US2544139A - Process for enameling aluminumrich alloys - Google Patents

Process for enameling aluminumrich alloys Download PDF

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US2544139A
US2544139A US758470A US75847047A US2544139A US 2544139 A US2544139 A US 2544139A US 758470 A US758470 A US 758470A US 75847047 A US75847047 A US 75847047A US 2544139 A US2544139 A US 2544139A
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enamel
alloy
chromate
temperature
enameling
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Alden J Deyrup
James H Peterson
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EIDP Inc
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EI Du Pont de Nemours and Co
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23DENAMELLING OF, OR APPLYING A VITREOUS LAYER TO, METALS
    • C23D3/00Chemical treatment of the metal surfaces prior to coating

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  • This invention relates to the enameling of aluminum-rich alloys, 1 e., alloys containing at least 80% by weight of aluminum. More particularly, this invention relates to the chemical and heat treatment of aluminum-rich alloy structures followed by the application and firing of a vitreous enamel on the treated surface of the structures.
  • the objects of this invention may be accomplished, in general, by pre-treating the surface to be enameled of an aluminum-rich alloy structure with an auqeous alkaline solution of a chromate followed by a heat-treatment at a temperature between 350 C. and the temperature at which the aluminum alloy structure is deleteriously af- 'fected by heat, usually about'600 (3., and then enameling the so-treated surface with a vitreous enamel.
  • the aqueous alkaline chromate solution may have substantially any degree of alkalinity between pH 8.0 and pH 14.
  • the desired degree of alkalinity may be imparted to the solution in any desired manner, for example, by the addition of alkali metal hydroxides or by the addition of salts, such as alkali metal carbonates or bicarbonates, which upon hydrolysis produce alkaline conditions.
  • Any chromate including dichromates, which is soluble in water may be used for the above-said pre-treatment since it appears that the chromate ions in the solution with which the alloy is treated impart the improved adherence of the enamel to the treated surface.
  • Alkali metal chromates are preferred. Dichromates, when added to the alkaline solution, will be converted to chromates.
  • the chromate content may Vary from 0.25% to 25%, expressed as potassium chromate, i. e., the chomate should be present in the solution in a concentration equivalent in ion content to a concentration of 0.25% to 25% potassium chromate.
  • the aluminum alloy structures need not generally be given a particular cleaning treatment before treatment with the chromate solution; however, if the surface of the alloy is very greasy it may be cleaned with grease solvents such as trichlorethylene, or the-like.
  • the chromate solution may be applied to the surface of the alloy to be enameled in any desired manner however, it is preferred to immerse the alloy structure in a bath of said chromate solution.
  • the chromate solution may vary in temperature from room temperature (about 20 0.). up to the boiling temperature of the solution (about C.). For convenience of operation, temperatures below room temperature are usually not employed.
  • the time of treatment may vary from one to thirty minutes. After the treatment with chromate solution, it is preferred to rinse the alloy structure with water to remove any adhering chromate solution therefrom.
  • the enamel should be fired at a temperature between 480 C. and 580 C., and in some cases preferably between 480 C. and 510 C. for a period of between two and thirty minutes. This applies to both ground and cover coats in case two enamel coats are applied.
  • the alloy after the chromate solution treatment and before enameling, be given a heat-treatment at a temperature between 350 C. and the heat tolerance limit of the alloy.
  • this heat treatment is carried out at a temperature of between 400 C. and 550 C.
  • Such heat treatment is necessary to obtain adequate adherence of enamel to the alloy.
  • the period of heat-treatment may vary from two to ten minutes.
  • the heat-treatment may be carried out in an oven at atmospheric conditions.
  • any of the above three aluminum alloys treated in accordance with the above-said preat a temperature of between 350 C. and the heat tolerance limit of the alloy before enameling.
