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EP0050380A1 - Device and process for the manufacture of blister-free explosive and/or propellant charges - Google Patents

Device and process for the manufacture of blister-free explosive and/or propellant charges Download PDF

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Publication number
EP0050380A1
EP0050380A1 EP81200997A EP81200997A EP0050380A1 EP 0050380 A1 EP0050380 A1 EP 0050380A1 EP 81200997 A EP81200997 A EP 81200997A EP 81200997 A EP81200997 A EP 81200997A EP 0050380 A1 EP0050380 A1 EP 0050380A1
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EP
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Prior art keywords
melt
casting
heat
heat transfer
transfer medium
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.)
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EP81200997A
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German (de)
French (fr)
Inventor
Richard Bührer
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Schweizerische Eidgenossenschaft
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Schweizerische Eidgenossenschaft
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Publication of EP0050380A1 publication Critical patent/EP0050380A1/en
Ceased legal-status Critical Current

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    • 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
    • F42B33/0214Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by casting
    • F42B33/0228Funnel arrangements therefor
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B21/00Apparatus or methods for working-up explosives, e.g. forming, cutting, drying
    • C06B21/0033Shaping the mixture
    • C06B21/0058Shaping the mixture by casting a curable composition, e.g. of the plastisol type
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S425/00Plastic article or earthenware shaping or treating: apparatus
    • Y10S425/043Rocket fuel core

Definitions

  • the present invention relates to a device according to claim 1 for the production of void-free explosives and / or propellant charges of predetermined spatial shape and composition by casting, the solidification process within the melt being progressively delayed from bottom to top, and to a method for producing these explosives - And / or propellant charges according to claims 9 and 10.
  • the previously known methods for producing explosive or propellant charges are carried out by pouring an explosive or fuel liquefied at elevated temperature into the corresponding shape of the ammunition object or cargo space.
  • the formation of harmful cavities in the casting was prevented as far as possible by external heat supply around or in the top section.
  • the corresponding devices for carrying out such casting processes require a relatively large amount of equipment and are difficult to control in their temperature behavior.
  • Heating boxes (CH-PS 389 449) or metallic heating rods (CH-PS 503 253 and DE-AS 1 796 168) are known for influencing continuous solidification of explosives.
  • this is achieved by a device in which an insulation sleeve is provided outside of the casting mold can be seen, whose radial heat transmission in any horizontal plane corresponds at least approximately to the radially flowing amount of heat released in the solidification of the melt in the cross-section located in the same horizontal plane.
  • the insulation sleeve including the heat transfer medium is heated in a first step for at least one hour to at least the melting temperature of the heat accumulator, in a second step the explosive and / or propellant charge is poured into the casting mold and in a third step the mold is cooled in at least two further temperature steps.
  • Claim 2 describes an advantageous and economically feasible insulation cover.
  • a device according to claim 3 proves to be particularly favorable in practice.
  • the heat capacity of an insulation sleeve can be significantly expanded and predetermined by a cavity for receiving a heat transfer medium.
  • the insulation sleeve can also be designed completely as a cavity and can be partially or completely filled with a heat transfer medium.
  • a heat transfer medium according to claim 6 is in place of liquid cargo to the outside until the areas of the cargo that are vulnerable to blow holes on the lower cross-sectional levels have solidified.
  • An embodiment according to claim 8 results in communicating vessels and thus brings about a particularly simple reflow of the solidifying melt into the casting mold.
  • the pouring opening of the mold represents the connecting line.
  • a casting method according to claim 9 or 10 has proven particularly useful.
  • a pouring funnel 2 is placed on a casting 1.
  • a jacket 5 made of poly is in a collar 4 made of polyvinyl chloride, which is positively attached to the casting 1 urethane foam used with a cavity 11.
  • the pouring funnel 2 is filled with melt to a level N in the usual way. During the solidification process, the melt can easily flow into the cargo space 6 through the relatively small pouring opening 6a, without forming voids.
  • a collar-shaped configuration of the pouring funnel 2 serves as a latent heat store 7, in which the melt solidifies from the outside inwards and thereby releases the latently stored heat energy to the outside, whereby in the area of the pouring opening 6a heat flow to the outside is delayed until the end, so that the melt solidified in this area of cargo last.
  • the insulation hood 9 (insulation sleeve) formed from the collar 4 and the jacket 5 is provided with a cover 10 in order to avoid radiation losses.
  • the entire insulation hood 9 together with the so-called lost head 8 can be easily removed by turning it manually.
  • the insulation hood 9 has a progressively increasing insulation; the cooling rate can be influenced by selecting the ambient temperature; the spatial solidification process in Giessling 1 is largely independent of this.
  • the thermal conductivity of the intended insulating material, the inner and outer radii and the heat transfer coefficient of the outer surface of the insulation hood 9 to the air must be known from the thermal insulation.
  • the casting 1 FIG. 2 has a larger pouring opening 6a, so that no latent heat store is required. Nevertheless, the Represent the solidification process as a result of the insulation hood 9 in a generally characteristic manner.
  • the calculation was based on a melt of pure trinitrotoluene (TNT) with a 20% solids content. The solids did not melt again; the result was a fine crystalline cast structure.
  • TNT trinitrotoluene
  • the insulation hood 9 was heated to the melting temperature of the TNT (approx. 80 °) for two hours, then the melt was poured into the pouring funnel 2 and then in two temperature steps, namely for two hours at a temperature of 70 ° to 80 ° C and then cooled to this at room temperature.
  • the devices and methods according to the invention are in no way limited to the use of TNT; any mixed explosives known per se which has solids in its liquid phase can be used for this.
  • the solid component can also be introduced by another high-performance explosive, such as octogen, hexogen, penta, etc.
  • the same also applies to the propellant charges known per se.

