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(11) |
EP 1 971 698 B1 |
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EUROPEAN PATENT SPECIFICATION |
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Mention of the grant of the patent: |
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05.06.2013 Bulletin 2013/23 |
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Date of filing: 26.10.2006 |
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International Patent Classification (IPC):
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International application number: |
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PCT/EP2006/010306 |
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International publication number: |
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WO 2007/051557 (10.05.2007 Gazette 2007/19) |
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METHOD FOR THE PRODUCTION OF A COMPOSITE MATERIAL OR A PRECURSOR PRODUCT FOR THE PRODUCTION
OF A COMPOSITE MATERIAL
VERFAHREN ZUR HERSTELLUNG EINES VERBUNDWERKSTOFFS ODER EINES VORLÄUFERPRODUKTS ZUR
HERSTELLUNG EINES VERBUNDWERKSTOFFS
PROCEDE DE PRODUCTION D'UN MATERIAU COMPOSITE OU D'UN PRODUIT PRECURSEUR POUR LA PRODUCTION
D'UN MATERIAU COMPOSITE
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Designated Contracting States: |
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AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE
SI SK TR |
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Priority: |
03.11.2005 DE 102005052470
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Date of publication of application: |
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24.09.2008 Bulletin 2008/39 |
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Proprietor: Neue Materialien Fürth GmbH |
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90762 Fürth (DE) |
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Inventors: |
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- LOHMÜLLER, Andreas
90765 Fürth (DE)
- HARTMANN, Mark
87437 Kempten (DE)
- SINGER, Robert F.
91054 Erlangen (DE)
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Representative: Gassner, Wolfgang |
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Dr. Gassner & Partner
Patentanwälte
Marie-Curie-Strasse 1 91052 Erlangen 91052 Erlangen (DE) |
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References cited: :
EP-B1- 0 409 966 US-B1- 6 360 576
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WO-A-00/49192
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| Note: Within nine months from the publication of the mention of the grant of the European
patent, any person may give notice to the European Patent Office of opposition to
the European patent
granted. Notice of opposition shall be filed in a written reasoned statement. It shall
not be deemed to
have been filed until the opposition fee has been paid. (Art. 99(1) European Patent
Convention).
|
[0001] The invention relates to a method for the production of a composite material or a
precursor product for the production of a precursor product for the production of
a composite material.
[0002] Metallic composite materials are generally known according to the prior art. In this
connection these are particularly composite materials for which a reinforcement phase
is included in a metallic matrix phase. Depending on the demands on the composite
material the reinforcement phase can be made of particles, in particular non-metallic
particles, or of fibers. According to the prior art it is furthermore known how to
produce molded parts made of composite materials by means of a casting method. For
this the melted metal is mixed in a container with the reinforcement phase by means
of a stirrer and then transferred to a casting device. According to the prior art
the problem occurs that the reinforcement phase is not distributed homogeneously in
the metallic matrix phase. This can be caused by the formation of agglomerates of
the particles forming the reinforcement phase. Regardless of this the reinforcement
phase can sink or swim in the molten mass due to differences in density. The thus
caused inhomogeneities lead to poor mechanical properties for the product produced
from the molten mass.
[0003] EP 0 409 966 A1 discloses a method for the production of a composite material for which metallic
material is fed to an extruder device. The metallic material can be an alloy with
a discontinuous phase.
[0004] WO 00/49192 describes a method for the production of a metal-matrix composite material. In this
connection the matrix-metal is plasticized in a processing unit comprising an extruder,
and a reinforcement component is fed to the extruder by means of a side-feeder device.
The mixture of plasticized matrix-metal and reinforcement component is homogenized
in the extruder.
[0005] US 6,360,576 B1 discloses a method for the production of a composite material having a metallic matrix
phase and a reinforcement phase with the following steps:
Feeding a solid preform into a first portion of an extruder;
transporting the preform by punch to heating means, where it is heated until it is
becomes thixotropic;
feeding reinforcement particles into a second portion of the extruder thereby producing
a mixture; and
cooling mixture below the solidus temperature of the metallic matrix phase during
transport of the mixture through the die.
[0006] The object of the invention is to eliminate the disadvantages according to the prior
art. In particular a method is to be specified for the production of a starting product
which makes possible the production of a composite material with improved homogeneity.
