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EP0808813B1 - Continuous process for the solventless production of pyrotechnical products having a thermosetting binder - Google Patents

Continuous process for the solventless production of pyrotechnical products having a thermosetting binder Download PDF

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Publication number
EP0808813B1
EP0808813B1 EP97401051A EP97401051A EP0808813B1 EP 0808813 B1 EP0808813 B1 EP 0808813B1 EP 97401051 A EP97401051 A EP 97401051A EP 97401051 A EP97401051 A EP 97401051A EP 0808813 B1 EP0808813 B1 EP 0808813B1
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European Patent Office
Prior art keywords
process according
binder
products
styrene
solid
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EP97401051A
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German (de)
French (fr)
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EP0808813A1 (en
Inventor
Alain Lefumeux
Dominique Wiencek
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Societe Nationale des Poudres et Explosifs
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Societe Nationale des Poudres et Explosifs
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    • 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
    • C06B21/0008Compounding the ingredient
    • C06B21/0025Compounding the ingredient the ingredient being a polymer bonded explosive or thermic component
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/001Fillers, gelling and thickening agents (e.g. fibres), absorbents for nitroglycerine

Definitions

  • the present invention relates to the field of composite pyrotechnic products and in particular composite powders for tube weapons, propellants composites for rocket engines and explosives composites for ammunition loading. More precisely the invention relates to a continuous process for solvent-free manufacturing of such pyrotechnic products comprising a thermosetting binder.
  • a pulverulent energy charge which can be a mineral charge such as for example ammonium nitrate, ammonium perchlorate or potassium perchlorate or else an organic charge and in particular a nitramine such as for example hexogen, oct
  • Binders usable for the manufacture of composite pyrotechnics can be thermoplastic binders or binders thermosetting.
  • thermoplastic binders have the advantage of relatively easily lend themselves to implementation continuously due to the fact that they soften by temperature rise. So the patent application French FR-A-2 723 086 describes a manufacturing process continuous and solvent-free of pyrotechnic products composites based on thermoplastic type binders.
  • thermoplastic type binders have the disadvantage of leading to products that have a poor temperature resistance due to the very softening of the binder when the temperature.
  • the man of profession needs pyrotechnic products presenting good temperature resistance.
  • thermosetting binder offer the advantage of presenting good temperature resistance.
  • US-A-4,405,534 describes a process for manufacturing composite explosives by cold compression of granules of explosives coated with a polyurethane film made plastic thanks to the presence of plasticizers. This process, apart from the fact that it is discontinuous, has the disadvantage additional to require the presence of a strong plasticizer content which is not always favorable to the energy plan.
  • thermosetting binders When the skilled person wants to implement with thermosetting binders a continuous process solvent-free it faces the problem of short "pot life" of these compositions which means that after mixture of the ingredients of the composition, it does have only a very short time to perform the shaping geometry of the product before the crosslinking of the binder does not make any mechanical work of the dough containing the different ingredients.
  • thermosetting binder Nevertheless the possibilities of application of these techniques are limited and the skilled person does not have not a general continuous manufacturing process and solvent-free composite pyrotechnic products to thermosetting binder.
  • the object of the present invention is precisely to propose such a process as well as an installation industrial allowing the implementation of this process.
  • the major originality of the process according to the invention lies in the fact that with the exception of the final phase during which the structure and composition of intermediate products are fixed by crosslinking, the different operations are carried out at a temperature at which the binder is, chemically, almost non-scalable. So the formulation of the product composition is perfectly reproducible insofar as it is fully carried out in start of the process without requiring any adjustment ulterior. The skilled person is not confronted with any condition of "pot life" and intermediate products whose geometric dimensions are imperfect can be recycled in manufacturing.
  • the process according to the invention uses a liquid thermosetting binder non-evolving during the process of which the apparent viscosity by use of fillers thickeners.
  • said solid thickening filler consists of a porous material whose particle size is between 0.1 and 10 ⁇ m (microns) and whose specific surface is between 60 and 500 m 2 / g .
  • this material will also have combustion modifying properties and will be chosen in the group consisting of carbon black, the colloidal silica, alumina, titanium oxide or polynorbornene.
  • the weight ratio between said thickening filler and said binder crosslinkable is between 0.05 and 0.25.
  • said solid thickening filler is constituted by a thermoplastic polymer with hydrocarbon units which may contain, in addition to carbon and hydrogen atoms, oxygen and nitrogen atoms and whose molecular mass weight average is between 3x10 5 and 3x10 6 .
  • thermoplastic polymers usable as solid thickening filler in the framework of the present invention is thus constituted by styrene / butadiene / styrene, styrene / isoprene / styrene copolymers, styrene / ethylene / butylene / styrene and styrene / ethylene / propylene.
  • thermoplastic polymers usable as solid thickening fillers in the framework of the present invention is constituted by the polyurethanes with polyether and polycarbonate patterns and by polyether / polyamide block copolymers.
  • the weight ratio between said thickening filler and said binder crosslinkable is between 10:90 and 50:50.
  • solid oxidizing energy charges we can also incorporate into the premix, consisting by the liquid binder and said thickening fillers, at least one solid reducing energy charge like, for example, aluminum or boron powder.
  • the method according to the invention thus makes it possible to obtain continuously, without time constraints linked to "pot life” issues and no use of solvents or energy-unwanted plasticizers, Composite pyrotechnic products with crosslinked binder. These products find their preferred applications as propellant powders in strands or in sticks for ammunition intended for the weapons with tube, like blocks of propellants for rocket and rocket engines, as explosive charges for ammunition explosives or as pyrotechnic charges for gas generators intended for both military applications than civil applications like automotive safety.
  • the invention also relates to an installation particularly suitable for the implementation of method according to the invention.
  • Figure 1 shows, so schematic, the preferred installation presented above.
  • Figure 2 shows, for reasons of clarity, a simplified top view of the rolling mill shear used.
  • the invention therefore consists in mixing, at temperature ambient the starting constituents of a composition composite pyrotechnic crosslinkable until obtained a homogeneous composite paste with a viscosity sufficient to be able, always at temperature ambient, be in the form of products intermediaries who already have a stable shape and final dimensions of the finished product that we want to get.
  • the form and composition of these intermediate products are then frozen by hot crosslinking so as to obtain the products desired completions.
  • thermosetting binder is liquid to room temperature and that its crosslinking cannot start only at a temperature above 40 ° C so as to be certain that as long as we stay at one ambient temperature below 40 ° C, this binder will remain chemically non-evolving.
  • binder liquid all of the liquid reactive constituents which, after crosslinking, will give the crosslinked binder solid.
  • the crosslinking reaction can be of the type polycondensation reaction, in which case the binders will in particular be of the polyurethane, polyesters or polyamides.
  • the crosslinking reaction can be of the type polyaddition reaction with opening of unsaturations ethylenic, in which case the binders will in particular be polyalkylenes, polyacrylates or polymethacrylates. In the latter case, the composition must contain crosslinking catalysts, such as for example peroxides.
  • said thickening fillers can be made of porous solid materials of small particle size.
  • certain additives usually used as modifiers of combustion like carbon black the process according to the invention in this case offers the advantage of allowing continuously obtaining pyrotechnic compositions already known but which were only accessible by discontinuous processes.
  • Said thickening fillers can also be made up of thermoplastic polymers high molecular weight solids so as to get a final product whose binder consists of a alloy of thermoplastic polymers and polymers cross-linked. This type of alloy allows obtaining composite products with characteristics particularly high mechanical properties.
  • the premix 2 thus formed may also contain other additives of the final composition. he should have the consistency of a thick fat of so that it can be transported continuously using a positive displacement pump while adhering, without sinking, on the surface of a cylinder rotating with a speed angular of a few tens of revolutions per minute.
  • This premix is therefore transported by means of a circulation pump 34, for example a gear, in a reserve 35 provided with a piston cover 36.
  • the premix is then taken up by a pump doser 5 with gear to be driven, in a equipment where the operations of mixing with solid energy charges and setting in the form of the composite paste thus obtained in the form of intermediate products that already have the ratings geometries of finished products.
  • These two operations can be carried out in a single device like for example a twin screw extruder whose head extrusion will be associated with a cutting device. But, preferentially, these two operations will be carried out by two separate devices, one placed following each other.
  • the premix 2 is transported by the pump 5 in a mixer which can be a traditional mixer as a "BUSS" co-kneader but which, preferably and as shown in Figure 1, is a rolling mill shear 6 consisting of two cylindrical rollers 7 and 8 of identical length and having grooves helical. Axes 9 and 10 of these two cylinders are parallel and located in the same horizontal plane being spaced so as to leave a slot 11 between the two rollers. Axes 9 and 10 are supported by support blocks 12 and 13, block 12 being a block engine driving in rotation the two cylinders 7 and 8 which rotate in opposite directions to each other at different speeds.
  • Such a shear rolling mill is known to those skilled in the art and described in numerous publications, for example in the patent application FR-A-2 723 086 already cited.
  • the pump 5 thus brings the premix 2 to the roller 7 which turns the fastest, the premix forming on this roll a sheet which coats this latest.
  • the premix is brought to the end 14 material inlet of the rolling mill 6.
  • At least one dosing hopper 16 pours between the material inlet end 14 and the end of material outlet 15 from rolling mill 6, the loads solid energy 17 on the premix sheet coating the roller 7. These solid energy charges are then intimately mixed with premix 2 thanks to the shearing action of the rolling mill 6 so as to form on roll 7 a sheet of composite dough homogeneous which already has sufficient viscosity to ability to maintain stable geometric dimensions.
  • Solid energy charges will mainly constituted by the oxidizing charges of the composition which can be mineral fillers such as ammonium perchlorate, potassium perchlorate or ammonium nitrate, or organic fillers and in particular nitramines such as hexogen, octogen, nitroguanidine or hexanitro-hexaazaisowurtzitane.
  • mineral fillers such as ammonium perchlorate, potassium perchlorate or ammonium nitrate
  • organic fillers and in particular nitramines such as hexogen, octogen, nitroguanidine or hexanitro-hexaazaisowurtzitane.
  • the different charges may be brought either in mixture by a single hopper, or separately by a succession of hoppers.
  • the composite dough sheet thus obtained is recovered in the form of granules 19 by a device for granulation 18 located at the outlet end 15 of the rolling mill 6.
  • a device for granulation 18 located at the outlet end 15 of the rolling mill 6.
  • the outlet ends of rollers 7 and 8 are not grooved but are smooth.
  • the granules 19 are then taken up continuously in an extruder 20, for example a twin extruder screw, fitted with an extrusion head 21 to be profiled in rods 23 driven by a conveyor belt 25.
  • an extruder 20 for example a twin extruder screw, fitted with an extrusion head 21 to be profiled in rods 23 driven by a conveyor belt 25.
  • a cutting device 22 cuts the rods profiles 23 leaving the extrusion head 21 in 24 intermediate products already with the ratings final of finished products.
  • the device cutting 22 has a movement controlled by the speed of progression of the mat 25 on which the rods rest 23.
  • the finished products 27 leaving the oven 26 can then be packaged in their packaging 28.
  • the method according to the invention thus makes it possible to manufacture in continuous series of products composite pyrotechnics with crosslinked binder, and in particular products of small dimensions, without constraint of "pot life", solvent-free and plasticizer-free undesirable.
  • the 7-hole and 19-hole multi-perforated cylindrical powder strands were produced by the continuous process according to the invention from the following three compositions: Composition 1 Composition 2 Composition 3 binder PBHT: 9% PBHT: 10.5% PAG: 13% thickening filler SIS 6% PE-PA: 4.5% PE-PA: 7% oxidizing charge RDX 85% RDX 85% RDX 80% particle size of the oxidizing charge 100 ⁇ m 150 ⁇ m 80 ⁇ m reducing load 0 0 0 0
  • Example 4 On 10 meters of propellant extruded continuously for each of the compositions, the dimensional variations obtained after hot cutting and crosslinking are as follows: Example 4 Example 5 Example 6 outer diameter in mm 30.5 ⁇ 0.002 30.0 ⁇ 0.02 29.9 ⁇ 0.02 inside diameter in mm 13.8 ⁇ 0.003 13.9 ⁇ 0.02 14.05 ⁇ 0.02 length in mm 121 ⁇ 0.1 120.5 ⁇ 0.15 120.4 ⁇ 0.1

