IP Library Granted Patent US 11,554,443
Granted Patent B2
US 11,554,443 · App. 15/406,306 · Granted Jan 17, 2023

Methods for producing forged products and other worked products

Inventors: Gen Satoh (Murrysville, PA); Daniel M. Myers (New Kensington, PA); Brandon H. Bodily (Broadview Heights, OH)
Assignee: Howmet Aerospace Inc.
B23K26/0093B21J5/002B23K15/0086B23K15/0093B23K15/08B23K26/342B23K26/354B23K26/3576B23K26/36B23K26/361B33Y10/00B23K2103/14
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Quick Facts
Patent No.
US 11,554,443
App. No.
15/406,306
Granted
Jan 17, 2023
Kind
B2
Abstract

The present disclosure is directed towards different embodiments of additively manufacturing and smoothing an AM preform to configure an AM preform for downstream processing (working, forging, and the like).

Claims (27)

1. A method, comprising:

a. using additive manufacturing to produce a metal shaped preform, wherein the metal shaped perform comprises a plurality of undulations on a surface of the metal shaped preform indicative of an additive manufacturing build;

b. smoothing the plurality of undulations on the surface of the metal shaped preform via an energy source sufficient to provide a workable preform configured for a further working operation;

wherein the smoothing comprises at least one of: electron beam smoothing, flash lamp melting, laser melting, arc melting, and laser ablation; and

wherein the smoothing comprises heating at least a portion of a single bead depth; and

c. working the metal shaped preform to form a final forged product, wherein the working comprises heating the metal shaped preform to a stock temperature, wherein the stock temperature is a target temperature of the preform prior to forging in a range of from 850° C. to 978° C., and wherein the final forged product is a structural aerospace component.

2. The method of claim 1 , wherein the metal shaped preform comprises smooth outer edges.

3. The method of claim 1 , wherein the using step includes using a non-powder based additive manufacturing process to build the metal shaped perform.

4. The method of claim 1 , wherein the smoothing step comprises using a first set of beam parameters to additively manufacture the metal shaped preform, followed by changing to a second set of beam parameters configured for smoothing, wherein a set of beam parameters comprises a plurality of beam variables.

5. The method of claim 4 , wherein the beam variables include: beam size, beam current, travel speed, wire feed rate, beam pattern, scan path, and combinations thereof.

6. The method of claim 5 , wherein the first set of beam parameters differ from the second set of beam parameters by a difference in at least one beam variable.

7. The method of claim 6 , wherein the wire feed rate is 0 during smoothing.

8. The method of claim 1 , comprising preheating a substrate with the energy source before the using step.

9. The method of claim 1 , wherein the using step comprises additively manufacturing the metal shaped perform via a continuous build plan.

10. The method of claim 1 , wherein the using step comprises additively manufacturing the metal shaped perform via a continuous exterior build plan.

11. The method of claim 1 , wherein the energy source for the using step is the same energy source for the smoothing step.

12. The method of claim 1 , wherein smoothing comprises, reducing a surface roughness of a measured portion of the surface of the metal shaped perform.

13. The method of claim 1 , wherein the smoothing step comprises reducing a depth to width ratio of valleys along a measured portion of the surface of the metal shaped preform.

14. The method of claim 1 , wherein the smoothing step comprises reducing a roughness along a measured portion of the metal shaped-preform, as detected with a blue light scan.

15. The method of claim 1 , wherein the smoothing step comprises increasing a temperature of a surface portion of the metal shaped preform in order to promote melting of the surface portion.

16. The method of claim 1 , wherein smoothing includes at least one of: melting, softening, and consolidating at least a portion of a deposited additive manufacturing path geometry in order to smooth the surface of the metal shaped preform.

17. The method of claim 1 , wherein smoothing comprises heating at least a portion of an exterior surface of an additive manufacturing deposit with an energy source.

18. The method of claim 1 , wherein smoothing comprises heating at least two or more bead depths into the metal shaped preform.

19. The method of claim 1 , wherein the smoothing step comprises:

defocusing the energy source from a first beam size of the energy source deployed in the using step to a second beam size for smoothing;

rastering the beam into a pattern; and

moving over the surface of the preform to affect smoothing of the surface.

Assignments (2)
CHANGE OF NAME Recorded Jun 30, 2020
From: ARCONIC INC.
To: HOWMET AEROSPACE INC.
Reel/Frame 053086/0762 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 19, 2018
From: SATOH, GEN; MYERS, DANIEL M.; BODILY, BRANDON H.
To: ARCONIC INC.
Reel/Frame 045591/0172 →
Continuity (2)
Provisional Application 62278753 · Jan 14, 2016
Related Publication 20170203386A1 · Jul 20, 2017