IP Library Granted Patent US 8,366,839
Granted Patent B2
US 8,366,839 · App. 12/617,803 · Granted Feb 5, 2013

Aluminum—copper—lithium products

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Quick Facts
Patent No.
US 8,366,839
App. No.
12/617,803
Granted
Feb 5, 2013
Kind
B2
Abstract

The present invention relates to extruded, rolled and/or forged products. Also provided are methods of making such products based on aluminum alloy wherein a liquid metal bath is prepared comprising 2.0 to 3.5% by weight of Cu, 1.4 to 1.8% by weight of Li, 0.1 to 0.5% by weight of Ag, 0.1 to 1.0% by weight of Mg, 0.05 to 0.18% by weight of Zr, 0.2 to 0.6% by weight of Mn and at least one element selected from Cr, Sc, Hf and Ti, the quantity of said element, if it is selected, being 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti, the remainder being aluminum and inevitable impurities. The products and methods of the present invention offer a particularly advantageous compromise between static mechanical strength and damage tolerance and are particularly useful in the field of aeronautical design.

Claims (165)

1. Extruded aluminum alloy product having a density less than 2.67 g/cm 3 obtained by a method comprising:

a) preparing a liquid metal bath comprising 2.45 to 2.65% by weight of Cu, 1.4 to 1.5% by weight of Li, 0.1 to 0.5% by weight of Ag, 0.1 to 1.0% by weight of Mg, 0.05 to 0.18% by weight of Zr, 0.2 to 0.6% by weight of Mn and at least one element selected from Cr, Sc, Hf or Ti, the quantity of said element being 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti, remainder aluminum and inevitable impurities;

b) casting an unwrought shape from said liquid metal bath;

c) homogenizing said unwrought shape at a temperature from 515° C. to 525° C. such that the equivalent time for homogenization

t

(

eq

)

=

exp

(

-

26100

/

T

)

t

exp

(

-

26100

/

T

ref

)

is from 5 to 20 hours, where T (in Kelvin) is the instantaneous treatment temperature, which varies with the time t (in hours), and T ref is a reference temperature set at 793 K;

d) hot working and optionally cold working said unwrought shape into an extruded product;

e) subjecting the product to a solution treatment and quenching;

f) stretching said product with a permanent set of 1 to 5%;

g) artificially aging said product by heating at 140 to 170° C. for 5 to 70 hours, wherein the toughness K Q (L-T) is at least 52 MPa√{square root over (m)} and the yield strength is at least 490 MPa.

2. Extruded product according to claim 1 comprising:

(a) the yield strength measured at 0.2% elongation in the L direction Rp 0.2 (L) expressed in MPa and the toughness thereof K Q (L-T), in the L-T direction expressed in MPa√{square root over (m)} are such that K Q (L-T)>132−0.17 Rp 0.2 (L); and/or

(b) the fracture strength thereof in the L direction R m (L) expressed in MPa and the toughness thereof K Q (L-T), in the L-T direction expressed in MPa√{square root over (m)} are such that

K Q (L-T)>182−0.25 R m (L).

3. Extruded product according to claim 1 wherein the thickness of at least one elementary rectangle thereof is at least 8 mm.

4. Structural element comprising and/or manufactured using at least one product according to claim 1 .

5. Structural element comprising at least one extruded product according to claim 1 used as a stiffener or frame for the manufacture of fuselage panels and/or aircraft wings.

6. Extruded aluminum alloy product having a density less than 2.67 g/cm 3 obtained by a method comprising:

a) preparing a liquid metal bath comprising 2.65 to 2.85% by weight of Cu, 1.5 to 1.7% by weight of Li, 0.1 to 0.5% by weight of Ag, 0.1 to 1.0% by weight of Mg, 0.05 to 0.18% by weight of Zr, 0.2 to 0.6% by weight of Mn and at least one element selected from Cr, Sc, Hf or Ti, the quantity of said element being 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti, remainder aluminum and inevitable impurities;

b) casting an unwrought shape from said liquid metal bath;

c) homogenizing said unwrought shape at a temperature from 515° C. to 525° C. such that the equivalent time for homogenization

t

(

eq

)

=

exp

(

-

26100

/

T

)

t

exp

(

-

26100

/

T

ref

)

is from 5 to 20 hours, where T (in Kelvin) is the instantaneous treatment temperature, which varies with the time t (in hours), and T ref is a reference temperature set at 793 K;

d) hot working and optionally cold working said unwrought shape into an extruded product;

e) subjecting the product to a solution treatment and quenching;

f) stretching said product with a permanent set of 1 to 5%;

g) artificially aging said product by heating at 140 to 170° C. for 5 to 70 hours, wherein the toughness K Q (L-T) is at least 45 MPa√{square root over (m)} and the yield strength is at least 520 MPa.

