FR2894871A1 - DEVICE FOR SHAPING COMPACTABLE MATERIAL AND METHOD OF USING THE DEVICE - Google Patents

DEVICE FOR SHAPING COMPACTABLE MATERIAL AND METHOD OF USING THE DEVICE Download PDF

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Publication number
FR2894871A1
FR2894871A1 FR0512835A FR0512835A FR2894871A1 FR 2894871 A1 FR2894871 A1 FR 2894871A1 FR 0512835 A FR0512835 A FR 0512835A FR 0512835 A FR0512835 A FR 0512835A FR 2894871 A1 FR2894871 A1 FR 2894871A1
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France
Prior art keywords
shells
cylindrical
bore
conical
shaping
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Granted
Application number
FR0512835A
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French (fr)
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FR2894871B1 (en
Inventor
Stephane Vaudez
Laurent Paret
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Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
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Commissariat a lEnergie Atomique CEA
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Priority to FR0512835A priority Critical patent/FR2894871B1/en
Priority to PCT/EP2006/069671 priority patent/WO2007068723A1/en
Publication of FR2894871A1 publication Critical patent/FR2894871A1/en
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Publication of FR2894871B1 publication Critical patent/FR2894871B1/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02Compacting only
    • B22F3/03Press-moulding apparatus therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B30PRESSES
    • B30BPRESSES IN GENERAL
    • B30B11/00Presses specially adapted for forming shaped articles from material in particulate or plastic state, e.g. briquetting presses, tabletting presses
    • B30B11/007Presses specially adapted for forming shaped articles from material in particulate or plastic state, e.g. briquetting presses, tabletting presses using a plurality of pressing members working in different directions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B30PRESSES
    • B30BPRESSES IN GENERAL
    • B30B15/00Details of, or accessories for, presses; Auxiliary measures in connection with pressing
    • B30B15/02Dies; Inserts therefor; Mounting thereof; Moulds
    • B30B15/022Moulds for compacting material in powder, granular of pasta form
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/5158Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on actinide compounds
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/515Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/58Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02Compacting only
    • B22F3/03Press-moulding apparatus therefor
    • B22F2003/031Press-moulding apparatus therefor with punches moving in different directions in different planes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/02Compacting only
    • B22F3/03Press-moulding apparatus therefor
    • B22F2003/033Press-moulding apparatus therefor with multiple punches working in the same direction
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C21/00Apparatus or processes specially adapted to the manufacture of reactors or parts thereof
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C21/00Apparatus or processes specially adapted to the manufacture of reactors or parts thereof
    • G21C21/02Manufacture of fuel elements or breeder elements contained in non-active casings
    • G21C21/04Manufacture of fuel elements or breeder elements contained in non-active casings by vibrational compaction or tamping of fuel in the jacket

Abstract

L'invention concerne un dispositif (1) de mise en forme de matériau à support (4) à alésage conique d'axe (X'X), logeant deux coquilles coniques (3a, 3b) s'emboîtant dans ledit alésage et comportant un alésage cylindrique selon (X'X), apte à loger deux coquilles cylindriques (2a, 2b) s'emboîtant dans ledit alésage cylindrique (16, 17 ; 16', 17'), lesdites coquilles cylindriques (2a, 2b) une fois serrées comportant un alésage traversant cylindrique selon (X'X), , une cavité apte à recevoir un matériau compactable étant formée d'espaces respectivement ménagés dans les coquilles coniques et cylindriques (2a, 2b ; 3a, 3b) lorsque les coquilles cylindriques (2a, 2b) sont serrées dans l'alésage cylindrique, l'alésage traversant étant destiné à recevoir un piston (6) en pression sur ledit matériau, la forme de la tête du piston (6) et de la cavité déterminant la forme (7) du matériau compacté.The invention relates to a device (1) for forming a support material (4) with a tapered bore with an axis (X'X), housing two conical shells (3a, 3b) fitting into said bore and comprising a cylindrical bore according to (X'X), adapted to accommodate two cylindrical shells (2a, 2b) fitting into said cylindrical bore (16, 17; 16 ', 17'), said cylindrical shells (2a, 2b) once tightened comprising a cylindrical through bore according to (X'X), a cavity adapted to receive a compactable material being formed of spaces respectively formed in the conical and cylindrical shells (2a, 2b, 3a, 3b) when the cylindrical shells (2a, 2b) are clamped in the cylindrical bore, the through bore being adapted to receive a piston (6) under pressure on said material, the shape of the piston head (6) and the cavity determining the shape (7) of the compacted material.

Description

DISPOSITIF DE MISE EN FORME DE MATERIAU COMPACTABLE ET PROCEDEDEVICE FOR SHAPING COMPACTABLE MATERIAL AND METHOD

D'UTILISATION DU DISPOSITIF L'invention concerne un dispositif de mise en forme d'un materiau compactable, notamment en corps spherique, ainsi qu'un procede d'utilisation du dispositif. La fabrication de pastilles ou de billes a partir de materiau compactable est connue et largement utilisee dans le domaine industriel, notamment dans le domaine de 1'industrie pharmaceutique, lorsque le materiau compactable est melange a un autre produit, le plus souvent en phase aqueuse liquide, de maniere a former un corps plus ou moins pateux. Mais la fabrication de pastilles ou de billes a partir de materiau compactable sec souleve beaucoup plus de difficulte dans d'autres industries, comme dans l'industrie nucleaire, lorsque les conditions d'environnement et/ou de securite interdisent 1'utilisation d'un autre produit en phase liquide aqueuse. Il est en effet delicat de presser un materiau compactable dans une matrice lorsqu'il est compose a partir de matiere particulaire, tout particulierement quand la forme a obtenir est une sphere. Dans le domaine de l'industrie nucleaire, des pastilles de materiau compactable sec de geometrie comportant un axe de revolution peuvent etre obtenues par l'utilisation d'une presse uniaxiale avec un ou deux poincons, mais les matrices standards ne sont pas utilisables pour fabriquer des spheres directement a partir de poudres. Actuellement, seuls des procedes par voie chimique liquide et/ou sol-gel sont utilises pour l'obtention de corps spheriques. Il reste donc a mettre en forme un procede efficace de realisation de mise en forme de corps spherique a partir d'un materiau sec. Par sec, on entend ici substantiellement exempt de produit en phase liquide. L'invention vise a remedier a ce probleme en proposant un dispositif de mise en forme de materiau compactable, particulierement adapte a la mise en forme de corps spherique, le dispositif etant particulierement simple d'utilisation. A cet effet, 1'objet de 1'invention concerne un dispositif de mise en forme de materiau compactable, notamment en corps spherique, comportant un support formant chemise A. alesage sensiblement conique d'axe donne et de grande base sur une surface dite surface de travail, apte a loger au moins deux coquilles sensiblement coniques  The invention relates to a device for shaping a compactable material, in particular a spherical body, and a method of using the device. The manufacture of pellets or beads from compactable material is known and widely used in the industrial field, particularly in the field of the pharmaceutical industry, when the compactable material is mixed with another product, most often in liquid aqueous phase , so as to form a more or less pasty body. But the manufacture of pellets or beads from dry compactable material raises much more difficulty in other industries, such as in the nuclear industry, where environmental and / or safety conditions prohibit the use of a other product in aqueous liquid phase. It is indeed delicate to press a compactable material into a matrix when it is composed from particulate matter, especially when the shape to be obtained is a sphere. In the field of the nuclear industry, pellets of dry compactable geometry material having a revolution axis can be obtained by using a uniaxial press with one or two pins, but the standard dies are not usable for manufacturing. spheres directly from powders. Currently, only liquid chemical and / or sol-gel methods are used to obtain spherical bodies. It remains, therefore, to form an effective method for producing spherical body shaping from a dry material. By dry is meant here substantially free of product in the liquid phase. The invention aims to remedy this problem by proposing a device for shaping compactable material, particularly adapted to the shaping of spherical body, the device being particularly easy to use. For this purpose, the object of the invention relates to a device for shaping compactable material, in particular spherical body, comprising a liner support A. substantially conical bore of a given axis and a large base on a so-called surface surface working, adapted to house at least two substantially conical shells