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  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Processes Of Treating Macromolecular Substances (AREA)
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Description

La présente invention se rapporte au domaine des produits pyrotechniques composites et notamment des poudres composites pour armes à tube, des propergols composites pour moteurs de fusée et des explosifs composites pour chargements de munitions. Plus précisément l'invention concerne un procédé continu de fabrication sans solvant de tels produits pyrotechniques comportant un liant thermodurcissable.The present invention relates to the field of composite pyrotechnic products and in particular composite powders for tube weapons, propellants composites for rocket engines and explosives composites for ammunition loading. More precisely the invention relates to a continuous process for solvent-free manufacturing of such pyrotechnic products comprising a thermosetting binder.

Les produits pyrotechniques composites constitués par un liant organique et par une charge énergétique pulvérulente qui peut être une charge minérale comme par exemple le nitrate d'ammonium, le perchlorate d'ammonium ou le perchlorate de potassium ou encore une charge organique et notamment une nitramine comme par exemple l'hexogène, l'octogène, la nitroguanidine ou le 2,4,6,8,10,12 hexanitro-2,4,6,8,10,12 hexaazatétracyclo (5.5.O.O 5,9.0 3,11) dodécane encore appelé hexanitrohexaaza-isowurtzitane sont très recherchés par l'homme de métier en raison de leur grande stabilité chimique et de leur faible vulnérabilité aux impacts et aux agressions thermiques.The composite pyrotechnic products constituted by an organic binder and by a pulverulent energy charge which can be a mineral charge such as for example ammonium nitrate, ammonium perchlorate or potassium perchlorate or else an organic charge and in particular a nitramine such as for example hexogen, octogen, nitroguanidine or 2,4,6,8,10,12 hexanitro-2,4,6,8,10,12 hexaazatetracyclo (5.5.OO 5,9. 0 3, 11 ) dodecane also called hexanitrohexaaza-isowurtzitane are highly sought after by those skilled in the art because of their high chemical stability and their low vulnerability to thermal impacts and aggressions.

Par ailleurs, pour des raisons de sécurité et de reproductibilité des fabrications, l'homme de métier préfère les procédés continus aux procédés discontinus.In addition, for security and safety reasons reproducibility of manufacturing, the skilled person prefers continuous processes to discontinuous processes.

Les liants utilisables pour la fabrication de produits pyrotechniques composites peuvent être des liants thermoplastiques ou des liants thermodurcissables.Binders usable for the manufacture of composite pyrotechnics can be thermoplastic binders or binders thermosetting.

Les liants thermoplastiques présentent l'intérêt de se prêter relativement facilement à une mise en oeuvre en continu grâce au fait qu'ils se ramollissent par élévation de la température. Ainsi la demande de brevet français FR-A-2 723 086 décrit un procédé de fabrication en continu et sans solvant de produits pyrotechniques composites à base de liants de type thermoplastique. Néanmoins les liants de type thermoplastique présentent l'inconvénient de conduire à des produits qui ont une mauvaise tenue en température en raison même du ramollissement du liant lorsqu'il y a élévation de la température. Or pour certaines applications, comme par exemple les armes à grande cadence de tir, l'homme de métier a besoin de produits pyrotechniques présentant une bonne tenue en température.Thermoplastic binders have the advantage of relatively easily lend themselves to implementation continuously due to the fact that they soften by temperature rise. So the patent application French FR-A-2 723 086 describes a manufacturing process continuous and solvent-free of pyrotechnic products composites based on thermoplastic type binders. However, thermoplastic type binders have the disadvantage of leading to products that have a poor temperature resistance due to the very softening of the binder when the temperature. However for certain applications, such as example weapons with a high rate of fire, the man of profession needs pyrotechnic products presenting good temperature resistance.

De ce point de vue les produits pyrotechniques à liant thermodurcissable offrent l'avantage de présenter une bonne tenue en température.From this point of view the pyrotechnic products to thermosetting binder offer the advantage of presenting good temperature resistance.