  • any particular aluminum alloy it can readily be determined whether or not sufficient enamel adherence to insure against waterspalling is obtained by any prescribed course of treatment. This can be determined by means of the following accelerated test which correlates with water exposure results which may take weeks or months. This accelerated test consists in chromate-treating and enameling pieces of the particular alloy to be tested, and then exposing the enamel-metal interface by gouging, filing, or scratching the same, and immersing the test sample in 5% aqueous ammonium chloride solution for 96 hours at room temperature. If no failure occurs back one-eighth inch from the edge of the exposed interface, excellent performance in water exposure will result from the chromate treatment and enameling conditions used.
  • Example I Parts by weight Sodium hydroxide 4 Potassium chromate Water 76 and having a temperature of 50 C. After five minutes, the sheet is removed, rinsed in tap water, dried, and heat treated at a temperature of about 500 C. for five minutes. The heattreated sheet, after cooling, is then dipped into a water slurry of an enamel consisting of 38.1% PbO, 25.3% SiOz, 2.2% LizO, 10.2% NazO, 8.3% K20, 8.7% TiOz, 2.9% SbzOs, and 4.3% B203.
  • the enamel-coated structure After firin and cooling, the enamel-coated structure is gouged through the enamel coating and is then placed for 96 hours in a 5% aqueous solution of ammonium chloride. The coated structure showed no perceptible water-spelling.
  • Example II Aluminum alloy castings compound of alumi- No. 1 No. 2
  • the temperature of the bath and the treatment period are adjusted for any specific alloy treated within the above-mentioned temperature ranges and treatment periods to obtain optimum results.
  • treatments of too short duration cause incomplete protection against water-spalling. This may be recognized by enameling test pieces and subjecting to the accelerated water-spalling test above. Treatments of too long duration result in considerable etching. This may result in a loosely adherent deposit which prevents the enamel from adhering, so that it comes off locally or generally during or shortly after cooling. It is practical to determine times of treatment, if
  • Aqueous alkaline chromate solutions have been used heretofore for treatment of aluminum to produce desired surface appearance and to improve corrosion resistance. Furthermore, the addition of even very large amounts of watersoluble chromates to enamel slurries and slips is without effect in preventing water-spalling. The 'reason why treatment with chromates and heattreatment prior to enameling in accordanc with this invention will prevent subsequent waterspalling of the enamel coating is unknown. It has, however, been definitely established thatthe final enameled alloy contains a chromium compound between the alloy and the enamel.
  • vitreous enamel coated aluminum-rich alloys having an improved enamel bond which comprises placing the alloy surface to be enameled in contact with an aqueous alkaline solution containing between 0.25% and 25% of a water-soluble chromate for a period of between 1 and 30 minutes, heat-treating the chromate-treated alloy at a temperature between 350 C. and the heat tolerance limit of the alloy for a period of 2 to minutes, and then enameling the so-treated surface with a vitreous enamel having a melting point below about 580 C. by applying said enamel to said heat-treated surface and firing the same above the fusing point of the enamel at a temperature between 480 C.
  • vitreous enamel coated aluminum-rich alloys having an improved enamel bond which comprises placing the alloy surface to be enameled in contact with an aqueous alkaline solution containing between 0.25% and of a water-soluble chromate and having a temperature between C. and the boiling temperature thereof for a period of between 1 and 30 minutes, heat-treating the chromatetreated alloy at a temperature between 350 C. and the heat tolerance limit of the allo for a period of 2 to 10 minutes, and then enameling the so-treated surface with a vitreous enamel having a melting point below about 580 C. by applying said enamel to said heat-treated surface and fusing the same above the fusing point of the enamel at a temperature between 480 C. and 580 C.
  • the process of producing vitreous enamel coated aluminum-rich alloys having an improved enamel bond which comprises placing the alloy surface to be enameled in contact with an aqueous alkaline solution containing between 0.25% and 25% of a water-soluble chromate and having a temperature between 20 C. and the boiling temperature thereof for a period of one to thirty minutes, heat-treating the chromate-treated alloy at a temperature of 400 C. to 550 C. for a period of 2 to 10 minutes, and then enameling the so-treated surface with a vitreous enamel having a melting point below 510 C., the enamel being fired at a temperature between 480 C. and 510 C.