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

Zur Herstellung lunkerfreier Sprengstoff- und/oder Treibladungen ist eine Isolationshülle (9) vorgesehen, deren radialer Wärmedurchlass in einem beliebigen Querschnitt der dort radial abfliessenden durch die Erstarrung der Schmelze frei gewordenen Wärmemenge entspricht. Durch die Isolationshülle (9) entsteht ohne nachträgliche Zufuhr von Fremdenergie (el. Heizung usw.) ein lunkerfreier Guss, selbst bei sehr kleinen Eingiessöffnungen (6a) im Giessling (1). Der erforderliche Wärmedurchlass in der Isolationshülle (9) lässt sich durch den Einsatz von Isolierteilen (4, 5, 10) und/oder Hohlräumen (11) mit Wärmeträgern, z.B. Schmelze, den thermischen Bedingungen des Giesslings (1) anpassen. Entsprechende Giessverfahren beruhen auf einem gezielten Vorwärmen und schrittweisen Abkühlen des Giesslings (1) samt Isolationshülle (9).For the production of void-free explosives and / or propellant charges, an insulating sleeve (9) is provided, the radial heat transmission of which, in any cross-section, corresponds to the amount of heat released radially there by the solidification of the melt. The insulation cover (9) creates a void-free casting without subsequent supply of external energy (electrical heating, etc.), even with very small pouring openings (6a) in the casting (1). The required heat transmission in the insulation cover (9) can be achieved by using insulating parts (4, 5, 10) and / or cavities (11) with heat transfer media, e.g. Adjust the melt to the thermal conditions of the casting (1). Corresponding casting processes are based on targeted preheating and gradual cooling of the casting (1) together with the insulation cover (9).

Description

Die vorliegende Erfindung bezieht sich auf eine Vorrichtung nach Anspruch 1 zur Herstellung lunkerfreier Sprengstoff-und/oder Treib-Ladungen vorgegebener Raumform und Zusammensetzung durch Giessen, wobei der Erstarrungsvorgang innerhalb der Schmelze von unten nach oben zunehmend verzögert erfolgt sowie auf ein Verfahren zur Herstellung dieser Sprengstoff- und/oder Treib-Ladungen gemäss den Ansprüchen 9 und 10.The present invention relates to a device according to claim 1 for the production of void-free explosives and / or propellant charges of predetermined spatial shape and composition by casting, the solidification process within the melt being progressively delayed from bottom to top, and to a method for producing these explosives - And / or propellant charges according to claims 9 and 10.

