Additively manufactured integrated casting core structure with ceramic shell

Patent metadata

Field	Value
Publication number	US-11235491-B2
Application number	US-201916531731-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

Abstract

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.

First claim

What is claimed is:

1. A ceramic casting mold comprising:
a ceramic core portion, a first ceramic shell portion comprising a first ceramic material, and a second ceramic shell portion comprising a second ceramic material at least partially covering the first ceramic shell portion,
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, wherein the plurality of filaments, the ceramic core portion, and the first ceramic shell portion are formed using an additive manufacturing process, and wherein 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 portion 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 casting mold of claim 1 , wherein the ceramic core portion and the first ceramic shell portion are formed of the first ceramic material and the second ceramic shell portion is formed of the second ceramic material that is different from the first ceramic material.

3. The ceramic casting mold of claim 2 , wherein the second ceramic material is added to the first ceramic shell portion and a wax component connected to the first ceramic shell portion by dipping the first ceramic shell portion and the wax component into a slurry.

4. The ceramic casting mold of claim 3 , wherein the wax component is connected to an opening in the first ceramic shell portion, wherein the opening is in fluid communication with the at least one cavity between the first ceramic shell portion and ceramic core portion.

5. The ceramic casting mold of claim 2 , wherein the plurality of filaments are formed of the first ceramic material, and wherein the ceramic core portion, the plurality of filaments, and the first ceramic shell portion are monolithically formed into an integral structure using the additive manufacturing process.

6. The ceramic casting mold of claim 5 , wherein the integral structure is dipped into a ceramic slurry of the second ceramic material that forms the second ceramic shell portion thereon to form the ceramic casting mold.

7. The ceramic casting mold of claim 1 , wherein the ceramic core portion and the first ceramic shell portion form a core-shell mold which defines a cavity for investment casting a turbine blade.

8. The ceramic casting mold of claim 7 , wherein the core-shell mold includes a passageway in fluid communication with the cavity for investment casting the turbine blade.

9. The ceramic casting mold of claim 1 , wherein the plurality of filaments are cylindrical in overall shape.

10. The ceramic casting mold of claim 1 , wherein the plurality of filaments are oval in overall shape.

11. The ceramic casting mold of claim 1 , wherein the plurality of filaments are curved or non-linear.

12. 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 .

13. The ceramic casting mold of claim 1 , wherein the plurality of filaments have a cross sectional area ranging from 0.05 to 0.15 mm 2 .

14. 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.

15. The ceramic casting mold of claim 1 , wherein the second ceramic shell portion provides a variable thermal conductivity to the ceramic casting mold.

16. The ceramic casting mold of claim 1 , wherein the plurality of filaments are formed of one of the first ceramic material or the second ceramic material.

Assignees

• Gen Electric

Inventors

• Yang Xi
• Cole Michael
• Brown Michael
• Garay Gregory Terrence
• Pang Tingfan
• Przeslawski Brian David
• Konitzer Douglas Gerard

Classifications

• F05D2230/211

  by precision casting, e.g. microfusing or investment casting · CPC title

• F01D5/187

  Convection cooling · CPC title

• B22C9/086

  Filters · CPC title

• F01D5/147

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title

• C04B2235/6026

  Computer aided shaping, e.g. rapid prototyping · CPC title