Description

highly moisture-laden atmospheres.
Patented Mar. 6, 1951 UNITED STATES PROCESS FOR ENAMELING ALUMINUM- RICH ALLOYS Alden J. Deyrup, Westfield, N. J., and James H. Peterson, Wilmington, Del., assignors to E. I. du Pont de Nemours & Company, Wilmington, Del., a corporation of Delaware No Drawing. Application July 1, 1947, Serial No. 758,470
4 Claims. 1
This invention relates to the enameling of aluminum-rich alloys, 1 e., alloys containing at least 80% by weight of aluminum. More particularly, this invention relates to the chemical and heat treatment of aluminum-rich alloy structures followed by the application and firing of a vitreous enamel on the treated surface of the structures.
In the copending application of Alden J. Deyrup, Serial No. 635,765, filed December 18, 1945, now Patent No. 2,467,114 issued April 12, 1949, there are pointed out the difficulties entailed in the enameling of aluminum and aluminum-rich alloy structures with a vitreous enamel. The above-said copending application relates to a new enamel composition which is particularly suitable for the enameling of aluminum and aluminum-rich alloy structures;
Although these new enamels have been highly successful in the enameling of aluminum-containing structures, in the presence of water or moisture-laden atmospheres the vitreous enamels do not adhere so tenaciously to so-called commercial aluminum-rich alloys as to commercial aluminum, i. e., substantially pure aluminum. Commercial aluminum contains 99% plus aluminum, whereas commercial aluminum-rich alloys contain from slightly greater than 1% to 20% of particular alloying ingredients, for example, manganese, magnesium, copper, chromium, zinc and silicon. The somewhat less tenacious adherence of vitreous enamel to aluminum-rich alloys has sometimes proven to be troublesome, particularly where the enameled aluminum is exposed for long periods of time to weathering or This results, not always but sporadically, in a phenomenon referred to as water-spalling, which is evidenced by a flaking-off of the enamel in tiny flakes exposing bare metal. Water-spalling starts at exposed metal-enamel interfaces, for example, at the edges of structures or atpinholes or other, normally immaterial, slight flaws in the enamel coating. Water-spalling may progress to minor failure or even to complete failure if subjected to long periods of exposure. Water-spalling may be a slow process and sometimes occurs only after weeks or months of exposure to tap water or weathering.
It is an object of this invention to provide vitreous enamel coated aluminum-rich alloys having an improved resistance to water-spalling.
It is another object of this invention to produce a vitreous enamel coated, aluminum-rich alloy which is free from water-spalling. I
It is still another obejctof this invention to provide a process for the chemical treatment of alun'1inum-richalloy structures and subsequently enameling the same with a vitreous enamel whereby to produce a product which is much less subject to, or free from, water-spalling.
Other objects of the invention will appear hereinafter.
The objects of this invention may be accomplished, in general, by pre-treating the surface to be enameled of an aluminum-rich alloy structure with an auqeous alkaline solution of a chromate followed by a heat-treatment at a temperature between 350 C. and the temperature at which the aluminum alloy structure is deleteriously af- 'fected by heat, usually about'600 (3., and then enameling the so-treated surface with a vitreous enamel.
The aqueous alkaline chromate solution may have substantially any degree of alkalinity between pH 8.0 and pH 14. The desired degree of alkalinity may be imparted to the solution in any desired manner, for example, by the addition of alkali metal hydroxides or by the addition of salts, such as alkali metal carbonates or bicarbonates, which upon hydrolysis produce alkaline conditions.
Any chromate, including dichromates, which is soluble in water may be used for the above-said pre-treatment since it appears that the chromate ions in the solution with which the alloy is treated impart the improved adherence of the enamel to the treated surface. Alkali metal chromates are preferred. Dichromates, when added to the alkaline solution, will be converted to chromates.
The chromate content may Vary from 0.25% to 25%, expressed as potassium chromate, i. e., the chomate should be present in the solution in a concentration equivalent in ion content to a concentration of 0.25% to 25% potassium chromate.
The aluminum alloy structures need not generally be given a particular cleaning treatment before treatment with the chromate solution; however, if the surface of the alloy is very greasy it may be cleaned with grease solvents such as trichlorethylene, or the-like.
The chromate solution may be applied to the surface of the alloy to be enameled in any desired manner however, it is preferred to immerse the alloy structure in a bath of said chromate solution. The chromate solution may vary in temperature from room temperature (about 20 0.). up to the boiling temperature of the solution (about C.). For convenience of operation, temperatures below room temperature are usually not employed. The time of treatment may vary from one to thirty minutes. After the treatment with chromate solution, it is preferred to rinse the alloy structure with water to remove any adhering chromate solution therefrom.