Die bisher bekannten Verfahren zur Herstellung von Spreng-oder Treib-Ladungen erfolgen durch Giessen eines bei erhöhter Temperatur verflüssigten Spreng- oder Treibstoffes in die entsprechende Form des Munitionsobjektes bzw. Ladungsraumes. Die Bildung von schädlichen Lunkern im Giessling wurde durch externe Wärmezufuhr um oder in der obersten Partie soweit möglich verhindert. Die entsprechenden Vorrichtungen zur Durchführung derartiger Giessverfahren erfordern einen relativ grossen apparativen Aufwand und sind in ihrem Temperaturverhalten schwierig zu steuern.The previously known methods for producing explosive or propellant charges are carried out by pouring an explosive or fuel liquefied at elevated temperature into the corresponding shape of the ammunition object or cargo space. The formation of harmful cavities in the casting was prevented as far as possible by external heat supply around or in the top section. The corresponding devices for carrying out such casting processes require a relatively large amount of equipment and are difficult to control in their temperature behavior.

Bekannt sind zur Beeinflussung einer kontinuierlichen Erstarrung von Sprengstoffen Heizkasten (CH-PS 389 449) oder metallische Heizstäbe (CH-PS 503 253 und DE-AS 1 796 168).Heating boxes (CH-PS 389 449) or metallic heating rods (CH-PS 503 253 and DE-AS 1 796 168) are known for influencing continuous solidification of explosives.

Es ist daher Aufgabe der Erfindung, eine Vorrichtung zu schaffen sowie ein Giessverfahren anzugeben, welche vollständig ohne schwer zu kontrollierende Wärmezufuhr zum Giesstrichter einen lunkerfreien Guss, selbst bei sehr kleinen Eingiessöffnungen, ermöglicht. Ferner sollen komplizierte Wärmevorrichtungen eingespart werden; die Abkühlungsphase soll von der Umgebungstemperatur relativ unabhängig sein.It is therefore an object of the invention to provide a device and to specify a casting method which enables a blow-free casting, even with very small pouring openings, completely without supplying heat to the casting funnel which is difficult to control. Furthermore, complicated heating devices are to be saved; the cooling phase should be relatively independent of the ambient temperature.

Erfindungsgemäss wird dies durch eine Vorrichtung erzielt, bei der ausserhalb der Giessform eine Isolationshülle vorgesehen ist, deren radialer Wärmedurchlass in einer beliebigen Horizontalebene wenigstens annähernd der bei der Erstarrung der Schmelze frei werdenden, radial abfliessenden Wärmemenge im in derselben Horizontalebene befindlichen Querschnitt entspricht.According to the invention, this is achieved by a device in which an insulation sleeve is provided outside of the casting mold can be seen, whose radial heat transmission in any horizontal plane corresponds at least approximately to the radially flowing amount of heat released in the solidification of the melt in the cross-section located in the same horizontal plane.

Gemäss dem erfindungsgemässen Verfahren wird die Isolationshülle samt Wärmeträger in einem 1. Schritt während mindestens einer Stunde auf wenigstens die Schmelztemperatur des Wärmespeichers aufgeheizt, in einem 2. Schritt die Sprengstoff- und/oder Treib-Ladung in die Giessform gegossen und in einem 3. Schritt die Giessform in wenigstens zwei weiteren Temperaturschritten abgekühlt.According to the method according to the invention, the insulation sleeve including the heat transfer medium is heated in a first step for at least one hour to at least the melting temperature of the heat accumulator, in a second step the explosive and / or propellant charge is poured into the casting mold and in a third step the mold is cooled in at least two further temperature steps.

Vorteilhafte Weiterbildungen der Erfindung sind in Unteransprüchen gekennzeichnet.Advantageous developments of the invention are characterized in the subclaims.

