Process for applying corrosion-resistant coatings to aluminium alloys and products obtained

Abstract: This invention provides an aluminum alloy conversion coating composition and a process for protecting aluminum alloys, especially the alloys having greater than 1.0% Cu with a conversion coating. The coating is placed on the aluminum alloy in a multi-­ step process. In a first step the alloy is treated with a composition having as essential ingredients aluminum nitrate and an alkali metal nitrate, in a second step the nitrate treated alloy is treated with an alkali metal permanganate composition and in the final step the alloy is treated with an alkali metal silicate composition. Also, alternatively, the first step composition is an alkali metal permanganate-­ borax composition, the second step composition is a composition containing phosphate, aluminum and nitrate ions, the third step composition is an alkali metal permanganate composition and the fourth step composition is an alkali metal silicate composition. The aluminum conversion coatings of this invention are provided without the need of using toxic chromium compounds.

Description: The present invention relates to a process of protecting aluminum alloys with an intermediate corrosion resistant conversion coating, especially aluminum alloys having greater than 1.0% Cu. BACKGROUND OF THE INVENTION Generally, aluminum alloys are protected by forming thereon an intermediate corrosion resistant conversion coating and then painting over the corrosion resistant coating. Therefore, the corrosion resistant coating must he intimately bonded to the aluminum surface and also provide the required adhesion with the desired final aluminum coating - i.e., paint. One of the widely used processes for protecting aluminum alloys with a corrosion resistant intermediate coating is to coat the surface of the aluminum alloys with a protective conversion coating of an acid based hexavalent chromium composition or other heavy metal such as zirconium and titanium. All of these processes leave a very thin film of a heavy metal salt on the aluminum alloy which prevents the metal from becoming dark when subjected to boiling water for Periods of time up to 30 minutes. These coatings also provide a suitable base for the application and retention of other coatings, such as paint, to the aluminum alloy surfaces. The hexavalent chromium provides a corrosion resistant coating which can withstand a salt fog bath for more than 168 hours. The coated aluminum alloy is placed in a salt fog at 35°C (95°F) according to ASTM method B-117 for at least 168 hours and then removed. This requirement is necessary for many application. Further, the hexavalent chromium composition provides an intermediate coating which is receptive to the application and retention of other coatings, such as paints, to the aluminum alloy surfaces. The excellent features of the hexavalent chromium composition, have made these compositions used extensively for the corrosion resistant protection of aluminum alloys and as an intermediate corrosion resistant coating. However, the hexavalent chromium compositions have a serious side effect. Chromium is highly toxic and the spent chromium compositions provide an ecological problem. Many people in the industry are attempting to eliminate this ecologically damaging waste problem and it is very costly. Corrosion resistant permanganate compositions have been suggested, as noted in US-A-4,711,667 and 4,755,224. SUMMARY OF THE INVENTION Our invention eliminates some of the problems of the hexavalent chromium and other heavy metal compositions by providing a corrosion resistant coating composition which contains no chromium or other similar toxic materials. For aluminum alloys having at least 1.0% Cu we provide a corrosion resistant conversion coating which can withstand a salt fog at 35°C (95°F) according to ASTM Method B-117 for at least 168 hours. The aluminum alloy having a Cu content of greater than 1.0%, i.e. 2024 aluminum alloy, is first degreased, cleaned, deoxidized, and then oxidized. The oxidized alloy is then treated with a non-chromium nitrate composition containing lithium nitrate and aluminum nitrate. This coating is rinsed with water and then treated with a non-chromium composition containing an alkali metal permanganate. The alloy is again rinsed and given a final treatment with a non-chromium composition containing alkali metal silicate and a final rinse. In the above process the preferred aluminum alloy to be protected are those in the 2000 series - i.e., 2024 aluminium alloy having an