Method for preparing a material made from aluminosilicate and method for preparing a composite material having an aluminosilicate matrix
US-2018009669-A1 · Jan 11, 2018 · US
US11642724B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11642724-B2 |
| Application number | US-201615772219-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 3, 2016 |
| Priority date | Nov 4, 2015 |
| Publication date | May 9, 2023 |
| Grant date | May 9, 2023 |
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A die or piston of a spark plasma sintering apparatus, wherein the die or piston is made from graphite and the outer surfaces of the die or piston are coated with a silicon carbide layer with a thickness of 1 to 10 micrometres, the silicon carbide layer being further optionally coated with one or more other layer(s) made from a carbide other than silicon carbide chosen from hafnium carbide, tantalum carbide and titanium carbide, the other layer(s) each having a thickness of 1 to 10 micrometres. A spark plasma sintering (SPS) apparatus comprising the die and two of the pistons, defining a sintering, densification or assembly chamber capable of receiving a powder to be sintered, a part to be densified, or parts to be assembled. A method of sintering a powder, densifying a part, or assembling two parts by means of a method of spark plasma sintering (SPS) in an oxidising atmosphere, using the spark plasma sintering (SPS) apparatus.
Opening claim text (preview).
The invention claimed is: 1. A conventional spark plasma sintering apparatus comprising a conventional die and two conventional pistons, defining a sintering, densification or assembly chamber capable of receiving a powder to be sintered, a part to be densified, or parts to be assembled, wherein said conventional die has been replaced with a coated die, wherein said coated die is made of graphite and the outer surface of said coated die is coated with a homogenous layer made of silicon carbide having a thickness of 1 to 10 μm, said layer made of silicon carbide being further optionally coated with one or more other layer(s) made of a carbide other than silicon carbide, chosen from hafnium carbide, tantalum carbide and titanium carbide, said other layer(s) each having a thickness of 1 to 10 μm, and wherein said die is configured to conduct a pulsed current from 200 to 6000 A and/or a voltage of 1 to 8 volts and wherein said die is further configured to resist degradation at temperatures of between 700° C. and 1450° C. 2. A conventional spark plasma sintering apparatus comprising a conventional die and two conventional pistons, defining a sintering, densification or assembly chamber capable of receiving a powder to be sintered, a part to be densified, or parts to be assembled, wherein both of said conventional pistons have been replaced with coated pistons, wherein each of said coated pistons is made of graphite and the outer surfaces of each of said coated pistons are coated with a homogenous layer made of silicon carbide having a thickness of 1 to 10 μm, said layer made of silicon carbide being further optionally coated with one or more other layer(s) made of a carbide other than silicon carbide, chosen from hafnium carbide, tantalum carbide and titanium carbide, said other layer(s) each having a thickness of 1 to 10 μm, and wherein each of said coated pistons are configured to conduct a pulsed current from 200 to 6000 A and/or a voltage of 1 to 8 volts and wherein said coated pistons are further configured to resist degradation at temperatures of between 700° C. and 1450° C. 3. The spark plasma sintering apparatus according to claim 1 , wherein the outer surfaces of said coated die are coated with a layer made of silicon carbide by a “CVD” chemical vapour deposition method, and said layer made of silicon carbide is further optionally coated with one or more other layer(s) made of a carbide other than silicon carbide, chosen from hafnium carbide, tantalum carbide and titanium carbide, by a “CVD” chemical vapour deposition method. 4. The spark plasma sintering apparatus according to claim 2 , in which the outer surfaces of each of said coated pistons are coated with a layer made of silicon carbide by a “CVD” chemical vapour deposition method, and said layer made of silicon carbide is further optionally coated with one or more other layer(s) made of a carbide other than silicon carbide, chosen from hafnium carbide, tantalum carbide and titanium carbide, by a “CVD” chemical vapour deposition method. 5. The spark plasma sintering apparatus according to claim 1 further comprising replacement of said conventional pistons with coated pistons, wherein each of said coated pistons is made of graphite and the outer surfaces of each of said coated pistons are coated with a layer made of silicon carbide having a thickness of 1 to 10 μm, said layer made of silicon carbide being further optionally coated with one or more other layer(s) made of a carbide other than silicon carbide, chosen from hafnium carbide, tantalum carbide and titanium carbide, said other layer(s) each having a thickness of 1 to 10 μm. 6. The spark plasma sintering apparatus according to claim 1 , further comprising a flexible graphite sheet placed within said sintering, densification or assembly chamber such that, when said powder is received therein, the flexible graphite sheet is between said powder and inner walls of said sintering, densification or assembly chamber, wherein said flexible graphite sheet is coated with a layer of boron nitride on a face thereof. 7. The spark plasma sintering apparatus according to claim 5 , wherein the two coated pistons comprise an upper piston and a lower piston, further comprising an upper electrode, a lower electrode, and a vacuum chamber, said vacuum chamber enclosing said die, said upper piston, and said lower piston, said upper electrode electrically conducted to said upper piston via upper spacers, plates or discs, said lower electrode electrically conducted to said lower piston via lower spacers, plates or discs. 8. The spark plasma sintering apparatus according to claim 7 , further comprising a flexible graphite sheet placed within said sintering, densification or assembly chamber such that, when said powder is received therein, the flexible graphite sheet is between said powder and inner walls of said sintering, densification or assembly chamber, wherein said flexible graphite sheet is coated with a layer of boron nitride on a face thereof.
Silicon carbide · CPC title
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