Anspruch 2 beschreibt eine vorteilhafte und wirtschaftlich zu realisierende Isolationshülle.Claim 2 describes an advantageous and economically feasible insulation cover.

Aus herstellungstechnischen Gründen erweist sich eine Vorrichtung nach Anspruch 3 in praxi als besonders günstig.For technical reasons, a device according to claim 3 proves to be particularly favorable in practice.

Die Wärmekapazität einer Isolationshülle lässt sich durch einen in Anspruch 4 angegebenen Hohlraum zur Aufnahme eines Wärmeträgers massgeblich erweitern und vorbestimmen. Die Isolationshülle kann auch vollständig als Hohlraum ausgebildet sein und teilweise oder vollständig mit einem Wärmeträger gefüllt werden.The heat capacity of an insulation sleeve can be significantly expanded and predetermined by a cavity for receiving a heat transfer medium. The insulation sleeve can also be designed completely as a cavity and can be partially or completely filled with a heat transfer medium.

Zur Erzielung eines optimalen Abkühlungsverlaufs der Ladung erweist sich ein Wärmeträger gemäss Anspruch 5 als günstig.In order to achieve an optimal cooling process for the load, a heat transfer medium has proven to be favorable.

Ein Wärmeträger nach Anspruch 6 gibt an Stelle der noch flüssigen Ladung so lange Wärme an die Umgebung nach aussen ab, bis die auf untern Querschnittsebenen gelegenen lunkergefährdeten Bereiche der Ladung erstarrt sind.A heat transfer medium according to claim 6 is in place of liquid cargo to the outside until the areas of the cargo that are vulnerable to blow holes on the lower cross-sectional levels have solidified.

Besonders vorteilhaft ist der Einsatz der Ladungs-Schmelze (vgl. Anspruch 7) als Wärmeträger, insbesondere aus Gründen der vereinfachten Manipulation.It is particularly advantageous to use the charge melt (see claim 7) as a heat carrier, in particular for reasons of simplified manipulation.

Eine Ausgestaltung gemäss Anspruch 8 ergibt kommunizierende Gefässe und bewirkt damit ein besonders einfaches Nachfliessen der erstarrenden Schmelze in die Giessform. Im einfachsten Fall stellt dabei die Eingiessöffnung der Form die Verbindungsleitung dar.An embodiment according to claim 8 results in communicating vessels and thus brings about a particularly simple reflow of the solidifying melt into the casting mold. In the simplest case, the pouring opening of the mold represents the connecting line.

Besonders bewährt hat sich ein Giessverfahren nach Anspruch 9 oder 10.A casting method according to claim 9 or 10 has proven particularly useful.

Nachfolgend werden anhand schematischer Zeichnungen Ausführungsbeispiele der Erfindung näher beschrieben. Es zeigen

  • Fig. 1 ein Geschoss mit aufgesetzter Isolationshaube in Schnittdarstellung während des Erstarrungsprozesses der Ladung und
  • Fig. 2 den oberen Teil eines weiteren Geschosses mit einer Wärmeisolation sowie einer eingezeichneten Isochronenschar.
Exemplary embodiments of the invention are described in more detail below with the aid of schematic drawings. Show it
  • Fig. 1 shows a floor with an attached insulation hood in a sectional view during the solidification process of the load and
  • Fig. 2 shows the upper part of a further floor with thermal insulation and a drawn isochronous family.

In beiden Zeichnungen sind gleichartig wirkende Teile mit gleichen Bezugszeichen versehen.Parts that act in the same way are provided with the same reference symbols in both drawings.