complementaires dudit alesage conique et s'emboitant de facon serree l'une contre l'autre clans ledit alesage, lesdites deux coquilles coniques une fois serrees 1'une contre l'autre comportant en leur partie cote surface de travail au moins un alesage sensiblement cylindrique et sensiblement axial selon ledit axe, apte a loger au moins deux coquilles sensiblement cylindriques complementaires dudit alesage cylindrique et s'emboitant de facon serree Tune contre 1'autre dans ledit alesage, lesdites coquilles cylindriques une fois serrees rune contre 1'autre comportant un alesage traversant sensiblement cylindrique et sensiblement axial selon ledit axe, les coquilles coniques et les coquilles cylindriques etant telles que, lorsque les coquilles cylindriques sont serrees Tune contre l'autre dans 1'alesage cylindrique, une cavite apte a recevoir un materiau compactable est presente, formee d'espaces respectivement formes dans les coquilles coniques et cylindriques, du cote oppose a la surface de travail, et 1'alesage traversant etant destine a recevoir un piston en pression sur ledit materiau, la forme de la tete du piston et de la cavite determinant la forme du materiau compacte. Dans un mode de realisation particulierement prefere, la tete du piston est sensiblement en creux de forme de calotte spherique et la forme est sensiblement spherique. Les deux coquilles coniques s'emboitent generalement dans la majeure partie de 1'alesage conique, depuis le cote surface de travail. Les deux coquilles cylindriques s'emboitent generalement dans la majeure partie, de preference dans la totalite, de 1'alesage cylindrique, depuis le cote surface de travail. De preference, le dispositif comporte en outre au moins un element de maintien et/ou au moins un element de mise en regard des coquilles coniques l'une par rapport A .1'autre. Un tel maintien et/ou une telle mise en regard correspondent generalement a la position oil. lesdites coquilles sont serrees rune contre 1'autre pour emboitement. Un element peut avoir A. la fois une fonction de maintien et une fonction de mise en regard. Les elements de maintien ont generalement une fonction de serrage, et sont donc generalement des elements de serrage. Les elements de maintien sont generalement aussi des elements utilisables en mise en regard, et sont plus particulierement utilises pour 1'usinage, generalement sans utilisation ulterieurement pour la mise en forme. Ce sont par exemple des trous pour vis  complementary to said conical boring and interlocking tightly against each other in said bore, said two tapered shells, when clamped against each other, having at least one substantially cylindrical bore in their working surface portion and substantially axially along said axis, adapted to accommodate at least two substantially cylindrical shells complementary to said cylindrical bore and interlocking tightly against each other in said bore, said cylindrical shells being clamped together against the other having a bore traversing substantially cylindrical and substantially axial along said axis, the conical shells and cylindrical shells being such that, when the cylindrical shells are pressed against one another in the cylindrical range, a cavity adapted to receive a compactable material is present, formed spaces respectively formed in the conical and cylindrical shells, the opposite side to the surface The shape of the workpiece, and the passageway therethrough for receiving a piston in pressure on said material, the shape of the piston head and the cavity determining the shape of the compact material. In a particularly preferred embodiment, the piston head is substantially hollow shaped spherical cap and the shape is substantially spherical. The two conical shells generally fit into most of the conical bearing, from the work surface side. The two cylindrical shells generally fit most, preferably all, of the cylindrical extension from the work surface side. Preferably, the device further comprises at least one holding element and / or at least one element for facing the conical shells with respect to each other. Such a maintenance and / or such a look-up generally corresponds to the oil position. said shells are tight against each other for interlocking. An element can have both a hold function and a lookup function. The holding members generally have a clamping function, and are therefore generally clamping members. The holding elements are generally also elements usable in facing, and are more particularly used for machining, usually without further use for shaping. These are, for example, screw holes