Mais, en raison même du fait que leur liant se durcit de manière irréversible à chaud par réticulation, ces produits présentent l'inconvénient de ne pas bien se prêter aux procédés continus.But, due to the very fact that their binder is irreversibly hardens when cross-linked, these products have the disadvantage of not being well lend to continuous processes.

Ces produits sont donc souvent mis en oeuvre au moyen de procédés discontinus. Ainsi le brevet US-A-4 128 441 décrit un procédé de fabrication discontinue par "coulée" de blocs de propergols. Ce procédé convient bien pour fabriquer des gros chargements pour moteurs de fusée, mais ne convient pas pour fabriquer industriellement en séries de petits objets.These products are therefore often used in using batch processes. So the patent US-A-4 128 441 describes a manufacturing process discontinuous by "pouring" of propellant blocks. This process is well suited for making large rocket engine loads but not suitable to manufacture industrially in series of small objects.

Le brevet US-A- 4,405,534 décrit quant à lui un procédé de fabrication d'explosifs composites par compression à froid de granulés d'explosifs enrobés par un film en polyuréthanne rendu plastique grâce à la présence de plastifiants. Ce procédé, hormis le fait qu'il soit discontinu, présente l'inconvénient supplémentaire de nécessiter la présence d'une forte teneur en plastifiant ce qui n'est pas toujours favorable au plan énergétique.US-A-4,405,534 describes a process for manufacturing composite explosives by cold compression of granules of explosives coated with a polyurethane film made plastic thanks to the presence of plasticizers. This process, apart from the fact that it is discontinuous, has the disadvantage additional to require the presence of a strong plasticizer content which is not always favorable to the energy plan.

Il a été proposé par la demande WO94/05607 un procédé semi-continu de fabrication avec solvant pour de tels produits, mais la nécessité d'avoir recours à un solvant qu'il faut ensuite éliminer limite l'intérêt de ce procédé.It was proposed by application WO94 / 05607 a semi-continuous solvent manufacturing process for such products, but the need to use a solvent which must then be removed limits the interest of this process.

Lorsque l'homme de métier veut mettre en oeuvre avec des liants thermodurcissables un procédé continu sans solvant il est confronté au problème de la courte "vie de pot" de ces compositions qui fait qu'après mélange des ingrédients de la composition, il ne dispose que de très peu de temps pour effectuer la mise en forme géométrique du produit avant que la réticulation du liant ne rende impossible tout travail mécanique de la pâte contenant les différents ingrédients.When the skilled person wants to implement with thermosetting binders a continuous process solvent-free it faces the problem of short "pot life" of these compositions which means that after mixture of the ingredients of the composition, it does have only a very short time to perform the shaping geometry of the product before the crosslinking of the binder does not make any mechanical work of the dough containing the different ingredients.

Il a bien été proposé d'allonger la "vie de pot" en retardant la réticulation finale par exemple par addition fractionnée de l'agent réticulant comme décrit dans le brevet US-A-4,657,607 ou encore en utilisant un double système de liants dont un des systèmes n'est réticulable que par un apport énergétique différent de la chaleur comme décrit dans la demande de brevet EP-A-0 367 445.It has been proposed to extend the "pot life" by delaying final crosslinking for example by fractional addition of the crosslinking agent as described in US-A-4,657,607 or using a double system of binders of which one of the systems is crosslinkable only by a different energy supply than heat as described in the patent application EP-A-0 367 445.

Néanmoins les possibilités d'application de ces techniques sont limitées et l'homme de métier ne dispose pas d'un procédé général de fabrication en continu et sans solvant de produits pyrotechniques composites à liant thermodurcissable. Nevertheless the possibilities of application of these techniques are limited and the skilled person does not have not a general continuous manufacturing process and solvent-free composite pyrotechnic products to thermosetting binder.

L'objet de la présente invention est précisément de proposer un tel procédé ainsi qu'une installation industrielle permettant la mise en oeuvre de ce procédé.The object of the present invention is precisely to propose such a process as well as an installation industrial allowing the implementation of this process.

L'invention concerne donc un procédé continu de fabrication sans solvant de produits pyrotechniques composites terminés dont les constituants de départ comprennent notamment un liant liquide qui est réticulable à une température supérieure à 40°C et au moins une charge énergétique oxydante solide, ledit procédé consistant notamment :

  • i) à mélanger les constituants de départ des dits produits de manière à obtenir une pâte composite homogène de viscosité suffisante pour pouvoir conserver des cotes géométriques stables,
  • ii) à mettre la pâte ainsi obtenue sous forme de produits intermédiaires ayant les cotes géométriques des produits terminés,
  • iii) à figer la forme et la composition des produits intermédiaires ainsi obtenus par réticulation du liant,
  • et étant caractérisé en ce que :
  • iv) ledit liant liquide de départ est d'abord mélangé à une charge épaississante solide sous forme pulvérulente de manière à obtenir un pré-mélange de consistance graisseuse qui est ensuite mélangé aux dites charges énergétiques,
  • v) les opérations de mélange et de mise en forme sont conduites à une température inférieure à 40°C.
  • The invention therefore relates to a continuous process for the manufacture without solvent of finished composite pyrotechnic products, the starting constituents of which comprise in particular a liquid binder which is crosslinkable at a temperature above 40 ° C. and at least one solid oxidizing energy charge, said process consisting especially :
  • i) mixing the starting constituents of said products so as to obtain a homogeneous composite paste of sufficient viscosity to be able to maintain stable geometric dimensions,
  • ii) putting the dough thus obtained in the form of intermediate products having the geometric dimensions of the finished products,
  • iii) freezing the form and composition of the intermediate products thus obtained by crosslinking the binder,
  • and being characterized in that:
  • iv) said starting liquid binder is first mixed with a solid thickening filler in pulverulent form so as to obtain a pre-mixture of greasy consistency which is then mixed with said energy charges,
  • v) the mixing and shaping operations are carried out at a temperature below 40 ° C.
  • Par rapport aux procédés connus de l'art antérieur, l'originalité majeure du procédé selon l'invention réside dans le fait qu'à l'exception de la phase finale au cours de laquelle la structure et la composition des produits intermédiaires sont figées par réticulation, les différentes opérations sont conduites à une température à laquelle le liant est, au plan chimique, quasiment non évolutif. Ainsi la formulation de la composition des produits est parfaitement reproductible dans la mesure où elle est intégralement effectuée en début de procédé sans nécessiter aucun ajustement ultérieur. L'homme de métier n'est confronté à aucune condition de "vie de pot" et les produits intermédiaires dont les cotes géométriques seraient imparfaites peuvent être recyclés dans la fabrication.Compared to the known methods of the prior art, the major originality of the process according to the invention lies in the fact that with the exception of the final phase during which the structure and composition of intermediate products are fixed by crosslinking, the different operations are carried out at a temperature at which the binder is, chemically, almost non-scalable. So the formulation of the product composition is perfectly reproducible insofar as it is fully carried out in start of the process without requiring any adjustment ulterior. The skilled person is not confronted with any condition of "pot life" and intermediate products whose geometric dimensions are imperfect can be recycled in manufacturing.

    Il faut enfin observer que grâce à l'emploi de charges épaississantes solides qui donnent au liant liquide non évolutif une tenue mécanique suffisante, aucun plastifiant n'est nécessaire dans le cadre du présent procédé qui permet ainsi d'obtenir des produits pyrotechniques de très hautes performances.Finally, it should be noted that thanks to the use of solid thickening fillers which give the binder non-evolving liquid sufficient mechanical strength, no plasticizer is required for the present process which thus makes it possible to obtain products very high performance pyrotechnics.

    On peut également dire que contrairement aux procédés antérieurs qui utilisent un liant thermodurcissable évolutif en cours de procédé dont on cherche à abaisser la viscosité par l'emploi d'un solvant et/ou d'un plastifiant, le procédé selon l'invention utilise un liant thermodurcissable liquide non évolutif en cours de procédé dont on élève la viscosité apparente par emploi de charges épaississantes.We can also say that unlike previous processes which use a binder thermosetting scalable during the process of which seeks to lower viscosity by using a solvent and / or a plasticizer, the process according to the invention uses a liquid thermosetting binder non-evolving during the process of which the apparent viscosity by use of fillers thickeners.