Gemäss Fig. 1 ist auf einen Giessling 1 ein Giesstrichter 2 aufgesetzt. In einen formschlüssig am Giessling 1 aufgesetzten Kragen 4 aus Polyvinilchlorid ist ein Mantel 5 aus Polyurethanschaum mit einem Hohlraum 11 eingesetzt. Der Giesstrichter 2 ist in üblicher Weise mit Schmelze bis zu einem Niveau N gefüllt. Die Schmelze vermag während des Erstarrungsprozesses durch die relativ kleine Eingiessöffnung 6a problemlos, ohne Lunkerbildung, in den Ladungsraum 6 nachfliessen. Dabei dient eine kragenförmige Ausbildung des Giesstrichters 2 als Latentwärmespeicher 7, in welchem die Schmelze von aussen nach innen erstarrt und dabei die latent gespeicherte Wärmeenergie nach aussen abgibt, wodurch im Bereiche der Eingiessöffnung 6a ein Wärmeabfluss nach aussen bis zuletzt verzögert wird, so dass die Schmelze in diesem Bereiche der Ladung zuletzt erstarrt.1, a pouring funnel 2 is placed on a casting 1. A jacket 5 made of poly is in a collar 4 made of polyvinyl chloride, which is positively attached to the casting 1 urethane foam used with a cavity 11. The pouring funnel 2 is filled with melt to a level N in the usual way. During the solidification process, the melt can easily flow into the cargo space 6 through the relatively small pouring opening 6a, without forming voids. Here, a collar-shaped configuration of the pouring funnel 2 serves as a latent heat store 7, in which the melt solidifies from the outside inwards and thereby releases the latently stored heat energy to the outside, whereby in the area of the pouring opening 6a heat flow to the outside is delayed until the end, so that the melt solidified in this area of cargo last.

Die aus dem Kragen 4 und dem Mantel 5 gebildete Isolationshaube 9 (Isolationshülle) ist zur Vermeidung von Strahlungsverlusten mit einer Abdeckung 10 versehen.The insulation hood 9 (insulation sleeve) formed from the collar 4 and the jacket 5 is provided with a cover 10 in order to avoid radiation losses.

Nach dem Erstarren kann die gesamte Isolationshaube 9 mitsamt dem sogenannten verlorenen Kopf 8 durch manuelles Drehen leicht abgenommen werden.After solidification, the entire insulation hood 9 together with the so-called lost head 8 can be easily removed by turning it manually.

Die Isolationshaube 9 weist eine progressiv nach oben zunehmende Isolation auf; durch Wahl der Umgebungstemperatur lässt sich die Abkühlungsgeschwindigkeit beeinflussen; der räumliche Erstarrungsverlauf im Giessling 1 ist davon weitgehendst unabhängig.The insulation hood 9 has a progressively increasing insulation; the cooling rate can be influenced by selecting the ambient temperature; the spatial solidification process in Giessling 1 is largely independent of this.

Zur Dimensionierung der Isolationshaube 9 bzw. deren Wärmedämmung auf einem bestimmten Horizontalquerschnitt müssen vom Sprengstoff (oder der Treibladung) folgende physikalische Daten bekannt sein:

  • Anteil an Festkörpern, welche als solche keine Latentwärme abzugeben vermögen, der Wärmeleitwert des erstarrten Spreng-stoffes, die Erstarrungswärme des flüssigen Sprengstoffes und die Dichte des erstarrten Sprengstoffes.
To dimension the insulation hood 9 or its thermal insulation on a certain horizontal cross-section, the following physical data must be known about the explosives (or the propellant charge):
  • Percentage of solids which as such are unable to give off latent heat, the thermal conductivity of the solidified explosive substance, the heat of solidification of the liquid explosive and the density of the solidified explosive.

Im weiteren müssen vom Giessling bekannt sein:

  • Dessen Wärmeleitwert sowie die inneren und äusseren Radien auf der jeweils zu berechnenden Querschnittsebene.
The Giessling must also know:
  • Its thermal conductivity as well as the inner and outer radii on the respective cross-sectional plane to be calculated.

Ausserdem müssen, ebenfalls im jeweiligen Querschnitt, von der Wärmedämmung der Wärmeleitwert des vorgesehenen Isoliermaterials, die inneren und äusseren Radien sowie die Wärmeübergangszahl der äusseren Oberfläche der Isolationshaube 9 an die Luft bekannt sein.In addition, also in the respective cross section, the thermal conductivity of the intended insulating material, the inner and outer radii and the heat transfer coefficient of the outer surface of the insulation hood 9 to the air must be known from the thermal insulation.

