 gegen die Auswerfernasen 35, so dass alle überzähligen Subprojektile 20.1 durch die Öffnungen 33 abgeführt werden und an den Gleitflächen 34 herunterrollen können. Der vierte Schritt ist der gleiche wie weiter oben beschrieben, wobei jedoch die Anzahl der Hubbewegungen entsprechend der Anzahl Reservoire 3 reduziert wird. Ein optimales Ergebnis kann erreicht werden, wenn die Anzahl Reservoire 3 gleich der Anzahl der benötigten Schichten ist, da dann für die Auffüllung eines Geschosskörpers nur ein einziger Hub des Schiebers erforderlich ist. In the further assembly centers 30 , when the slide 36 is lifted, the lowermost of the excess sub-projectiles 20.1 hit the ejector lugs 35, so that all of the excess sub-projectiles 20.1 are discharged through the openings 33 and can roll down on the sliding surfaces 34 . The fourth step is the same as described above, but the number of lifting movements is reduced according to the number of reservoirs 3 . An optimal result can be achieved if the number of reservoirs 3 is equal to the number of layers required, since then only a single stroke of the slide is required to fill up a projectile body.

    BezugszeichenlisteReference list

    11
    MontagezentrierungAssembly centering
    22nd
    Abdeckungcover
    33rd
    Reservoirreservoir
    44th
    DeckplatteCover plate
    55
    Schlitzslot
    66
    Flanschflange
    77
    ' Schieber'Slider
    7.17.1
    I SchrägflächenI sloping surfaces
    7.27.2
    SchrägflächenBevels
    88th
    GriffHandle
    99
    Durchbruchbreakthrough
    1010th
    Ansatzapproach
    1111
    HalteringRetaining ring
    1212th
    AussparungenRecesses
    1313
    Öffnungenopenings
    1414
    GleitflächenSliding surfaces
    1515
    Obere EckpunkteUpper corner points
    1616
    AuffangbehälterCollecting container
    1717th
    GrundplatteBase plate
    1818th
    ZuführflächenFeed areas
    2020th
    SubprojektileSubprojectiles
    20.120.1
    SubprojektileSubprojectiles
    3030th
    Weitere MontagezentrierungenFurther assembly centers
    3131
    DurchbrücheBreakthroughs
    3232
    AussparungenRecesses
    3333
    Öffnungenopenings
    3434
    GleitflächenSliding surfaces
    3535
    AuswerfernasenEjector noses
    3636
    Weiterer SchieberAnother slider
    3737
    NutenGrooves
    4040
    Schichtlayer
    4141
    Geschosskörperteil Projectile body part
    4242
    Hohlraumcavity
    4343
    LängsachseLongitudinal axis
    dd
    Durchmesser
    (Subprojektile)
    diameter
    (Subprojectile)
    UU
    UmkreisRadius
    DD
    Durchmesser
    (Umkreis)
    diameter
    (Radius)
    bb
    Abstand (Länge des rechteckigen Querschnittes des Reservoirs)Distance (length of the rectangular cross section of the reservoir)

    Claims (17)