comportant en miroir chacun au moins une partie filetee destinee a ce qu'une vis soit introduite et serree en leur sein. Dans le cadre de l'invention, it est par exemple possible que deux plans transversaux des deux coquilles coniques, en position serrees 1'une contre 1'autre pour emboitement, comportent chacun deux trous pour vis paralleles Fun a 1'autre, traversant les parties pleines des deux coquilles, et disposes tete-beche. Un element de mise en regard permet avantageusement de maintenir les deux coquilles coniques l'une par rapport a 1'autre, avant leur emboitement, generalement simultane, dans la chemise. Ce sont par exemple des trous pour goupilles. Selon un mode de realisation prefere de l'invention, le dispositif est tel que les deux coquilles cylindriques s'emboitent de fawn serree dans ledit alesage conique, sensiblement en affleurement de la surface de travail desdites coquilles coniques. Ainsi la pression, qui est revue cote surface de travail sur les coquilles cylindriques et sur les coquilles coniques, est de fawn avantageuse egalement repartie sur les surfaces de ces coquilles. Selon un mode de realisation prefere de l'invention, le dispositif est tel que le piston est apte a s'emboiter dans ledit alesage traversant, sensiblement en affleurement de la surface cote surface de travail desdites coquilles cylindriques. Cela permet avantageusement de realiser la forme desiree, par exemple une sphere, a affleurement du piston avec ladite surface. Ainsi, it est possible de diminuer les risques de trop presser le materiau compactable une fois la mise en forme obtenue, c'est-a-dire que, quand le piston est en affleurement, la pression qui est revue cote surface de travail pour inserer puis enfoncer le piston dans le dispositif, est supportee au moins par les coquilles cylindriques et non par le piston. Ce qui protege tres avantageusement le materiau compacte. Cette pression est d'ailleurs, dans un mode de realisation particulierement avantageux, supportee a la fois par les coquilles cylindriques et les coquilles coniques si les deux coquilles cylindriques s'emboitent de fawn serree rune contre 1'autre dans ledit alesage cylindrique, sensiblement en affleurement de la surface de travail des coquilles coniques. Dans un mode de realisation encore plus avantageux, quand toutes les surfaces cote surface de travail sont coplanaires, cette pression est supportee par les coquilles cylindriques, les coquilles coniques et la chemise.  mirror each of at least one threaded portion for a screw to be inserted and tightened therein. In the context of the invention, it is for example possible that two transverse planes of the two conical shells, in the interlocked position against each other for interlocking, each comprise two holes for screws parallel to each other, passing through the solid parts of both shells, and arranged head-beaks. An interleaving element advantageously allows the two conical shells to be held relative to one another before they are interlocked, generally simultaneously, in the liner. These are, for example, holes for pins. According to a preferred embodiment of the invention, the device is such that the two cylindrical shells snugly fit into said conical bore, substantially flush with the working surface of said conical shells. Thus, the pressure, which is reviewed on the working surface of the cylindrical shells and on the conical shells, is also advantageously distributed over the surfaces of these shells. According to a preferred embodiment of the invention, the device is such that the piston is adapted to fit into said through bore, substantially flush with the working surface dimension surface of said cylindrical shells. This advantageously makes it possible to produce the desired shape, for example a sphere, flush with said surface. Thus, it is possible to reduce the risk of over-pressing the compactable material once the shaping obtained, that is to say that, when the piston is flush, the pressure which is reviewed work surface side to insert then push the piston into the device, is supported at least by the cylindrical shells and not by the piston. This protects very advantageously the compact material. This pressure is also, in a particularly advantageous embodiment, supported both by the cylindrical shells and the conical shells if the two cylindrical shells fit snugly against one another in said cylindrical bore, substantially outcrop of the working surface of conical shells. In an even more advantageous embodiment, when all surface surfaces working surface are coplanar, this pressure is supported by cylindrical shells, conical shells and the jacket.

Dans tous les cas, 1'etat des surfaces cote surface de travail est tel que ces surfaces doivent &viter au maximum la retention de materiau compactable, si it en est verse sur une de ces surfaces. Un simple arasement, par exemple manuel, doit permettre d'&viter 1'exces de materiau compactable qui serait verse par megarde sur une de ces surfaces. De preference, 1'ensemble des coquilles cylindriques une fois serrees rune contre 1'autre presente une symetrie axiale selon ledit axe, ou bien 1'ensemble des coquilles coniques une fois serrees rune contre 1'autre presente une symetrie axiale selon ledit axe. De fawn particulierement prefer-6e, 1'ensemble des coquilles cylindriques une fois serrees rune contre 1'autre presente une symetrie axiale selon ledit axe et 1'ensemble des coquilles coniques une fois serrees 1'une contre 1'autre presente une symetrie axiale selon ledit axe.  In any case, the state of the working surface surfaces is such that these surfaces must avoid maximizing the retention of compactable material, if it is poured onto one of these surfaces. A simple leveling, for example manual, must allow to avoid the excess of compactable material which would be poured by megarde on one of these surfaces. Preferably, the set of cylindrical shells, when clamped against each other, has an axial symmetry along said axis, or the set of conical shells, when clamped against each other, has an axial symmetry along said axis. Particularly preferably, all of the cylindrical shells, when clamped against each other, have an axial symmetry along said axis, and the set of conical shells, when clamped against each other, have an axial symmetry along the axis. said axis.

L'invention concerne aussi un procede de mise en forme de materiau compactable par utilisation d'un dispositif selon l'invention, tel que l'on procede aux &tapes successives suivantes : 1) le dispositif est mis en place, par emboitement des coquilles coniques, eventuellement maintenues et/ou serrees rune contre 1'autre, dans la chemise, puis par emboitement des coquilles cylindriques dans les coquilles coniques, 1'axe etant de preference sensiblement vertical, 2) le materiau compactable est introduit dans la cavite a partir de la surface de travail, de preference par gravite, 3) un piston est introduit dans 1'alesage traversant sensiblement cylindrique, pour exercer une pression sur le materiau compactable de facon a le compacter sensiblement dans la forme d&sir&e. De preference, le procede selon l'invention est tel que, le piston etant apte a s'emboiter dans ledit alesage traversant sensiblement en affleurement de la surface cote surface de travail desdites coquilles cylindriques, la fin du procede de mise en forme est determinee par ledit affleurement. C'est un benefice tres avantageux du procede selon l'invention de permettre la mise en forme en une seule &tape, 1'etape 3), au cours de laquelle on passe d'un materiau compactable a une forme, de preference une sphere, compactee. De facon particulierement preferee selon l'invention, le materiau compactable est une poudre ou materiau particulaire eventuellement  The invention also relates to a process for shaping compactable material by using a device according to the invention, as the following successive steps are carried out: 1) the device is put in place, by interlocking the conical shells , possibly held together and / or clamped against each other in the jacket, then by interlocking cylindrical shells in the conical shells, the axis being preferably substantially vertical, 2) the compactable material is introduced into the cavity from the working surface, preferably by gravity; 3) a piston is introduced into the substantially cylindrical through-gap, to exert pressure on the compactable material so as to compact it substantially in the desired shape. Preferably, the method according to the invention is such that, the piston being able to fit into said through bore substantially flush with the working surface surface area of said cylindrical shells, the end of the forming process is determined by said outcrop. It is a very advantageous benefit of the method according to the invention to allow forming in one step, step 3), during which a compactable material is passed to a shape, preferably a sphere, compacted. In a particularly preferred manner according to the invention, the compactable material is a powder or particulate material, if appropriate.

melange A. au moins un liant. Au sens de la presente invention, on entend definir par "poudre" un ensemble de particules dont les dimensions sont habituellement inferieures A. 1 millimetre. L'utilisation d'un materiau d'une granulometrie superieure est neanmoins possible selon l'invention, par realisation de corps, par exemple spheriques, de plus gros diametres que pour une granulometrie plus fine. Selon une mise en oeuvre particulierement avantageuse du procede selon l'invention, on gore la mise en forme par la masse de materiau a compacter.  mixture A. at least one binder. For the purposes of the present invention, the term "powder" is intended to mean a set of particles whose dimensions are usually less than 1 millimeter. The use of a material of greater particle size is however possible according to the invention, by making bodies, for example spherical, larger diameters than for a finer particle size. According to a particularly advantageous implementation of the method according to the invention, the shaping is carried out by the mass of material to be compacted.