    Selon une première variante préférée de l'invention ladite charge épaississante solide est constituée par un matériau poreux dont la granulométrie est comprise entre 0,1 et 10 µm (microns) et dont la surface spécifique est comprise entre 60 et 500 m2/g.According to a first preferred variant of the invention, said solid thickening filler consists of a porous material whose particle size is between 0.1 and 10 μm (microns) and whose specific surface is between 60 and 500 m 2 / g .

    Avantageusement ce matériau possédera également des propriétés modificatrices de combustion et sera choisi dans le groupe constitué par le noir de carbone, la silice colloïdale, l'alumine, l'oxyde de titane ou le polynorbornène.Advantageously, this material will also have combustion modifying properties and will be chosen in the group consisting of carbon black, the colloidal silica, alumina, titanium oxide or polynorbornene.

    Selon cette première variante le rapport pondéral entre ladite charge épaississante et ledit liant réticulable est compris entre 0,05 et 0,25.According to this first variant, the weight ratio between said thickening filler and said binder crosslinkable is between 0.05 and 0.25.

    Selon une seconde variante préférée de l'invention ladite charge épaississante solide est constituée par un polymère thermoplastique à motifs hydrocarbonés pouvant comporter, en plus des atomes de carbone et d'hydrogène, des atomes d'oxygène et d'azote et dont la masse moléculaire moyenne en poids est comprise entre 3x105 et 3x106.According to a second preferred variant of the invention, said solid thickening filler is constituted by a thermoplastic polymer with hydrocarbon units which may contain, in addition to carbon and hydrogen atoms, oxygen and nitrogen atoms and whose molecular mass weight average is between 3x10 5 and 3x10 6 .

    Un premier groupe de polymères thermoplastiques utilisables comme charge épaississante solide dans le cadre de la présente invention est ainsi constitué par les copolymères styrène/butadiène/styrène, styrène/isoprène/styrène, styrène/éthylène/butylène/styrène et styrène/éthylène/propylène.A first group of thermoplastic polymers usable as solid thickening filler in the framework of the present invention is thus constituted by styrene / butadiene / styrene, styrene / isoprene / styrene copolymers, styrene / ethylene / butylene / styrene and styrene / ethylene / propylene.

    Un second groupe de polymères thermoplastiques utilisables comme charges épaississantes solides dans le cadre de la présente invention est constitué par les polyuréthannes à motifs polyéthers et polycarbonates et par les copolymères blocs polyéthers/polyamides.A second group of thermoplastic polymers usable as solid thickening fillers in the framework of the present invention is constituted by the polyurethanes with polyether and polycarbonate patterns and by polyether / polyamide block copolymers.

    Selon cette seconde variante le rapport pondéral entre ladite charge épaississante et ledit liant réticulable est compris entre 10:90 et 50:50.According to this second variant, the weight ratio between said thickening filler and said binder crosslinkable is between 10:90 and 50:50.

    En plus des charges énergétiques oxydantes solides on pourra également incorporer au pré-mélange, constitué par le liant liquide et lesdites charges épaississantes, au moins une charge énergétique réductrice solide comme, par exemple, de l'aluminium ou du bore en poudre.In addition to solid oxidizing energy charges we can also incorporate into the premix, consisting by the liquid binder and said thickening fillers, at least one solid reducing energy charge like, for example, aluminum or boron powder.

    Ce n'est que lorsque les opérations de mélange et de mise en forme des produits intermédiaires sont terminées et sont jugées satisfaisantes que l'on fait évoluer le liant en provoquant sa réticulation par chauffage à une température supérieure à 40°C de manière à obtenir des produits terminés réticulés.Only when the mixing and form of intermediate products are completed and are deemed satisfactory that we do evolve the binder by causing it to crosslink by heating at a temperature above 40 ° C so to obtain finished crosslinked products.

    Le procédé selon l'invention permet ainsi d'obtenir en continu, sans contrainte de temps liée à des questions de "vie de pot" et sans emploi de solvants ou de plastifiants indésirables au plan énergétique, des produits pyrotechniques composites à liant réticulé. Ces produits trouvent leurs applications préférentielles comme poudres propulsives en brins ou en sticks pour les munitions destinées aux armes à tube, comme blocs de propergols pour les moteurs de roquettes et de fusées, comme chargements explosifs pour les munitions explosives ou encore comme chargements pyrotechniques pour les générateurs de gaz destinés aussi bien aux applications militaires qu'aux applications civiles comme la sécurité automobile. The method according to the invention thus makes it possible to obtain continuously, without time constraints linked to "pot life" issues and no use of solvents or energy-unwanted plasticizers, Composite pyrotechnic products with crosslinked binder. These products find their preferred applications as propellant powders in strands or in sticks for ammunition intended for the weapons with tube, like blocks of propellants for rocket and rocket engines, as explosive charges for ammunition explosives or as pyrotechnic charges for gas generators intended for both military applications than civil applications like automotive safety.

    L'invention concerne également une installation convenant particulièrement bien à la mise en oeuvre du procédé selon l'invention.The invention also relates to an installation particularly suitable for the implementation of method according to the invention.

    Cette installation est caractérisée en ce qu'elle comprend dans le sens de progression de la matière :

  • i) un laminoir à cisaillement constitué par deux rouleaux cylindriques de longueur identique portant des rainures hélicoïdales et dont les axes sont parallèles et situés dans un même plan horizontal en étant espacés de manière à laisser subsister une fente entre les deux rouleaux qui tournent en sens contraire l'un de l'autre,
  • ii) une pompe volumétrique qui amène à l'extrémité, d'entrée de matière du laminoir le pré-mélange constitué par le liant liquide et la charge épaississante,
  • iii) au moins une trémie doseuse déversant, entre l'extrémité d'entrée de matière et l'extrémité de sortie de matière du laminoir, les charges énergétiques solides sur les rouleaux de ce dernier,
  • iv) un dispositif de granulation de la pâte homogène ainsi constituée qui est situé à l'extrémité de sortie du laminoir,
  • v) une extrudeuse dans laquelle sont repris les granulés provenant du dispositif de granulation,
  • vi) un dispositif de découpage en produits intermédiaires des joncs extrudés sortant de l'extrudeuse,
  • vii) un tapis roulant qui assure le transport et le passage dans un four thermique des produits intermédiaires ainsi découpés.
  • This installation is characterized in that it comprises, in the direction of progression of the material:
  • i) a shear rolling mill consisting of two cylindrical rollers of identical length carrying helical grooves and whose axes are parallel and located in the same horizontal plane being spaced so as to leave a gap between the two rollers which rotate in opposite directions one of the other,
  • ii) a positive displacement pump which brings the premix consisting of the liquid binder and the thickening charge to the end of the material inlet of the rolling mill
  • iii) at least one dosing hopper pouring, between the material inlet end and the material outlet end of the rolling mill, the solid energy charges on the rollers of the latter,
  • iv) a device for granulating the homogeneous dough thus formed which is situated at the outlet end of the rolling mill,
  • v) an extruder in which the granules from the granulation device are taken up,
  • vi) a device for cutting into intermediate products the extruded rods leaving the extruder,
  • vii) a conveyor belt which ensures the transport and the passage through a thermal oven of the intermediate products thus cut.
  • On donne ci-après une description détaillée de la mise en oeuvre préférée du procédé selon l'invention en se référant à la figure 1 qui représente, de manière schématique, l'installation préférée présentée ci-dessus. La figure 2 représente, pour des raisons de clarté, une vue de dessus simplifiée du laminoir à cisaillement utilisé.A detailed description of the preferred implementation of the method according to the invention in referring to Figure 1 which shows, so schematic, the preferred installation presented above. Figure 2 shows, for reasons of clarity, a simplified top view of the rolling mill shear used.