Zur eigentlichen Berechnung dienen die Systemvoraussetzungen, dass einerseits die bei der Erstarrung des Sprengstoffes frei werdende Wärmemenge dQL gleich sein soll, wie die durch die Wärmeleitung an die Luft abgegebene Wärmemenge dQV:

Figure imgb0001

  • wobei ΔT die Temperaturdifferenz zwischen Sprengstofferstarrungszone und Aussenraum,
  • dt die zur Abkühlung der erstarrten Sprengstoffmasse erforderliche Zeit und
  • R der thermische Widerstand zwischen Sprengstofferstarrungszone und äusserer Oberfläche sind.
For the actual calculation, the system requirements are that, firstly, the heat released during the solidification of the explosive heat quantity dQ L should be equal, as given by the heat conduction to the air heat quantity dQ V:
Figure imgb0001
  • where ΔT is the temperature difference between the explosive solidification zone and the outside space,
  • dt the time required to cool the solidified explosive mass and
  • R are the thermal resistance between the explosive solidification zone and the outer surface.

Der Giessling 1 Fig. 2 weist im Gegensatz zu demjenigen in Fig. 1 eine grössere Eingiessöffnung 6a auf, so dass kein Latentwärmespeicher benötigt wird. Trotzdem lässt sich der Erstarrungsprozess als Folge der Isolationshaube 9 allgemein charakteristisch darstellen. Die eingezeichnete Isochronenschar 3, in stündlichen Abständen eingezeichnet, zeigt deutlich wie der Erstarrungsbereich von unten nach oben fortschreitet und dabei die Schmelze im Bereich der Eingiessöffnung 6a nach über 6 Stunden in einem zentralen konzentrischen Bereich noch flüssig ist und somit einen hochwertigen lunkerfreien Sprengeinsatz ergibt.In contrast to that in FIG. 1, the casting 1 FIG. 2 has a larger pouring opening 6a, so that no latent heat store is required. Nevertheless, the Represent the solidification process as a result of the insulation hood 9 in a generally characteristic manner. The drawn in isochronous family 3, drawn in at hourly intervals, clearly shows how the solidification area progresses from bottom to top and the melt in the area of the pouring opening 6a is still liquid after more than 6 hours in a central concentric area and thus results in a high-quality blow-free blasting operation.

Randseitig sind die Horizontalebenen A - H bezeichnet, welche der vorgängig betrachteten Berechnung der Isolationshaube 9 dienten.At the edge, the horizontal planes A - H are designated, which served the previously considered calculation of the insulation hood 9.

Im vorliegenden Fall wurde der Berechnung eine Schmelze aus reinem Trinitrotoluol (TNT) mit einem 20%igen Anteil an Festkörpern zugrunde gelegt. Ein Wiederaufschmelzen der Festkörper erfolgte nicht; es resultierte ein feinkristallines Gussgefüge.In the present case, the calculation was based on a melt of pure trinitrotoluene (TNT) with a 20% solids content. The solids did not melt again; the result was a fine crystalline cast structure.

Die Isolationshaube 9 wurde während zwei Stunden auf die Schmelztemperatur des TNT (ca. 80°) aufgeheizt, anschliessend die Schmelze in den Giesstrichter 2 eingegossen und dann in zwei Temperaturschritten, nämlich während zwei Stunden bei einer Temperatur von 70° bis 80° C und anschliessend bei Raumtemperatur auf diese abgekühlt.The insulation hood 9 was heated to the melting temperature of the TNT (approx. 80 °) for two hours, then the melt was poured into the pouring funnel 2 and then in two temperature steps, namely for two hours at a temperature of 70 ° to 80 ° C and then cooled to this at room temperature.

