Process for making a turbulator by additive manufacturing

Patent metadata

Field	Value
Publication number	US-9511447-B2
Application number	US-201314104363-A
Country	US
Kind code	B2
Filing date	Dec 12, 2013
Priority date	Dec 12, 2013
Publication date	Dec 6, 2016
Grant date	Dec 6, 2016

Abstract

A turbulator fabrication process and a fabricated article are provided. The turbulator fabrication process includes providing a system configured for directing a first fusion energy and a second fusion energy, positioning a turbulator material on a substrate, and directing the first fusion energy and the second fusion energy toward the turbulator material and the substrate. The directing of the first fusion energy and the second fusion energy modifies the turbulator material forming one or more turbulators on the substrate. The fabricated article includes a substrate and one or more turbulators formed on the substrate. Each of the one or more turbulators includes at least one root portion providing a concave transition between the substrate and the turbulator.

First claim

What is claimed is:

1. A turbulator fabrication process, comprising:
providing a system configured for directing a first fusion energy and a second fusion energy;
positioning a turbulator material on a substrate; and then
concurrently directing the first fusion energy toward a first side of the turbulator material extending from the substrate and the second fusion energy toward a second side of the turbulator material opposite the first side and extending from the substrate;
wherein the directing of the first fusion energy and the second fusion energy shapes the first side of the turbulator material to have a first contour and the second side of the turbulator material to have a second contour, thereby forming one or more turbulators on the substrate.

2. The fabrication process of claim 1 , wherein the first fusion energy is selected from the group consisting of laser energy, an arc beam, a plasma beam, and combinations thereof.

3. The fabrication process of claim 1 , wherein the second fusion energy is selected from the group consisting of laser energy, an arc beam, a plasma beam, and combinations thereof.

4. The fabrication process of claim 1 , wherein the substrate is a portion of a combustion liner.

5. The fabrication process of claim 4 , wherein at least one of the one or more turbulators extends around the combustion liner and the forming of the turbulator is a linear uninterrupted process.

6. The fabrication process of claim 4 , wherein the turbulator extends around portions of the combustion liner and the forming of the turbulator is a linear interrupted process.

7. The fabrication process of claim 4 , wherein the turbulator extends around portions of the combustion liner and the forming of the turbulator is a non-linear process.

8. The fabrication process of claim 1 , wherein the substrate comprises a surface selected from the group consisting of a concave surface, a convex surface, a planar surface, and combinations thereof.

9. The fabrication process of claim 1 , wherein the turbulator material is a bead at least substantially devoid of concave surfaces prior to the directing the first fusion energy and the second fusion energy.

10. The fabrication process of claim 1 , wherein the directing of the first fusion energy and the second fusion energy proceeds in a direction of formation at a rate of at least 15 inches per minute.

11. The fabrication process of claim 1 , wherein the first contour and the second contour each includes a concave region.

12. A turbulator fabrication process, comprising:
providing a system configured for directing a first fusion energy and a second fusion energy;
positioning a turbulator material on a substrate; and
directing the first fusion energy and the second fusion energy toward the turbulator material and the substrate;
wherein the directing of the first fusion energy and the second fusion energy modifies the turbulator material forming one or more turbulators on the substrate; and
wherein the turbulator extends from the substrate with a first root portion proximal to the substrate providing a concave transition between the substrate and a first side of a convex region of the turbulator.

13. The fabrication process of claim 12 , wherein the first fusion energy is selected from the group consisting of laser energy, an arc beam, a plasma beam, and combinations thereof.

14. The fabrication process of claim 12 , wherein the second fusion energy is selected from the group consisting of laser energy, an arc beam, a plasma beam, and combinations thereof.

15. The fabrication process of claim 12 , wherein the substrate comprises a surface selected from the group consisting of a concave surface, a convex surface, a planar surface, and combinations thereof.

16. The fabrication process of claim 12 , wherein the turbulator material is a bead at least substantially devoid of concave surfaces prior to the directing the first fusion energy and the second fusion energy.

17. The fabrication process of claim 12 , wherein the directing of the first fusion energy and the second fusion energy proceeds in a direction of formation at a rate of at least 15 inches per minute.

18. The fabrication process of claim 12 , wherein the substrate is a portion of a combustion liner.

19. The fabrication process of claim 18 , wherein at least one of the one or more turbulators extends around the combustion liner and the forming of the turbulator is a linear uninterrupted process.

20. The fabrication process of claim 18 , wherein the turbulator extends around the portions of the combustion liner and the forming of the turbulator is a linear interrupted process.

21. The fabricated article of claim 18 , wherein the turbulator extends around portions of the combustion liner and the forming of the turbulator is a non-linear process.

22. The fabrication process of claim 12 , wherein the turbulator extends from the substrate with a second root portion proximal to the substrate providing a concave transition between the substrate and a second side of a convex region of the turbulator.

23. The fabrication process of claim 22 , wherein the first root portion and the second root portion are raised from the substrate to form at least a portion of the convex region extending from the substrate.

24. The fabrication process of claim 23 , further comprising directing a third fusion energy toward the substrate, wherein the first concave portion is formed by the second fusion energy, the second concave portion is formed by the third fusion energy, and the convex region is formed by the first fusion energy.

25. The fabrication process of claim 24 , wherein the process forms at least ninety of the turbulators.

26. The fabrication process of claim 24 , wherein the first root portion is formed by the second fusion energy and the second root portion is formed by the third fusion energy.

27. The fabrication process of claim 24 , wherein the second fusion energy and the third fusion energy trail the first fusion energy in a direction of formation.

Assignees

• Gen Electric

Inventors

• Lin Dechao
• Kottilingam Srikanth Chandrudu
• Cui Yan
• Bucci David Vincent
• Diao Xiaoxue

Classifications

• B23K26/342

  Build-up welding · CPC title

• F23R2900/03045

  Convection cooled combustion chamber walls provided with turbolators or means for creating turbulences to increase cooling · CPC title

• B23K26/354

  by melting · CPC title

• B23K2101/001

  Turbines · CPC title

• F23R3/005

  Combined with pressure or heat exchangers · CPC title