Method for manufacturing a metallic component

Patent metadata

Field	Value
Publication number	US-9808865-B2
Application number	US-201514610063-A
Country	US
Kind code	B2
Filing date	Jan 30, 2015
Priority date	Jan 30, 2015
Publication date	Nov 7, 2017
Grant date	Nov 7, 2017

Abstract

A method for manufacturing a metallic component is disclosed. The method includes forming a metallic component with a support structure using an additive manufacturing process. The support structure includes support walls arranged to form flow passages with a predetermined cross-sectional area. The method also includes placing the metallic component with the support structure into a chamber and sealing the chamber. The method further includes introducing a fuel mixture into the chamber after sealing the chamber. The method still further includes igniting the fuel mixture in the chamber to remove one or more of the support walls of the support structure from the metallic component.

First claim

What is claimed is:

1. A method for manufacturing a metallic component, the method comprising:
forming the metallic component with a support structure using an additive manufacturing process, the support structure including support walls arranged to form flow passages with each passage including a cross-sectional area that is large enough to allow a fuel mixture to flow there through and a flame to propagate there through without choking the flow of the fuel mixture and without choking the flame propagation;
placing the metallic component with the support structure into a chamber and sealing the chamber;
introducing the fuel mixture into the chamber after sealing the chamber; and
igniting the fuel mixture in the chamber to remove one or more of the support walls of the support structure from the metallic component.

2. The method of claim 1 , wherein introducing the fuel mixture into the chamber includes introducing the fuel mixture into at least one of the flow passages.

3. The method of claim 2 , wherein the support walls that form the at least one of the flow passages are removed by igniting the fuel mixture.

4. The method of claim 1 , further comprising:
introducing a second fuel mixture into the chamber after igniting the fuel mixture; and
igniting the second fuel mixture to remove one or more of the support walls of the support structure from the metallic component.

5. The method of claim 1 , wherein each of the support walls includes a thickness up to 0.020 inches.

6. The method of claim 1 , wherein each of the support walls includes a thickness from 0.002 inches to 0.020 inches.

7. The method of claim 1 , further comprising pressurizing the chamber prior to igniting the fuel mixture.

8. The method of claim 1 , further comprising evacuating the air from the chamber after sealing the chamber and before introducing the fuel mixture into the chamber.

9. A method for manufacturing a metallic component, the method comprising:
determining a layout for a support structure for an overhanging surface of the metallic component, the support structure including support walls arranged in a lattice structure and forming flow passages with each passage including a cross-sectional area larger than a predetermined amount;
forming the metallic component with the support structure using an additive manufacturing process;
placing the metallic component with the support structure into a chamber and sealing the chamber;
introducing a fuel mixture into the chamber after sealing the chamber; and
igniting the fuel mixture in the chamber to remove one or more of the support walls of the support structure from the metallic component.

10. The method of claim 9 , wherein each of the support walls includes a thickness up to 0.020 inches.

11. The method of claim 9 , further comprising pressurizing the chamber prior to igniting the fuel mixture.

12. The method of claim 9 , further comprising evacuating the air from the chamber after sealing the chamber and before introducing the fuel mixture into the chamber.

13. The method of claim 9 , wherein the steps of introducing the fuel mixture into the chamber and igniting the fuel mixture in the chamber are performed multiple times until all of the support structure is removed from the metallic component.

14. The method of claim 9 , wherein introducing the fuel mixture into the chamber includes introducing the fuel mixture into at least one of the flow passages.

15. A method for manufacturing a metallic component, the method comprising:
forming the metallic component with a support structure using an additive manufacturing process, the support structure including support walls with a thickness up to 0.020 inches arranged in a lattice structure and forming flow passages with each passage including a cross-sectional area that is large enough to allow a fuel mixture and a flame to propagate there through without choking the flow and the flame propagation;
removing the metallic component and the support structure from a build plate used during the forming of the metallic component;
placing the metallic component with the support structure removed from the build plate into a chamber that is explosion-proof and sealing the chamber;
introducing the fuel mixture into the chamber after sealing the chamber including introducing the fuel mixture into at least one of the flow passages; and
igniting the fuel mixture in the chamber to remove one or more of the support walls of the support structure from the metallic component.

16. The method of claim 15 , further comprising pressurizing the chamber prior to igniting the fuel mixture.

17. The method of claim 16 , wherein the support walls that form the at least one of the flow passages are removed by igniting the fuel mixture.

18. The method of claim 15 , wherein the steps of introducing the fuel mixture into the chamber and igniting the fuel mixture in the chamber are performed multiple times until all of the support structure is removed from the metallic component.

19. The method of claim 15 , further comprising evacuating the air from the chamber after sealing the chamber and before introducing the fuel mixture into the chamber.

20. The method of claim 15 , wherein the fuel mixture includes fuel and oxygen.

Assignees

• Solar Turbines Inc

Inventors

• Rogers Thomas John Chipman

Classifications

• B22F10/64

  by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title

• B22F10/47

  characterised by structural features · CPC title

• B22F10/28 Primary

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

• B22F3/1055 Primary

  Operations & Transport · mapped topic

• B22F2003/1058

  Operations & Transport · mapped topic