Die erfindungsgemässen Vorrichtungen und Verfahren sind keineswegs auf die Verwendung von TNT beschränkt, jeder an sich bekannte Mischsprengstoff, welcher in seiner flüssigen Phase Festkörper aufweist, ist hierfür anwendbar. Der Festkörperanteil kann auch durch einen anderen Hochleistungssprengstoff eingebracht werden, wie beispielsweise Octogen, Hexogen, Penta etc. Das gleiche gilt auch für die an sich bekannten Treibladungen.The devices and methods according to the invention are in no way limited to the use of TNT; any mixed explosives known per se which has solids in its liquid phase can be used for this. The solid component can also be introduced by another high-performance explosive, such as octogen, hexogen, penta, etc. The same also applies to the propellant charges known per se.

Claims (10)

1. Vorrichtung zur Herstellung lunkerfreier Sprengstoff-und/oder Treib-Ladungen vorgegebener Raumform und Zusammensetzung durch Giessen, wobei der Erstarrungsvorgang innerhalb der Schmelze von unten nach oben zunehmend verzögert erfolgt, dadurch gekennzeichnet, dass ausserhalb der Giessform eine Isolationshülle (9) vorgesehen ist, deren radialer Wärmedurchlass in einer beliebigen Horizontalebene (B-H) wenigstens annähernd der bei der Erstarrung der Schmelze frei werdenden, radial abfliessenden Wärmemenge im in derselben Horizontalebene befindlichen Querschnitt entspricht. (Fig. 2)1. Device for producing void-free explosives and / or propellant charges of predetermined spatial shape and composition by casting, the solidification process within the melt being progressively delayed from bottom to top, characterized in that an insulation sleeve (9) is provided outside the casting mold, whose radial heat transmission in any horizontal plane (BH) corresponds at least approximately to the radially flowing amount of heat released in the cross section in the same horizontal plane when the melt solidifies. (Fig. 2) 2. Vorrichtung nach Anspruch 1, dadurch gekennzeichnet, dass die Isolationshülle (9) aus wenigstens einem Kunststoff besteht. (Fig. 1)2. Device according to claim 1, characterized in that the insulation sleeve (9) consists of at least one plastic. (Fig. 1) 3. Vorrichtung nach Anspruch 2, dadurch gekennzeichnet, dass die Isolationshülle (9) wenigstens zum Teil aus Polypropylen und/oder geschäumtem Polyurethan besteht. (Fig. 1)3. Device according to claim 2, characterized in that the insulation sleeve (9) consists at least partially of polypropylene and / or foamed polyurethane. (Fig. 1) 4. Vorrichtung nach einem der Ansprüche 1 bis 3, dadurch gekennzeichnet, dass die Isolationshülle (9) wenigstens einen Hohlraum (11) zur Aufnahme eines Wärmeträgers aufweist. (Fig. 1)4. Device according to one of claims 1 to 3, characterized in that the insulation sleeve (9) has at least one cavity (11) for receiving a heat transfer medium. (Fig. 1) 5. Vorrichtung nach Anspruch 4, dadurch gekennzeichnet, dass der Wärmeträger eine gleiche oder gegenüber der Schmelze höhere Wärmekapazität aufweist. (Fig. 1)5. The device according to claim 4, characterized in that the heat transfer medium has the same or a higher thermal capacity than the melt. (Fig. 1) 6. Vorrichtung nach Anspruch 4, dadurch gekennzeichnet, dass der Wärmeträger ein latente Wärme speicherndes Medium ist. (Fig. 1)6. The device according to claim 4, characterized in that the heat transfer medium is a latent heat-storing medium. (Fig. 1) 7. Vorrichtung nach Anspruch 6, dadurch gekennzeichnet, dass der Wärmeträger Schmelze ist. (Fig. 1)7. The device according to claim 6, characterized in that the heat transfer medium is melt. (Fig. 1) 8. Vorrichtung nach Anspruch 7, dadurch gekennzeichnet, dass eine Verbindungsleitung zwischen der in der Giessform befindlichen Schmelze und der im Hohlraum (11) befindlichen Schmelze vorgesehen ist. (Fig. 1)8. The device according to claim 7, characterized in that a connecting line between the melt located in the casting mold and the melt located in the cavity (11) is provided. (Fig. 1) 9. Verfahren zur Herstellung lunkerfreier Sprengstoff- und/ oder Treib-Ladungen mit einer Vorrichtung nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass die Isolationshülle samt Wärmeträger in einem 1. Schritt während mindestens einer Stunde auf wenigstens die Schmelztemperatur des Wärmespeichers aufgeheizt wird, dass in einem 2. Schritt die Sprengstoff- und/oder Treib-Ladung in die Giessform gegossen wird und dass in einem 3. Schritt die Giessform in wenigstens zwei Temperaturschritten abgekühlt wird.9. A method for producing void-free explosives and / or propellant charges with a device according to one of claims 1 to 8, characterized in that the insulation sleeve together with the heat transfer medium is heated in a first step for at least one hour to at least the melting temperature of the heat accumulator that in a second step the explosive and / or propellant charge is poured into the mold and that in a third step the mold is cooled in at least two temperature steps. 10. Verfahren nach Anspruch 8, dadurch gekennzeichnet, dass die Giessform während wenigstens zwei Stunden bei einer Temperatur von 70 - 80° C und anschliessend bei 20* C abgekühlt wird.10. The method according to claim 8, characterized in that the mold is cooled for at least two hours at a temperature of 70-80 ° C and then at 20 * C.
EP81200997A 1980-09-15 1981-09-09 Device and process for the manufacture of blister-free explosive and/or propellant charges Ceased EP0050380A1 (en)