[0007] This object is solved with the features of claim 1. Advantageous embodiments of the
invention result from the features of claims 2 to 15.
[0008] According to the invention the method defined in claim 1 is provided
[0009] The suggested method provides a relatively simple and inexpensive way to produce
a composite material or a precursor product for the production of a composite material
in which the reinforcement phase is homogeneously distributed. Segregation processes
are avoided by using an extruder device as suggested by the invention. In accordance
with the purpose of the present invention the term "extruder device" is understood
to be a device with which the metallic matrix phase and the reinforcement particles
are mixed intensively, in particular using the effects of shearing force, and in this
connection the mixture which is forming is transported in the direction of an outlet
opening or a die.
[0010] Such extruder devices are also called "compounders." Use of such an extruder device
surprisingly enables the production of a homogeneous mixture from a granulate with
grains having an average grain size in the range of 1 µm to 10 mm which forms the
metallic matrix phase and a reinforcement phase which is, for example, formed from
particles with an average grain diameter of less than 100 µm or short fibers with
a thickness of 5 to 10 µm. The production of a homogenous mixture starting with materials
with such different average grain diameters has not been possible up to now according
to the prior art.
[0011] The composite material which can be produced with the method is present in solid
form. In this connection these can particularly be conventional profiles which can
be produced by means of extrusion. The profiles can be rods, hollow profiles and similar
for example. Furthermore the method according to the invention can also be used to
produce precursor products for the production of a composite material. Such precursor
products can be either solid or fluid. A solid precursor product can be a granulate
in particular which can be produced by breaking up previously produced rods. While
still in fluid form the precursor product can however also be fed after passing through
the outlet opening of the extruder device directly to a further device for the production
of molded parts.
[0012] According to the method of the invention it is provided that the reinforcement particles
and the at least partially melted metallic matrix phase are mixed. In this connection
it can happen that the reinforcement particles are brought into contact with the metallic
matrix phase before or during the partial melting of same. It is advantageous, however,
when the metallic matrix phase is at least partially melted before being brought into
contact with the reinforcement phase. A "partial melting" of the metallic matrix phase
is done by heating same to a temperature above the solidus temperature and below the
liquidus temperature. In this connection the metallic matrix phase can first be heated
to a temperature above the liquidus temperature and then cooled to the range between
liquidus and solidus temperature. However, it is also possible to only heat the metallic
matrix phase to a temperature above the solidus temperature and below the liquidus
temperature. By cooling the mixture to a temperature below the solidus temperature
of the metallic matrix phase before or during passing through the die, it is advantageously
possible to break up the solidified mixture into a granulate. However, it is also
possible to cut the solidified mixture into rod-shaped semi-finished products, wires,
bars or rods with a predetermined length.
[0013] According to an advantageous embodiment it is provided that the metallic matrix phase
and/or the reinforcement particles are fed to the extruder device in an atmosphere
of inert gas. This makes it relatively easy to avoid an undesired reaction with oxygen
and/or nitrogen.
[0014] According to a further embodiment it is provided that the metallic matrix phase is
fed in the form of solid metal particles. The metal particles are advantageously made
of magnesium, zinc or aluminum or an alloy predominantly containing one of the preceding
metals.
[0015] Although the feeding of the metallic matrix phase in the form of solid metal particles
is preferred, it is also possible to feed the metallic matrix phase to the extruder
device in a melted or partially melted state.
[0016] The reinforcement particles can be produced from a metallic and/or a non-metallic,
inorganic material. In case metallic materials are used, materials which have a low
solubility during the metallic matrix phase are selected. Such non-metallic materials
include in particular ceramic materials, for example aluminum oxide or SiC, or other
suitable reinforcement phases.
[0017] The reinforcement particles can be in the form of fibers and/or particles. In this
connection the fibers advantageously have a thickness in the range of 3 to 20 µm.
Furthermore they can have a length in the range of 5 µm to 10 mm.
[0018] The particles advantageously have an average diameter of 10 nm to 100 µm. The method
according to the invention enables the production of a homogeneous starting product
even when the average diameter of the metal particles and the reinforcement particles
significantly differ from one another.