The above-said chromate solution treatmentof aluminum-rich alloys improves the adherence to aluminum of any vitreous enamel having a melting point below about 580 C. Best results have, however, been obtained by the use of enamels of the type disclosed in copending application Serial No. 635,765, above-mentioned. Such enamels contain:
10 to 18 mole percent PbO 38 to 65 mole per cent SiOz 5 to 12 mole per cent Li2O to 22 moles per cent NazO 0 to 20 mole per cent K20, and 0 to 11 mole per cent TiOz the total alkali metal oxide content (LizO-i-NazO-l-KzO) of the enamel bein between 25 and 36 mole per cent, and the ratio of the sum of said silica content and twice the said titanium oxide content of the enamel to the total alkali metal oxide content of the enamel being between 1.8 and 3.0, all of said oxides being melted into the enamel composition.
In order to obtain best results in adhesion of the enamel to the chromate-treated surfaces, the enamel should be fired at a temperature between 480 C. and 580 C., and in some cases preferably between 480 C. and 510 C. for a period of between two and thirty minutes. This applies to both ground and cover coats in case two enamel coats are applied.
It is essential that the alloy, after the chromate solution treatment and before enameling, be given a heat-treatment at a temperature between 350 C. and the heat tolerance limit of the alloy. Preferably, this heat treatment is carried out at a temperature of between 400 C. and 550 C. Such heat treatment is necessary to obtain adequate adherence of enamel to the alloy. The period of heat-treatment may vary from two to ten minutes. The heat-treatment may be carried out in an oven at atmospheric conditions.
The optimum conditions of chromate content in the alkaline chromate solution, time and temperature of treatment in the chromate solution, and firing time and temperature of the enamel will vary, dependent upon the composition of the alloy being treated. For example, in the case of the pre-enameling chromate treatment of aluminum alloy 61, containing about 0.25% copper, 0.6% silicon, 1.0% magnesium, and 0.25% chromium, with a bath containing four parts by weight sodium hydroxide, 20 parts by weight potassium chromate and the remainder water, it
is preferred to treat the same for five minutes with the temperature of the bath at 50 C. In treatin aluminum alloy 43, containing about silicon with the same chromate bath composition, it is preferred to treat it for five minutes with the bath heated at 40 C. When treating aluminum alloy 3, containing about 1.2% manganese, with the same bath, it is preferred to treat it for fifteen minutes at a temperature of 40 0. Any of the above three aluminum alloys treated in accordance with the above-said preat a temperature of between 350 C. and the heat tolerance limit of the alloy before enameling.
In the case of any particular aluminum alloy, it can readily be determined whether or not sufficient enamel adherence to insure against waterspalling is obtained by any prescribed course of treatment. This can be determined by means of the following accelerated test which correlates with water exposure results which may take weeks or months. This accelerated test consists in chromate-treating and enameling pieces of the particular alloy to be tested, and then exposing the enamel-metal interface by gouging, filing, or scratching the same, and immersing the test sample in 5% aqueous ammonium chloride solution for 96 hours at room temperature. If no failure occurs back one-eighth inch from the edge of the exposed interface, excellent performance in water exposure will result from the chromate treatment and enameling conditions used. The particular optimum treatment and enameling conditions for a specific alloy can thereby be established. Once optimum treatment conditions for a given alloy have been established and a chromate bath is used for continued treatment of the alloy structures or articles, it will, of course, be desirable to periodically analyze the treating bath and keep the chromate content and alkalinity of the bath within a few per cent of their initial value.
The following examples are given to illustrate certain preferred embodiments of the present invention, it being understood that the details set forth in these examples are not to be considered as limitativar Example I Parts by weight Sodium hydroxide 4 Potassium chromate Water 76 and having a temperature of 50 C. After five minutes, the sheet is removed, rinsed in tap water, dried, and heat treated at a temperature of about 500 C. for five minutes. The heattreated sheet, after cooling, is then dipped into a water slurry of an enamel consisting of 38.1% PbO, 25.3% SiOz, 2.2% LizO, 10.2% NazO, 8.3% K20, 8.7% TiOz, 2.9% SbzOs, and 4.3% B203. To the water slurry is also added 3% of boric acid and 0.5% of potassium chromate, based on the weight of the water in the slurry for the purpose of obtaining better enameling. The liquid and solid contents of the slurry are mixed in such proportions that the sheet, after dipping in the slurry and draining, will contain between 15 and grams (based on dry weight of enamel) per square foot for each coating; several enamel coatings, which may contain pig- 'ments or opacifying agents, with separate firings being applied if desired. The enamel is fired at a temperature between 480 C. and 515 C.
After firin and cooling, the enamel-coated structure is gouged through the enamel coating and is then placed for 96 hours in a 5% aqueous solution of ammonium chloride. The coated structure showed no perceptible water-spelling.
