Multifunctional coating of aluminium pieces

Patent metadata

Field	Value
Publication number	US-9334577-B2
Application number	US-86605509-A
Country	US
Kind code	B2
Filing date	Jan 7, 2009
Priority date	Feb 8, 2008
Publication date	May 10, 2016
Grant date	May 10, 2016

Abstract

The invention relates to a method for application of a multifunctional coating to the surface of a workpiece made from aluminum or an aluminum alloy. The invention further relates to a workpiece, which may be produced by such a method.

First claim

The invention claimed is:

1. A method for applying a multifunctional coating to the surface of an untreated workpiece made of aluminium or of an aluminium alloy, wherein the method comprises the following:
a) treating a surface of the untreated workpiece made of aluminium or of an aluminium alloy with an acidic solution which contains rare-earth metal ions, to produce a treated workpiece with a first oxide layer thereon, wherein the acidic solution has a pH of <1 and the treating of step a) occurs at a processing temperature of 50° C. to 80° C; and
b) anodising the treated workpiece to produce a second oxide layer, the treated workpiece serving as anode of an electrical cell in the presence of an aqueous sulphuric acid-containing solution and the first oxide layer produced in step a) being retained, wherein the anodising of step b) occurs at a processing temperature of 15 to 35° C.

2. The method according to claim 1 , wherein the rare-earth metal ions are cerium (IV).

3. The method according to claim 1 , wherein the concentration of the rare-earth metal ions in the acidic solution in step a) is between 0.005 and 1 mol/l.

4. The method according to claim 1 , wherein the first oxide layer produced in step a) has a thickness of from 20 to 100 nm.

5. The method according to claim 1 , wherein the solution used in step a) further contains sulphuric acid.

6. The method according to claim 1 , wherein the treatment in step a) lasts from 2 minutes to 60 minutes.

7. The method according to claim 1 , wherein the rare earth metal ions are selected from the group consisting of praseodymium, neodymium, samarium, europium, terbium and ytterbium ions.

8. The method according to claim 1 , wherein a tartaric acid-sulphuric acid (TSA) or a sulphuric acid (SAA) solution is used as the solution containing sulphuric acid in step b).

9. The method according to claim 8 , wherein the TSA solution contains from 10 to 200 g/l of sulphuric acid and from 5 to 200 g/l of L (+) tartaric acid.

10. The method according to claim 9 , wherein the TSA solution contains from 20 to 80 g/l of sulphuric acid and from 30 to 120 g/l of L (+) tartaric acid.

11. The method according to claim 10 , wherein the TSA solution contains approximately 40 g/l of sulphuric acid and approximately 80 g/l of L (+) tartaric acid.

12. The method according to claim 1 , wherein a second oxide layer with a layer thickness of from 2 to 8 μm is produced in step b).

13. The method according to claim 1 , wherein the anodising duration in step b) is from 10 to 40 minutes.

14. The method according to claim 1 , wherein the untreated workpiece is made of the aluminium alloy and the aluminium alloy is selected from alloys of the AA 7XXX, AA 6XXX, AA 5XXX, AA 2XXX series and from AlLi alloys.

15. The method according to claim 1 , wherein before treating the untreated workpiece with the rare-earth metal ions and anodising the treated workpiece, there is an additional step of contacting the surface of the untreated workpiece with an alkaline cleaning solution is carried out to remove impurities.

16. The method according to claim 1 , wherein following anodizing the treated workpiece, there is a step of utilising the treated workpiece as a component for aircraft construction.

17. The method according to claim 1 , wherein the concentration of the rare-earth metal ions in the acidic solution in step a) is between 0.01 and 0.5 mol/l.

18. The method according to claim 1 , wherein the concentration of the rare-earth metal ions in the acidic solution in step a) is between 0.1 and 0.3 mol/l.

Assignees

• Kock Erich
• Vulliet Philippe
• Airbus Operations Gmbh

Inventors

• Kock Erich
• Vulliet Philippe

Classifications

• C25D11/08 Primary

  containing inorganic acids · CPC title

• C25D11/16

  Pretreatment {, e.g. desmutting} · CPC title

• C23C22/83

  Chemical after-treatment · CPC title

• C23C22/56

  Treatment of aluminium or alloys based thereon · CPC title