    L'invention consiste donc à mélanger, à température ambiante les constituants de départ d'une composition pyrotechnique composite réticulable jusqu'à obtention d'une pâte composite homogène présentant une viscosité suffisante pour pouvoir, toujours à température ambiante, être mise sous forme de produits intermédiaires présentant déjà, de manière stable, la forme et les dimensions finales du produit terminé que l'on veut obtenir. La forme et la composition de ces produits intermédiaires sont alors figés par réticulation à chaud de manière à obtenir les produits terminés voulus.The invention therefore consists in mixing, at temperature ambient the starting constituents of a composition composite pyrotechnic crosslinkable until obtained a homogeneous composite paste with a viscosity sufficient to be able, always at temperature ambient, be in the form of products intermediaries who already have a stable shape and final dimensions of the finished product that we want to get. The form and composition of these intermediate products are then frozen by hot crosslinking so as to obtain the products desired completions.

    Pour ce faire on commence, comme représenté à la figure 1 par fabriquer dans un mélangeur à bras multiples 1 un pré-mélange 2 constitué principalement par le liant 3 thermodurcissable à l'état liquide et par des charges solides épaississantes 4. To do this we start, as shown in figure 1 by manufacturing in an arm mixer multiples 1 a premix 2 consisting mainly by the binder 3 thermosetting in the liquid state and by thickening solid fillers 4.

    Il est impératif dans le cadre de la présente invention que le liant thermodurcissable soit liquide à température ambiante et que sa réticulation ne puisse commencer qu'à une température supérieure à 40°C de manière à être certain que, tant que l'on restera à une température ambiante inférieure à 40°C, ce liant demeurera non évolutif au plan chimique.It is imperative in the context of this invention that the thermosetting binder is liquid to room temperature and that its crosslinking cannot start only at a temperature above 40 ° C so as to be certain that as long as we stay at one ambient temperature below 40 ° C, this binder will remain chemically non-evolving.

    On entend dans la présente description par "liant liquide" l'ensemble des constituants réactifs liquides qui, après réticulation, donneront le liant réticulé solide.In the present description is meant by "binder liquid "all of the liquid reactive constituents which, after crosslinking, will give the crosslinked binder solid.

    La réaction de réticulation peut être du type réaction de polycondensation, auquel cas les liants seront notamment du type polyuréthannes, polyesters ou polyamides.The crosslinking reaction can be of the type polycondensation reaction, in which case the binders will in particular be of the polyurethane, polyesters or polyamides.

    La réaction de réticulation peut être du type réaction de polyaddition avec ouverture d'insaturations éthyléniques, auquel cas les liants seront notamment du type polyalkylènes, polyacrylates ou polyméthacrylates. Dans ce dernier cas la composition devra contenir des catalyseurs de réticulation, comme par exemple des peroxydes.The crosslinking reaction can be of the type polyaddition reaction with opening of unsaturations ethylenic, in which case the binders will in particular be polyalkylenes, polyacrylates or polymethacrylates. In the latter case, the composition must contain crosslinking catalysts, such as for example peroxides.

    Comme il a déjà été indiqué plus haut dans la description, lesdites charges épaississantes peuvent être constituées par des matériaux solides poreux de faible granulométrie. Dans ce cas on utilisera avantageusement comme charges épaississantes certains additifs employés habituellement comme modificateurs de combustion comme le noir de carbone ; le procédé selon l'invention offre dans ce cas l'avantage de permettre l'obtention en continu de compositions pyrotechniques déjà connues mais qui n'étaient accessibles que par des procédés discontinus. As already indicated above in the description, said thickening fillers can be made of porous solid materials of small particle size. In this case we will use advantageously as thickening fillers certain additives usually used as modifiers of combustion like carbon black; the process according to the invention in this case offers the advantage of allowing continuously obtaining pyrotechnic compositions already known but which were only accessible by discontinuous processes.

    Les dites charges épaississantes peuvent également être constituées par des polymères thermoplastiques solides de haute masse moléculaire de manière à obtenir un produit final dont le liant est constitué par un alliage de polymères thermoplastiques et de polymères réticulés. Ce type d'alliages permet l'obtention de produits composites présentant des caractéristiques mécaniques particulièrement élevées.Said thickening fillers can also be made up of thermoplastic polymers high molecular weight solids so as to get a final product whose binder consists of a alloy of thermoplastic polymers and polymers cross-linked. This type of alloy allows obtaining composite products with characteristics particularly high mechanical properties.

    Le pré-mélange 2 ainsi constitué pourra également contenir d'autres additifs de la composition finale. Il devra avoir la consistance d'une graisse épaisse de manière à pouvoir être transporté en continu au moyen d'une pompe volumétrique tout en adhérant, sans couler, à la surface d'un cylindre tournant avec une vitesse angulaire de quelques dizaines de tours par minute.The premix 2 thus formed may also contain other additives of the final composition. he should have the consistency of a thick fat of so that it can be transported continuously using a positive displacement pump while adhering, without sinking, on the surface of a cylinder rotating with a speed angular of a few tens of revolutions per minute.

    Ce pré-mélange est donc transporté au moyen d'une pompe de circulation 34, par exemple une pompe à engrenage, dans une réserve 35 munie d'un couvercle-piston 36. Le pré-mélange est alors repris par une pompe doseuse 5 à engrenage pour être conduit, dans un appareillage où seront effectuées les opérations de mélange avec les charges énergétiques solides et de mise en forme de la pâte composite ainsi obtenue sous forme de produits intermédiaires possédant déjà les cotes géométriques des produits terminés. Ces deux opérations peuvent être effectuées dans un appareillage unique comme par exemple une extrudeuse bi-vis dont la tête d'extrusion sera associée à un dispositif de découpage. Mais, préférentiellement, ces deux opérations seront effectuées par deux appareillages distincts placés l'un à la suite de l'autre. This premix is therefore transported by means of a circulation pump 34, for example a gear, in a reserve 35 provided with a piston cover 36. The premix is then taken up by a pump doser 5 with gear to be driven, in a equipment where the operations of mixing with solid energy charges and setting in the form of the composite paste thus obtained in the form of intermediate products that already have the ratings geometries of finished products. These two operations can be carried out in a single device like for example a twin screw extruder whose head extrusion will be associated with a cutting device. But, preferentially, these two operations will be carried out by two separate devices, one placed following each other.

    Le pré-mélange 2 est transporté par la pompe 5 dans un mélangeur qui peut être un mélangeur traditionnel comme un co-malaxeur "BUSS" mais qui, préférentiellement et comme représenté à la figure 1, est un laminoir à cisaillement 6 constitué par deux rouleaux cylindriques 7 et 8 de longueur identique et portant des rainures hélicoïdales. Les axes 9 et 10 de ces deux cylindres sont parallèles et situés dans un même plan horizontal en étant espacés de manière à laisser une fente 11 entre les deux rouleaux. Les axes 9 et 10 sont supportés par des blocs supports 12 et 13, le bloc 12 étant un bloc moteur entraínant en rotation les deux cylindres 7 et 8 qui tournent en sens contraire l'un de l'autre à des vitesses différentes. Un tel laminoir à cisaillement est connu de l'homme de métier et décrit dans de nombreuses publications, par exemple dans la demande de brevet FR-A-2 723 086 déjà citée.The premix 2 is transported by the pump 5 in a mixer which can be a traditional mixer as a "BUSS" co-kneader but which, preferably and as shown in Figure 1, is a rolling mill shear 6 consisting of two cylindrical rollers 7 and 8 of identical length and having grooves helical. Axes 9 and 10 of these two cylinders are parallel and located in the same horizontal plane being spaced so as to leave a slot 11 between the two rollers. Axes 9 and 10 are supported by support blocks 12 and 13, block 12 being a block engine driving in rotation the two cylinders 7 and 8 which rotate in opposite directions to each other at different speeds. Such a shear rolling mill is known to those skilled in the art and described in numerous publications, for example in the patent application FR-A-2 723 086 already cited.

    La pompe 5 amène ainsi le pré-mélange 2 sur le rouleau 7 qui tourne le plus vite, le pré-mélange formant sur ce rouleau une feuille qui enrobe ce dernier. Le pré-mélange est amené à l'extrémité 14 d'entrée de matière du laminoir 6.The pump 5 thus brings the premix 2 to the roller 7 which turns the fastest, the premix forming on this roll a sheet which coats this latest. The premix is brought to the end 14 material inlet of the rolling mill 6.

