Al—Zn—Cu—Mg alloys and their manufacturing process

Patent metadata

Field	Value
Publication number	US-11976347-B2
Application number	US-201816627970-A
Country	US
Kind code	B2
Filing date	Jun 28, 2018
Priority date	Jul 3, 2017
Publication date	May 7, 2024
Grant date	May 7, 2024

Abstract

The invention concerns an extruded, rolled and/or forged aluminum-based alloy product having a thickness of at least 25 mm comprising (in weight %): Zn 6.70-7.40; Mg 1.50-1.80; Cu 2.20-2.60, with a Cu to Mg ratio of at least 1.30; Zr 0.04-0.14; Mn 0-0.5; Ti 0-0.15; V 0-0.15; Cr 0-0.25; Fe 0-0.15; Si 0-0.15; impurities ≤0.05 each and ≤0.15 total. The invention also concerns a method of making such a product. Products according to the invention are particularly advantageous because they exhibit simultaneously a low sensitivity to environmentally assisted cracking under conditions of high stress and humid environment, high strength and high toughness properties.

First claim

The invention claimed is:

1. An extruded, rolled and/or forged aluminum-based alloy product having a thickness of at least 25 mm comprising (in weight %):
Zn 6.70-7.40
Mg 1.50-1.80
Cu 2.35-2.55, wherein the Cu to Mg ratio is at least 1.30, wherein Cu+Mg is at least 3.8 wt. %,
Zr 0.04-0.14
Mn 0.2-0.5
Ti 0-0.15
V 0-0.15
Fe 0-0.15
Si 0-0.15
impurities ≤0.05 each and ≤0.15 total, and
wherein the alloy product does not contain Cr,
wherein said product has the following properties:
a) minimum life without failure after Environmentally Assisted Cracking (EAC) under conditions of high stress, at a short transverse (ST) stress level of 80% of the product tensile yield strength in ST direction, and humid environment with 85% relative humidity at a temperature of 70° C., of at least 30 days,
b) conventional tensile yield strength measured in the L direction at quarter thickness of at least 515-0.279*t MPa (t being the thickness of the product in mm),
c) K 1C toughness in the L-T direction measured at quarter thickness of at least 42-0.1 t MPa√m (t being the thickness of the product in mm).

2. The product according to claim 1 , wherein the maximum Cu/Mg ratio is 1.70.

3. The product according to claim 1 , wherein the Cu/Mg ratio is from 1.35 to 1.65.

4. The product according to claim 1 , wherein a Zn/Mg ratio is from 4.0 to 4.6.

5. The product according to claim 1 , wherein Zn+Cu+Mg is at least 10.7 wt. %.

6. The product according to claim 1 , wherein Zn+Cu+Mg is at least 11.2 wt. % and Cu+Mg is at least 4.0 wt. %.

7. The product according to claim 1 wherein the thickness thereof is from 25 to 200 mm.

8. The product according to claim 1 wherein the thickness thereof is from 50 to 150 mm.

9. The product according to claim 1 , wherein said product has the following properties:
a) a minimum life without failure after Environmentally Assisted Cracking (EAC) under conditions of high stress, at a short transverse (ST) stress level of 80% of the product tensile yield strength in ST direction, and humid environment with 85% relative humidity at a temperature of 70° C., of at least 40 days,
b) a conventional tensile yield strength measured in the L direction at quarter thickness of at least 535-0.279*t MPa (t being the thickness of the product in mm),
c) a K 1C toughness in the L-T direction measured at quarter thickness of at least 47-0.1 t MPa√m (t being the thickness of the product in mm).

10. A structural member suitable for the construction of aircraft wherein said structural member is used in wing ribs, spars and frames, comprising the product according to claim 1 .