Example II Aluminum alloy castings compound of alumi- No. 1 No. 2
P1118 by Parts by weigh weight Water 89. 90. 0 Potassium chromate 2. 0 0.5 Sodium bicarbonate 2.0 2.5 Sodium carbonate 7.0 7.0
The temperature of the bath and the treatment period are adjusted for any specific alloy treated within the above-mentioned temperature ranges and treatment periods to obtain optimum results.
Successful enameling with subsequent high resistance to failure of bond under prolonged water exposure may be readily obtained by adhering generally to the following principles:
In variation of time of treatment, treatments of too short duration cause incomplete protection against water-spalling. This may be recognized by enameling test pieces and subjecting to the accelerated water-spalling test above. Treatments of too long duration result in considerable etching. This may result in a loosely adherent deposit which prevents the enamel from adhering, so that it comes off locally or generally during or shortly after cooling. It is practical to determine times of treatment, if
preferred conditions are departed from, at which these two defects begin to occur, and then select a time midway between for practical use.
In variation of temperature of treatment, it is found that higher temperatures require shorter times. Speedier operation may thus be secured by appropriate temperature increase, if desired.
In variation of alkalinity, it is found that more alkaline baths cause more rapid treatment. It is desirable to avoid too rapid treatment so that time of treatment ma be practically controlled at its optimal duration.
In variation of chromate content, increase of chromate content generally gives more flexibility A in time duration of treatment with favorable re- 5 sults, but decreases the speed of action.
Aqueous alkaline chromate solutions have been used heretofore for treatment of aluminum to produce desired surface appearance and to improve corrosion resistance. Furthermore, the addition of even very large amounts of watersoluble chromates to enamel slurries and slips is without effect in preventing water-spalling. The 'reason why treatment with chromates and heattreatment prior to enameling in accordanc with this invention will prevent subsequent waterspalling of the enamel coating is unknown. It has, however, been definitely established thatthe final enameled alloy contains a chromium compound between the alloy and the enamel.
Reference in the specification and claims to parts, proportions and percentages, unless otherwise specified, refers to parts, proportions and percentages by weight.
Since it is obvious that many changes and modifications can be made in the above-described details without departing from the nature and spirit of the invention, it is to be understood that the invention is not to be limited to said details except as set forth in the appended claims.
What is claimed is:
l. The process of producing vitreous enamel coated aluminum-rich alloys having an improved enamel bond which comprises placing the alloy surface to be enameled in contact with an aqueous alkaline solution containing between 0.25% and 25% of a water-soluble chromate for a period of between 1 and 30 minutes, heat-treating the chromate-treated alloy at a temperature between 350 C. and the heat tolerance limit of the alloy for a period of 2 to minutes, and then enameling the so-treated surface with a vitreous enamel having a melting point below about 580 C. by applying said enamel to said heat-treated surface and firing the same above the fusing point of the enamel at a temperature between 480 C.
and 580 C.
2. The process of producing vitreous enamel coated aluminum-rich alloys having an improved enamel bond which comprises placing the alloy surface to be enameled in contact with an aqueous alkaline solution containing between 0.25% and of a water-soluble chromate and having a temperature between C. and the boiling temperature thereof for a period of between 1 and 30 minutes, heat-treating the chromatetreated alloy at a temperature between 350 C. and the heat tolerance limit of the allo for a period of 2 to 10 minutes, and then enameling the so-treated surface with a vitreous enamel having a melting point below about 580 C. by applying said enamel to said heat-treated surface and fusing the same above the fusing point of the enamel at a temperature between 480 C. and 580 C.
3. The process of producing vitreous enamel coated aluminum-rich alloys having an improved enamel bond which comprises placing the alloy surface to be enameled in contact with an aqueous alkaline solution containing between 0.25% and 25% of a water-soluble chromate and having a temperature between 20 C. and the boiling temperature thereof for a period of one to thirty minutes, heat-treating the chromate-treated alloy at a temperature of 400 C. to 550 C. for a period of 2 to 10 minutes, and then enameling the so-treated surface with a vitreous enamel having a melting point below 510 C., the enamel being fired at a temperature between 480 C. and 510 C.
4. The process as defined in claim 2 in which the water-soluble chromate is an alkali metal chromate.
' ALDEN J. DEYRUP.
JAMES H. PETERSON.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,230,958 Warga June 26, 1917 1,971,240 Tosterud Aug. 21, 1934 FOREIGN PATENTS Number Country Date 273,956 Great Britain July 14, 1927 463,790 Great Britain Mar. 30, 1937

