Manufacturing of a ceramic article from a metal preform or metal matrix composite preform provided by 3D-printing or 3D-weaving
10294160 ยท 2019-05-21
Assignee
Inventors
- David John Jarvis (Voorschoten, NL)
- Wayne Eric Voice (Nottingham, GB)
- Nicholas John Elsworth Adkins (Nantwich, GB)
- Hany Salamam Sayed Ali Hassanin (Birmingham, GB)
Cpc classification
B22F10/32
PERFORMING OPERATIONS; TRANSPORTING
B33Y10/00
PERFORMING OPERATIONS; TRANSPORTING
C04B35/58
CHEMISTRY; METALLURGY
C04B35/547
CHEMISTRY; METALLURGY
B33Y80/00
PERFORMING OPERATIONS; TRANSPORTING
C04B2235/40
CHEMISTRY; METALLURGY
B22F10/38
PERFORMING OPERATIONS; TRANSPORTING
C04B35/58
CHEMISTRY; METALLURGY
C04B35/65
CHEMISTRY; METALLURGY
C04B38/0025
CHEMISTRY; METALLURGY
C04B2235/614
CHEMISTRY; METALLURGY
B22F10/28
PERFORMING OPERATIONS; TRANSPORTING
B22F3/11
PERFORMING OPERATIONS; TRANSPORTING
C04B35/547
CHEMISTRY; METALLURGY
C04B38/0025
CHEMISTRY; METALLURGY
C04B2111/00982
CHEMISTRY; METALLURGY
C04B2235/46
CHEMISTRY; METALLURGY
Y02P10/25
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
B22F5/00
PERFORMING OPERATIONS; TRANSPORTING
C04B38/00
CHEMISTRY; METALLURGY
B22F3/11
PERFORMING OPERATIONS; TRANSPORTING
C04B35/65
CHEMISTRY; METALLURGY
C04B35/58
CHEMISTRY; METALLURGY
C04B35/547
CHEMISTRY; METALLURGY
Abstract
The present invention relates to a method of manufacturing a ceramic article (3) from a metal or metal matrix composite preform (1) provided by 3D-printing or by 3D-weaving. The preform (1) is placed in a heating chamber (2), and a predetermined time-temperature profile is applied in order to controllably react the preform (1) with a gas introduced into the heating chamber (2). The metal, the gas and the time-temperature profile are chosen so as to induce a metal-gas reaction resulting in at least a part of the preform (1) transforming into a ceramic. Preferred embodiments of the invention comprises a first oxidation stage involving a metal-gas reaction in order to form a supporting oxide layer (5) at the surface of the metal, followed by a second stage in which the heating chamber (2) is heated to a temperature above the melting point of the metal to increase the kinetics of the chemical reaction. The invention also relates to a number of advantageous uses of a ceramic article manufactured as described.
Claims
1. Method of manufacturing a ceramic article, the method comprising: providing a metal or metal matrix composite preform, placing the preform in a heating chamber, heating the heating chamber by applying a predetermined time-temperature profile in order to controllably react the preform with a gas introduced into the heating chamber, wherein the metal, the gas and the time-temperature profile are chosen so as to induce a metal-gas reaction resulting in at least a part of the preform transforming into a ceramic, wherein the time-temperature profile comprises a first oxidation stage in which the heating chamber is heated to below the melting point of the metal to allow metal-gas reaction in order to form a supporting oxide layer at the surface of the metal followed by a second stage in which the heating chamber is heated to a temperature above the melting point of the metal to increase the kinetics of the chemical reaction, wherein the first stage has a duration resulting in a thick enough oxide layer forming so that the article does not slump when heated to more elevated temperatures in the second stage, and a contiguous oxide layer forming so that the not yet reacted metal does not leak out when melting during the second stage, wherein there is a third stage in which the heating chamber is heated to a higher temperature than in the second stage so that phase transformation of the ceramic material takes place, and wherein the preform is provided by 3D-printing or by 3D-weaving.
2. Method according to claim 1, wherein the preform is 3D-printed using an additive manufacturing method selected from the group consisting of powder-bed, blown-powder and wire-fed.
3. Method according to claim 1, wherein the 3D-printing process deploys one or more heat sources selected from the group consisting of: laser, electron beam, plasma and incoherent light, to melt the metal.
4. Method according to claim 1, wherein the metal pre-form is 3D-printed into a shape selected from the group consisting of: a lattice, an open cellular foam, a porous article, a mould and die.
5. Method according to claim 1, comprising a first stage of oxidation treatment by a chemical, electro-chemical or plasma electrolytic anodising process in order to form a supporting oxide layer at the surface of the metal before the preform is placed in the heating chamber and then placing the preform in the heating chamber, followed by a second stage in which the heating chamber is heated to a temperature above the melting point of the metal to increase the kinetics of the chemical reaction.
6. Method according to claim 1, wherein the metal-gas reaction(s) take place at a gas pressure in the heating chamber of 0.1-10 atm.
