Method and apparatus for improving core manufacturing for gas turbine components
A system for producing a core including a core profile for use in casting. The system comprises a cavity block including an upper portion, a lower portion, and a recessed cavity in each of the upper portion and the lower portion; an adapter insert including a first portion and a second portion, the adapter insert sized to fit within the recessed cavity in each of the upper portion and the lower portion of the cavity block; and a core die insert sized to fit and be positioned within the adapter insert. The core die insert includes a sacrificial material and a hollow internal profile, with the hollow profile of the core die insert corresponding to the core profile.
1. A system for producing a core, the core having a core profile, the core for use in casting, the core profile including an external core profile, the system comprising:
a cavity block including an upper portion, a lower portion, and a recessed cavity in each of the upper portion and the lower portion,
an adapter insert including a first portion and a second portion, the adapter insert sized to fit within the recessed cavity in each of the upper portion and the lower portion of the cavity block; and,
a core die insert separate from the adapter insert and sized to fit and be positioned within the adapter insert, the core die insert including a sacrificial material, the core die insert including a hollow internal profile, the hollow internal profile of the core die insert corresponding to the core profile.
2. The system of claim 1 , wherein the cavity block includes a split line, and the system further including a feed plate positioned at the split line in the cavity block through which a core die material is capable of being injected into the system.
3. The system of claim 2 , wherein the feed plate includes an interchangeable feed plate.
4. The system of claim 3 , wherein the cavity block further includes a channel, the channel being in fluidic communication and aligned with the feed plate.
5. The system of claim 4 , wherein the core die insert includes an inlet, the channel being in fluidic communication with the inlet.
6. The system of claim 5 , wherein the adapter insert fits in the recessed cavities for supplying the core die material to the core and applying the pressure to the core die material.
7. The system of claim 1 , wherein the adapter insert includes additively manufactured material.
8. The system of claim 1 , wherein the adapter insert includes a plastic or a metallic material.
9. The system of claim 1 , wherein the core die insert includes additively manufactured material.
10. The system of claim 1 , wherein the core die insert is a single piece.
11. The system of claim 1 , wherein the core die insert includes multiple pieces.
12. The system of claim 1 , wherein the core die insert includes an internal chamber corresponding to a shape of the core for use in casting a gas turbine component.
13. The system of claim 12 , wherein the core die insert includes an internal chamber profile corresponding to the external core profile of the core.
14. The system of claim 12 , wherein the core die insert includes an external profile, where the external profile of the core die insert corresponds to a profile of the first portion of the adapter insert and the second portion of the adapter insert.
15. The system of claim 1 , wherein the sacrificial material includes water soluble material.
16. The system of claim 1 , wherein the sacrificial material includes a polymer.
17. The system of claim 16 , wherein the polymer is a water-soluble 3-D printable polymer.
18. A system for producing a gas turbine component core, the gas turbine component core having a core profile, the core profile including an external core profile, the gas turbine component core for use in casting a gas turbine component, the system comprising:
a cavity block including an upper portion, a lower portion, and a recessed cavity in each of the upper portion and the lower portion;
an adapter insert including a first portion and a second portion, the adapter insert sized to fit within the recessed cavity in each of the upper portion and the lower portion of the cavity block; and,
a core die insert separate from the adapter insert and sized to fit and be positioned within the adapter insert, the core die insert including a sacrificial material, the core die insert including a hollow internal profile, the hollow internal profile of the core die insert corresponding to the core profile.
19. The system of claim 18 , wherein the core die insert includes an internal chamber corresponding to a shape of the core for use in casting the gas turbine component;
the core die insert includes an internal chamber profile corresponding to the external core profile of the gas turbine component core;
the core die insert includes an external profile; and
wherein the external profile of the core die insert corresponds to a profile of the first portion of the adapter insert and the second portion of the adapter insert.
20. The system of claim 18 , wherein the cavity block includes a split line, and the system further includes a feed plate positioned at the split line in the cavity block through which a core die material is capable of being injected into the system;
the feed plate includes an interchangeable feed plate;
the cavity block further includes a channel, the channel being in fluidic communication and aligned with the feed plate;
the core die insert includes an inlet, the channel being in fluidic communication with the inlet; and
wherein the adapter insert fits precisely in the recessed cavities for supplying the core die material to the gas turbine component core and applying the pressure to the core die material.