IP Library Granted Patent US 10,119,184
Granted Patent B2
US 10,119,184 · App. 14/847,303 · Granted Nov 6, 2018

High strength forged aluminum alloy products

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Quick Facts
Patent No.
US 10,119,184
App. No.
14/847,303
Granted
Nov 6, 2018
Kind
B2
Abstract

High strength forged aluminum alloys and methods for producing the same are disclosed. The forged aluminum alloy products may have grains having a high aspect ratio in at least two planes, generally the L-ST and the LT-ST planes. The forged aluminum alloy products may also have a high amount of texture. The forged products may realize increased strength relative to conventionally prepared forged products of comparable product form, composition and temper.

Claims (29)

1. A forged aluminum alloy product comprising:

a crystalline microstructure having grains;

wherein the grains include first type grains and second type grains;

wherein the crystalline microstructure comprises from 5 vol. % to 50 vol. % of the first type grains;

wherein the first type grains at least include representative first grains;

wherein the representative first grains make up 60-90 vol. % of the first type grains;

wherein the representative first grains have an average aspect ratio of from 3.5:1 to 20:1 in the LT-ST plane;

wherein the representative first grains have an average aspect ratio of from 6:1 to 30:1 in the L-ST plane; and

wherein at least portions of the forged aluminum alloy product have a sectional thickness of at least 1 inch; and

wherein the aluminum alloy of the forged aluminum alloy product is a 2xxx aluminum alloy.

2. The forged aluminum alloy product of claim 1 , wherein the representative first grains have an average aspect ratio of at least 7:1 in the L-ST plane.

3. The forged aluminum alloy product of claim 1 , wherein the forged aluminum alloy product realizes a maximum ODF intensity of at least 30.

4. The forged aluminum alloy product of claim 1 , wherein a (111) pole figure of the forged aluminum alloy product comprises a plurality of maximum intensity representations, and wherein the maximum intensity representations are substantially symmetrical.

5. The forged aluminum alloy product of claim 1 , wherein the forged aluminum alloy product realizes a longitudinal (L) tensile yield strength of at least 72 ksi.

6. The forged aluminum alloy product of claim 5 , wherein the forged aluminum alloy product realizes a long transverse (LT) tensile yield strength of at least 76 ksi, and wherein the strength properties are realized at the sectional thickness of at least 1 inch of the forged product.

7. The forged aluminum alloy product of claim 5 , wherein at least portions of the forged aluminum alloy product have a sectional thickness of at least 2 inches, and wherein the strength properties are realized at the sectional thickness of at least 2 inches of the forged aluminum alloy product.

8. The forged product of claim 1 , wherein the representative first grains have an average aspect ratio of at least 5.5:1 in the LT-ST plane.

9. The forged product of claim 1 , wherein the representative first grains have an average aspect ratio of at least 6:1 in the LT-ST plane.

10. The forged aluminum alloy product of claim 8 , wherein the representative first grains have an average aspect ratio of at least 7:1 in the L-ST plane.

11. The forged aluminum alloy product of claim 8 , wherein the representative first grains have an average aspect ratio of at least 9:1 in the L-ST plane.

12. The forged aluminum alloy product of claim 8 , wherein the representative first grains have an average aspect ratio of at least 11:1 in the L-ST plane.

13. The forged aluminum alloy product of claim 8 , wherein the representative first grains have an average aspect ratio of at least 13:1 in the L-ST plane.

14. The forged aluminum alloy product of claim 8 , wherein the representative first grains have an average aspect ratio of at least 14:1 in the L-ST plane.

15. The forged product of claim 14 , wherein the representative first grains have an average aspect ratio of not greater than 30:1 in the L-ST plane.

16. The forged product of claim 10 , wherein the forged aluminum alloy product realizes a maximum ODF intensity of at least 40.

17. The forged product of claim 11 , wherein the forged aluminum alloy product realizes a maximum ODF intensity of at least 50.

18. The forged product of claim 12 , wherein the forged aluminum alloy product realizes a maximum ODF intensity of at least 55.

19. The forged product of claim 1 , wherein the 2xxx aluminum alloy comprises 2-6 wt. % Cu, 0.1-1.0 wt. % Mg, up to 2 wt. % Li, up to 1 wt. % Mn, and up to 1 wt. % Ag.

20. The forged product of claim 1 , wherein the 2xxx aluminum alloy is a 2xxx+Li aluminum alloy.

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 Sep 8, 2015
From: BUSH, DUSTIN M.; COLVIN, EDWARD L.; RIOJA, ROBERTO J.; SAWTELL, RALPH R.
To: ALCOA INC.
Reel/Frame 036513/0882 →