7. Method according to claim 1, wherein the preform is fully transformed to make a fully ceramic article.
8. Method according to claim 1, wherein the preform is only partially transformed into ceramic to make a ceramic-metal composite.
9. Method according to claim 8, wherein the partially transformed ceramic-metal composite is further leached in a leaching solution to remove any remaining metal so as to create hollow ceramic tubes.
10. Method according to claim 1, wherein the preform is made of or comprises a material selected from the group consisting of aluminium, zirconium, yttrium, cerium, titanium, hafnium, tungsten, vanadium, niobium, tantalum, beryllium, iron, cobalt nickel, copper, lanthanum, lead, zinc, tin, indium, silicon, germanium, magnesium, calcium and an alloy thereof.
11. Method according to claim 1, wherein the gas introduced into the heating chamber is selected from the group consisting of is air, oxygen, nitrogen, silane, borane, methane, ammonia, hydrogen, hydrogen sulphide, halogen, phosphine, carbon dioxide and a mixture thereof.
12. Method according to claim 1, wherein the ceramic article is made of a material selected from the group consisting of a metal-oxide, a metal-nitride, a metal-silicide, a metal-boride, a metal-carbide, a metal-hydride, a metal-sulphide, metal-phosphide, metal-halide and a mixed ceramic material.
13. Method according to claim 1, wherein the type of gas in the heating chamber is changed during the process so as to create a layered ceramic article of varying composition.
14. Method according to claim 1, further comprising a subsequent step of reacting the formed ceramic article with acid.
15. Method according to claim 1 further comprising chemically washing an active metal catalyst onto the ceramic article to form a catalytic substrate lattice.
16. Method according to claim 1 further comprising providing the metal or metal matrix preform configured such that the manufactured ceramic article is configured to be used as a medical device, selected from the group consisting of a biomedical implant, an orthopaedic device, an artificial bone structure and a stem-cell scaffold.
17. Method according to claim 1 further comprising providing the metal or metal matrix preform configured such that the manufactured ceramic article is configured to be used for an application selected from the group consisting of RF antenna, dielectric, microwave, embedded sensors and photonic applications.
Description
BRIEF DESCRIPTION OF THE FIGURES
(1) The method of manufacturing a ceramic article according to the invention will now be described in more detail with regard to the accompanying figures. The figures show one way of implementing the present invention and is not to be construed as being limiting to other possible embodiments falling within the scope of the attached claim set.
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DETAILED DESCRIPTION OF AN EMBODIMENT
(12) An overall idea behind the present invention is the possibility of transforming a 3D preform into a ceramic by applying a process involving an increased temperature which results in chemical metal-gas reactions.
(13) The 3D-printing can e.g. be done by using a powder-bed, blown-powder or wire-fed additive manufacturing method, and the 3D-printing process typically deploys one or more heat sources selected from: laser, electron beam, plasma or incoherent light, to melt the metal. The actual choice may depend on what is available but also on the actual materials as some may only be available e.g. as powder.
(14) An alternative to providing the preform 1 by 3D-printing is to use 3D-weaving of metal wire; an example of such a 3D-woven preform is shown schematically in
(15) In some embodiments of the invention, the time-temperature profile comprises a first oxidation stage in which the heating chamber 2 is heated to below the melting point of the metal to allow metal-gas reaction in order to form a supporting oxide layer at the surface of the metal, followed by a second stage in which the heating chamber 2 is heated to a temperature above the melting point of the metal to increase the kinetics of the chemical reaction. This is illustrated schematically and in cross-sectional view in
(16) There may optionally be a third stage in which the heating chamber is heated to a higher temperature than in the second stage so that phase transformation of the ceramic material takes place. The three stages are shown as an exemplary time-temperature profile in
(17) An example of a ceramic article 3 in the form of a lattice manufactured as described above is shown in
(18) In some embodiments of the invention, the preform 1 is only partially transformed into ceramic to make a ceramic-metal composite. In this case, a cross sectional view of a lattice could look as shown schematically in
(19) For applications where high strength and stiffness is important, the most advantageous would often be to have a material that is fully transformed into ceramic or having the metal core areas remaining. Materials having material removed would result in a lower density and more cavities. They could e.g. find use for thermal insulation possibly in combination with aerogel being filled into the cavities.
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(22) Although the present invention has been described in connection with the specified embodiments, it should not be construed as being in any way limited to the presented examples. The scope of the present invention is set out by the accompanying claim set. In the context of the claims, the terms comprising or comprises do not exclude other possible elements or steps. Also, the mentioning of references such as a or an etc. should not be construed as excluding a plurality. The use of reference signs in the claims with respect to elements indicated in the figures shall also not be construed as limiting the scope of the invention. Furthermore, individual features mentioned in different claims, may possibly be advantageously combined, and the mentioning of these features in different claims does not exclude that a combination of features is not possible and advantageous.