L'invention vise tout particulierement le cas ou le materiau compactable est sec, et ou la forme desiree est sensiblement une sphere ou corps spherique, cas pour lequel aucune solution n'existe dans fart anterieur. De plus, un des avantages du procede de l'invention est que le demoulage de la forme realisee est particulierement aise. L'invention est maintenant decrite en reference aux dessins annexes, non limitatifs, dans lesquels : - la figure 1 est une vue schematique en coupe d'un dispositif selon l'invention, avant assemblage ; - la figure 2 est une vue schematique en coupe du dispositif de la figure 1, apres assemblage; - la figure 3 est une vue schematique d'une variante partielle du dispositif de l'invention ; - la figure 4 est une vue d'une coupe schematique de la variante de la figure 3 ; - la figure 5 est une vue schematique d'une coupe de la variante de la figure 3 ; et - la figure 6 est une vue schematique d'une coupe de la variante de la figure 3 - la figure 7 est une reproduction photographique de deux spheres realisees selon l'invention, et - la figure 8 est une reproduction photographique de deux spheres realisees selon l'invention.  The invention is particularly directed to the case where the compactable material is dry, and the desired shape is substantially a sphere or spherical body, in which case no solution exists in the prior art. In addition, one of the advantages of the method of the invention is that the demolding of the embodiment is particularly comfortable. The invention is now described with reference to the accompanying nonlimiting drawings, in which: - Figure 1 is a schematic sectional view of a device according to the invention, before assembly; - Figure 2 is a schematic sectional view of the device of Figure 1, after assembly; FIG. 3 is a schematic view of a partial variant of the device of the invention; - Figure 4 is a schematic sectional view of the variant of Figure 3; - Figure 5 is a schematic view of a section of the variant of Figure 3; and FIG. 6 is a schematic view of a section of the variant of FIG. 3; FIG. 7 is a photographic reproduction of two spheres made according to the invention, and FIG. 8 is a photographic reproduction of two spheres made. according to the invention.

La figure 1 est une vue schematique en coupe d'un dispositif 1 selon l'invention, avant assemblage. La figure 2 est une vue schematique en coupe du dispositif 1, apres assemblage. Dans ces  Figure 1 is a schematic sectional view of a device 1 according to the invention, before assembly. Figure 2 is a schematic sectional view of the device 1, after assembly. In these

figures, le materiau compactable n'a pas ete represents. Le dispositif 1 comporte un support formant chemise 4 a alesage conique 14 d'axe donne (X'X) et de grande base sur une surface 28 dite surface de travail. L'alesage 14 est apte a loger deux coquilles 3a et 3b coniques, complementaires dudit alesage conique 14 et s'emboitant de fawn serree l'une 3a contre 1'autre 3b dans ledit alesage 14. Il reste un petit espace en partie cote inferieur des figures 1 et 2, non rempli par lesdites coquilles 3a et 3b coniques. Cet espace permet avantageusement de s'assurer que les coquilles coniques sont bien positionnees (bon emboitement conique et bon serrage des coquilles entre elles). Les coquilles 3a et 3b une fois emboitees comportent en leur partie cote surface de travail 28 (qui est ici le cote superieur des figures 1 et 2) un alesage cylindrique (16, 17) axial selon 1axe (X'X). L'alesage cylindrique (16, 17) est forme de deux parties semblables et, selon une mise en forme preferee de l'invention presentee dans cette execution, en miroir rune de 1'autre. Ce sont les parties 16, alesage demi-cylindrique de la coquille 3a, et 17, alesage demi-cylindrique de la coquille 3b. Ledit alesage (16, 17) est apte a loger deux coquilles cylindriques 2a et 2b, complementaires dudit alesage conique (16, 17) et s'emboitant de fawn serree Tune contre 1'autre dans ledit alesage (16, 17). Les coquilles cylindriques 2a et 2b une fois serrees rune contre 1'autre comportent un alesage traversant cylindrique (29, 30) et axial selon 1'axe (X'X). L'alesage traversant cylindrique (29, 30) est forme de deux parties semblables et, selon une mise en forme preferee de l'invention presentee dans cette execution, en miroir rune contre 1'autre. Ce sont les parties 29, alesage traversant demi-cylindrique de la coquille 2a, et 30, alesage traversant demi-cylindrique de la coquille 2b. Les coquilles coniques 3a et 3b et les coquilles cylindriques 2a et 2b sont telles que, lorsque les coquilles cylindriques 2a et 2b sont serrees rune contre 1'autre dans 1'alesage cylindrique (16, 17) (voir figure 2), une cavite est presente, formee des espaces 10, 11, 12, 13 respectivement formes dans les coquilles 2a, 2b, 3a et 3b. Cette cavite 10-13 est formee du cote oppose A. la surface de travail 28. Elie est donc presente dans la partie dans laquelle lesdites coquilles 2a, 2b, 3a et 3b sont en regard (voir figure 2).  figures, the compactable material has not been represented. The device 1 comprises a support forming a liner 4 having a conical bore 14 of axis (X'X) and a large base on a surface 28 called working surface. The bore 14 is able to accommodate two conical shells 3a and 3b, complementary to said conical bore 14 and interlocking tightly one 3a against the other 3b in said bore 14. There remains a small space in part lower side Figures 1 and 2, not filled by said shells 3a and 3b conical. This space advantageously ensures that the tapered shells are well positioned (good conical nesting and good tightening of the shells between them). The shells 3a and 3b once nested have their working surface portion 28 (which is here the upper side of Figures 1 and 2) a cylindrical bore (16, 17) axial axis 1 (X'X). The cylindrical bore (16, 17) is formed of two similar parts and, according to a preferred shaping of the invention presented in this embodiment, in a mirror of the other. These are the parts 16, semi-cylindrical bore of the shell 3a, and 17, semi-cylindrical bore of the shell 3b. Said bore (16, 17) is adapted to accommodate two cylindrical shells 2a and 2b, complementary to said conical bore (16, 17) and interlocking tightly against each other in said bore (16, 17). The cylindrical shells 2a and 2b, when clamped against each other, have a cylindrical (29, 30) axial through bore (X'X). The cylindrical through bore (29, 30) is formed of two similar parts and, in a preferred shaping of the invention presented in this embodiment, mirrored against the other. These are the parts 29, semi-cylindrical through bore of the shell 2a, and 30, semi-cylindrical through bore of the shell 2b. The conical shells 3a and 3b and the cylindrical shells 2a and 2b are such that when the cylindrical shells 2a and 2b are pressed against one another in the cylindrical bearing (16, 17) (see FIG. 2), a cavity is presented, formed spaces 10, 11, 12, 13 respectively formed in the shells 2a, 2b, 3a and 3b. This cavity 10-13 is formed on the opposite side A. the working surface 28. Elie is present in the part in which said shells 2a, 2b, 3a and 3b are opposite (see Figure 2).