average composition of 4.4% Cu, 0.6% Mn, 1.52% Mg and 93.5% Al. The outer oxide layer is removed preferably with nitric acid. The permanganate coating solution contains: 0.2 to 6.3% by weight alkali metal permanganate, preferably 0.2 to 0.5% by weight with the alkali metal being potassium. The aluminum nitrate-lithium nitrate solution contains: 0.2 to 2.0% by weight aluminum nitrate and 0.2 to 2.0% by weight lithium nitrate, preferably 0.5% to 1.5% by weight of each. In another embodiment of our invention, the oxidized alloy is first treated with a permanganate solution. Be permanganate coated alloy is then treated with a phosphate, aluminum and nitrate composition. This coating is rinsed and then the alloy is coated with a second permanganate solution. The alloy is again rinsed and given a final treatment with an alkali metal silicate and a final rinse. The first permanganate coating solution contains: 0.2 to 6.3% by weight alkali metal permanganate - preferably 2 to 4% with the alkali metal being potassium, and 0.05 to 9% by weight alkali metal borates and their hydrates - preferably 0.5 to 2% Borax ·10(Na₂B₄0₇·10H₂0). The second permanganate solutions contain in addition to the alkali metal permanganate and the alkali metal borate, 0.05 to 10% by weight of alkali metal chloride - preferably 0.5 to 2% lithium chloride. The alkali metal permanganate compositions may be applied in any acceptable manner (i.e., immersion, spraying, misting or spreading by an appropriate applicator). The aluminum alloy surface is normally immersed in our aqueous alkali metal permanganate solution. The temperature of the solution is between room temperature and the boiling point of the composition. The preferred temperature is between 15.5°C (60°F) and 82.3°C (180°F), with the most preferred between 37.8°C (100°F) and 82.3°C (180°F). However, as the temperature is raised, less immersion time is necessary to form the desired coating. The alkali metal as referred to herein is selected from potassium, sodium or lithium. The preferred alkali metal permanganate is potassium or sodium permanganate. The concentration of the permanganate, to provide 168 hours of salt fog protection for the aluminum alloys is of a sufficient amount to provide at least 700 ppm of manganese in the coating solution with the practical maximum being the saturation point of the permanganate. When potassium permanganate is used, a concentration of 0.2% by weight is about 700 ppm manganese. At room temperature, a saturated KMn0₄ solution is 6.3% by weight; 0°C (32°F) is 2.8% by weight and at 100°C (212°F) is 28% by weight. The sodium permanganate is infinitely soluble and, therefore, has no practical upper limit. Other compounds may be added to the permanganate solutions if desired, providing the compounds do not interfere with the desired corrosion resistant protection of the aluminum alloy surfaces. The cleaning compounds for the aluminum alloy surfaces are sodium hydroxide, alkaline solutions of sodium nitrate, hydrofluoric acid, sulfuric acid, nitric acid, sodium carbonate, borax, and a commercial non-ionic surfactant polyoxyethylene or polyoxypropylene derivatives of organic acids, alcohols, alkylphenols or amines, a commercial non-ionic surfactant which has been used is a polyoxyethylene derivative of organic acids such as "Triton X-100" sold by Rohm and Haas Corp. It is also recommended that neither the cleaning composition nor the corrosion resistant alkali metal Permanganate composition contain a fatty acid, or any compound which would interfere with adhesion or formation of a protective coating on the aluminum alloy surface. In the following Examples 1 and 2, aluminum alloy 2024 is multi-coated with the above non-chromium corrosion protective coating compositions. Aluminum alloy 2024 is usually used for or in combination with heavy equipment. This type of alloy generally needs an intermediate protective coating for long periods of time. EXAMPLE 1 An aluminum alloy panel of "2024" alloy (has on average a composition of: 4.4%Cu, 0.6% Mn, 1.5% Mg and 93.5% Al) was degreased with mineral spirits and cleaned to a break-free surface with a commercial non-ionic surfactant such as Triton X-100 from Rohm and Haas Corp. After rinsing with water, the panel was deoxidized in a 10% nitric acid solution at 29.4°C (85°F) for 20 minutes. After rinsing with deionized water, the panel was placed in deionized water at 90.5-100°C (195°-212°F) for five minutes to form a layer of boehmite (Al0...0H) on the metal surface. The oxidized alloy was further treated in a 1.0% aluminum nitrate, 1.0% lithium