Method for manufacturing anodized aluminum alloy parts without surface discoloration

Patent metadata

Field	Value
Publication number	US-10415128-B2
Application number	US-201816005183-A
Country	US
Kind code	B2
Filing date	Jun 11, 2018
Priority date	Feb 16, 2015
Publication date	Sep 17, 2019
Grant date	Sep 17, 2019

Abstract

A method for manufacturing a part including steps of (1) casting an ingot, (2) scalping the ingot to yield a scalped ingot, (3) homogenizing the scalped ingot to yield a homogenized ingot, (4) breakdown of the homogenized ingot to yield a slab, (5) rolling the slab to yield a rolled aluminum material, (6) annealing the rolled aluminum material to yield an aluminum starting material, (7) cold working the aluminum starting material to obtain an aluminum cold worked material, and (8) forming the part from the aluminum cold worked material.

First claim

What is claimed is:

1. A method for manufacturing a part from an aluminum starting material, the method comprising:
cold working the aluminum starting material to obtain an aluminum cold worked material;
forming the part from the aluminum cold worked material, wherein the forming includes forming the part to have a non-planar configuration;
solution heat treating the part, thereby yielding a solution heat treated part having a recrystallized grain structure; and
anodizing the solution heat treated part.

2. The method of claim 1 wherein the part is an aircraft lipskin.

3. The method of claim 1 wherein the aluminum starting materiel comprises a 2xxx series aluminum alloy.

4. The method of claim 1 wherein the aluminum starting material comprises 2219 aluminum alloy.

5. The method of claim 1 wherein the aluminum starting material is in plate form.

6. The method of claim 1 wherein the cold working comprises stretching the aluminum starting material.

7. The method of claim 1 wherein the cold working comprises rolling the aluminum starting material.

8. The method of claim 1 wherein the cold working is performed at a cold working temperature, and wherein the cold working temperature is at most about 50 percent of a melting point, in degrees kelvin, of the aluminum starting material.

9. The method of claim 1 wherein the cold working is performed at a cold working temperature, and wherein the cold working temperature is at most about 300° F.

10. The method of claim 1 wherein the cold working is performed at a cold working temperature, and wherein the cold working temperature is at most about 200° F.

11. The method of claim 1 wherein the cold working is performed to achieve at least about 2 percent cold work.

12. The method of claim 1 wherein the cold working is performed to achieve about 3 percent to about 20 percent cold work.

13. The method of claim 1 wherein the cold working is performed to achieve about 5 percent to about 15 percent cold work.

14. The method of claim 1 wherein the forming comprises at least one of spin forming and die-stamping.

15. The method of claim 1 wherein the aluminum starting material includes a plurality of individual grains, and wherein the cold working results in accumulation of strain energy in the individual grains of the aluminum cold worked material.

16. The method of claim 1 wherein the solution heat treating includes heating the formed part to a temperature ranging from about 975° F. to about 1015° F.

17. The method of claim 1 wherein the solution heat treating includes heating the formed part to a temperature ranging from about 975° F. to about 1015° F. for about 10 minutes to about 240 minutes.

18. The method of claim 1 further comprising performing a sizing step after the solution heat treating.

19. The method of claim 18 wherein the sizing step includes at least one of spin forming and die-stamping.

20. The method of claim 1 further comprising preparing the aluminum starting material, the preparing the aluminum starting material comprising:
casting an ingot;
scalping the ingot to yield a scalped ingot;
homogenizing the scalped ingot to yield a homogenized ingot;
breakdown of the homogenized ingot to yield a slab;
rolling the slab to yield a rolled aluminum material;
annealing the rolled aluminum material to yield the aluminum starting material.

Assignees

• Boeing Co

Inventors

• Gane David H
• Glamm Ryan J
• Weber Gary R
• Johnson Ricole A
• Tomt Terry C
• Pugh Azzreal
• Kane Daniel J
• Verge Peter D

Classifications

• C25D11/04

  of aluminium or alloys based thereon · CPC title

• C22F1/04 Primary

  of aluminium or alloys based thereon · CPC title

• C21D9/0081

  for slabs; for billets · CPC title

• B23P15/00

  Making specific metal objects by operations not covered by a single other subclass or a group in this subclass · CPC title

• B22D7/005

  from non-ferrous metals · CPC title