    1. Method for filling a cavity of a projectile with cylindrical submunitions, the submunitions being so arranged in the cavity that their length extends in the direction of the longitudinal axis of the projectile,
      characterised in that
      prior to the filling of the cavity the submunitions (20) are combined into layers (40) which are as thick as the submunitions (20) are long, and which are located in planes at a right angle to the longitudinal axis (43) of the projectile, the submunitions (20) in each layer (40) assuming a position that corresponds to their geometric arrangement in the cavity (42) of a projectile element (41), and the circumference of the layers (40) being shaped in such a manner that after the layers (40) have been inserted into the cavity (42) the submunitions (20) are held in said cavity (42) in a manner that retains the geometrical arrangement previously formed.
    2. Method according to claim 1,
      characterised in that in a first step the submunitions (20) are passed to a reservoir (3) in which they drop vertically downwards onto a first limit stop, thereby partly moulding the particular geometric arrangement and the circumference of a layer (40),
      in a second step the submunitions (20) drop by a given amount onto a second, lower-lying limit stop, and the geometric arrangement and the partly moulded circumference of the layer (40) are retained,
      in a third step the submunitions (20) located between the first and second limit stop are pushed out of the reservoir (3), with final moulding of the circumference of the layer (40) taking place,
      at the same time the submunitions (20) of a following layer in the reservoir (3) are held on the first limit stop, and
      in a fourth step the finally shaped layers (40) are introduced into the cavity (42) of the projectile element (41), with the preceding layers (40) being displaced by the respective following layer (40), until the cavity (42) has been filled.
    3. Method according to claim 2, the submunitions (20) consisting of bodies presenting cylindrical generated surfaces and whose axes run parallel to the longitudinal axis (43) of the projectile element (41),
      characterised in that
      the circumference of the layer (40) containing the submunitions (20) is moulded into a regular hexagon.
    4. Method according to claim 2, the submunitions (20) consisting of bodies presenting cylindrical generated surfaces and whose axes run parallel to the longitudinal axis (43) of the projectile element (41),
      characterised in that
      the circumference of the layer (20) containing the submunitions (20) is moulded into an irregular hexagon.
    5. Method according to claim 3,
      characterised in that
      the given amount corresponds to the diameter of the circle circumscribing the hexagon.
    6. Method according to claim 2,
      characterised in that
      a plurality of layers (40) are produced simultaneously and one behind the other are simultaneously inserted into the cavity (42) of the projectile (41).
    7. Device for carrying out the method according to claim 2,
      in which a vertically arranged U-shaped centring fitting (1) is joined to a cover (2), thereby forming a reservoir (3) which in cross-section has the shape of a slot-like rectangle,
      secured to the centring fitting (1) in the lower region of the reservoir (3) is a flange (6) in which there is horizontally guided a slide (7) whose width matches the length of the slot-like rectangle,
      on its upper face the slide (7) features a V-shaped notched area which extends in the longitudinal direction thereof,
      on its lower face the slide (7) features a roof-shaped construction which extends in the longitudinal direction thereof,
      in the centring fitting (1) is a passage (9) running coaxially with the slide (7) and which in a first portion coincides approximately with the basic outline of the slide (7) and in a second portion coincides approximately with the basic outline of the layer (40),
      provided at the exit of the passage (9) is a shoulder (10) for guiding the submunitions (20) with which the projectile element (41) is to be filled, and
      extending coaxially with the shoulder (10) a holding ring (11) is secured to the centring fitting (1).
    8. Device according to claim 7,
      characterised in that
      the upper face of the slide (7) forms a first limit stop for the submunitions (20) situated in the reservoir (3), and the lower part of the passage (9), or rather of the reservoir (3), forms a second limit stop for the submunitions (20).
    9. Device according to claim 7,
      characterised in that
      the upper face of the slide (7) and the lower part of the passage (9) are moulded in such a way that the arrangement of the submunitions (20) in the layer (40) is the same on the slide (7) and in the passage (9).
    10. Device according to claim 7,
      characterised in that
      the oblique surfaces (7.1) of the V-shaped notched area and the oblique surfaces (7.2) of the roof-shaped construction in each case enclose an angle of 120 degrees and correspond to the sides of a regular hexagon.
    11. Device according to claim 7,
      characterised in that
      the oblique surfaces (7.1) of the V-shaped notched area and the oblique surfaces (7.2) of the roof-shaped construction in each case enclose an angle of 120 degrees and correspond to the sides of an irregular hexagon.
    12. Device according to claim 11,
      characterised in that
      the distance between the tip of the V-shaped notched area and the tip of the roof-shaped construction of the slide (7) is approximately the same as the diameter (D) of the circle (U) circumscribing the hexagon.
    13. Device according to claim 11,
      characterised in that
      provided at the sides of the centring fitting (1) are recesses (12) which communicate with the passage (9) via openings (13), and that the recesses (12) incorporate sliding surfaces (14) which are downwardly inclined by a given angle from the horizontal and which commence approximately at the top corner points (15) of the vertical sides of the hexagon formed by the passage (9).
    14. Device according to claim 11,
      characterised in that
      the width of the slot-like rectangle of the reservoir (3) is the same as the length of cylindrical submunitions (20) and the length of the slot-like rectangle is the same as the distance (b) between two parallel sides of the hexagon.
    15. Device according to claim 7,
      characterised in that
      between one centring fitting (1) and the cover (2) there are provided one or more additional U-shaped centring fittings (30), there being formed the same number of reservoirs (3) as the number of centring fittings (1, 30), and that provided in the additional centring fittings (30) are passages (31) which in a first portion of the additional centring fittings (30) have the same shape in cross-section as the first part of the passage (9) of the centring fitting (1) and which extend concentrically to said first part.
    16. Device according to claim 15,
      characterised in that
      provided on the sides of the additional centring fittings (30) are recesses (32) which communicate via openings (33) with the passage (31), and that the recesses (32) feature sliding surfaces (34) which are downwardly inclined by a given angle from the horizontal, and which commence approximately at top corner points of the vertical sides, formed by the passage (9), of a hexagon.
    17. Device according to claim 16,
      characterised in that
      arranged in the second part of the passage (31) are knockout lugs (35) which project into slots (37) of an additional slide (36) which is adapted to be displaceable through the passages (31, 9).
    EP95118419A 1995-04-05 1995-11-23 Method and device for carrying out the method of filling projectiles with submunitions Expired - Lifetime EP0736745B1 (en)