La cavite 10-13 est bien sur apte a recevoir un materiau compactable. L'alesage traversant (29, 30) des coquilles cylindriques 2a et 2b est destine A. recevoir un piston 6 en pression sur ledit materiau. La forme  The cavity 10-13 is of course adapted to receive a compactable material. The through bore (29, 30) of the cylindrical shells 2a and 2b is intended to A. receive a piston 6 under pressure on said material. The form

de la tete du piston 31 est une calotte spherique. La cavite 10-13 et la tete de piston 31 determinent la forme 7 du materiau a compacter. Dans cette execution, la forme est une sphere 7. Dans la forme de realisation des figures 1 et 2, les surfaces superieures 32 des coquilles coniques et 28 des coquilles cylindriques sont en affleurement. De plus, le piston 6 est tel que, une fois emboite, sa surface superieure est en affleurement desdites surfaces 28 et 32. Cela veut aussi dire que la pression transmise au materiau a compacter n'est pas plus elevee que la pression necessaire pour que le piston 6 soit emboite. Toute pression plus elevee que ladite pression necessaire, par exemple transmise par une presse de type hydraulique, s'exerce sur les surfaces 28 et 32 et non sur le piston 6. Cela permet avantageusement de ne pas trop travailler le materiau une fois compacte, et donc d'eviter de le fragiliser voire de le briser. Cela est un avantage par rapport aux dispositifs de fart anterieur oil ion gere le compactage par la pression exercee. Dans 1'execution de l'invention, on gere donc le compactage principalement par la masse de materiau a compacter. La figure 3 est une vue schematique d'une variante partielle du dispositif de l'invention. Dans cette variante, les deux coquilles coniques 3a et 3b du dispositif 1 des figures 1 et 2 ont ete remplacees par des coquilles coniques 3'a et 3'b, qui comportent des moyens de maintien et de mise en regard. Les coquilles 3'a et 3'b definissent respectivement des alesages demi-cylindriques 16' et 17', et des espaces 12' et 13' destines a former une cavite. Les coquilles 3'a et 3'b peuvent former un dispositif 1' selon l'invention, en combinaison avec la chemise 4 et les coquilles cylindriques 2a et 2b. Les coupes IV-IV, V- V et VI-VI, respectivement montrees dans les figures 4, et 5 et 6, completent la figure 3 pour cette execution. La figure 5 montre, dans un plan transversal, deux trous 18 et 19 pour goupilles. L'insertion de deux goupilles (non representees) permet la mise en regard des deux coquilles coniques 3'a et 3'b. La figure 6 montre deux trous pour vis : 26 et sa partie filetee 22, et 27 et sa partie filetee 23. Ces trous sont tous paralleles l'un a 1'autre et traversant les parties pleines des deux coquilles en position tete-beche Fun de 1'autre, c'est-a-dire que le trou (26,22) est en position tete-beche par rapport au trou (27, 23). La figure 4 montre deux trous pour vis 21 et sa partie filetee 20, 25 et sa partie filetee 24. Ces trous sont tous  of the piston head 31 is a spherical cap. The cavity 10-13 and the piston head 31 determine the shape 7 of the material to be compacted. In this embodiment, the shape is a sphere 7. In the embodiment of Figures 1 and 2, the upper surfaces 32 of the conical shells and cylindrical shells are flush. In addition, the piston 6 is such that, once nested, its upper surface is flush with said surfaces 28 and 32. This also means that the pressure transmitted to the material to be compacted is not higher than the pressure necessary for the piston 6 is nested. Any pressure higher than said required pressure, for example transmitted by a hydraulic type press, is exerted on the surfaces 28 and 32 and not on the piston 6. This advantageously makes it possible not to overwork the material once compacted, and therefore to avoid weakening or even breaking it. This is an advantage over prior art devices in which the compacting is carried out by the pressure exerted. In the execution of the invention, the compaction is thus managed mainly by the mass of material to be compacted. Figure 3 is a schematic view of a partial variant of the device of the invention. In this variant, the two conical shells 3a and 3b of the device 1 of FIGS. 1 and 2 have been replaced by conical shells 3'a and 3'b, which comprise holding and facing means. The shells 3'a and 3'b respectively define half-cylindrical bores 16 'and 17', and spaces 12 'and 13' intended to form a cavity. The shells 3'a and 3'b may form a device 1 'according to the invention, in combination with the liner 4 and the cylindrical shells 2a and 2b. Sections IV-IV, V-V and VI-VI, respectively shown in Figures 4, and 5 and 6, complete Figure 3 for this execution. Figure 5 shows, in a transverse plane, two holes 18 and 19 for pins. The insertion of two pins (not shown) allows the facing of the two conical shells 3'a and 3'b. Figure 6 shows two screw holes: 26 and its threaded portion 22, and 27 and its threaded portion 23. These holes are all parallel to each other and through the solid parts of the two shells in head-to-head Fun the other, that is to say that the hole (26,22) is in head-beak position relative to the hole (27, 23). FIG. 4 shows two screw holes 21 and its threaded portion 20, 25 and its threaded portion 24. These holes are all

paralleles Pun a 1'autre et traversant les parties pleines des deux coquilles en position tete-beche Fun de 1'autre, c'est-a-dire que le trou (21,20) est en position tete-beche par rapport au trou (25,24). Dans cette execution, ces trous (21, 20 ; 25, 24 ; 26, 22 ; 27, 23) sont des moyens de maintien des coquilles coniques en position serree Tune par rapport A. 1'autre, qui sont avantageusement utilises lors de 1'usinage pour permettre un usinage tres precis. Mais it est possible selon l'invention de disposer d'un autre dispositif dans lequel les moyens de maintien ne sont pas presents, 1'usinage etant alors realise differemment, et le moyen de mise en regard (18,19) etant seul present. Les figures 7 et 8 sont explicitees ci-apres dans les exemples de mise en oeuvre.  parallel to each other and passing through the solid portions of the two shells in the head-to-head position of the other, that is to say that the hole (21, 20) is in the head-to-head position relative to the hole (25,24). In this embodiment, these holes (21, 20; 25, 24; 26, 22; 27, 23) are means for holding the conical shells in a tight position relative to each other, which are advantageously used during machining to allow very precise machining. But it is possible according to the invention to have another device in which the holding means are not present, the machining then being performed differently, and the means of facing (18,19) being alone present. Figures 7 and 8 are explained below in the examples of implementation.