[0019] According to a further advantageous embodiment it is provided that the metal particles
are only partially melted while being transported in the direction of the die in the
second portion of the extruder device. The partially melting of the metal particles
is done by setting a temperature which is in the 2-phase area between the solidus
and the liquidus temperature. In this range the matrix phase is only partially fluid,
i.e. it consists of a mixture of solid phase and molten mass. Reinforcement particles
introduced therein are distributed particularly homogeneously. In particular the crystals
already located in the molten mass prevent segregation by gravitational sinking and/or
the creation of agglomerates. This enables a particularly homogeneous mixture with
the reinforcement particles.
[0020] According to a further embodiment the mixture which is leaving the die in a fluid
state is fed to a casting device. The casting device can be a device for performing
a gravitational casting method, a pressure casting method, an injection casting method
or a thixomolding method. Energy can be saved with the suggested method. Regardless
of this, this can be used to accelerate a method for the production of a molded part.
[0021] According to a further advantageous embodiment a contact time between the at least
partially melted metallic matrix phase and the reinforcement phase is less than 20
minutes, preferably less than 15 minutes. Due to this extremely short contact time
undesired reactions between the metallic molten mass and the reinforcement phase and/or
the formation of undesired metastable phases can be avoided. A composite material
produced from the starting product according to the invention exhibits improved properties.
[0022] The extruder device can have at least one, preferably two, worm shafts for the transport.
In particular, a double worm shaft extruder device which has two parallel arranged,
advantageously partially intermeshing worm shafts has been shown to be particularly
suitable for performing the method according to the invention. An outstanding homogeneity
of the produced mixture can be achieved therewith.
[0023] The homogeneity can still be increased even more according to a further embodiment
by means of equipping the extruder device with at least one mixing device. These can
be intermeshing, gear wheel-like devices on the worm shafts of the double worm shaft
extruder device.
[0024] According to a further provision the use of the precursor product according to the
invention is provided for the production of a molded part produced by a casting method.
The casting method can be a gravitational casting method, a pressure casting method,
an injection casting method and similar. It has been shown to be particularly advantageous
to use the starting product for the so-called "thixomolding method". Thixomolding
methods are known for example from
EP 0 409 966 B1.
[0025] Hereinafter, an example of an embodiment of the invention will be explained in more
detail with reference to the drawings. The figures are listed below:
- Fig. 1
- a picture of the texture of a first composite material,
- Fig. 2
- a picture of the texture of a second composite material (prior art) and
- Fig. 3
- a schematic sectional view of an extruder device.
[0026] Fig. 1 shows a reflected light microscopic view of a composite material produced
by means of the method according to the invention. A magnesium alloy has been used
as the starting material for the metallic phase, which contains 9 % in weight aluminum
and 1% in weight zinc (AZ91). Particles produced from SiC with an average grain size
of 5 to 15 µm, preferably approximately 10 µm, have been used for the reinforcement
phase. The portion of the reinforcement phase has been 10 % by volume.
[0027] The metallic matrix phase has been heated to a temperature in the range between the
solidus and the liquidus temperature to produce the composite material. The reinforcement
phase has been added to the partially fluid molten mass. Due to the crystals, magnesium
mixed crystals in this case, contained in the partially fluid molten mass, segregation
or formation of agglomerates does not occur between the reinforcement phase. The particles
of the reinforcement phase are kept uniformly distributed in the volume, wherein segregations
are prevented by the primary crystals located between the reinforcement phase.
[0028] Fig. 2 (prior art) shows the same alloy, wherein the metallic matrix phase has been
heated here however to a temperature above the liquidus temperature and then the reinforcement
phase has been added. It can be observed here that the reinforcement phase is not
as uniformly distributed as with the method using a partially fluid metal molten mass.
This is attributed to the circumstance that, due to the lack of the magnesium primary
phase, the reinforcement phase has more freedom of movement in the molten mass and
therefore there a formation of segregations and/or agglomerates has a higher probability.
[0029] For the extruder device shown in Fig. 3 a worm shaft which can be driven with a drive
3 is housed in a cylinder 1. According to an advantageous embodiment two worm shafts
2 can also be provided in the cylinder 1. A die which is advantageously provided with
a cooler is designated with the reference numeral 4. A first feeder device 5 is provided
for feeding metal granulate in a first portion of the cylinder 1 located in the vicinity
of the drive 3. The first feeder device comprises a suction conveyor 6, a first feeding
hopper 7 set downstream, a first dosing worm shaft 8 and a first feeding shaft 9 which
is provided with a first connection 10 for feeding inert gas. The inert gas can be
argon for example.