    Applications Claiming Priority (3)

    Application Number Priority Date Filing Date Title
    CH00978/95A CH690309A5 (en) 1995-04-05 1995-04-05 Method and apparatus for implementing the method for filling of projectile bodies having sub-projectiles.
    CH978/95 1995-04-05
    CH97895 1995-04-05

    Publications (2)

    Publication Number Publication Date
    EP0736745A1 EP0736745A1 (en) 1996-10-09
    EP0736745B1 true EP0736745B1 (en) 2001-08-22

    Family

    ID=4199631

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP95118419A Expired - Lifetime EP0736745B1 (en) 1995-04-05 1995-11-23 Method and device for carrying out the method of filling projectiles with submunitions

    Country Status (10)

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    US (2) US6049957A (en)
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    SE535304C2 (en) * 2010-03-18 2012-06-19 Bae Systems Bofors Ab Berry grenade packed with fin-stabilized penetrators
    PL242033B1 (en) * 2018-08-16 2023-01-09 International Tobacco Machinery Poland Spółka Z Ograniczoną Odpowiedzialnością Method of filling containers with bar-like articles

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    US2682983A (en) * 1949-07-01 1954-07-06 Ici Ltd Apparatus for feeding cylindrical wrappers
    US3093072A (en) * 1957-01-30 1963-06-11 George L Pigman Spin-induced dispersal bomb
    US3027694A (en) * 1959-06-15 1962-04-03 B H Hadley Packaging rectangular objects and embedding them in a matrix
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    US4586314A (en) * 1984-10-30 1986-05-06 Nestec S.A. Filling method and apparatus
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    JPH08285499A (en) 1996-11-01
    US6142054A (en) 2000-11-07
    NO955348D0 (en) 1995-12-29
    CA2169039C (en) 2000-02-01
    EP0736745A1 (en) 1996-10-09
    US6049957A (en) 2000-04-18
    NO955348L (en) 1996-10-07
    CA2169039A1 (en) 1996-10-06
    ZA961978B (en) 1996-09-17
    DE59509535D1 (en) 2001-09-27
    SG44047A1 (en) 1997-11-14
    CH690309A5 (en) 2000-07-14
    IL116978A0 (en) 1996-05-14
    IL116978A (en) 1998-12-27

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