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DE3501286A1 (en) * 1984-01-19 1985-08-01 Aktiebolaget Bofors, Bofors METHOD AND DEVICE FOR CASTING EXPLOSIVE
DE3428501A1 (en) * 1984-08-02 1986-02-13 Diehl GmbH & Co, 8500 Nürnberg CAST FUNNEL FOR FILLING BULLETS WITH EXPLOSIVE
DE4319919C1 (en) * 1993-06-16 1995-01-19 Diehl Gmbh & Co Casting apparatus for spherical explosive pieces
CN110595302A (en) * 2019-09-19 2019-12-20 西安庆华民用爆破器材股份有限公司 Preparation method of delay element for detonator

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EP0217770B1 (en) * 1985-09-27 1992-01-22 Nobel Kemi AB A method of phlegmatization of crystalline explosives and other explosive crystalline substances, as well as a method of producing plastic bound explosives and substances produced according to the method
SE452760B (en) * 1985-09-27 1987-12-14 Nobel Kemi Ab SET TO MAKE HEXOTONAL AND OKTONAL MIX EXPLOSIONS
US4813331A (en) * 1987-04-06 1989-03-21 The United States Of America As Represented By The Secretary Of The Army Apparatus and method for filling individual munitions items with explosive
US6635197B2 (en) * 2001-06-25 2003-10-21 American Ordinance Llc Method and apparatus for casting molten materials using phase-change material

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GB191419565A (en) * 1914-09-09 1915-10-11 It Prodotti Esplodenti Soc Improvements in the Preparation of the Charges for Explosive Projectiles.
US2435610A (en) * 1941-04-30 1948-02-10 Charles F Schneider Funnel for casting explosive charges
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Cited By (6)

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Publication number Priority date Publication date Assignee Title
DE3501286A1 (en) * 1984-01-19 1985-08-01 Aktiebolaget Bofors, Bofors METHOD AND DEVICE FOR CASTING EXPLOSIVE
DE3428501A1 (en) * 1984-08-02 1986-02-13 Diehl GmbH & Co, 8500 Nürnberg CAST FUNNEL FOR FILLING BULLETS WITH EXPLOSIVE
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DE4319919C1 (en) * 1993-06-16 1995-01-19 Diehl Gmbh & Co Casting apparatus for spherical explosive pieces
CN110595302A (en) * 2019-09-19 2019-12-20 西安庆华民用爆破器材股份有限公司 Preparation method of delay element for detonator
CN110595302B (en) * 2019-09-19 2021-11-02 西安庆华民用爆破器材股份有限公司 Preparation method of delay element for detonator

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CA1160485A (en) 1984-01-17
US4380186A (en) 1983-04-19

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