[0030] A second feeder device 11 for feeding reinforcement phase is provided in a second
portion of the cylinder 1 which is located in the vicinity of the die 4, downstream
to the first portion. The second feeder device 11 comprises a second feeding hopper
12, a second dosing worm shaft 13 set downstream, a second feeding shaft 14 with a
second connection 15 for feeding inert gas. Reference numeral 16 designates a fixed
strand leaving the die 4 and reference numeral 17 designates strip heaters which surround
the cylinder 1.
[0031] The device is operated as follows to perform the method according to the invention:
[0032] For example magnesium granulate having grains with an average diameter of 4 mm is
drawn in by the suction conveyor 6 and is fed to the cylinder 1 in the first portion
via the first feeding hopper 7 as well as the first dosing worm shaft 8 via the feeding
shaft 9 under an atmosphere of inert gas. The magnesium granulate is transported with
the worm shaft 2 in the direction of the die 4. In this connection it is heated to
a temperature above the solidus temperature with the strip heaters 17. The magnesium
granulate is at least partially melted in the region of the second portion. In the
second portion reinforcement particles are added in turn under an atmosphere of inert
gas via the second feeding hopper 12, the second dosing worm shaft 13 and the second
feeding shaft 14. In this connection this can be short fibers with a thickness of
5 to 10 µm which are several centimeters in length. In the second portion the reinforcement
phase is mixed intensively with the partially melted magnesium by means of the rotation
of the worm shaft 2 and then enters the die 4. There the mixture is cooled and leaves
the die in the form of the strand 16. The strand 16 can then be broken up into granules.
The produced granulate is used as the starting product for the production of composite
materials. In particular it can be processed further with the thixomolding method.
[0033] According to a variant of the suggested method, it is also possible to feed the mixture
while still in its fluid state when it leaves the die 4, for example, directly to
a casting device set downstream, in particular a thixomolding device or a pressure
casting device.
List of Reference Numerals
[0034]
| 1 |
Cylinder |
| 2 |
Worm shaft |
| 3 |
Drive |
| 4 |
Die |
| 5 |
First feeder device |
| 6 |
Suction conveyor |
| 7 |
First feeding hopper |
| 8 |
First dosing worm shaft |
| 9 |
First feeding shaft |
| 10 |
First connection |
| 11 |
Second feeder device |
| 12 |
Second feeding hopper |
| 13 |
Second dosing worm shaft |
| 14 |
Second feeding shaft |
| 15 |
Second connection |
| 16 |
Strand |
| 17 |
Strip heaters |
1. Method for the production of a composite material having a metallic matrix phase and
a reinforcement phase or of a precursor product for the production of a composite
material with the following steps:
Providing an extruder device having at least one worm shaft (2) for transport and
a die (4),
Feeding the metallic matrix phase in a first portion of the extruder device,
Transport of the metallic matrix phase in the direction of the die (4) by means of
rotation of the worm shaft (2),
At least partially melting the metallic matrix phase,
Feeding reinforcement particles forming the reinforcement phase in the region of a
second portion of the extruder device,
Producing a mixture created from the reinforcement particles and the at least partially
melted metallic matrix phase by means of the rotation of the worm shaft and further
transport of the mixture through the die (4) by means of rotation of the worm shaft,
wherein the mixture is cooled to a temperature below the solidus temperature of the
metallic matrix phase before or during passing through the die (4).
2. Method according to claim 1, wherein the metallic matrix phase and/or the reinforcement
particles are fed to the extruder device under an atmosphere of inert gas.
3. Method according to one of the preceding claims, wherein the metallic matrix phase
is fed in the form of solid metal particles.
4. Method according to claim 3, wherein the metal particles are formed from magnesium,
zinc or aluminum or an alloy predominantly containing one of the preceding metals.
5. Method according to one of claims 3 or 4, wherein the metal particles form a granulate
with grains having an average diameter in the range of 1, µm to 10 mm.
