Lightweight honeycomb thermal insulation structure
US-2018281339-A1 · Oct 4, 2018 · US
US2024253333A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2024253333-A1 |
| Application number | US-202318162940-A |
| Country | US |
| Kind code | A1 |
| Filing date | Feb 1, 2023 |
| Priority date | Feb 1, 2023 |
| Publication date | Aug 1, 2024 |
| Grant date | — |
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A method of assembling a composite panel includes disposing a pliable matrix material between a first side of a ceramic core structure and a ceramic matrix composite face sheet, wherein the ceramic core structure comprises a plurality of hollow cells defined by a plurality of walls extending from the first side of the ceramic core structure to a second side of the ceramic core structure opposite the first side; and densifying the pliable matrix material to bond the pliable matrix material with the ceramic core structure and the ceramic matrix composite face sheet.
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We claim: 1 . A method of assembling a composite panel, the method comprising: disposing a pliable matrix material between a first side of a ceramic core structure and a ceramic matrix composite face sheet, wherein the ceramic core structure comprises a plurality of hollow cells defined by a plurality of walls extending from the first side of the ceramic core structure to a second side of the ceramic core structure opposite the first side; and densifying the pliable matrix material to bond the pliable matrix material with the ceramic core structure and the ceramic matrix composite face sheet. 2 . The method of claim 1 , wherein the pliable matrix material comprises a liquid carrier, a powder, and a polymeric binder. 3 . The method of claim 2 , wherein the powder comprises 10 percent to 90 percent carbon by weight. 4 . The method of claim 2 , wherein the powder comprises carbon and silicon carbide. 5 . The method of claim 4 , wherein the powder comprises 45 percent to 55 percent carbon by weight and 45 percent to 55 percent silicon carbide by weight. 6 . The method of claim 2 , wherein the liquid carrier comprises 50% to 70% by volume of the pliable matrix material. 7 . The method of claim 1 , wherein the pliable matrix material comprises a pliable matrix material paste. 8 . The method of claim 7 , wherein the pliable matrix material forms a fillet between the ceramic matrix composite face sheet and the ceramic core structure. 9 . The method of claim 1 , wherein the pliable matrix material comprises a pliable matrix material ply. 10 . The method of claim 1 , wherein densifying the pliable matrix material comprises densifying via melt infiltration. 11 . The method of claim 10 , wherein a densifying material is silicon, germanium, boron, or combinations thereof. 12 . The method of claim 1 , wherein densifying the pliable matrix material comprises densifying via chemical vapor infiltration. 13 . The method of claim 1 , wherein densifying the pliable matrix material comprises densifying via polymer infiltration and pyrolysis. 14 . The method of claim 1 , further comprising additively manufacturing the ceramic core structure. 15 . The method of claim 1 , wherein the plurality of walls are unitarily and monolithically formed to define the plurality of hollow cells. 16 . The method of claim 1 , further comprising disposing the pliable matrix material between the second side of the ceramic core structure and a ceramic matrix composite back sheet; and densifying the pliable matrix material to bond the pliable matrix material with the ceramic core structure and the ceramic matrix composite back sheet. 17 . A composite panel comprising: a ceramic core structure comprising a plurality of hollow cells defined by a plurality of walls extending from a first side of the ceramic core structure to a second side of the ceramic core structure, the second side opposite the first side; a ceramic matrix composite face sheet disposed at the first side of the ceramic core structure; and a matrix material that is densified and bonded with both the ceramic core structure and the ceramic matrix composite face sheet. 18 . The composite panel of claim 17 , wherein the matrix material comprises silicon carbide. 19 . The composite panel of claim 17 , further comprising: a ceramic matrix composite back sheet disposed at the second side of the ceramic core structure; and additional matrix material that is densified and bonded to both the ceramic core structure and the ceramic matrix composite back sheet. 20 . A composite panel comprising: an additively-manufactured ceramic core structure comprising a plurality of hollow cells defined by a plurality of walls extending from a top face to a bottom face; a ceramic matrix composite face sheet; and a conformal interface layer bonding the top face of the additively-manufactured ceramic core structure to the ceramic matrix composite face sheet.
Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class · CPC title
comprising such {particular} substance as the main or only constituent of a layer, {which is} next to another layer of {the same or of} a {different material (next to a glass layer B32B17/06; layered products with at least two ceramic layers composed mainly of ceramic B32B18/00)} · CPC title
comprising one layer of ceramic material, e.g. porcelain, ceramic tile (layered products with at least two ceramic layers composed mainly of ceramic B32B18/00) · CPC title
Sound absorbing structures or liners · CPC title
Carbon interlayers · CPC title
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