Aluminum alloy with additions of copper, lithium and at least one alkali or rare earth metal, and method of manufacturing the same

Patent metadata

Field	Value
Publication number	US-11846010-B2
Application number	US-202117326492-A
Country	US
Kind code	B2
Filing date	May 21, 2021
Priority date	Apr 11, 2017
Publication date	Dec 19, 2023
Grant date	Dec 19, 2023

Abstract

A method for making an aluminum alloy includes steps of (1) weighing out starting materials to achieve a mass of material having a composition that includes aluminum, about 1.8 to about 5.6 percent by weight copper, about 0.6 to about 2.6 percent by weight lithium, and at least one of lanthanum up to about 1.5 percent by weight, strontium up to about 1.5 percent by weight, cerium up to about 1.5 percent by weight, and praseodymium up to about 1.5 percent by weight; (2) loading said starting materials into a crucible; (3) inserting said crucible into a chamber; (4) evacuating said chamber to a predetermined vacuum level; (5) melting said starting materials to form a molten mass; and (6) casting said molten mass into a mold.

First claim

What is claimed is:

1. A method for manufacturing an aluminum alloy comprising:
subjecting an aluminum alloy to a solid-state joining process, wherein the aluminum alloy comprises:
aluminum;
about 1.8 to about 5.6 percent by weight copper;
about 0.6 to about 2.6 percent by weight lithium; and
at least one of lanthanum, cerium, and praseodymium in a range of between 0.5 to about 1.5 percent by weight,

wherein T1 phase is precipitated during the solid-state joining process; and
aging the aluminum alloy before the solid-state joining process.

2. The method of claim 1 wherein the solid-state joining process comprises friction stir welding.

3. The method of claim 1 wherein aging the aluminum alloy before the solid-state joining process comprises artificially aging at about 300 to about 320° F. for about 29 to about 35 hours.

4. The method of claim 1 wherein the aluminum alloy further comprises titanium in a non-zero quantity up to about 0.15 percent by weight.

5. The method of claim 1 wherein the aluminum alloy further comprises silver in a non-zero quantity up to about 0.7 percent by weight.

6. The method of claim 1 wherein the aluminum alloy further comprises silicon in a non-zero quantity up to about 0.20 percent by weight.

7. The method of claim 1 wherein the aluminum alloy further comprises iron in a non-zero quantity up to about 0.30 percent by weight.

8. The method of claim 1 wherein the aluminum alloy further comprises manganese in a non-zero quantity up to about 0.6 percent by weight.

9. The method of claim 1 wherein the aluminum alloy further comprises chromium in a non-zero quantity up to about 0.10 percent by weight.

10. The method of claim 1 wherein the aluminum alloy further comprises zirconium in a non-zero quantity up to about 0.16 percent by weight.

11. The method of claim 1 wherein the aluminum alloy further comprises at least one of nickel up to about 0.05 percent by weight, gallium up to about 0.05 percent by weight and vanadium up to about 0.05 percent by weight.

12. The method of claim 1 wherein the aluminum alloy further comprises magnesium in a non-zero quantity up to about 1.9 percent by weight.

13. The method of claim 1 wherein the aluminum alloy further comprises magnesium in a range of about 0.05 to about 1.9 percent by weight.

14. The method of claim 1 wherein the aluminum alloy further comprises zinc in a non-zero quantity up to about 1.0 percent by weight.

15. The method of claim 1 wherein the aluminum alloy further comprises zinc in a range of about 0.03 to about 1.0 percent by weight.

16. The method of claim 1 wherein at least one of lanthanum and praseodymium is in a range of between 0.5 to about 1.5 percent by weight.

17. The method of claim 16 wherein the aluminum alloy further comprises magnesium in a non-zero quantity up to about 1.9 percent by weight.

18. The method of claim 16 wherein the aluminum alloy further comprises magnesium in a range of about 0.05 to about 1.9 percent by weight.

19. The method of claim 16 wherein the aluminum alloy further comprises zinc in a non-zero quantity up to about 1.0 percent by weight.

20. The method of claim 16 wherein the aluminum alloy further comprises zinc in a range of about 0.03 to about 1.0 percent by weight.

Assignees

• Boeing Co

Inventors

• Mann Austin E
• Baker Andrew H
• Mishra Rajiv
• Palanivel Sivanesh

Classifications

• B22D7/005

  from non-ferrous metals · CPC title

• C22F1/002

  by rapid cooling or quenching; cooling agents used therefor · CPC title

• C22F1/057 Primary

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

• C22C21/12 Primary

  with copper as the next major constituent · CPC title

• C22C21/18

  with zinc · CPC title