6. Method according to one of the preceding claims, wherein the reinforcement particles
are produced from a metallic and/or non-metallic, inorganic material.
7. Method according to one of the preceding claims, wherein the reinforcement particles
are present in the form of fibers and/or particles.
8. Method according to claim 7, wherein the fibers have a thickness in the range of 3
to 20 µm.
9. Method according to one of claims 7 or 8, wherein the fibers have a length in the
range of 5 µm to 10 mm.
10. Method according to one of the preceding claims, wherein the particles have an average
diameter in the range of 10 nm to 100 µm.
11. Method according to one of the preceding claims, wherein the metal particles are at
least partially melted in the second portion of the extruder device during the transport
in the direction of the die (4).
12. Method according to one of the preceding claims, wherein the solidified mixture is
broken up into granules.
13. Method according to one of the preceding claims, wherein a contact time between the
at least partially melted metallic matrix phase and the reinforcement phase is less
than 20 minutes, preferably less than 15 minutes.
14. Method according to one of the preceding claims, wherein the extruder device has two
partially intermeshing worm shafts for the transport.
15. Method according to one of the preceding claims, wherein the extruder device has at
least one mixing equipment.
1. Verfahren zur Herstellung eines eine metallische Matrixphase und eine Verstärkungsphase
aufweisenden Verbundwerkstoffs oder eines Vorprodukts zur Herstellung eines Verbundwerkstoffs
mit folgenden Schritten:
Bereitstellen einer Extrudiervorrichtung mit zumindest einer Schneckenwelle (2) zum
Transport und einem Mundstück (4),
Zuführen der metallischen Matrixphase in einem ersten Abschnitt der Extrudiervorrichtung,
Transport der metallischen Matrixphase in Richtung des Mundstücks (4) mittels einer
Drehung der Schneckenwelle (2),
zumindest teilweises Aufschmelzen der metallischen Matrixphase,
Zuführen von die Verstärkungsphase bildenden Verstärkungspartikeln im Bereich eines
zweiten Abschnitts der Extrudiervorrichtung,
Herstellen eines aus den Verstärkungspartikeln und der zumindest teilweise aufgeschmolzenen
metallischen Matrixphase gebildeten Gemischs mittels der Drehung der Schneckenwelle
und weiterer Transport des Gemischs durch das Mundstück (4) mittels einer Drehung
der Schneckenwelle, wobei das Gemisch vor oder während des Durchtritts durch das Mundstück
(4) auf eine Temperatur unterhalb der Solidustemperatur der metallischen Matrixphase
abgekühlt wird.
2. Verfahren nach Anspruch 1, wobei die metallische Matrixphase und/oder die Verstärkungspartikel
unter einer Schutzgasatmosphäre der Extrudiervorrichtung zugeführt werden.
3. Verfahren nach einem der vorhergehenden Ansprüche, wobei die metallische Matrixphase
in Form fester Metallpartikel zugeführt wird.
4. Verfahren nach Anspruch 3, wobei die Metallpartikel aus Magnesium, Zink oder Aluminium
oder aus einer eines der vorgenannten Metalle vorwiegend enthaltenden Legierung gebildet
sind.
5. Verfahren nach einem der Ansprüche 3 oder 4, wobei die Metallpartikel ein Granulat
mit Körnern bilden, welchen einen mittleren Durchmesser im Bereich von 1 µm bis 10
mm aufweisen.
6. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Verstärkungspartikel
aus einem metallischen und/oder nichtmetallischen anorganischen Material hergestellt
sind.
7. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Verstärkungspartikel
in Form von Fasern und/oder Partikeln vorliegen.
8. Verfahren nach Anspruch 7, wobei die Fasern eine Dicke im Bereich von 3 bis 20 µm
aufweisen.
9. Verfahren nach einem der Ansprüche 7 oder 8, wobei die Fasern eine Länge im Bereich
von 5 µm bis 10 mm aufweisen.
10. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Partikel einen mittleren
Durchmesser von 10 nm bis 100µm aufweisen.
11. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Metallpartikel beim Transport
in Richtung des Mundstücks (4) im zweiten Abschnitt der Extrudiervorrichtung zumindest
teilweise aufgeschmolzen werden.
