Multi-piece integrated core-shell structure with standoff and/or bumper for making cast component
US-2018161855-A1 · Jun 14, 2018 · US
US11235378B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11235378-B2 |
| Application number | US-201916531842-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 5, 2019 |
| Priority date | Jun 28, 2017 |
| Publication date | Feb 1, 2022 |
| Grant date | Feb 1, 2022 |
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Integrated core-shell investment casting molds include a filament structure corresponding to a cooling hole pattern in the surface of the turbine blade, stator vane, or shroud.
Opening claim text (preview).
What is claimed is: 1. A ceramic casting mold comprising: a ceramic core portion, a first ceramic shell portion comprising a first ceramic material, a ceramic cover, and a second ceramic shell portion comprising a second ceramic material at least partially covering the first ceramic shell portion and the ceramic cover, wherein the ceramic casting mold further comprises at least one cavity between the ceramic core portion and the first ceramic shell portion, the at least one cavity adapted to define a shape of a cast component upon casting and removal of the ceramic casting mold, wherein the ceramic casting mold further comprises a plurality of filaments joining the ceramic core portion and the first ceramic shell portion, the plurality of filaments, the ceramic core portion and the first ceramic shell portion formed using an additive manufacturing process, where each of the plurality of filaments is monolithically formed with the ceramic core portion and the first ceramic shell portion and spans between the ceramic core and first ceramic shell portion, the plurality of filaments adapted to define a plurality of holes providing fluid communication between a cavity within the cast component defined by the ceramic core portion and an outer surface of the cast component upon removal of the ceramic casting mold. 2. The ceramic casting mold of claim 1 , wherein the ceramic cover is adapted to define the shape of the cast component upon casting and removal of the ceramic casting mold. 3. The ceramic casting mold of claim 1 , wherein the ceramic cover defines a portion of the first cavity. 4. The ceramic casting mold of claim 1 , further comprising a passageway in fluid communication with the at least one cavity, the passageway comprising a gate portion attached to the ceramic casting mold. 5. The ceramic casting mold of claim 4 , wherein the second ceramic shell portion at least partially covers the gate portion. 6. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion is formed by a dipping process followed by sintering. 7. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion is formed by a spraying process followed by sintering. 8. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion is configured to provide structural properties to covered portions of the first ceramic shell portion and the ceramic cover. 9. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion is configured to increase durability of covered portions of the first ceramic shell portion and the ceramic cover. 10. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion is configured to provide thermal properties to covered portions of the first ceramic shell portion and the ceramic cover. 11. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion is configured to provide variable thermal conductivity to the ceramic casting mold. 12. The ceramic casting mold of claim 1 , wherein the plurality of filaments are cylindrical or oval in shape. 13. The ceramic casting mold of claim 1 , wherein the plurality of filaments are curved or non-linear. 14. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.01 to 2 mm 2 . 15. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.01 to 0.15 mm 2 . 16. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.05 to 0.1 mm 2 . 17. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.05 to 0.2 mm 2 . 18. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.1 to 0.18 mm 2 . 19. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.01 to 2 mm 2 . 20. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a length ranging from 0.5 to 5 mm or an angle relative to the first ceramic shell portion of 5 to 35 degrees.
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