Claims (1)

1. THE PROCESS OF PRODUCING VITREOUS ENAMEL COATED ALUMINUM-RICH ALLOYS HAVING AN IMPROVED ENAMEL BOND WHICH COMPRISES PLACING THE ALLOY SURFACE TO BE ENAMELED IN CONTACT WITH AN AQUEOUS ALKALINE SOLUTION CONTAINING BETWEEN 0.25% AND 25% OF A WATER-SOLUBLE CHROMATE FOR A PERIOD OF BETWEEN 1 AND 30 MINUTES, HEAT-TREATING THE CHROMATE-TREATED ALLOY AT A TEMPERATURE BETWEEN 350* C. AND THE HEAT TOLERANCE LIMIT OF THE ALLOY FOR A PERIOD OF 2 TO 10 MINUTES, AND THEN ENAMELING THE SO-TREATED SURFACE WITH A VITREOUS ENAMEL HAVING A MELTING POINT BELOW ABOUT 580* C. BY APPLYING SAID ENAMEL TO SAID HEAT-TREATED SURFACE AND FIRING THE SAME ABOVE THE FUSING POINT OF THE ENAMEL AT A TEMPERATURE BETWEEN 480* C. AND 580* C.
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Cited By (16)

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Publication number Priority date Publication date Assignee Title
US2698258A (en) * 1954-12-28 Figure i
US2719796A (en) * 1954-03-24 1955-10-04 Aluminum Co Of America Process for enameling aluminum
US2858245A (en) * 1956-08-16 1958-10-28 Amchem Prod Process for enameling aluminum
US2858244A (en) * 1954-05-14 1958-10-28 Solar Aircraft Co Oxidizing process for ferrous alloys containing at least 5% chromium
US2932585A (en) * 1955-10-24 1960-04-12 Robertson Co H H Enameled aluminum products and methods of making the same
US3066390A (en) * 1957-12-30 1962-12-04 Aluminium Lab Ltd Welding of metal sheets
US3205051A (en) * 1962-05-25 1965-09-07 Robertson Co H H Light-colored porcelain-enameled aluminum articles and clad-aluminum sheets therefor
US3210316A (en) * 1961-07-24 1965-10-05 Ransburg Electro Coating Corp Paint containing aluminum pigment coated with an electrically insulating coating
US3222266A (en) * 1958-08-20 1965-12-07 Kaiser Aluminium Chem Corp Method of enameling anodized aluminum
US3364080A (en) * 1964-10-22 1968-01-16 Amchem Prod Method of improving the corrosion resistance of chromate conversion coated aluminum surface
US3475141A (en) * 1966-12-07 1969-10-28 Robertson Co H H Porcelain-enamel on galvanized steels by means of an aluminum coat
US3725137A (en) * 1971-03-10 1973-04-03 Reactor Ct Nl Method for the blackening of aluminum alloys
US4330344A (en) * 1980-12-29 1982-05-18 Sumitomo Light Metal Industries, Ltd. Selective absorber of solar energy and process for producing same
US4332628A (en) * 1980-02-20 1982-06-01 Sumitomo Light Metal Industries, Ltd. Selective absorber of solar energy and process for producing same
US4504325A (en) * 1982-03-19 1985-03-12 The Boeing Company Method for sealing an aluminum oxide film
CN101302615B (en) * 2007-05-10 2011-05-11 东莞新科技术研究开发有限公司 Surface treating method of welding point