    Au moins une trémie doseuse 16 déverse, entre l'extrémité d'entrée de matière 14 et l'extrémité de sortie de matière 15 du laminoir 6, les charges énergétiques solides 17 sur la feuille de pré-mélange enrobant le rouleau 7. Ces charges énergétiques solides sont alors intimement mélangées au pré-mélange 2 grâce à l'action de cisaillement du laminoir 6 de manière à former sur le rouleau 7 une feuille de pâte composite homogène qui présente déjà une viscosité suffisante pour pouvoir conserver des cotes géométriques stables. At least one dosing hopper 16 pours between the material inlet end 14 and the end of material outlet 15 from rolling mill 6, the loads solid energy 17 on the premix sheet coating the roller 7. These solid energy charges are then intimately mixed with premix 2 thanks to the shearing action of the rolling mill 6 so as to form on roll 7 a sheet of composite dough homogeneous which already has sufficient viscosity to ability to maintain stable geometric dimensions.

    Les charges énergétiques solides seront principalement constituées par les charges oxydantes de la composition qui peuvent être des charges minérales comme par exemple le perchlorate d'ammonium, le perchlorate de potassium ou le nitrate d'ammonium, ou des charges organiques et notamment des nitramines comme l'hexogène, l'octogène, la nitroguanidine ou l'hexanitro-hexaazaisowurtzitane.Solid energy charges will mainly constituted by the oxidizing charges of the composition which can be mineral fillers such as ammonium perchlorate, potassium perchlorate or ammonium nitrate, or organic fillers and in particular nitramines such as hexogen, octogen, nitroguanidine or hexanitro-hexaazaisowurtzitane.

    A côté des charges oxydantes solides, il pourra y avoir des charges énergétiques réductrices solides comme l'aluminium ou le bore et même des additifs solides qui n'auraient pas été incorporés au pré-mélange 2.Besides solid oxidizing charges, there may have solid reducing energy charges like aluminum or boron and even solid additives which would not have been incorporated into premix 2.

    Dans ce cas les différentes charges pourront être apportées soit en mélange par une trémie unique, soit séparément par une succession de trémies.In this case the different charges may be brought either in mixture by a single hopper, or separately by a succession of hoppers.

    La feuille de pâte composite ainsi obtenue est récupérée sous forme de granulés 19 par un dispositif de granulation 18 situé à l'extrémité de sortie 15 du laminoir 6. Préférentiellement comme représenté sur la figure 1, les extrémités de sortie des rouleaux 7 et 8 ne sont pas rainurées mais sont lisses.The composite dough sheet thus obtained is recovered in the form of granules 19 by a device for granulation 18 located at the outlet end 15 of the rolling mill 6. Preferably as shown in the Figure 1, the outlet ends of rollers 7 and 8 are not grooved but are smooth.

    Les granulés 19 sont alors repris en continu dans une extrudeuse 20, par exemple une extrudeuse à deux vis, munie d'une tête d'extrusion 21 pour être profilés en joncs 23 entraínés par un tapis roulant 25.The granules 19 are then taken up continuously in an extruder 20, for example a twin extruder screw, fitted with an extrusion head 21 to be profiled in rods 23 driven by a conveyor belt 25.

    Un dispositif de découpage 22 découpe les joncs profilés 23 sortant de la tête d'extrusion 21 en produits intermédiaires 24 possédant déjà les cotes définitives des produits terminés. Le dispositif de découpage 22 a un déplacement asservi à la vitesse de progression du tapis 25 sur lequel reposent les joncs 23.A cutting device 22 cuts the rods profiles 23 leaving the extrusion head 21 in 24 intermediate products already with the ratings final of finished products. The device cutting 22 has a movement controlled by the speed of progression of the mat 25 on which the rods rest 23.

    Il est à observer que jusqu'à cette opération de découpage, aucun chauffage de la composition pyrotechnique n'a eu lieu, l'extrudeuse 20 pouvant même être refroidie. Le liant de la composition pyrotechnique n'a donc pas évolué et les produits intermédiaires 24 peuvent, s'il sont jugés non satisfaisants, être recyclés dans le circuit de fabrication.It should be noted that until this operation of cutting, no heating of the composition pyrotechnic did not take place, the extruder 20 being able even be cooled. The binder of the pyrotechnic composition has therefore not changed and the intermediate products 24 may, if they are found to be unsatisfactory, be recycled in the manufacturing circuit.

    Ces produits intermédiaires 24, lorsqu'ils sont jugés satisfaisants, sont alors repris en continu par le tapis roulant 25 qui assure leur transport et leur passage dans un four thermique 26 où leur forme géométrique et leur composition sont définitivement figées par réticulation de leur liant, à une température supérieure à 40°C. Avec les compositions usuelles connues de l'homme de métier la réticulation sera souvent effectuée à une température voisine de 120°C pendant environ 5 minutes.These intermediate products 24, when they are deemed satisfactory, are then taken up continuously by the conveyor belt 25 which ensures their transport and passage through a thermal oven 26 where their shape geometric and their composition are definitely frozen by crosslinking their binder, at a temperature higher than 40 ° C. With the usual compositions known to those skilled in the art, the crosslinking will be often performed at a temperature close to 120 ° C for about 5 minutes.

    Les produits terminés 27 sortant du four 26 peuvent alors être conditionnés dans leur emballage 28.The finished products 27 leaving the oven 26 can then be packaged in their packaging 28.

    Le procédé selon l'invention permet ainsi de fabriquer en séries continues des produits pyrotechniques composites à liant réticulé, et notamment des produits de petites dimensions, sans contrainte de "vie de pot", sans solvant et sans plastifiant indésirable.The method according to the invention thus makes it possible to manufacture in continuous series of products composite pyrotechnics with crosslinked binder, and in particular products of small dimensions, without constraint of "pot life", solvent-free and plasticizer-free undesirable.

    Les exemples qui suivent illustrent certaines possibilités de mise en oeuvre de l'invention.The following examples illustrate some possibilities of implementing the invention.

    Dans ces exemples, on a utilisé les abréviations suivantes :

    PBHT =
    liant à base de polybutadiène à terminaisons hydroxyles réticulé par un polyisocyanate.
    PAG =
    liant à base de polyazoture de glycidyle à terminaisons hydroxyles réticulé par un polyisocyanate
    S.B.S. =
    copolymère styrène/butadiène/styrènes
    S.I.S. =
    copolymère styrène/isoprène/styrène
    PE-PA =
    copolymère bloc polyéther/polyamide 60/40
    RDX =
    hexogène
    PA =
    perchlorate d'ammonium
    In these examples, the following abbreviations have been used:
    PBHT =
    binder based on polybutadiene with hydroxyl endings crosslinked by a polyisocyanate.
    PAG =
    binder based on glycidyl polyazide with hydroxyl endings crosslinked by a polyisocyanate
    SBS =
    styrene / butadiene / styrene copolymer
    SIS =
    styrene / isoprene / styrene copolymer
    PE-PA =
    polyether / polyamide block copolymer 60/40
    RDX =
    hexogenic
    PA =
    ammonium perchlorate

    Tous les pourcentages indiqués dans les exemples sont des pourcentages en masse, les pourcentages indiqués pour le liant incluant les additifs éventuels utilisés.All the percentages given in the examples are percentages by mass, the percentages indicated for the binder including any additives used.