EXEMPLES DE MISE EN OEUVRE Il a ete utilise un dispositif 1 selon l'invention, pour compactage de materiau particulaire sec, pour lequel toutes les pieces etaient en acier inoxydable de type 316, et le poincon ou piston utilise etait en acier Z160CDU12 (apres traitement thermique 60HRC). Les dimensions des pieces etaient, pour une forme de sphere de 3, 4 mm de diametre • Pour la chemise, une forme externe cylindrique de hauteur de 60 mm et de diametre de 70 mm, et un alesage conique de grande base (cote surface de travail) de 45 mm, une profondeur d'alesage conique de 60 mm, et un angle de conicite de 7 ; • Pour les deux demi coquilles coniques, une hauteur de 58 mm, un diametre de grande base (cote surface de travail) de 45 mm, une profondeur d'alesage cylindrique de 15, 8 mm, et un diametre d'alesage cylindrique de 15 mm, et un espace de partie spherique de diametre 1,7 mm menage dans 1'ensemble de ces coquilles ; • Pour les deux demi coquilles cylindriques, une longueur de 15,8 mm, et un espace de partie spherique de diametre 1,7 mm menage dans 1'ensemble de ces coquilles ; • Pour le piston une longueur de 15,8mm pour un diametre de 3mm, une calotte creuse pour sphere de 3,4 mm etant menagee en extremite.  EXAMPLES OF IMPLEMENTATION It was used a device 1 according to the invention, for compacting dry particulate material, for which all parts were made of stainless steel type 316, and the punch or piston used was Z160CDU12 steel (after treatment thermal 60HRC). The dimensions of the pieces were, for a spherical shape of 3, 4 mm in diameter. • For the jacket, an external cylindrical shape with a height of 60 mm and a diameter of 70 mm, and a conical bore of large base (surface dimension of working) of 45 mm, a conical boring depth of 60 mm, and a conic angle of 7; • For the two tapered half-shells, a height of 58 mm, a diameter of large base (working surface dimension) of 45 mm, a cylindrical boring depth of 15.8 mm, and a cylindrical boring diameter of 15 mm. mm, and a spherical portion space of diameter 1.7 mm household in all of these shells; • For the two cylindrical half-shells, a length of 15.8 mm, and a spherical portion space of diameter 1.7 mm household in all of these shells; • For the piston a length of 15.8mm for a diameter of 3mm, a hollow shell for sphere of 3.4 mm being end-shaped.

Il a ete valide des dispositifs dans lesquels le diametre des formes spheriques (matrices) realisees etait respectivement de 3,4 mm et de 1 mm. Des essais de poudre de nitrure de titane ont ete concluants pour ces deux diametres.  Devices in which the diameters of the spherical shapes (matrices) made were respectively 3.4 mm and 1 mm were valid. Tests of titanium nitride powder have been conclusive for these two diameters.

La figure 7 est une reproduction photographique de deux spheres en nitrure de titane realisees selon l'invention, dans des matrices spheriques de 1 mm et de 3,4 mm de diametres respectifs.  FIG. 7 is a photographic reproduction of two titanium nitride spheres made according to the invention, in spherical dies of 1 mm and 3.4 mm in respective diameters.

Dans le cadre de l'utilisation dun seul dispositif pour realisation de spheres de matieres combustibles UPuN et UPuC, huit essais concluants ont aussi ete realises pour des formes spheriques de diametre 2,7 mm.  In the context of the use of a single device for producing UPuN and UPuC combustible material spheres, eight conclusive tests have also been carried out for spherical shapes with a diameter of 2.7 mm.

Pour la realisation de spheres de matieres combustibles UPuN, ces essais sont repris ci-apres dans le Tableau, qui reprend les mesures effectuees sur UPuN apres un traitement de densification. Masse D1 D2 D3 D4 Diametre Volume MVG MVG/ (g) (mm) (mm) (mm) (mm) moyen (mm3) (g.cm- MVTh (mm) 3) (%) 1 0,091 2,431 2,404 2,431 2,393 2,41 7,37 12,34 86 2 0,090 2,408 2,393 2,425 2,389 2,40 7,27 12,38 86 3 0,091 2,418 2,417 2, 432 2,420 2,42 7,44 12,24 85 4 0,087 2,396 2,397 2,385 2,408 2,40 7,21 12,07 84 5 0,083 2,414 2,338 2,327 2,315 2,35 6,78 12,24 85 6 0,092 2,423 2,419 2,420 2,423 2,42 7,43 12,38 86 7 0,092 2,391 2,395 2,481 2,448 2,43 7,50 12,26 86 8 0,092 2,453 2,435 2,439 2,487 2,45 7,73 11,90 83 Ou : MVG : Masse Volumique Geometrique et DTh : Densite 20 Theorique. I1 a ete constate, sur les spheres ainsi formees, un retrait a la mise en forme (spheres obtenues d'environ 2,3 a 2,5 mm de diametre), pour ce materiau UPuN. Les essais ainsi realises ont ete juges concluants car le procede de 25 mise en forme etait facile a mettre en oeuvre et n'a fourni que tres peu de rebuts. De plus, la dispersion de taille etait tres faible, la sphericite etait bonne et les spheres obtenues apres mises en forme etaient de bonne tenue mecanique. La figure 8 est une reproduction photographique de deux spheres realisees selon l'invention, dans la meme matrice spherique de 2,7 mm 5 de diametre.  For the production of UPuN fuel material spheres, these tests are given below in the Table, which shows the measurements made on UPuN after a densification treatment. Mass D1 D2 D3 D4 Diameter Volume MVG MVG / (g) (mm) (mm) (mm) (mm) average (mm3) (g.cm-MVTh (mm) 3) (%) 1 0.091 2,431 2,404 2,431 2,393 2 , 41 7.37 12.34 86 2 0.090 2.408 2.393 2.425 2.399 2.40 7.27 12.38 86 3 0.091 2.418 2.417 2, 432 2.420 2.42 7.44 12.24 85 4 0.087 2.369 2.39 2.385 2.408 2 , 40 7,21 12.07 84 5 0.083 2,414 2,338 2,327 2,315 2,35 6.78 12.24 85 6 0.092 2,423 2,419 2,420 2,423 2,42 7.43 12.38 86 7 0.092 2,391 2,395 2,481 2,448 2.43 7,50 12,26 86 8 0,092 2,453 2,435 2,439 2,487 2,45 7,73 11,90 83 Or: MVG: Geometric Density and DTh: Density 20 Theoretical. Spheres thus formed showed shrinkage at shaping (spheres obtained about 2.3 to 2.5 mm in diameter) for this UPuN material. The tests thus carried out were found to be conclusive because the forming process was easy to carry out and provided very little scrap. In addition, the size dispersion was very low, the sphericity was good and the spheres obtained after shaping were of good mechanical strength. FIG. 8 is a photographic reproduction of two spheres made according to the invention, in the same spherical matrix 2.7 mm in diameter.

