Titanium and magnesium compound for corrosion-resistant coatings

Patent metadata

Field	Value
Publication number	US-11999871-B2
Application number	US-202318154469-A
Country	US
Kind code	B2
Filing date	Jan 13, 2023
Priority date	Aug 15, 2019
Publication date	Jun 4, 2024
Grant date	Jun 4, 2024

Abstract

A crystalline titanium and magnesium compound having an X-ray diffraction pattern having interplanar spacing (d-spacing) values at about 5.94, 3.10, 2.97, 2.10, 1.98, 1.82, and 1.74±0.1 angstroms may be used in protective coatings for metal or metal alloy substrates. The coatings exhibit excellent corrosion resistances and provide corrosion protection equal to or better than typical non-chromate coatings.

First claim

What is claimed is:

1. A crystalline titanium and magnesium compound, having an X-ray diffraction (XRD) pattern having interplanar spacing (d-spacing) values at 5.94, 3.10, and 2.97 angstroms.

2. The crystalline titanium and magnesium compound of claim 1 , wherein the XRD pattern has additional interplanar spacing (d-spacing) values at 1.98, 1.82, and 1.74 angstroms.

3. The crystalline titanium and magnesium compound of claim 1 , further having a cubic symmetry and a lattice parameter from about 10.225 angstroms to about 10.325 angstroms.

4. The crystalline titanium and magnesium compound of claim 1 , further having an XRD pattern, produced with an x-ray wavelength of 1.54 angstroms (Cu k alpha), having peaks at 14.89°, 28.78°, and 30.09°±0.25 2θ.

5. The crystalline titanium and magnesium compound of claim 4 , further having XRD peaks, produced with an x-ray wavelength of 1.54 angstroms (Cu k alpha), at 45.85°, 50.20°, and 52.66°±0.25 2θ.

6. The crystalline titanium and magnesium compound of claim 1 , wherein titanium is present at about 15 at % to about 25 at % and magnesium is present at about 1 at % to about 8 at %.

7. The crystalline titanium and magnesium compound of claim 6 , further comprising oxygen and fluorine.

8. The crystalline titanium and magnesium compound of claim 7 , wherein the oxygen is present at about 30 at % to about 45 at % and the fluorine is present at about 30 at % to about 40 at %.

9. The crystalline titanium and magnesium compound of claim 8 , wherein titanium is present at about 25 at %, magnesium is present at about 5 at %, oxygen is present at about 35 at %, and fluorine is present at about 35 at %.

10. A protective coating comprising a crystalline titanium and magnesium compound having an X-ray diffraction (XRD) pattern having interplanar spacing (d-spacing) values at 5.94, 3.10, and 2.97 angstroms.

11. The protective coating of claim 10 , further comprising titanium dioxide.

12. The protective coating of claim 10 , having a thickness of about 500 nm to about 10 μm.

13. The protective coating of claim 10 , having a polarization resistance of 80 kOhms-cm 2 to 3,000 kOhms-cm 2 .

14. The protective coating of claim 13 , having a polarization resistance of 100 kOhms-cm 2 to 400 kOhms-cm 2 .

15. A method comprising,
preparing a titanium/magnesium solution comprising a titanium compound, boric acid, sodium tetraborate, and a magnesium compound; and
precipitating, from the titanium/magnesium solution, a crystalline titanium and magnesium compound having an X-ray diffraction (XRD) pattern having interplanar spacing (d-spacing) values at 5.94, 3.10, and 2.97 angstroms.

16. The method of claim 15 , wherein the titanium compound comprises ammonium hexafluorotitanate and the magnesium compound comprises one or more of magnesium acetate, magnesium sulfate, magnesium chloride, or magnesium nitrate.

17. The method of claim 15 , wherein preparing the titanium/magnesium solution comprises:
dissolving the boric acid, the sodium tetraborate, and the magnesium compound in water to form a first solution;
dissolving the titanium compound in water to form a second solution; and
pouring the second solution into the first solution.

18. The method of claim 15 , further comprising:
reacting a metal surface with the titanium/magnesium solution; and
drying the metal surface with the titanium/magnesium solution to form a titanium/magnesium protective coating on the metal surface.

19. The method of claim 18 , further comprising applying a primer and/or a paint on the titanium/magnesium protective coating.

20. The method of claim 18 , wherein the metal surface comprises aluminum or an aluminum alloy substrate selected from 2024-T3 aluminum alloy, 6061 aluminum alloy, or 7075 aluminum alloy.

Assignees

• Boeing Co

Inventors

• Vajo John J
• Graetz Jason
• Adjorlolo Alain A

Classifications

• Y02E60/10

  Energy storage using batteries · CPC title

• C09D5/10 Primary

  containing metal dust · CPC title

• C01G23/002

  Compounds containing titanium, with or without oxygen or hydrogen, and containing two or more other elements (C01G23/001, C01G23/003 take precedence) · CPC title

• C09D7/61

  inorganic · CPC title

• C23C22/54

  Treatment of refractory metals or alloys based thereon · CPC title