Regenerating an additively manufactured component to cure defects and alter microstructure

Patent metadata

Field	Value
Publication number	US-9364888-B2
Application number	US-201414784849-A
Country	US
Kind code	B2
Filing date	Apr 17, 2014
Priority date	Apr 19, 2013
Publication date	Jun 14, 2016
Grant date	Jun 14, 2016

Abstract

One embodiment includes a method to regenerate a component. The method includes additively manufacturing the component with at least a portion of the component in a near finished shape. The component is encased in a shell mold, the shell mold is cured, the encased component is placed in a furnace and the component is melted, the component is solidified in the shell mold, and the shell mold is removed from the solidified component.

First claim

The invention claimed is:

1. A method to manufacture a component, the method comprising:
additively manufacturing the component, at least a portion of which is in a near finished shape;
encasing the component in a shell mold;
curing the shell mold;
placing the encased component in a furnace and melting the component;
solidifying the component in the shell mold; and
removing the shell mold from the solidified component.

2. The method of claim 1 , wherein the component is additively manufactured to have voids greater than 0 percent but less than approximately 15 percent by volume.

3. The method of claim 1 , wherein the component is additively manufactured to have up to 15 percent additional material by volume in the near finished shape compared to a desired finished configuration.

4. The method of claim 3 , wherein the component is a blade or vane and the up to 15 percent additional material by volume is located at a root or a tip of an airfoil of the component.

5. The method of claim 1 , wherein encasing the component in a shell mold comprises encasing an entirety of the component in the shell mold such that an entire external surface of the component is covered by the shell mold.

6. The method of claim 5 , wherein encasing the component in the shell mold comprises a process of:
(a) dipping the entirety of the component in a ceramic slurry to form a layer of the shell mold on the entirety of the component, such that the layer is a ceramic layer; and
(b) drying the layer of the shell mold; and
(c) repeating steps (a) and (b) until an acceptable shell mold thickness is formed to encase the entirety of the component.

7. The method of claim 1 , wherein the component is additively manufactured using at least one of selective laser sintering, selective laser melting, direct metal deposition, direct metal laser sintering, direct metal laser melting, and electron beam melting.

8. The method of claim 7 , wherein the component is additively manufactured to be of a metal selected from the group consisting of a nickel-based superalloy, cobalt-based superalloy, iron-based superalloy, and mixtures thereof.

9. The method of claim 1 , wherein the component is additively manufactured to have a polycrystalline microstructure in the near finished shape.

10. The method of claim 9 , wherein solidifying the component comprises directionally solidifying the component to form a columnar grain microstructure.

11. The method of claim 9 , wherein solidifying the component comprises directionally solidifying the component to form a single crystal microstructure.

12. The method of claim 11 , wherein the single crystal structure is formed using at least one of a starter seed and a grain selector used to influence initial directional solidification of the component.

13. The method of claim 11 , and further comprising:
fusing a starter seed to the additively manufactured component.

14. The method of claim 11 , wherein the single crystal structure is formed using a pigtail grain selector on the component.

15. The method of claim 14 , wherein the pigtail is additively manufactured to be integrally and monolithically formed with a remainder of the component.

16. A method to make a component with internal passageways, the method comprising:
additively manufacturing the component with an internal passageway, at least a portion of which is in a near finished shape;
filling the internal passageway with a slurry;
curing the slurry to form a core;
encasing the component in a shell mold;
curing the shell mold;
placing the encased component in a furnace and melting the component;
solidifying the component in the shell mold; and
removing the shell mold and core from the solidified component.

17. The method of claim 16 , wherein the component is additively manufactured to have voids greater than 0 percent but less than approximately 15 percent by volume.

18. The method of claim 16 , wherein the component is additively manufactured to have up to 15 percent additional material by volume in the near finished shape compared to a desired finished configuration.

19. The method of claim 16 , wherein the component is additively manufactured to have a polycrystalline structure and wherein solidifying the component comprises directionally solidifying the component to form a single crystal or columnar grain microstructure.

20. The method of claim 19 , wherein the single crystal microstructure is formed using a pigtail grain selector on the component.

Assignees

• United Technologies Corp

Inventors

• Mcbrien John
• Castle Lea Kennard
• Spangler Brandon W
• Xu Jinquan

Classifications

• F01D5/28

  Selecting particular materials; {Particular measures relating thereto;} Measures against erosion or corrosion · CPC title

• B22C7/02 Primary

  Lost patterns · CPC title

• B22F10/25

  Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• B32B9/005

  comprising one layer of ceramic material, e.g. porcelain, ceramic tile (layered products with at least two ceramic layers composed mainly of ceramic B32B18/00) · CPC title