IP Library Granted Patent US 9,447,484
Granted Patent B2
US 9,447,484 · App. 14/043,994 · Granted Sep 20, 2016

Methods for forming oxide dispersion-strengthened alloys

Inventors: Harry Lester Kington (Scottsdale, AZ); Donald G. Godfrey (Phoenix, AZ); Mark C. Morris (Phoenix, AZ); Michael G. Volas (Gilbert, AZ); Brian Hann (Avondale, AZ); Robert J. Dawson (Gilbert, AZ)
Assignee: HONEYWELL INTERNATIONAL INC.
C22C1/0491B22F3/1055C22C1/10C22C32/0026B22F5/04B22F9/082Y02P10/295
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Quick Facts
Patent No.
US 9,447,484
App. No.
14/043,994
Granted
Sep 20, 2016
Kind
B2
Abstract

In accordance with an exemplary embodiment, a method of forming a oxide dispersion-strengthened alloy metal includes the steps of providing, in a powdered form, an oxide dispersion-strengthened alloy composition that is capable of achieving a dispersion-strengthened microstructure, directing a low energy density energy beam at a portion of the alloy composition, withdrawing the energy beam from the portion of the powdered alloy composition, and cooling the portion of the powdered alloy composition at a rate greater than or equal to about 10 6 ° F. per second, thereby forming the oxide dispersion-strengthened alloy metal.

Claims (21)

1. A method of forming an oxide dispersion-strengthened alloy metal comprising the steps of:

providing, in a powdered form, an oxide dispersion-strengthened alloy composition that is capable of achieving a dispersion-strengthened microstructure, wherein providing the oxide dispersion-strengthened alloy composition in powdered form comprises mixing a plurality of metals and oxides forming the alloy to form a mixture, melting the mixture to form a melted mixture, and atomizing the melted mixture into the powdered form;

directing a low energy density energy beam at a portion of the alloy composition, wherein the portion of the alloy composition is provided in a layer having a thickness of less than 0.025 mm;

withdrawing the energy beam from the portion of the powdered alloy composition; and cooling the portion of the powdered alloy composition at a rate greater than or equal to 10 7 ° F. per second, thereby forming the oxide dispersion-strengthened alloy metal.

2. The method of claim 1 , wherein providing the oxide dispersion-strengthened alloy composition comprises providing a nickel chromium powder composition.

3. The method of claim 1 , wherein providing the oxide dispersion-strengthened alloy composition comprises providing a nickel aluminide powder composition.

4. The method of claim 1 , wherein providing the oxide dispersion-strengthened alloy composition comprises providing an iron aluminide or an iron-chromium-aluminium powder composition.

5. The method of claim 1 , wherein directing a low energy density energy beam at a portion of the powdered alloy composition comprises subjecting the powdered alloy composition to an additive manufacturing procedure that employs a low energy density laser beam.

6. The method of claim 5 , wherein subjecting the powdered alloy composition to the additive manufacturing procedure comprises subjecting the powdered alloy composition to a direct metal laser sintering procedure.

7. The method of claim 1 , wherein cooling the portion of the powdered alloy composition occurs immediately upon withdrawal of the energy beam.

8. The method of claim 7 , wherein cooling the portion of the powdered alloy composition occurs as a result of the withdrawal of the energy beam.

9. The method of claim 1 , further comprising directing the low energy density energy beam at a further portion of the alloy composition.

10. The method of claim 9 , further comprising withdrawing the energy beam from the further portion of the powdered alloy composition.

11. The method of claim 10 , further comprising cooling the further portion of the powdered alloy composition at a rate greater than or equal to 10 7 ° F. per second, thereby forming additional oxide dispersion-strengthened alloy metal.

12. The method of claim 11 , wherein the steps of directing the low energy density energy beam, withdrawing the energy beam, and cooling the portion of the powdered alloy composition are performed as a result of an additive manufacturing process applied to the powdered alloy composition.

13. The method of claim 12 , wherein the additive manufacturing process is direct metal laser sintering.

14. The method of claim 1 , wherein forming the oxide-dispersion strengthened alloy metal comprises forming a turbine engine component.

15. The method of claim 14 , wherein forming the turbine engine component comprises forming a turbine blade, a turbine vane, or a turbine nozzle.

16. The method of claim 1 , wherein providing the oxide-dispersion strengthened alloy in powdered form comprises providing a powder dispersion created by hydrometallurgical processing.

17. The method of claim 1 , wherein providing the oxide-dispersion strengthened alloy comprises providing an alloy having oxide dispersoids therein selected from the group consisting of: yttria, hafnia, silica, zirconia, and magnesia.

18. The method of claim 1 , wherein providing the oxide-dispersion strengthened alloy comprises providing a nickel or nickel chromium alloy having thorium oxide (ThO 2 ) dispersoids therein.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 2, 2013
From: KINGTON, HARRY LESTER; GODFREY, DONALD G.; MORRIS, MARK C.; VOLAS, MICHAEL G.; HANN, BRIAN; DAWSON, ROBERT J.
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 031332/0361 →
Continuity (1)
Related Publication 20150093279A1 · Apr 2, 2015