Integrated casting core-shell structure for making cast component with cooling holes in inaccessible locations
The present disclosure generally relates to integrated core-shell investment casting molds that provide filament structures corresponding to cooling hole patterns in the surface of the turbine blade or stator vane, including in locations that are inaccessible due to the presence of protrusion patterns. The filament structures also provide a leaching pathway for the core portion after metal casting. The invention also relates to core filaments that can be used to supplement the leaching pathway, for example in a core tip portion of the mold.
1. A method for fabricating a ceramic mold, comprising:
(a) contacting a cured portion of a workpiece with a liquid ceramic photopolymer;
(b) irradiating a portion of the liquid ceramic photopolymer adjacent to the cured portion through a window contacting the liquid ceramic photopolymer;
(c) removing the workpiece from the uncured liquid ceramic photopolymer; and
(d) repeating steps (a)-(c) until a ceramic mold is formed, the ceramic mold comprising:
(1) a core portion and a shell portion with at least one cavity between the core portion and the shell portion, the cavity adapted to define the shape of a cast component upon casting and removal of the ceramic mold, and
(2) a plurality of filaments joining the core portion and the shell portion where each filament spans between the core and shell and defines a hole in the cast component upon removal of the mold, wherein the filament intersects the core at a first point and the filament intersects the shell at a second point, and an imaginary line joining the first point and the second point also intersects an outer portion of the cavity that extends further away from the center of the mold than the second point.
2. The method of claim 1 , wherein the process comprises, after step (d), a step (e) comprising pouring a liquid metal into a casting mold and solidifying the liquid metal to form the cast component.
3. The method of claim 2 , wherein the process comprises, after step (e), a step (f) comprising removing the mold from the cast component.
4. The method of claim 3 , wherein removing the mold from the cast component comprises a combination of mechanical force and chemical leaching.
5. The method of claim 1 , wherein the outer portion forms at least part of a root component of a turbine blade or stator vane.
6. The method of claim 1 , wherein the outer portion forms at least part of a trailing edge of a turbine blade or stator vane.
7. The method of claim 1 , the outer portion forms at least part of an overhang in a turbine blade or stator vane.
8. A method of preparing a cast component comprising:
(a) pouring a liquid metal into a ceramic casting mold and solidifying the liquid metal to form the cast component, the ceramic casting mold comprising:
(1) a core portion and a shell portion with at least one cavity between the core portion and the shell portion, the cavity adapted to define the shape of a cast component upon casting and removal of the ceramic mold, and
(2) a plurality of filaments joining the core portion and the shell portion where each filament spans between the core and shell and defines a hole in the cast component, wherein the filament intersects the core at a first point and the filament intersects the shell at a second point, and an imaginary line joining the first point and the second point also intersects an outer portion of the cavity that extends further away from the center of the mold than the second point;
(b) removing the ceramic casting mold from the cast component by leaching at least a portion of the ceramic core through the holes in the cast component.
9. The method of claim 8 , wherein removing the ceramic casting mold from the cast component comprises a combination of mechanical force and chemical leaching.
10. The method of claim 8 , wherein the outer portion is part of a root component or trailing edge of a turbine blade or stator vane.
11. The method of claim 8 , wherein the outer portion is an overhang in a turbine blade or stator vane.
12. A ceramic casting mold comprising:
a core portion and a shell portion with at least one cavity between the core portion and the shell portion, the cavity adapted to define the shape of a cast component upon casting and removal of the ceramic mold, and
a plurality of filaments joining the core portion and the shell portion where each filament spans between the core and shell and defines a hole in the cast component, wherein the filament intersects the core at a first point and the filament intersects the shell at a second point, and an imaginary line joining the first point and the second point also intersects an outer portion of the cavity that extends further away from the center of the mold than the second point;
wherein the outer portion forms at least part of a root component of a turbine blade or stator vane, at least part of a trailing edge of a turbine blade or stator vane, or at least part of an overhang in a turbine blade or stator.
13. A single crystal metal turbine blade or stator vane having an inner cavity and an outer surface, a plurality of cooling holes providing fluid communication between the inner cavity and outer surface, wherein at least one hole is wherein at least one cooling hole is located such that an imaginary line joining a first point at the intersection of the cooling hole with the inner cavity and a second point at the intersection of the cooling hole with the outer surface intersects an outer portion of the turbine blade or stator vane extending further away from the center of the turbine blade or stator vane than the second point;
wherein the outer portion forms at least part of a trailing edge of a turbine blade or stator vane, or at least part of an overhang in a turbine blade or stator vane.