Claims (10)

REVENDICATIONS 1. Dispositif (1, 1') de mise en forme de materiau compactable, notamment en corps spherique, comportant un support formant chemise (4) a alesage sensiblement conique (14) d'axe (X'X) donne et de grande base sur une surface (28) dite surface de travail, apte a loger au moins deux coquilles sensiblement coniques (3a, 3b ; 3'a, 3'b) complementaires dudit alesage conique (14) et s'emboitant de fawn serree rune contre l'autre dans ledit alesage (14), lesdites deux coquilles coniques (3a, 313 ; 3'a, 3'b) une fois serrees rune contre 1'autre comportant en leur partie cote surface de travail (28) au moins un alesage sensiblement cylindrique (16, 17 ; 16', 17') et sensiblement axial selon ledit axe (X'X), apte a loger au moins deux coquilles sensiblement cylindriques (2a, 2b) complementaires dudit alesage cylindrique (16, 17 ; 16', 17') et s'emboitant de fawn serree rune contre 1'autre dans ledit alesage (16, 17 ; 16', 17'), lesdites coquilles cylindriques (2a, 2b) une fois serrees rune contre 1'autre comportant un alesage traversant sensiblement cylindrique (29, 30) et sensiblement axial selon ledit axe (X'X), les coquilles coniques (3a, 3b ; 3'a, 3'b) et les coquilles cylindriques etant telles que, lorsque les coquilles cylindriques (2a, 2b) sont serrees 1'une contre 1'autre dans 1'alesage (16, 17' ; 16', 17) cylindrique, une cavite (10-13) apte a recevoir un materiau compactable est presente, formee d'espaces respectivement menages dans les coquilles coniques et cylindriques (2a, 2b ; 3a, 3b), du cote oppose a la surface de travail (28), et 1'alesage (29, 30) traversant etant destine a recevoir un piston (6) en pression sur ledit materiau, la forme de la tete (31) du piston (6) et de la cavite (10-13) determinant la forme (7) du materiau compacte.  1. Device (1, 1 ') for shaping compactable material, in particular spherical body, comprising a liner support (4) with substantially conical bore (14) of axis (X'X) gives and large base on a surface (28) said working surface, adapted to accommodate at least two substantially conical shells (3a, 3b, 3'a, 3'b) complementary to said conical boring (14) and interlocking tightly against the other in said bore (14), said two tapered shells (3a, 313; 3'a, 3'b) when tightened against each other having in their work surface side portion (28) at least one bore substantially cylindrical (16, 17; 16 ', 17') and substantially axial along said axis (X'X), able to accommodate at least two substantially cylindrical shells (2a, 2b) complementary to said cylindrical bore (16, 17; 16 ', 17 ') and interlocking tightly against one another in said bore (16, 17; 16', 17 '), said cylindrical shells (2a, 2b) once tightened against each other. The other having a substantially cylindrical through-bore (29, 30) and substantially axial along said axis (X'X), the conical shells (3a, 3b; 3'a, 3'b) and the cylindrical shells being such that when the cylindrical shells (2a, 2b) are clamped against each other in the cylindrical bore (16, 17 ', 16', 17) a cavity (10-13) adapted to receive a compactable material is provided, formed respectively by spaces in the conical and cylindrical shells (2a, 2b, 3a, 3b) on the opposite side to the working surface (28). and the recess (29, 30) therethrough for receiving a piston (6) under pressure on said material, the shape of the head (31) of the piston (6) and the cavity (10-13) defining the shape (7) of the compact material. 2. Dispositif (1, 1') selon la revendication precedente tel que la tete du piston (31) est sensiblement en creux de forme de calotte spherique, et la forme (7) est sensiblement spherique.  2. Device (1, 1 ') according to the preceding claim such that the piston head (31) is substantially recessed spherical cap, and the shape (7) is substantially spherical. 3. Dispositif (1, 1') selon rune des revendications precedentes comportant en outre au moins un element de maintien (20-27) et/ou au moins un element de mise en regard (18, 19) des coquilles coniques (3'a, 3'b) 1'une par rapport a l'autre.  3. Device (1, 1 ') according to rune preceding claims further comprising at least one holding member (20-27) and / or at least one setting element (18, 19) conical shells (3') a, 3'b) relative to each other. 4. Dispositif (1, 1') selon rune des revendications precedentes tel que les deux coquilles cylindriques (2a, 2b) s'emboitent de fawn serree rune contre 1'autre dans ledit alesage conique (16, 17 ; 16', 17'), sensiblement en affleurement (32) de la surface de travail (28) desdites coquilles coniques (3a, 3b ; 3'a, 3'b).  4. Device (1, 1 ') according to one of the preceding claims such that the two cylindrical shells (2a, 2b) fit snugly against one another in said conical bore (16, 17; 16', 17 ' ), substantially flush (32) of the working surface (28) of said conical shells (3a, 3b, 3'a, 3'b). 5. Dispositif (1, 1') selon rune des revendications precedentes tel que le piston (6) est apte a s'emboiter dans ledit alesage traversant (29, 30), sensiblement en affleurement de la surface (32) cote surface de travail (28) desdites coquilles cylindriques (2a, 2b).  5. Device (1, 1 ') according to rune preceding claims such that the piston (6) is adapted to fit into said through bore (29, 30), substantially flush with the surface (32) dimension work surface (28) said cylindrical shells (2a, 2b). 6. Dispositif (1, 1') selon 1'une des revendications precedentes tel que 1'ensemble des coquilles cylindriques (2a, 2b) une fois serrees rune contre 1'autre presente une symetrie axiale selon ledit axe (X', X), et/ou 1'ensemble des coquilles coniques (3a, 3b ; 3'a, 3'b) une fois serrees rune contre 1'autre presente une symetrie axiale selon ledit axe (X', X).  6. Device (1, 1 ') according to one of the preceding claims such that the set of cylindrical shells (2a, 2b) once tightened rune against each other has an axial symmetry along said axis (X', X) and / or the set of conical shells (3a, 3b; 3'a, 3'b) when clamped against each other has an axial symmetry along said axis (X ', X). 7. Procede de mise en forme de materiau compactable par utilisation d'un dispositif (1, 1') selon 1'une des revendications precedentes, tel que 1'on procede aux etapes successives suivantes : 1) le dispositif (1, 1') est mis en place, par emboitement des coquilles coniques (3a, 3b), eventuellement maintenues et/ou serrees rune contre 1'autre, dans la chemise (4), puis par emboitement des coquilles cylindriques (2a, 2b) dans les coquilles coniques (3a, 3b), 1'axe (X', X) etant de preference sensiblement vertical, 2) le materiau compactable est introduit dans la cavite (10-13) a partir de la surface de travail (28), de preference par gravite, 3) un piston (6) est introduit dans 1'alesage traversant sensiblement cylindrique (29, 30), pour exercer une pression sur le materiau compactable de facon a le compacter sensiblement dans la forme (7) desiree.  7. Process for shaping compactable material by use of a device (1, 1 ') according to one of the preceding claims, as the following successive steps are carried out: 1) the device (1, 1') ) is put in place, by interlocking the conical shells (3a, 3b), possibly held and / or tightened rune against the other, in the jacket (4), then by interlocking cylindrical shells (2a, 2b) in the shells conical (3a, 3b), the axis (X ', X) being preferably substantially vertical, 2) the compactable material is introduced into the cavity (10-13) from the working surface (28), preferably 3) a piston (6) is introduced into the substantially cylindrical through-gap (29, 30) to exert pressure on the compactable material to substantially compact it in the desired shape (7). 8. Procede de mise en forme de materiau compactable selon la revendication precedente, tel que, le piston (6) etant apte a s'emboiter dans ledit alesage traversant (29, 30) sensiblement en affleurement de la surface (32) cote surface de travail (28) desdites coquilles cylindriques (2a, 2b), la fin du procede de mise en forme est determinee par ledit affleurement.  8. Method of shaping compactable material according to the preceding claim, such that, the piston (6) being adapted to fit into said through bore (29, 30) substantially flush with the surface (32) surface area of working (28) said cylindrical shells (2a, 2b), the end of the shaping process is determined by said outcropping. 9. Procede de mise en forme de materiau compactable selon rune des revendications 7 ou 8, tel que le materiau compactable est une poudre.  9. Process for shaping compactable material according to one of claims 7 or 8, such that the compactable material is a powder. 10. Procede de mise en forme de materiau compactable selon lune des revendications 7 a 9 dans lequel on gere la mise en forme par la masse de materiau a compacter.  10. Process for shaping compactable material according to one of claims 7 to 9 in which the shaping is carried out by the mass of material to be compacted.
FR0512835A 2005-12-16 2005-12-16 DEVICE FOR SHAPING COMPACTABLE MATERIAL AND METHOD OF USING THE DEVICE Expired - Fee Related FR2894871B1 (en)