11. An extruded, rolled and/or forged aluminum-based alloy product having a thickness of at least 25 mm consisting essentially of (in weight %):
Zn 6.70-7.40
Mg 1.50-1.80
Cu 2.35-2.55, wherein the Cu to Mg ratio is at least 1.30, wherein Cu+Mg is at least 3.8
wt. %,
Zr 0.04-0.14
Mn 0.2-0.5
Ti 0-0.15
V 0-0.15
Fe 0-0.15
Si 0-0.15
impurities ≤0.05 each and ≤0.15 total
and the balance aluminum
wherein said product has the following properties:
a) minimum life without failure after Environmentally Assisted Cracking (EAC) under conditions of high stress, at a short transverse (ST) stress level of 80% of the product tensile yield strength in ST direction, and humid environment with 85% relative humidity at a temperature of 70° C., of at least 30 days,
b) conventional tensile yield strength measured in the L direction at quarter thickness of at least 515-0.279*t MPa (t being the thickness of the product in mm),
c) K 1C toughness in the L-T direction measured at quarter thickness of at least 42-0.1 t MPa√m (t being the thickness of the product in mm).

12. The product according to claim 11 wherein the thickness thereof is from 50 to 150 mm.

13. An extruded, rolled and/or forged aluminum-based alloy product having a thickness of at least 25 mm consisting of (in weight %):
Zn 6.70-7.40
Mg 1.50-1.80
Cu 2.35-2.55, wherein the Cu to Mg ratio is at least 1.30, wherein Cu+Mg is at least 3.8 wt. %,
Zr 0.04-0.14
Mn 0.2-0.5
Ti 0-0.15
V 0-0.15
Fe 0-0.15
Si 0-0.15
impurities ≤0.05 each and ≤0.15 total
and the balance aluminum,
wherein said product has the following properties:
a) minimum life without failure after Environmentally Assisted Cracking (EAC) under conditions of high stress, at a short transverse (ST) stress level of 80% of the product tensile yield strength in ST direction, and humid environment with 85% relative humidity at a temperature of 70° C., of at least 30 days,
b) conventional tensile yield strength measured in the L direction at quarter thickness of at least 515-0.279*t MPa (t being the thickness of the product in mm),
c) K 1C toughness in the L-T direction measured at quarter thickness of at least 42-0.1 t MPa√m (t being the thickness of the product in mm).

14. The product according to claim 13 wherein the thickness thereof is from 50 to 150 mm.

15. A process for manufacture of an extruded, rolled and/or forged aluminum-based alloy product comprising:
a) casting an ingot comprising, (in weight-%)
Zn 6.70-7.40
Mg 1.50-1.80
Cu 2.35-2.55, wherein the Cu to Mg ratio is at least 1.30, wherein Cu+Mg is at least 3.8 wt. %,
Zr 0.04-0.14
Mn 0.2-0.5
Ti 0-0.15
V 0-0.15
Fe 0-0.15
Si 0-0.15

impurities ≤0.05 each and ≤0.15 total
and the balance aluminum, wherein the alloy product does not contain Cr,
b) homogenizing the ingot or billet
c) hot working said homogenized ingot or billet to an extruded, rolled and/or forged product with a final thickness of at least 25 mm;
d) solution heat treating and quenching the product;
e) stretching the product;
f) artificial aging,
wherein said product has the following properties:
a) minimum life without failure after Environmentally Assisted Cracking (EAC) under conditions of high stress, at a short transverse (ST) stress level of 80% of the product tensile yield strength in ST direction, and humid environment with 85% relative humidity at a temperature of 70° C., of at least 30 days,
b) conventional tensile yield strength measured in the L direction at quarter thickness of at least 515-0.279*t MPa (t being the thickness of the product in mm),
c) K 1C toughness in the L-T direction measured at quarter thickness of at least 42-0.1 t MPa√m (t being the thickness of the product in mm).

16. The process according to claim 15 wherein equivalent aging time t(eq) is comprised between 8 and 30 hours,
the equivalent time t(eq) at 155° C. being defined by formula:

t
⁡
(
eq
)

=

∫

exp
⁡
(

-
1

⁢
6
⁢
000
/
T

)

⁢
dt

exp
⁡
(

-
1

⁢

Assignees

• Constellium Issoire

Inventors

• Whelchel Ricky
• Nizery Erembert
• Koschel Diana
• Ehrstrom Jean-Christophe
• Arbab Alireza

Classifications

• C22F1/053 Primary

  of alloys with zinc as the next major constituent · CPC title

• C22C21/10 Primary

  with zinc as the next major constituent · CPC title