INTEGRATED CASTING CORE-SHELL STRUCTURE WITH PRINTED TUBES FOR MAKING CAST COMPONENT
The present disclosure generally relates to integrated core-shell investment casting molds that provide filament structures corresponding to cooling hole patterns on the surface of the turbine blade or stator vane, which 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 at least a portion of the filament and/or the core portion is in the shape of a hollow tube.
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 diameter of the filament has a cross sectional area ranging from 0.01 to 2 mm 2 .
6 . The method of claim 1 , wherein the filament hollow tube has an inner diameter cross-sectional area that is at least 50% of the cross sectional area of the outer diameter of the filament.
7 . The method of claim 1 , wherein the core portion is defined by a core hollow tube structure.
8 . The method of claim 1 , wherein the core hollow tube structure has an inner diameter cross-sectional area that is at least 80% of the cross sectional area of the outer diameter of the core portion.
9 . 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 at least a portion of the filament and/or the core portion is in the shape of a hollow tube;
(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.
10 . The method of claim 9 , wherein removing the ceramic casting mold from the cast component comprises a combination of mechanical force and chemical leaching.
11 . The method of claim 9 , wherein the outer diameter of the filament has a cross sectional area ranging from 0.01 to 2 mm 2 .
12 . The method of claim 9 , wherein the inner diameter of the tube has a cross-sectional area that is at least 50% of the cross sectional area of the outer diameter of the filament.
13 . The method of claim 9 , wherein the core portion is defined by a core hollow tube structure and the core hollow tube structure has an inner diameter cross-sectional area that is at least 80% of the cross sectional area of the outer diameter of the core portion.
14 . 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 at least a portion of the filament and/or the core portion is in the shape of a hollow tube.
15 . The ceramic casting mold of claim 14 , wherein the outer diameter of the filament has a cross sectional area ranging from 0.01 to 2 mm 2 .
16 . The ceramic casting mold of claim 15 , wherein the inner diameter of the tube has a cross-sectional area that is at least 50% of the cross sectional area of the outer diameter of the filament.
17 . The ceramic casting mold of claim 15 , wherein the inner diameter of the tube has a cross-sectional area that is at least 60% of the cross sectional area of the outer diameter of the filament.
18 . The ceramic casting mold of claim 14 , wherein the filament has a curved outer surface.
19 . The ceramic casting mold of claim 14 , wherein the core portion is defined by a core hollow tube structure.
20 . The ceramic casting mold of claim 14 , wherein the core hollow tube structure has an inner diameter cross-sectional area that is at least 80% of the cross sectional area of the outer diameter of the core portion.