7. Extruded product according to claim 6 comprising:

(a) the yield strength measured at 0.2% elongation in the L direction Rp 0.2 (L) expressed in MPa and the toughness thereof K Q (L-T), in the L-T direction expressed in MPa√{square root over (m)} are such that K Q (L-T)>132−0.17 Rp 0.2 (L); and/or

(b) the fracture strength thereof in the L direction R m (L) expressed in MPa and the toughness thereof K Q (L-T), in the L-T direction expressed in MPa√{square root over (m)} are such that

K Q (L-T)>182−0.25 R m (L).

8. Extruded product according to claim 1 wherein the thickness of at least one elementary rectangle thereof is at least 8 mm.

9. Method to manufacture an extruded product based on an aluminum alloy, said method comprising:

a) preparing a liquid metal bath comprising 2.45 to 2.65% by weight of Cu, 1.4 to 1.5% by weight of Li, 0.1 to 0.5% by weight of Ag, 0.1 to 1.0% by weight of Mg, 0.05 to 0.18% by weight of Zr, 0.2 to 0.6% by weight of Mn and at least one element selected from Cr, Sc, Hf or Ti, the quantity of said element being 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti, remainder aluminum and inevitable impurities;

b) casting an unwrought shape from said liquid metal bath;

c) homogenizing said unwrought shape at a temperature from 515° C. to 525° C. such that the equivalent time for homogenization

t

(

eq

)

=

exp

(

-

26100

/

T

)

t

exp

(

-

26100

/

T

ref

)

is from 5 to 20 hours, where T (in Kelvin) is the instantaneous treatment temperature, which varies with the time t (in hours), and T ref is a reference temperature set at 793 K;

d) hot working and optionally cold working said unwrought shape into an extruded product;

e) subjecting the product to a solution treatment and quenching;

f) stretching said product with a permanent set of 1 to 5%;

g) artificially aging said product by heating at 140 to 170° C. for 5 to 70 hours; and

wherein the toughness K Q (L-T) is at least 52 MPa√{square root over (m)} and the yield strength is at least 490 MPa.

10. Method according claim 9 , wherein the silver content of said liquid metal bath is from 0.15 to 0.35% by weight.

11. Method according to claim 9 wherein the magnesium content of said liquid metal bath is less than 0.4% by weight.

12. Method according to claim 9 wherein the manganese of said liquid metal bath is not more than 0.35% by weight.

13. Method according to claim 9 wherein said inevitable impurities comprise iron and silicon, said impurities having a content less than 0.08% by weight and 0.06% by weight for iron and silicon, respectively, the other impurities having a content less than 0.05% by weight each and 0.15% by weight in total.

14. Method according to claim 9 wherein said equivalent time for homogenization is between 6 and 15 hours.

15. Method according to claim 9 wherein the homogenization temperature is about 520° C. and the treatment time is from 8 to 20 hours.

16. Method according to claim 9 wherein said artificial aging is carried out by heating at 148 to 155° C. for 10 to 40 hours.

17. Method to manufacture an extruded product based on an aluminum alloy, said method comprising:

a) preparing a liquid metal bath comprising 2.65 to 2.85% by weight of Cu, 1.5 to 1.7% by weight of Li, 0.1 to 0.5% by weight of Ag, 0.1 to 1.0% by weight of Mg, 0.05 to 0.18% by weight of Zr, 0.2 to 0.6% by weight of Mn and at least one element selected from Cr, Sc, Hf or Ti, the quantity of said element being 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti, remainder aluminum and inevitable impurities;

b) casting an unwrought shape from said liquid metal bath;

c) homogenizing said unwrought shape at a temperature from 515° C. to 525° C. such that the equivalent time for homogenization

t

(

eq

)

=

exp

(

-

26100

/

T

)

t

exp

(

-

26100

/

T

ref

)

is from 5 to 20 hours, where T (in Kelvin) is the instantaneous treatment temperature, which varies with the time t (in hours), and T ref is a reference temperature set at 793 K;

d) hot working and optionally cold working said unwrought shape into an extruded product;

e) subjecting the product to a solution treatment and quenching;

f) stretching said product with a permanent set of 1 to 5%;

g) artificially aging said product by heating at 140 to 170° C. for 5 to 70 hours; and

wherein the toughness K Q (L-T) is at least 45 MPa√{square root over (m)} and the yield strength is at least 520 MPa.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE CONVEYING PARTY PREVIOUSLY RECORDED AT REEL: 040423 FRAME: 0118. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Jan 8, 2018
From: CONSTELLIUM FRANCE
To: CONSTELLIUM ISSOIRE
Reel/Frame 045948/0577 →
CHANGE OF NAME Recorded Oct 19, 2016
From: CONSTELLIUM FRANCE SAS
To: CONSTELLIUM ISSOIRE
Reel/Frame 040423/0118 →
CHANGE OF NAME Recorded Jan 5, 2012
From: ALCAN RHENALU
To: CONSTELLIUM FRANCE
Reel/Frame 027489/0240 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 4, 2010
From: HEYMES, FABRICE; EBERL, FRANK; POUGET, GAELLE
To: ALCAN RHENALU
Reel/Frame 023897/0683 →