High temperature sintering furnace systems and methods
US-2024167767-A1 · May 23, 2024 · US
US2025256331A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2025256331-A1 |
| Application number | US-202318996648-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 17, 2023 |
| Priority date | Jul 22, 2022 |
| Publication date | Aug 14, 2025 |
| Grant date | — |
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An installation for sintering a preform includes a sintering furnace in which a load is disposed, wherein the load includes a revolution preform disposed around at least one holding tool, the at least one holding tool including a disk and a crown present on the periphery of the disk, the crown being made of compressible material capable of being eliminated by thermal oxidation, a portion of the preform being in contact with the crown before sintering.
Opening claim text (preview).
1 . An installation for sintering a revolution preform comprising a sintering furnace wherein a load is disposed, wherein the load comprises a revolution preform disposed around at least one holding tool, the at least one holding tool comprising a disk and a crown present on a periphery of the disk, the crown being made of compressible material capable of being eliminated by thermal oxidation, a portion of the preform being in contact with the crown before sintering. 2 . The installation according to claim 1 , wherein the compressible material is expanded graphite. 3 . The installation according to claim 1 , wherein the disk is made of monolithic ceramic. 4 . The installation according to claim 1 , wherein the at least one holding tool is disposed at one end of the preform along its axis of revolution. 5 . The installation according to claim 1 , wherein the revolution preform comprises matrix precursor particles in its porosities. 6 . A method for manufacturing a composite material revolution part comprising: impregnating a fibrous preform of revolution at least by particles of one or more matrix precursors, placing the fibrous preform of revolution comprising the matrix precursor particles around at least one holding tool, the at least one holding tool comprising a disk and a crown present on a periphery of the disk, the crown being made of compressible material capable of being eliminated by thermal oxidation, a portion of the preform being in contact with the crown, sintering the fibrous preform comprising the matrix precursor particles in order to form a matrix in the porosities of said fibrous preform to obtain a composite material part, the majority of the compressible material of the crown being decomposed by oxidation at the end of the sintering, removing the at least one holding tool from the composite material part obtained. 7 . The method according to claim 6 , wherein the compressible material is expanded graphite. 8 . The method according to claim 6 , wherein the impregnating of the fibrous preform also comprises the impregnation of said preform with a binder, the method further comprising debinding the fibrous preform of revolution disposed around the holding tool before the sintering. 9 . The method according to claim 6 , wherein a positioning and centering device is used during the placing the fiber preform around the at least one holding tool, the positioning device comprising at least one rod and one support, an end of the fiber preform along its axis of revolution furthest from the portion of the fiber preform in contact with the holding tool resting on the support, said support being fixed to the rod and the at least one holding tool being fixed to the rod by their center during the placement step.
with support for articles to be sintered · CPC title
of porous nature · CPC title
the porous products being formed by impregnation (B22F3/1137, B22F3/26 take precedence) · CPC title
Thermal properties, e.g. thermal expansion coefficient · CPC title
Carbon, e.g. graphite · CPC title
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