nitrate solution at 90.5-100°C (195°-212°F) for five minutes. This was followed by a rinse in deionized water. The rinsed oxide coated alloy was then treated in 0.3% potassium permanganate (KMn0₄) (PH=5.0-8.0) at 60°C (140°F) for five minutes. The coated panel was then rinsed and given a final seal coating by being immersed in a potassium silicate solution (0.83% K₂0 and 2.1% Si0₂) at 90.5-100°C (195-212°F) for one minute. The panel was removed from the silicate solution and rinsed with deionized water. The panel was then placed in a salt-fog at 35°C (95°F) according to ASTM Standard B-117. After 168 hours of exposure, the panel showed only minor pitting. EXAMPLE 2 An aluminum alloy panel of "2024" alloy (has on average a composition of: 4.4% Cu, 0.6% Mn, 1.5% Mg and 93.5% Al) was degreased and cleaned to a break-free finish with a commercial non-ionic surfactant such as Triton X-100 from Rohm and Haas Corp. The outer oxide layer of the metal was removed by dipping the panel in a solution of 15% sulfuric acid, 10% nitric acid and 75% water at 140°F for seven minutes. After further treatment in 70% nitric acid for one minute, the panel was rinsed in deionized water and placed in deionized water containing less than 1.0 PPM total impurities at 90.5-100°C (195°-212°F) for five minutes to form a thin layer of boehmite (Al0···0H) on the surface of the panel. Treatment of the panel at 68.3°-71.1°C (155°-160°F) for 2 minutes in a solution of: 3.0% Potassium Permanganate (KMn0₄), 1.0% Borax (Na₂B₄0₇·10H₂0) and 96.0% water was followed by rinsing with deionized water and treatment for two minutes at 135°-140°F in a solution of: 2.5% aluminum nitrate (Al(N0₃)₃)·9H₂0), 0.9% phosphoric acid (85%) (H₃PO₄) and 96.6% water. After again rinsing in deionized water the panel was given a two minute treatment in a solution of: 3.0% Potassium Permanganate (KMn0₄), 1.0% Borax (Na₂B₄0₇·1OH₂0), 1.0% Lithium Chloride (LiCl) and 95% water at 68.3°-71.1°C (155°-160°F). After rinsing with deionized water the panel was given a final treatment in an aqueous solution of potassium silicate (0.83% K₂0 and 2.1% Si0₂) at 90.5-93.4°C (195°-200°F) for five minutes and rinsed again with deionized water. The panel was placed in a salt-fog at 35°C (95°F) according to ASTM standard B-117 (sample at a 6° angle). After 168 hours of exposure, there were no noticeable pits in the treated area of the panel. Our examples show use of protective compositions that do not have toxicity of chromates and are therefore more environmentally effective.

Claims: A process of protecting aluminum alloys with an intermediate corrosion resistant coating characterized by multi-coating the alloy with at least one non-chromium composition containing aluminum ions and nitrate ions, a second non-chromium composition containing an alkali metal permanganate and a third non-chromium composition containing an alkali metal silicate. The process of claim 1 characterized by first treating the alloy with a lithium nitrate and aluminum nitrate solution, then treating with a potassium permanganate solution and then treating with an alkali metal silicate composition The process of claim 1 characterized by treating the alloy first with a potassium permanganate-borax composition; second with a composition of phosphate, nitrate and aluminum ions; third with a potassium permanganate, borax and lithium chloride composition; and fourth with an alkali metal silicate composition. The process of claim 2 characterized in that the aluminum alloy is first coated with a solution containing 0.2-2.0% by weight aluminum nitrate and 0.2-2.0% by weight lithium nitrate; then coated with a solution containing 0.2 to 6.3% by weight alkali metal permanganate; and finally with a solution of alkali metal silicate. The process of claim 3 characterized in that the aluminum alloy is first coated with a solution of 0.2-6.3% by weight alkali metal permanganate and 0.05 to 9% by weight alkali metal borate; then coated with a solution containing 0.2 to 40% aluminum nitrate and 0.3 to 30% phosphoric acid; then coated with a solution of 0.2-6.3% by weight alkali metal permanganate and 0.05 to 10% by weight alkali metal chloride; and a final coating of alkali metal silicate. The process of claims 4 or 5 characterized in that prior to coating the aluminum alloy, the alloy is cleaned, degreased, deoxidized and then oxidized, and in between each coating, the alloy is rinsed with deionized water.

Inventors: BIBBER JOHN W, BIBBER, JOHN W.
Applicants: SANCHEM INC, SANCHEM, INC.
Application year: 1989
Main classification: C23C22
IPC codes: C23C22