IP Library Granted Patent US 10,307,814
Granted Patent B2
US 10,307,814 · App. 15/069,686 · Granted Jun 4, 2019

Methods for producing forged products and other worked products

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Quick Facts
Patent No.
US 10,307,814
App. No.
15/069,686
Granted
Jun 4, 2019
Kind
B2
Abstract

Methods for producing forged products and other worked products are disclosed. In one embodiment, a method comprises using additive manufacturing to produce a metal shaped-preform and, after the using step, forging the metal shaped-preform into a final forged product. The final forged product may optionally be annealed.

Claims (44)

1. A method comprising:

(a) using additive manufacturing to produce a metal shaped-preform, wherein the metal shaped-preform comprises a nickel alloy, wherein the additive manufacturing comprises:

depositing layers of a first material on an upper side of a building substrate; and

depositing layers of a second material on an opposing lower side of the building substrate;

wherein at least one of the first material, the second material and the building substrate comprises the nickel alloy;

(b) after the using step (a), forging the metal shaped-preform, with the building substrate therein, into a final forged product having the building substrate therein;

wherein the forging step (b) comprises non-uniformly applying strain to the metal shaped-preform via an impression die.

2. The method of claim 1 , wherein the forging step comprises a single die forging step, wherein the single die forging step is using a single blocker die to die forge the metal-shaped preform into the final forged product.

3. The method of claim 1 , wherein at least one of the first material, the second material, or the building substrate of the metal shaped-preform comprises INCONEL.

4. The method of claim 1 , wherein the forging step comprises:

heating the metal shaped-preform to a stock temperature; and

contacting the metal shaped-preform with a forging die, wherein, when the contacting step is initiated, the forging die is a temperature that is at least 10° F. lower than the stock temperature.

5. The method of claim 4 , wherein the contacting step comprises applying sufficient force to the metal shaped-preform via the forging die to realize a true strain of from 0.05 to 1.10 in the metal shaped-preform.

6. The method of claim 1 , wherein the final forged product is a blade for a jet engine.

7. The method of claim 1 , comprising:

prior to the using step, designing the shape of the building substrate such that, after the forging step, the building substrate is located in a predetermined area of low strain of the final forged product.

8. A method comprising:

(a) using additive manufacturing to produce a metal shaped-preform, wherein the metal shaped-preform comprises an aluminum alloy, wherein the additive manufacturing comprises:

depositing layers of a first material on an upper side of a building substrate; and

depositing layers of a second material on an opposing lower side of the building substrate;

wherein at least one of the first material, the second material and the building substrate comprises the aluminum alloy;

(b) after the using step (a), forging the metal shaped-preform, with the building substrate therein, into a final forged product having the building substrate therein;

wherein the forging step (b) comprises non-uniformly applying strain to the metal shaped-preform via an impression die.

9. The method of claim 8 , wherein the forging step comprises a single die forging step, wherein the single die forging step is using a single blocker die to die forge the metal-shaped preform into the final forged product.

10. The method of claim 8 , wherein the forging step comprises:

heating the metal shaped-preform to a stock temperature; and

contacting the metal shaped-preform with a forging die, wherein, when the contacting step is initiated, the forging die is a temperature that is at least 10° F. lower than the stock temperature.

11. The method of claim 10 , wherein the contacting step comprises applying sufficient force to the metal shaped-preform via the forging die to realize a true strain of from 0.05 to 1.10 in the metal shaped-preform.

12. The method of claim 8 , wherein the final forged product is a blade for a jet engine.

13. The method of claim 8 , comprising:

prior to the using step, designing the shape of the building substrate such that, after the forging step, the building substrate is located in a predetermined area of low strain of the final forged product.

14. The method of claim 1 , wherein the building substrate is a pre-wrought base plate.

15. The method of claim 1 , wherein the first material is different than the building substrate.

16. The method of claim 8 , wherein the building substrate is a pre-wrought base plate.

17. The method of claim 8 , wherein the first material is different than the building substrate.

18. A method comprising:

(a) using additive manufacturing to produce a metal shaped-preform, wherein the metal shaped-preform comprises a titanium alloy, wherein the additive manufacturing comprises:

depositing layers of a first material on an upper side of a building substrate;

wherein at least one of the first material and the building substrate comprises the titanium alloy;

wherein the building substrate is a pre-wrought base plate; and

(b) after the using step (a), forging the metal shaped-preform, with the building substrate therein, into a final forged product having the building substrate therein;

wherein the forging step (b) comprises non-uniformly applying strain to the metal shaped-preform via an impression die.

19. The method of claim 18 , wherein the forging step (b) comprises a single die forging step, wherein the single die forging step is using a single blocker die to die forge the metal-shaped preform into the final forged product.

20. The method of claim 18 , wherein the method comprises annealing the final forged product.

Assignments (5)
CHANGE OF NAME Recorded Dec 21, 2020
From: ARCONIC INC.
To: HOWMET AEROSPACE INC.
Reel/Frame 054821/0882 →
MERGER Recorded Dec 11, 2020
From: ARCONIC INC.
To: ARCONIC INC.
Reel/Frame 054698/0521 →
MERGER Recorded Dec 11, 2020
From: ARCONIC INC.
To: ARCONIC INC.
Reel/Frame 054698/0580 →
CHANGE OF NAME Recorded Nov 11, 2016
From: ALCOA INC.
To: ARCONIC INC.
Reel/Frame 040599/0309 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 14, 2016
From: BUSH, DUSTIN M.; ROEGNER, ERIC V.; COLVIN, EDWARD L.; MUELLER, LARRY N.; RIOJA, ROBERTO J.; BODILY, BRANDON HENDRICKSON
To: ALCOA INC.
Reel/Frame 037972/0261 →