2XXX series aluminum lithium alloys

Patent metadata

Field	Value
Publication number	US-12565695-B2
Application number	US-201213399975-A
Country	US
Kind code	B2
Filing date	Feb 17, 2012
Priority date	Feb 17, 2011
Publication date	Mar 3, 2026
Grant date	Mar 3, 2026

Abstract

Thick wrought 2xxx aluminum lithium alloy products are disclosed. The wrought aluminum alloy products have a thickness of at least 12.7 mm and contain from 3.00 to 3.80 wt. % Cu, from 0.05 to 0.35 wt. % Mg, from 0.975 to 1.385 wt. % Li, wherein −0.3*Mg−0.15Cu+1.65≤Li≤−0.3*Mg−0.15Cu+1.85, from 0.05 to 0.50 wt. % of at least one grain structure control element, wherein the grain structure control element is selected from the group consisting of Zr, Sc, Cr, V, Hf, other rare earth elements, and combinations thereof, up to 1.0 wt. % Zn, up to 1.0 wt. % Mn, up to 0.12 wt. % Si, up to 0.15 wt. % Fe, up to 0.15 wt. % Ti, up to 0.10 wt. % of any other element, with the total of these other elements not exceeding 0.35 wt. %, the balance being aluminum.

First claim

What is claimed is:

1 . An aluminum alloy product, the aluminum alloy consisting of:
from 3.20 to 3.60 wt. % Cu; from 0.15 to 0.30 wt. % Mg; from 1.05 to 1.25 wt. % Li; from 0.05 to 0.50 wt. % of at least one grain structure control element, wherein the at least one grain structure control element is selected from the group consisting of Zr, Sc, Cr, V, Hf, and combinations thereof; from 0.20 to 1.0 wt. % Zn; from 0.2 to 0.5 wt. % Mn; up to 0.12 wt. % Si; up to 0.15 wt. % Fe; up to 0.15 wt. % Ti; up to 0.05 wt. % of any other element, with the total of these other elements not exceeding 0.15 wt. %, wherein the other elements include silver (Ag); and the balance being aluminum, wherein the aluminum alloy product has a thickness of 50.8-76.2 mm and realizes a strength-toughness relationship that satisfies the expression:
FT-SL≥=−0.199(TYS−ST)+116;

wherein TYS-ST is the ST tensile yield strength of the plate in MPa as measured in accordance with ASTM Standard E8 and ASTM B557,
wherein FT-SL is the S-L plane strain fracture toughness (KIC) of the plate in MPa√Vm as measured in accordance with ASTM E399,
wherein the aluminum alloy product realizes a TYS-ST of at least 400 MPa, and wherein the aluminum alloy product realizes a FT-SL of at least about 22 MPa√m.

2 . The aluminum alloy product of claim 1 , wherein the grain structure control element is at least Zr, and wherein the alloy contains 0.05 to 0.20 wt. % Zr.

3 . The aluminum alloy product of claim 1 , comprising at least 3.40 wt. % Cu.

4 . The aluminum alloy product of claim 1 , comprising not greater than 0.25 wt. % Mg.

5 . The aluminum alloy product of claim 4 , comprising at least 1.150 wt. % Li.

6 . The aluminum alloy product of claim 4 , comprising not greater than 0.50 wt. % Zn.

Assignees

• Boselli Julien
• Rioja Roberto J
• Venema Gregory B
• Sawtell Ralph R
• Arconic Tech Llc

Inventors

• Boselli Julien
• Rioja Roberto J
• Venema Gregory B
• Sawtell Ralph R

Classifications

• C22C21/18

  with zinc · CPC title

• C22C21/16

  with magnesium · CPC title

• C22F1/057

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

• C22C21/12 Primary

  with copper as the next major constituent · CPC title

• C22F1/04

  of aluminium or alloys based thereon · CPC title