Corrosion-resistant coating for metal substrate
A novel coating composition is provided for imparting corrosion and wear resistance to metal substrates. The novel coating composition is thermally applied and comprises an aluminum alloy mixed with a hard, inert matrix. The coating composition has found particular use in providing corrosion and wear resistance to metal seat rails used to secure aircrafts seats to the aircraft frame.
1. An aluminum or aluminum alloy metal substrate coated by a high-velocity oxygen fuel thermal spray coating process with a corrosion- and wear-resistant coating composition comprising an aluminum-zinc alloy containing 0.1–10 wt. % zinc mixed with a hard, inert matrix.
2. The coated substrate of claim 1 wherein said matrix is selected from the group consisting of metal oxides, metal carbides, metal nitrides, borosilicate glasses, and mixtures thereof.
3. The coated substrate of claim 1 wherein said matrix comprises 10–75% by volume of said composition.
4. The coated substrate of claim 1 wherein said matrix comprises 25–50% by volume of said composition.
5. The coated substrate of claim 2 wherein said matrix comprises alumina.
6. The coated substrate of claim 1 wherein said aluminum-zinc alloy consists essentially of aluminum and from 1–5 wt. % zinc.
7. The coated substrate of claim 6 wherein said matrix consists essentially of alumina.
8. The coated substrate of claim 1 wherein said matrix has a Vickers hardness of at least 700.
9. The coated substrate of claim 8 wherein said matrix has a Vickers hardness of at least 2,000.
10. In a seat rail for securing an aircraft seat, wherein said seat rail is formed of aluminum or aluminum alloy, the improvement comprising said seat rail being coated with a corrosion-and-wear-resistant coating composition comprising an aluminum alloy mixed with a hard, inert matrix.
11. In the seat rail of claim 10 , wherein said seat rail contains a top surface having a longitudinal groove and spaced holes along said groove, said holes having a circumferential edge and a bottom, said coating composition coating said top and at least along said edges of said holes.
12. In the seat rail of claim 11 wherein said seat rail includes a lateral flange, said lateral flange being coated with said composition.
13. In the seat rail of claim 10 wherein said matrix comprises 10–75% by volume of said composition.
14. In the seat rail of claim 10 wherein said matrix comprises alumina.
15. In the seat rail of claim 10 wherein said aluminum alloy coating is an aluminum-zinc alloy.
16. In the seat rail of claim 15 wherein said aluminum-zinc alloy consists essentially of aluminum and from 1–5 wt. % zinc.
17. In the seat rail of claim 16 wherein said matrix consists essentially of alumina.
18. A seat rail for supporting an aircraft seat, wherein said seat rail is formed of aluminum or aluminum alloy, and wherein said seat rail comprises at least one surface that can be worn and/or corroded and which allows said seat to be installed and manipulated along said rail, and wherein said at least one surface is coated with a corrosion-and-wear-resistant coating composition comprising an aluminum alloy mixed with a hard, inert matrix.
19. The seat rail of claim 18 containing a top surface having a longitudinal groove and spaced holes along said groove, said holes having a circumferential edge and a bottom, said coating composition coating said top and at least along said edges of said holes.
20. The seat rail of claim 19 wherein said seat rail includes a lateral flange, said lateral flange being coated with said composition.
21. The seat rail of claim 18 wherein said matrix comprises 10–75% by volume of said composition.
22. The seat rail of claim 18 wherein said matrix comprises alumina.
23. The seat rail of claim 18 wherein said aluminum alloy coating is an aluminum-zinc alloy.
24. The seat rail of claim 23 wherein said aluminum-zinc alloy consists essentially of aluminum and from 1–5 wt. % zinc.
25. The seat rail of claim 24 wherein said matrix consists essentially of alumina.
26. A method of coating a metal surface with a powder coating composition comprising applying an aluminum alloy mixed with a hard, inert matrix by a high-velocity oxygen fuel thermal spray coating process, wherein said aluminum alloy comprises aluminum and from about 0.1–10 wt. % of Zn.
27. The method of claim 26 wherein said matrix is selected from the group consisting of metal oxides, metal carbides, metal nitrides, borosilicate glasses, and mixtures thereof.
28. The method of claim 26 wherein said aluminum alloy is aluminum and 1–5 wt. % zinc.
29. The method of claim 28 wherein said matrix is alumina.