Intermediate additively manufactured component

Patent metadata

Field	Value
Publication number	US-9482103-B2
Application number	US-201615167162-A
Country	US
Kind code	B2
Filing date	May 27, 2016
Priority date	Apr 19, 2013
Publication date	Nov 1, 2016
Grant date	Nov 1, 2016

Abstract

An intermediate component with an internal passageway includes a solid metallic additively manufactured component with an internal passageway in a near finished shape. The component has voids greater than 0 percent but less than approximately 15 percent by volume and up to 15 percent additional material by volume in the near finished shape compared to a desired finished configuration. Also included are a ceramic core disposed within the internal passageway of the component and an outer ceramic shell mold encasing an entirety of the component, such that an entire external surface of the component is covered by the outer ceramic shell mold.

First claim

The invention claimed is:

1. An intermediate component with an internal passageway, the intermediate component comprising:
a solid metallic additively manufactured component with an internal passageway in a near finished shape, wherein the component has voids greater than 0 percent but less than approximately 15 percent by volume and up to 15 percent additional material by volume in the near finished shape compared to a desired finished configuration;
a ceramic core disposed within the internal passageway of the component; and
an outer ceramic shell mold encasing an entirety of the component, such that an entire external surface of the component is covered by the outer ceramic shell mold.

2. The intermediate component of claim 1 , wherein the component has voids greater than 0 percent but less than approximately 1 percent by volume.

3. The intermediate component of claim 1 , wherein the component has voids greater than 0 percent but less than approximately 0.1 percent by volume.

4. The intermediate component of claim 1 , wherein the component is a fuel nozzle.

5. The intermediate component of claim 1 , wherein the component is selected from a group consisting of a turbine blade and a turbine vane.

6. The intermediate component of claim 5 , wherein the component comprises:
an airfoil; and
a root adjacent the airfoil.

7. The intermediate component of claim 6 , wherein the component further comprises:
a platform adjacent the root and the airfoil.

8. The intermediate component of claim 7 , wherein the airfoil, root, and platform are integrally formed.

9. The intermediate component of claim 6 , wherein the additional material by volume is located at the root.

10. The intermediate component of claim 6 , wherein the additional material by volume is located at a tip of the airfoil.

11. The intermediate component of claim 1 , wherein the additional material by volume is located at a position on the component where the additional material can be machined.

12. The intermediate component of claim 1 , wherein the ceramic core substantially conforms to a shape of the internal passageway.

13. The intermediate component of claim 1 , wherein the component is a metal selected from the group consisting of a nickel-based superalloy, a cobalt-based superalloy, an iron-based superalloy, and mixtures thereof.

14. The intermediate component of claim 1 , wherein the ceramic core is a material selected from the group consisting of silica, alumina, zircon, cobalt, mullite, and kaolin.

15. The intermediate component of claim 1 , wherein the ceramic shell mold is a material selected from the group consisting of silica, alumina, zircon, cobalt, mullite, kaolin, and mixtures thereof.

16. The intermediate component of claim 1 , wherein the ceramic shell mold has a thickness ranging from approximately 5 millimeters to approximately 32 millimeters.

17. The intermediate component of claim 1 , wherein the voids comprise a subsurface defect.

18. The intermediate component of claim 17 , wherein the subsurface defect is selected from a group consisting of pores and cracks.

19. The intermediate component of claim 1 , wherein the component comprises a plurality of internal passageways.

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

• B23K15/0086

  welding for purposes other than joining, e.g. build-up welding · CPC title