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Publication number Priority date Publication date Assignee Title
US1230958A (en) * 1917-01-10 1917-06-26 Kalman Warga Ornamenting and protecting metal surfaces.
GB273956A (en) * 1926-11-27 1927-07-14 Aladar Pacz Process for the production of coatings upon aluminium and aluminium alloys
US1971240A (en) * 1930-12-17 1934-08-21 Aluminum Co Of America Method of coloring aluminum
GB463790A (en) * 1935-07-30 1937-03-30 Sindey Rowland Sheppard Improvements in and relating to the coating and protection of aluminium

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1230958A (en) * 1917-01-10 1917-06-26 Kalman Warga Ornamenting and protecting metal surfaces.
GB273956A (en) * 1926-11-27 1927-07-14 Aladar Pacz Process for the production of coatings upon aluminium and aluminium alloys
US1971240A (en) * 1930-12-17 1934-08-21 Aluminum Co Of America Method of coloring aluminum
GB463790A (en) * 1935-07-30 1937-03-30 Sindey Rowland Sheppard Improvements in and relating to the coating and protection of aluminium

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2698258A (en) * 1954-12-28 Figure i
US2719796A (en) * 1954-03-24 1955-10-04 Aluminum Co Of America Process for enameling aluminum
US2858244A (en) * 1954-05-14 1958-10-28 Solar Aircraft Co Oxidizing process for ferrous alloys containing at least 5% chromium
US2932585A (en) * 1955-10-24 1960-04-12 Robertson Co H H Enameled aluminum products and methods of making the same
US2858245A (en) * 1956-08-16 1958-10-28 Amchem Prod Process for enameling aluminum
US3066390A (en) * 1957-12-30 1962-12-04 Aluminium Lab Ltd Welding of metal sheets
US3222266A (en) * 1958-08-20 1965-12-07 Kaiser Aluminium Chem Corp Method of enameling anodized aluminum
US3210316A (en) * 1961-07-24 1965-10-05 Ransburg Electro Coating Corp Paint containing aluminum pigment coated with an electrically insulating coating
US3205051A (en) * 1962-05-25 1965-09-07 Robertson Co H H Light-colored porcelain-enameled aluminum articles and clad-aluminum sheets therefor
US3364080A (en) * 1964-10-22 1968-01-16 Amchem Prod Method of improving the corrosion resistance of chromate conversion coated aluminum surface
US3475141A (en) * 1966-12-07 1969-10-28 Robertson Co H H Porcelain-enamel on galvanized steels by means of an aluminum coat
US3725137A (en) * 1971-03-10 1973-04-03 Reactor Ct Nl Method for the blackening of aluminum alloys
US4332628A (en) * 1980-02-20 1982-06-01 Sumitomo Light Metal Industries, Ltd. Selective absorber of solar energy and process for producing same
US4330344A (en) * 1980-12-29 1982-05-18 Sumitomo Light Metal Industries, Ltd. Selective absorber of solar energy and process for producing same
US4504325A (en) * 1982-03-19 1985-03-12 The Boeing Company Method for sealing an aluminum oxide film
CN101302615B (en) * 2007-05-10 2011-05-11 东莞新科技术研究开发有限公司 Surface treating method of welding point

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GB642228A (en) 1950-08-30
FR968583A (en) 1950-11-30

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