    Exemples 1 à 3Examples 1 to 3

    On a fabriqué par le procédé continu selon l'invention des brins de poudre cylindriques multiperforés à 7 trous et à 19 trous à partir des trois compositions suivantes : Composition 1 Composition 2 Composition 3 liant PBHT : 9% PBHT : 10,5% PAG : 13% charge épaississante S.I.S 6% PE-PA : 4,5% PE-PA : 7% charge oxydante RDX 85% RDX 85% RDX 80% granulométrie de la charge oxydante 100 µm 150 µm 80 µm charge réductrice 0 0 0 The 7-hole and 19-hole multi-perforated cylindrical powder strands were produced by the continuous process according to the invention from the following three compositions: Composition 1 Composition 2 Composition 3 binder PBHT: 9% PBHT: 10.5% PAG: 13% thickening filler SIS 6% PE-PA: 4.5% PE-PA: 7% oxidizing charge RDX 85% RDX 85% RDX 80% particle size of the oxidizing charge 100 µm 150 µm 80 µm reducing load 0 0 0

    Pour une température de matière de 35°C lors de l'extrusion, les géométries suivantes ont été obtenues : 7 trous 19 trous Composition 1 web (mm) 0,34 ± 0,01 1,48 ± 0,01       d (mm) 0,29 ± 0,005 0,40 ± 0,01 Composition 2 web (mm) 0,35 ± 0,01 1,51 ± 0,01       d (mm) 3,30 ± 0,005 0,40 ± 0,005 Composition 3 web (mm) 0,34 ± 0,01 1,49 ± 0,01       d (mm) 0,31 ± 0,005 0,39 ± 0,01 web = épaisseur à brûler
    d = diamètre des trous
    For a material temperature of 35 ° C during extrusion, the following geometries have been obtained: 7 holes 19 holes Composition 1 web (mm) 0.34 ± 0.01 1.48 ± 0.01 d (mm) 0.29 ± 0.005 0.40 ± 0.01 Composition 2 web (mm) 0.35 ± 0.01 1.51 ± 0.01 d (mm) 3.30 ± 0.005 0.40 ± 0.005 Composition 3 web (mm) 0.34 ± 0.01 1.49 ± 0.01 d (mm) 0.31 ± 0.005 0.39 ± 0.01 web = thickness to burn
    d = hole diameter

    Exemples 4 à 6Examples 4 to 6

    On a fabriqué par le procédé continu selon l'invention des blocs de propergols cylindriques à canal central pour moteurs de petits missiles à partir des trois compositions suivantes : Composition 4 Composition 5 Composition 6 liant PBHT : 10% PBHT : 12,2% PBHT : 10,5% charge épaississante polynorbornène = 4% noir de carbone alumine poreuse (150m 2 /g) :1,8% (80m 2 /g:3,5%) charge oxydante PA : 85% PA / 85% PA : 85% charge réductrice Al : 1% Al : 1% Al : 1% La filière était une filière cylindrique de diamètre extérieur 30mm et de diamètre intérieur 14mm.Blocks of central channel cylindrical propellants for small missile engines were manufactured by the continuous process according to the following compositions: Composition 4 Composition 5 Composition 6 binder PBHT: 10% PBHT: 12.2% PBHT: 10.5% thickening filler polynorbornene = 4% carbon black porous alumina (150m 2 / g): 1.8% (80m 2 / g: 3.5%) oxidizing charge PA: 85% PA / 85% PA: 85% reducing load Al: 1% Al: 1% Al: 1% The die was a cylindrical die with an outside diameter of 30mm and an inside diameter of 14mm.

    Sur 10 mètres de propergol extrudé en continu pour chacune des compositions, les variations dimensionnelles obtenues après découpage et réticulation à chaud sont les suivantes : Exemple 4 Exemple 5 Exemple 6 diamètre extérieur en mm 30,5 ± 0,002 30,0 ± 0,02 29,9 ± 0,02 diamètre intérieur en mm 13,8 ± 0,003 13,9 ± 0,02 14,05 ± 0,02 longueur en mm 121 ± 0,1 120,5 ± 0,15 120,4 ± 0,1 On 10 meters of propellant extruded continuously for each of the compositions, the dimensional variations obtained after hot cutting and crosslinking are as follows: Example 4 Example 5 Example 6 outer diameter in mm 30.5 ± 0.002 30.0 ± 0.02 29.9 ± 0.02 inside diameter in mm 13.8 ± 0.003 13.9 ± 0.02 14.05 ± 0.02 length in mm 121 ± 0.1 120.5 ± 0.15 120.4 ± 0.1

    Exemple 7Example 7

    On a fabriqué par le procédé continu selon l'invention des bandes d'explosif composite d'épaisseur comprise entre 2 et 5mm à partir de la composition suivante :

    • liant PBHT   =   11%
    • charge épaississante = SIS   =   4%
    • charge oxydante : RDX (3µm et 90µm) =85%
    Strips of composite explosive with a thickness of between 2 and 5 mm were produced by the continuous process according to the invention from the following composition:
    • PBHT binder = 11%
    • thickening load = SIS = 4%
    • oxidizing charge: RDX (3 µ m and 90 µ m) = 85%

    On a extrudé en continu 10 mètres de bande de largeur 90mm avec des épaisseurs de 2,3 et 5mm. Après réticulation du liant la variation dimensionnelle des bandes était de : épaisseur d'extrusion 2 mm épaisseur d'extrusion 3 mm épaisseur d'extrusion 5 mm épaisseur en mm 1,98 ± 0,01 2,95 ± 0,015 4,99 ± 0,02 largeur en mm 89,5 ± 0,05 90,2 ± 0,06 89,8 ± 0,04 10 meters of 90mm wide strip with thicknesses of 2.3 and 5mm were continuously extruded. After crosslinking the binder, the dimensional variation of the bands was: extrusion thickness 2 mm extrusion thickness 3 mm extrusion thickness 5 mm thickness in mm 1.98 ± 0.01 2.95 ± 0.015 4.99 ± 0.02 width in mm 89.5 ± 0.05 90.2 ± 0.06 89.8 ± 0.04

    Exemple 8Example 8

    On a fabriqué par le procédé continu selon l'invention des blocs de propergols pour générateur pyrotechnique de gaz à partir de la composition suivante :

    • liant PBHT :   15,8%
    • charge épaississante = SBS :   9,2%
    • charge oxydante : PA (90µm, 15µm, 3µm) :   73%
    • charge réductrice : Al =   2%
    Blocks of propellants for a pyrotechnic gas generator were manufactured by the continuous process according to the invention from the following composition:
    • PBHT binder: 15.8%
    • thickening filler = SBS: 9.2%
    • oxidizing charge: PA (90 µ m, 15 µ m, 3 µ m): 73%
    • reducing load: Al = 2%

    Les blocs avaient la forme de cylindres pleins de dimensions :

    • diamètre : 30mm + 0,025mm
    • longueur : 90mm + 0,10mm
    The blocks were in the form of cylinders full of dimensions:
    • diameter: 30mm + 0.025mm
    • length: 90mm + 0.10mm

    Ces blocs ont été tirés au banc d'essai et ont donné les résultats suivants :

    • vitesse de combustion à 13 MPa = 25,3mm/s
    • exposant de pression   = 0,35
    These blocks were drawn on the test bench and gave the following results:
    • combustion speed at 13 MPa = 25.3mm / s
    • pressure exponent = 0.35

    Claims (11)