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PCT/EP2006/069671 WO2007068723A1 (en) 2005-12-16 2006-12-13 Device for shaping compactable material and method for using the device

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Cited By (1)

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Publication number Priority date Publication date Assignee Title
WO2010100123A3 (en) * 2009-03-04 2010-11-11 Commissariat A L'energie Atomique Et Aux Energies Alternatives Pressing tool

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Publication number Priority date Publication date Assignee Title
US1838518A (en) * 1927-02-17 1931-12-29 Simonds Worden White Company Knockdown mold
GB404492A (en) * 1932-12-24 1934-01-18 Mij Exploitatie Octrooien Nv Improved method of and apparatus for the manufacture of compressed masses of normally non-coherent substances, in particular coal dust, browncoal dust and the like
FR1346567A (en) * 1962-12-26 1963-12-20 Asea Ab High pressure apparatus, in particular for the transformation of graphite into diamond
GB1278254A (en) * 1968-06-26 1972-06-21 Atomic Energy Authority Uk Improvements in or relating to forming spherical bodies by pressing powder
DE2350286A1 (en) * 1973-10-06 1975-04-24 Vaw Ver Aluminium Werke Ag Vibration moulding of dense plastics articles - by exposing plastics mass to vibration in vertical and horizontal planes simultaneously
GB1443823A (en) * 1973-03-28 1976-07-28 Atomic Energy Authority Uk Manufacture of compact bodies from particulate material
US4230653A (en) * 1978-08-28 1980-10-28 Ptx-Pentronix, Inc. Method for producing spherical articles
FR2506210A1 (en) * 1981-05-25 1982-11-26 Inst Vysokikh Temperatur Akade Powder metal compactor with die - uses collet tab design punch and die channel for precision sphericals

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1838518A (en) * 1927-02-17 1931-12-29 Simonds Worden White Company Knockdown mold
GB404492A (en) * 1932-12-24 1934-01-18 Mij Exploitatie Octrooien Nv Improved method of and apparatus for the manufacture of compressed masses of normally non-coherent substances, in particular coal dust, browncoal dust and the like
FR1346567A (en) * 1962-12-26 1963-12-20 Asea Ab High pressure apparatus, in particular for the transformation of graphite into diamond
GB1278254A (en) * 1968-06-26 1972-06-21 Atomic Energy Authority Uk Improvements in or relating to forming spherical bodies by pressing powder
GB1443823A (en) * 1973-03-28 1976-07-28 Atomic Energy Authority Uk Manufacture of compact bodies from particulate material
DE2350286A1 (en) * 1973-10-06 1975-04-24 Vaw Ver Aluminium Werke Ag Vibration moulding of dense plastics articles - by exposing plastics mass to vibration in vertical and horizontal planes simultaneously
US4230653A (en) * 1978-08-28 1980-10-28 Ptx-Pentronix, Inc. Method for producing spherical articles
FR2506210A1 (en) * 1981-05-25 1982-11-26 Inst Vysokikh Temperatur Akade Powder metal compactor with die - uses collet tab design punch and die channel for precision sphericals

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010100123A3 (en) * 2009-03-04 2010-11-11 Commissariat A L'energie Atomique Et Aux Energies Alternatives Pressing tool
US8702411B2 (en) 2009-03-04 2014-04-22 Commissariat A L'energie Atomique Et Aux Energies Alternatives Press tooling

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FR2894871B1 (en) 2008-01-18

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