Coating for aerospace aluminum parts

• US 6,171,704 B1
• Filed: 12/29/1995
• Issued: 01/09/2001
• Est. Priority Date: 12/29/1995
• Status: Expired due to Term

• Current Assignee: Teleflex Medical Incorporated (Teleflex Incorporated)
• Original Assignee: Sermatech International, Inc. (Linde Plc)
• Inventors: Greaser, James H., Mosser, Mark F.
• Primary Examiner(s): Jones, Deborah
• Assistant Examiner(s): LA VILLA, MICHAEL EUGENE
• Application Number:
  US08/580,562
• Time in Patent Office: 1,838 Days
• Field of Search: 428/650, 428/654, 428/457, 428/687, 428/447, 428/450, 428/469, 428/472.2, 428/689, 428/704, 428/615, 428/621, 428/622, 428/626, 428/632, 428/36.9, 428/36.91, 428/328, 428/331, 428/472.1, 428/446, 428/448, 148/253, 148/255, 148/257, 106/1.25, 106/14.12, 106/14.21, 106/286.5, 244/126, 244/133
• US Class Current: 428/450
• CPC Class Codes: B64D 29/00 Power-plant nacelles, fairings, or cowlings nacelles not otherwise provided for B64C
• CPC Class Codes: C04B 2111/00525 for metallic surfaces
• CPC Class Codes: C04B 2111/00982 as construction elements for space vehicles or aeroplanes
• CPC Class Codes: C04B 2111/1075 Chromium-free or very low chromium-content materials
• CPC Class Codes: C04B 22/04 Metals, e.g. aluminium used as blowing agent
• CPC Class Codes: C04B 28/34 containing cold phosphate binders
• CPC Class Codes: C04B 41/4961 Polyorganosiloxanes, i.e. polymers with a Si-O-Si-O-chain; "silicones"
• CPC Class Codes: C04B 41/5155 Aluminium
• CPC Class Codes: C09D 5/103 containing Al
• CPC Class Codes: C23C 22/74 for obtaining burned-in conversion coatings
• CPC Class Codes: Y10T 428/12569 Synthetic resin
• CPC Class Codes: Y10T 428/12736 Al-base component
• CPC Class Codes: Y10T 428/12764 Next to Al-base component
• CPC Class Codes: Y10T 428/12993 Surface feature [e.g., rough, mirror]
• CPC Class Codes: Y10T 428/1393 Multilayer [continuous layer]
• CPC Class Codes: Y10T 428/31663 As siloxane, silicone or silane
• CPC Class Codes: Y10T 428/31678 Of metal

Abstract

A coated aerospace aluminum alloy part, such as a lipskin of a nacelle or a leading edge of a wing or tail, is disclosed which part is protected from corrosion due to severe environmental stresses, including high and low temperatures, and rain drop erosion, by a multilayer coating comprising a phosphate bonded metal containing basecoat and a resin based topcoat. A method of coating the part is disclosed.

Claims

1. A multilayer coated aerospace grade aluminum-copper alloy part, said part coated with a coating comprising a phosphate bonded aluminum-filled basecoat and an aluminum silicone paint topcoat, wherein the coating prevents corrosion of the part due to environmental stresses of temperature of 190°

C., high salt concentrations, and water droplet erosion, is resistant to deicing at a temperature of about 190°

C., is resistant to a temperature of −

55°

C. for one hour, resistant to temperature of 150°

C. for 100 hours, wherein the multi-layer coating is repairable when damaged, and wherein the repaired area is aerodynamically virtually indistinguishable from the physical point of view of the non-damaged area of the part.

2. The coated part of claim 1, wherein the part is selected from the group consisting of a lipskin of a nacelle and a leading edge of a wing or tail.

3. The coated part of claim 2 wherein the aluminum copper alloy is a 2XXX alloy.

4. The coated part of claim 3 wherein the 2XXX alloy is selected from the group consisting of AA2219 and AA2024.

5. The coated part of claim 4 wherein the alloy is AA2219.

6. The coated part of claim 1 wherein the basecoat is cured at a temperature of 190°

C. or less.

7. The multilayer coating of claim 1 wherein the coating is also resistant to a temperature up to 232°

C.

8. A multilayer coated part selected from the group consisting of a lipskin or a leading edge of a wing of an aircraft, the lipskin or leading edge comprising an aerospace aluminum-copper alloy, which is coated with a multilayer coating comprised of a basecoat of a phosphate bonded aluminum-filled coating and a topcoat of an aluminum silicone paint, which multilayer coating is resistant to deicing at a temperature of about 190°

C., resistant to temperature of 150°

C. for 100 hours, meets the cross-hatch ASTM D3359 adhesion test (method B (ISO

     2409)), has a rating of “

5”

(no coating pickoff) in said adhesion test, withstands a direct impact test at 1.38 Kg meter impact measured by ASTM D2792, resistant to a temperature of −

55°

C. for one hour, resistant to corrosion as measured by the salt spray corrosion test, ASTM B117, after 3000 hours exposure to the salt spray test environment of ASTM B117 without substrate corrosion, and by the filiform corrosion test, ISO 4623, after 24 hours exposure to the salt spray test environment of ASTM B117, followed by 1,000 hours exposure to 80±

5% relative humidity at 40±

2°

C., with no filaments extending more than 2 mm from scribe lines at 20-25°

C., resistant to erosion from high velocity water droplets as measured by exposure to water drop of a mean drop diameter of 2 mm, at an impact velocity of 223 meters/second, at an impact angle of 90°

, at an intensity of 25 mm/hour for 10 minutes, and a damaged area of the multilayer coating being repairable so as to be virtually undistinguishable from an adjacent non-damaged area.

9. The coated part of claim 8 wherein the aerospace aluminum-copper alloy is a 2XXX alloy.

10. The coated part of claim 8 in which the basecoat is also free of chromium.

11. The coated part of claim 8, wherein the aluminum-copper alloy further comprises metal selected from the group consisting of magnesium, manganese, titanium, vanadium, and zirconium.

12. The coated part of claim 11, wherein the metal is zirconium.

13. The coated part of claim 8 in which the basecoat also comprises chromium.

14. A multilayer coated aerospace grade aluminum alloy part, said part is coated with a coating comprising a phosphate bonded metal-filled basecoat and an aluminum silicone paint topcoat, wherein the coating prevents corrosion of the part due to environmental stresses of temperature of 190°

C., high salt concentrations, and water droplet erosion, is resistant to deicing at a temperature of about 190°

C., is resistant to a temperature of −

55°

C. for one hour, is resistant to a temperature of 150°

C. for 100 hours, wherein the multi-layer coating is repairable when damaged, and wherein the repaired area is aerodynamically virtually indistinguishable from the physical point of view of the non-damaged area of the part.

15. The coated part of claim 14 wherein the base coat is cured at a temperature of 190°

C. or less.