    1. Continuous process for the solventless manufacture of terminated composite pyrotechnic products of which the starting constituents comprise in particular a liquid binder which can be cross-linked at a temperature above 40°C and at least one solid oxidizing energetic charge, the process consisting in particular of:
      (i) mixing the starting constituents of the said products so as to obtain a homogeneous composite paste with sufficient viscosity to be able to preserve stable geometric dimensions,
      (ii) putting the paste thus obtained into the form of intermediate products having the geometric dimensions of the said terminated products.
      (iii) setting the form and composition of the intermediate products thus obtained by cross-linking the binder,
      characterized in that :
      (iv) the said starting liquid binder is first of all mixed with a solid thickening filler in powdered form so as to obtain a premix with a greasy consistency which is then mixed with the said energetic charges,
      (v) the mixing and forming operations are carried out at a temperature below 40°C.
    2. Process according to claim 1, characterized in that the said solid thickening filler consists of a porous material of which the particle size lies between 0.1 and 10µm and of which the specific area lies between 60 and 500 m2/g.
    3. Process according to claim 2 characterized in that the said material is chosen from the group consisting of carbon black, colloidal silica, alumina, titanium oxide and polynorbornene.
    4. Process according to claim 1, characterized in that the said solid thickening filler consists of a thermoplastic polymer with hydrocarbon units which can carry oxygen and nitrogen atoms of which the mean molecular mass by weight lies between 3×105 and 3×106.
    5. Process according to claim 4 characterized in that the said thickening filler is chosen from the group consisting of styrene/butadiene/styrene, styrene/isoprene/styrene, styrene/ethylene/butylene/styrene, styrene/ethylene/propylene copolymers.
    6. Process according to claim 4 characterized in that the said thickening filler is chosen from the group consisting of polyurethanes based on polyethers and polycarbonates and of polyether/polyamide block copolymers.
    7. Process according to claim 4 characterized in that the weight ratio between the said thickening filler and the said cross-linking binder lies between 10:90 and 50:50.
    8. Process according to claim 2 characterized in that the weight ratio between the said thickening filler and the said cross-linking binder lies between 0.05 and 0.25.
    9. Process according to claim 1, characterized in that in addition to the said solid oxidizing energetic charges, at least one solid reducing energetic charge is used.
    10. Process according to claim 9 characterized in that the said reducing energetic charge consists of powdered aluminium or boron.
    11. Installation for implementing the process according to any one of claims 1 to 10, characterized in that it comprises, in the direction of the progression of the material :
      (i) a shearing rolling mill (6) consisting of two grooved cylindrical rollers (7,8) with identical length carrying helical grooves and of which the axes are parallel and situated in the same horizontal plane while being spaced so as to leave a slit (11) between the two rollers which rotate in opposite directions to each other,
      (ii) a volumetric pump (5) which brings the premix (2) consisting of the liquid binder and the thickening filler to the material inlet end (14) of the rolling mill (6),
      (iii) at least one metering hopper (16) discharging, between the material inlet end (14) and the material outlet end of the rolling mill (6), solid energetic charges (17) onto the rollers of the latter,
      (iv) a granulating device (18) for the homogeneous paste thus constituted which is situated on the outlet end (15) of the rolling mill,
      (v) an extruder (20) in which granules coming from the granulating device are taken up,
      (vi) a device (22) for cutting the extruded beads (23) leaving the extruder into intermediate products (24),
      (vii) a conveyer belt (25) which ensures the transport and passage of the intermediate products thus cut into a heating oven (26).
    EP97401051A 1996-05-23 1997-05-12 Continuous process for the solventless production of pyrotechnical products having a thermosetting binder Expired - Lifetime EP0808813B1 (en)

    Applications Claiming Priority (2)

    Application Number Priority Date Filing Date Title
    FR9606397 1996-05-23
    FR9606397A FR2749008B1 (en) 1996-05-23 1996-05-23 CONTINUOUS PROCESS FOR THE SOLVENT-FREE MANUFACTURE OF THERMOSETTING COMPOSITE PYROTECHNICS

    Publications (2)

    Publication Number Publication Date
    EP0808813A1 EP0808813A1 (en) 1997-11-26
    EP0808813B1 true EP0808813B1 (en) 2001-08-22

    Family

    ID=9492385

    Family Applications (1)

    Application Number Title Priority Date Filing Date
    EP97401051A Expired - Lifetime EP0808813B1 (en) 1996-05-23 1997-05-12 Continuous process for the solventless production of pyrotechnical products having a thermosetting binder

    Country Status (8)

    Country Link
    US (1) US5831339A (en)
    EP (1) EP0808813B1 (en)
    JP (1) JP3826226B2 (en)
    CA (1) CA2204840C (en)
    DE (1) DE69706228T2 (en)
    FR (1) FR2749008B1 (en)
    IL (1) IL120670A (en)
    NO (1) NO307084B1 (en)

    Families Citing this family (7)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US6315930B1 (en) * 1999-09-24 2001-11-13 Autoliv Asp, Inc. Method for making a propellant having a relatively low burn rate exponent and high gas yield for use in a vehicle inflator
    US6736913B1 (en) * 2000-10-31 2004-05-18 Alliant Techsystems Inc. Method for processing explosives containing 2,4,6,8,10,12-hexanitro-2,4,6,8,10,12-hexaazatetracyclo [5.5.0.05,903,11]-dodecan (CL-20) with naphthenic and paraffinic oils
    GB0205559D0 (en) * 2002-03-11 2002-04-24 Bae Systems Plc Improvements in and relating to the filling of explosive ordnance
    RU2218316C1 (en) * 2002-03-28 2003-12-10 Федеральный центр двойных технологий "Союз" Method for production of charge of composite solid propellant
    JP2006044975A (en) * 2004-08-03 2006-02-16 Ihi Aerospace Co Ltd Solid propellant
    US7854811B1 (en) 2009-07-11 2010-12-21 Kemzecur, Inc. Mouldable plastic explosives and inert simulants for mouldable plastic explosives
    CN109704892A (en) * 2019-03-03 2019-05-03 浏阳市浏河机械有限公司 Pyrotechnic composition mixed tide material prilling

    Family Cites Families (17)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    US2995432A (en) * 1958-08-04 1961-08-08 Phillips Petroleum Co Solid composite rubber base propellants containing reinforcing agent of resinous aldehyde condensate
    US4776993A (en) * 1974-05-14 1988-10-11 The United States Of America As Represented By The Secretary Of The Navy Extrusion method for obtaining high strength composite propellants
    US4177227A (en) * 1975-09-10 1979-12-04 The United States Of America As Represented By The Secretary Of The Air Force Low shear mixing process for the manufacture of solid propellants
    US4098627A (en) * 1976-12-15 1978-07-04 The United States Of America As Represented By The Secretary Of The Navy Solvolytic degradation of pyrotechnic materials containing crosslinked polymers
    DE3010052C2 (en) * 1980-03-15 1982-09-09 Friedrich-Ulf 8899 Rettenbach Deisenroth Process for the production of plastic-bound explosives
    US4375522A (en) * 1980-07-21 1983-03-01 The United States Of America As Represented By The Secretary Of The Navy Thixotropic restrictor, curable at room temperature, for use on solid propellant grains
    FR2577919B1 (en) * 1985-02-27 1987-02-20 Poudres & Explosifs Ste Nale PROCESS FOR THE MANUFACTURE WITHOUT SOLVENT OF COMPOSITE PYROTECHNIC PRODUCTS WITH THERMOSETTING BINDER AND PRODUCTS THUS OBTAINED, IN PARTICULAR COMPOSITE PROPULSIVE POWDERS
    US4726919A (en) * 1985-05-06 1988-02-23 Morton Thiokol, Inc. Method of preparing a non-feathering nitramine propellant
    US4650617A (en) * 1985-06-26 1987-03-17 Morton Thiokol Inc. Solvent-free preparation of gun propellant formulations
    US4889571A (en) * 1986-09-02 1989-12-26 Morton Thiokol, Inc. High-energy compositions having castable thermoplastic binders
    DE3635296C2 (en) * 1986-10-16 1995-12-21 Nitrochemie Gmbh Process for producing propellant powder
    GB8730153D0 (en) * 1987-12-24 1988-02-03 Univ Manchester Polymer compositions
    SE465572B (en) * 1989-06-21 1991-09-30 Nobel Kemi Ab SET AND DEVICE FOR PREPARING EXPLOSIVE SUBSTANCES
    EP0417912B1 (en) * 1989-08-25 1994-11-09 Idemitsu Petrochemical Company Limited Thermoplastic resin-based molding composition
    US4994212A (en) * 1990-05-24 1991-02-19 Trw Vehicle Safety Systems Inc. Process for manufacturing a gas generating material
    US5486248A (en) * 1994-05-31 1996-01-23 Morton International, Inc. Extrudable gas generant for hybrid air bag inflation system
    FR2723086B1 (en) * 1994-07-29 1996-09-13 Poudres & Explosifs Ste Nale CONTINUOUS PROCESS FOR THE SOLVENT-FREE MANUFACTURE OF COMPOSITE PYROTECHNIC PRODUCTS

    Also Published As

    Publication number Publication date
    NO972318D0 (en) 1997-05-21
    FR2749008A1 (en) 1997-11-28
    NO307084B1 (en) 2000-02-07
    IL120670A (en) 2000-07-26
    DE69706228T2 (en) 2002-05-16
    IL120670A0 (en) 1997-08-14
    NO972318L (en) 1997-11-24
    EP0808813A1 (en) 1997-11-26
    US5831339A (en) 1998-11-03
    MX9703466A (en) 1997-11-29
    JPH1053484A (en) 1998-02-24
    CA2204840A1 (en) 1997-11-23
    JP3826226B2 (en) 2006-09-27
    FR2749008B1 (en) 1998-06-26
    DE69706228D1 (en) 2001-09-27
    CA2204840C (en) 2002-01-08

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