Protective coatings for metal parts to be used at high temperatures

• US 5,158,663 A
• Filed: 10/25/1991
• Issued: 10/27/1992
• Est. Priority Date: 08/18/1991
• Status: Expired due to Fees

• Current Assignee: Joseph Yahalom
• Original Assignee: Joseph Yahalom
• Inventors: Yahalom, Joseph
• Primary Examiner(s): Valentine, Donald R.
• Assistant Examiner(s): Leader, William T.
• Application Number:
  US07/783,023
• Time in Patent Office: 368 Days
• Field of Search: 204/37.1, 204/42, 205/50, 205/171, 205/175, 205/224, 205/229, 205/917, 428/472.2
• US Class Current: 205/50
• CPC Class Codes: C25D 11/12 Anodising more than once, e.g. in different baths
• CPC Class Codes: C25D 11/26 of refractory metals or alloys based thereon
• CPC Class Codes: Y10S 205/917 Treatment of workpiece between coating steps

Abstract

A method for producing protecting layers on a metal selected from aluminum, titanium and zirconium, or alloys thereof, involves at least two anodic oxidation steps producing oxide layers and a thermal treatment which is carried out before the last anodic oxidation step. The treated metal according to the invention is protected even at high temperatures and under conditions of thermal cycling.

Claims

1. A method for providing a protective surface layer on a machine part made of a metal capable of anodic surface oxidation to protect such metal part from corrosive conditions, consisting essentially of the steps of:

(a) oxidizing by anodic oxidation the surface of said metal part to form a surface layer of an oxide of the metal to be protected;

(b) thermally treating the part at a temperature which is at least equal to the highest temperature to which the metal part is intended to be subjected during use, said treating temperature being at least 250°

C. and being sufficient to cause cracks to form in the formed oxide surface layer, thereby exposing the metal to be protected; and

(c) subjecting the anodized and heat treated surface of the part to another anodic oxidation step under conditions whereby an oxide of the metal to be protected will be formed mainly in the regions where the metal is exposed, the additional oxide serving to anchor the oxide surface layer to the metal and to block the cracks by forming additional oxidation below said cracks so that no metal is exposed.

2. A method in accordance with claim 1, further including the steps of repeating steps (b) and (c) at least once.

3. A method according to claim 1, wherein said metal is selected from the group consisting of aluminum, titanium, zirconium, and alloys thereof.

4. A method according to claim 1, wherein said step (a) is carried out in an acidic medium.

5. A method according to claim 4, wherein said acidic medium is selected from the group consisting of sulfuric acid, phosphoric acid, lactic acid, oxalic acid, chromic acid and mixtures thereof.

6. A method according to claim 1, wherein said step (a) is carried out in a neutral or alkaline medium.

7. A method according to claim 1, wherein said metal is aluminum or an aluminum alloy capable of anodic surface oxidation.

8. A method according to claim 1, wherein said metal is titanium, zirconium, or an alloy thereof capable of anodic surface oxidation.

9. A protected metal machine part produced by the process of claim 1.

11. A protected aluminum or aluminum alloy part produced by the process of claim 9.

10. A method for providing a protective surface layer on a part of aluminum or an aluminum alloy capable of anodic surface oxidation to protect such metal part from corrosive conditions, comprising the steps of:

(a) oxidizing the surface of said aluminum or aluminum alloy part by anodic oxidation in an acidic medium so as to form a porous oxidized surface layer with a barrier layer between the pores and the aluminum or aluminum alloy;

(b) oxidizing the part resulting from step (a) by anodic oxidation in a neutral medium so as to increase the thickness of the barrier layer;

(c) thermally treating the part at a temperature which is at least equal to the highest temperature to which the metal part is intended to be subjected during use said treating temperature being at least 250°

C. and being sufficient to cause cracks to form int he formed oxide surface layer, thereby exposing the metal to be protected; and

(d) subjecting the anodized and heat treated surface of the part to another anodic oxidation step under conditions whereby an oxide of the metal to be protected will be formed mainly in the regions where the metal is exposed, the additional oxide serving to anchor the oxide surface layer to the metal so as to block said cracks by forming additional oxidation below said cracks so that no metal is exposed.

12. A method in accordance with claim 10, further including the steps of repeating said steps (c) and (d) at least once.

13. A protected aluminum or aluminum alloy part produced by the process of claim 10.

14. In a method which includes anodizing the surface of a machine part made of a metal capable of anodic surface oxidation to protect the metal machine part from corrosive conditions and subjecting said machine part to corrosive conditions at temperatures above about 250°

C., the improvement wherein said anodizing step comprises;

(a) oxidizing by anodic oxidation the surface of said metal part to form a surface layer of an oxide of the metal to be protected;

(b) thermally treating the part at a temperature which is at least equal to the highest temperature to which the part is to be subjected in said subjecting step, said temperature being sufficient to cause cracks to form in the formed oxide surface layer, thereby exposing the metal to be protected; and

(c) subjecting the anodized and heat treated surface of the part to another anodic oxidation step under conditions whereby an oxide of the metal to be protected will be formed mainly in the regions where the metal is exposed, the additional oxide serving to anchor the oxide surface layer to the metal and to block the cracks by forming additional oxidation below said cracks so that no metal is exposed.