Rapid processing of laminar composite components
US-12180120-B2 · Dec 31, 2024 · US
US10494309B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10494309-B2 |
| Application number | US-201615746835-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2016 |
| Priority date | Aug 20, 2015 |
| Publication date | Dec 3, 2019 |
| Grant date | Dec 3, 2019 |
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A composite material comprising 50 to 95 mass % grains of primary material selected from the group consisting of talc, mica, graphite and hexagonal boron nitride, and 0.01 to 40 mass % fibers having a length of 0.05 to 20 mm, and a ratio of length to diameter of at least 5. The grains of the primary material have a mean size of 3 to 50 microns.
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The invention claimed is: 1. Composite material comprising 50 to 95 mass % grains of primary material, in which the primary material consists of talc; grains of secondary material comprising silicon carbide, zircon, mullite or garnet; and 0.01 to 40 mass % fibres having a mean length of 0.05 to 20 mm, and a ratio of length to diameter of at least 5; in which the grains of the primary material have a mean size of 3 to 150 microns; and the fibres consist of any of carbon, SiC and alumina. 2. The composite material as claimed in claim 1 , wherein the fibres have a mean length of at least 0.1 mm, the ratio of length to diameter is at least 10 and the grains of the primary material have a mean size of 5 microns. 3. The composite material as claimed in claim 1 , comprising 0.01 to 40 mass % grains of a secondary material comprising material selected from the group consisting of ceramic material, cubic boron nitride (cBN) or diamond. 4. The composite material as claimed in claim 3 , in which the secondary hard material grains have a mean size of 1 to 200 microns. 5. The composite material as claimed in claim 1 , in which the mean length of the fibres is at least 20 times their mean diameter. 6. The composite material as claimed in claim 1 , comprising at least 0.1 mass % fibres, and in which the fibres have a mean length of at least 0.5 mm. 7. The composite material as claimed in claim 1 , in which the fibres are in the form of continuous fibres, tangled fibres, multi-fibres, single fibres, or chopped fibres. 8. The composite material as claimed in claim 1 , in which at least 50% of the fibres have a length within 20% of the mean length of the fibres. 9. The composite material as claimed in claim 1 , comprising inorganic binder material. 10. The composite material as claimed in claim 1 , in which the fibres consist of carbon. 11. The composite material as claimed in claim 1 , comprising grains of cBN crystals having a mean size of at least 10 microns. 12. The composite material as claimed in claim 1 , in the form of a compact having density of at least 95% of the theoretical density of its constituent materials, the density contribution of each material weighted according to its mass % in the composite material. 13. The composite material as claimed in claim 1 , in the form of a non-bonded aggregation of powder grains. 14. A component comprising composite material as claimed in claim 1 . 15. A component as claimed in claim 14 , for a capsule for an ultra-high pressure press, comprising a gasket, a containment vessel, an electrically conducting heater element, an electrical insulation component, or a reaction compact. 16. A component as claimed in claim 14 , consisting of a gasket for a belt-type press, a tetrahedral-type press or a cubic-type press for pressurising a reaction assembly at an ultra-high pressure of at least 1 GPa; comprising composite material as claimed in claim 1 . 17. A component as claimed in claim 14 , consisting of a heater element for a belt-type press, a tetrahedral-type press or a cubic-type press for pressurising a reaction assembly at an ultra-high pressure of at least 1 GPa; comprising composite material as claimed in claim 11 . 18. A component as claimed in claim 14 , consisting of a reaction compact for synthesising cBN crystals in a belt-type press, a tetrahedral-type press or a cubic-type press for pressurising a reaction assembly at an ultra-high pressure of at least 1 GPa; comprising composite material as claimed in claim 1 . 19. A method of using a component as claimed in claim 14 , in which the component is for a capsule assembly for an ultra-high pressure press, and the method includes assembling a capsule including the component within the ultra-high pressure press, and using the ultra-high pressure press to pressurise at least a volume of the capsule assembly to at least 1 GPa. 20. A method of using a component as claimed in claim 19 , in which the component consists of a gasket for a belt-type ultra-high pressure press comprising a pair of opposable anvils and a die, and the method includes providing a pair of the components; and assembling the capsule assembly within the die, in which each component is placed against a respective end of the die. 21. A method of using a component as claimed in claim 19 , in which the component consists of a gasket for a cubic-type ultra-high pressure press, comprising three pairs of opposable anvils, and the method includes assembling the capsule assembly including the component between all three pairs of anvils.
Graphite (C04B35/536 takes precedence) · CPC title
characterised by the diameter of the fibers · CPC title
rich in magnesium oxide {, e.g. forsterite (C04B35/195 takes precedence)} · CPC title
based on boron nitride · CPC title
based on silicates other than clay {(zircon C04B35/48)} · CPC title
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