12. Verfahren nach einem der vorhergehenden Ansprüche, wobei das erstarrte Gemisch zu
einem Granulat zerkleinert wird.
13. Verfahren nach einem der vorhergehenden Ansprüche, wobei eine Kontaktzeit zwischen
der zumindest teilweise aufgeschmolzenen metallischen Matrixphase und der Verstärkungsphase
weniger als 20 Minuten, vorzugsweise weniger als 15 Minuten, beträgt.
14. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Extrudiervorrichtung
zum Transport zwei teilweise ineinandergreifende Schneckenwellen aufweist.
15. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Extrudiervorrichtung
zumindest eine Mischeinrichtung aufweist.
1. Procédé de fabrication d'un matériau composite comportant une phase de matrice métallique
et une phase de renfort ou d'un produit précurseur pour la fabrication d'un matériau
composite selon les étapes suivantes:
mise à disposition d'un dispositif d'extrusion comportant au moins un arbre de vis
sans fin (2) pour le transport et une buse (4),
chargement de la phase de matrice métallique sur une première partie du dispositif
d'extrusion,
transport de la phase de matrice métallique dans la direction de la buse (4) par rotation
de l'arbre de vis sans fin (2),
fusion au moins partielle de la phase de matrice métallique,
chargement des particules de renfort constituant la phase de renfort dans la zone
d'une seconde partie du dispositif d'extrusion,
fabrication d'un mélange créé à partir des particules de renfort et de la phase de
matrice métallique au moins partiellement fondue par rotation de l'arbre de vis sans
fin et transport ultérieur du mélange à travers la buse (4) par rotation de l'arbre
de vis sans fin, où le mélange est refroidi à une température en dessous de la température
de solidification de la phase de matrice métallique avant ou durant le passage à travers
la buse (4).
2. Procédé selon la revendication 1, où la phase de matrice métallique et/ou les particules
de renfort sont chargées sur le dispositif d'extrusion sous atmosphère de gaz inerte.
3. Procédé selon l'une des revendications précédentes, où la phase de matrice métallique
est chargée sous forme de particules métalliques solides.
4. Procédé selon la revendication 3, où les particules métalliques sont formées à partir
de magnésium, de zinc ou d'aluminium ou d'un alliage principalement contenu dans l'un
des métaux précédents.
5. Procédé selon l'une des revendications 3 ou 4, où les particules métalliques forment
un granulé avec des grains d'un diamètre moyen dans une plage comprise entre 1 µm
et 10 mm.
6. Procédé selon l'une des revendications précédentes, où les particules de renfort sont
fabriquées à partir d'un matériau inorganique métallique et/ou non métallique.
7. Procédé selon l'une des revendications précédentes, où les particules de renfort sont
présentes sous forme de fibres et/ou de particules.
8. Procédé selon la revendication 7, où les fibres ont une épaisseur dans une plage comprise
entre 3 et 20 µm.
9. Procédé selon l'une des revendications 7 ou 8, où les fibres ont une longueur dans
une plage comprise entre 5 µm et 10 mm.
10. Procédé selon l'une des revendications précédentes, où les particules ont un diamètre
moyen dans une plage comprise entre 10 nm et 100 µm.
11. Procédé selon l'une des revendications précédentes, où les particules métalliques
sont au moins partiellement fondues dans la seconde partie du dispositif d'extrusion
durant le transport dans la direction de la buse (4).
12. Procédé selon l'une des revendications précédentes, où le mélange solidifié est concassé
en granulés.
13. Procédé selon l'une des revendications précédentes, où un temps de contact entre la
phase de matrice métallique au moins partiellement fondue et la phase de renfort est
inférieur à 20 minutes, de préférence inférieur à 15 minutes.
14. Procédé selon l'une des revendications précédentes, où le dispositif d'extrusion a
deux arbres de vis sans fin partiellement entrecroisés pour le transport.
15. Procédé selon l'une des revendications précédentes, où le dispositif d'extrusion a
au moins un équipement mélangeur.
REFERENCES CITED IN THE DESCRIPTION
This list of references cited by the applicant is for the reader's convenience only.
It does not form part of the European patent document. Even though great care has
been taken in compiling the references, errors or omissions cannot be excluded and
the EPO disclaims all liability in this regard.
Patent documents cited in the description