US2428749A - Surface treatment of magnesium alloys - Google Patents
Surface treatment of magnesium alloys Download PDFInfo
- Publication number
- US2428749A US2428749A US550314A US55031444A US2428749A US 2428749 A US2428749 A US 2428749A US 550314 A US550314 A US 550314A US 55031444 A US55031444 A US 55031444A US 2428749 A US2428749 A US 2428749A
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- magnesium
- per cent
- solution
- acid
- coating
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- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C22/05—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions
- C23C22/06—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6
- C23C22/34—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6 containing fluorides or complex fluorides
- C23C22/37—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6 containing fluorides or complex fluorides containing also hexavalent chromium compounds
Definitions
- This invention relates to an improved method of producing a protective coating on the surface of aluminum-containing magnesium-base alloys.
- Articles of magnesium-base alloys are conventionally protected against corrosion during shipment, storage, and machining, and provided with a paint base by applying to the surface thereof some type of chemical finish, of which the socalled chrome-pickle, produced by immersing the article in an aqueous solution of chromic acid or a soluble chromate and a strong mineral acid, usually nitric acid, is by far the most common. It has been observed, however, that when the chrome-pickle treatment is applied to certain aluminum-containing magnesium-base alloys, there is sometimes obtained, instead of the expected uniform iridescent brass-colored finish ordinarily produced, a coating consisting in part of a loose deposit of a heavy dark gray powder.
- This powder which has been identified as an intermetallic compound of magnesium and a-luminum (probably MgsAlz OI"Mg'4A13)', not, only seriously detracts from the appearance of the treated article but also constitutes a distinct fire hazard, since, in addition to being easily ignited, it produces sparks on the application of slight frictional forces. Unless precautions are taken, simple wire-brushing or grinding of powdercoated parts may cause minor fires in accumulated dust, and even the striking together of two coated articles results in serious sparking. The occasional occurrence of this powder, then, is a serious practical disadvantage in the application of the chrome-pickle treatment to magnesiumbase alloys of all types.
- the chrome-pickle solution appears to etch ormains on the surface of the treated article and gives rise to the non-uniform appearance and sparking hazard mentioned.
- An object of the invention is to provide a ooatingmethod' for magnesium-base alloys which retains the advantages of the chromepic'kle process and at the same time eliminates formation of the powdery gray deposit Without altering the physicalcharacteristics of the articles treated.
- the treating solution used in the process is an aqueous solution containing as the effective ingredients chromic acid or a water-soluble salt thereof, a strong mineral acid, and hydrofluoric acid or a water-soluble salt thereof.
- the chromate constituent is ordinarily added in the form of chromic anhydride (0103) or an alkali metal or ammonium chromate or bichromate, sodium bichromate' being'convenient'. Concentrations of chromic acid or soluble chromate of at least 2 per cent by weight of the solution are ordinarily added in a proportion sufficient to maintain the pH value of the solution below about 2.0, preferably about 0.3 to 1.0.
- Nitric acid is most satisfactory in producing a coating useful as an adherent paint base.
- the fluoride ingredient is conveniently aqueous hydrofluoric acid or a solid alkali metal or ammonium fluoride or bifluoride, such as sodium fluoride or ammonium bifluoride (NHiHFz), although other simple fluorides are: operable. Complex fluo-acids and their salts are not effective.
- the hydrofluoric acid or fluoride should be added in a proportion corresponding to between about 0.06 and about 1.7 per cent by weight of combined fluorine in the solution, values of 0.23 to 0.67 per cent being most ad. vantageous. If concentrations below about 0.06 per cent are used the efiectiveness of the solu:
- tion is impaired, whereas at fluoride concentrations much above 1.3 to 1.7 per cent the solu-' .tion no longer produces chromate-type coatings but tends to form non-adherent deposits of mottled appearance.
- the magnesiumbase alloy article to be coated is first cleaned by' conventional methods such as solvent degreasing
- the article is then immersed in the coating bath as described above for a time sufficient to produce a satisfactory finish, usually for 0.2 minute or more, usually about one minute, after which it is withdrawn from the bath, allowed to drain free of solution, washed, and dried.
- the temperature of the coating bath is not critical, room temperature being-customary.
- the coatings produced in the manner described are of a uniform color, usually brass-like, are extremely adherent to the base metal, and afford protection against corrosion at least equal to that of the standard chrome-pickle. They provide an excellent base for subsequent siccative coatings, such as paints or enamels.
- the process of the invention while effective in producing chromate-type finishes on magnesium-v base alloys of all types, is particularly advan'-' tageous in treating alloys containing at least 85 per cent magnesium and from 4 to 12 per cent of aluminum, with or without lesser proportions of other minor alloying elements such as manganese, zinc, silver, and silicon, since these alloys are the ones which, in certain states of heat treatment, ordinarily contain amagnesium-aluminum intermetallic compound. With such compound containing alloys, the new method is essential in' securing a useful coating.
- Example 1 A sand-cast workpiece of Dowmetal C (a magnesium-base alloy containing 9.0 per cent alumi'e jnum, 2.0 per cent zinc, and 0.1 per cent'maltgae crete phase in the metal, was coated according to the invention. The article was first cleaned of dirt and oily matter by alkaline cleaning, and was then immersed for one minute at room temperature in a solution having the following composition: a V
- Vlfater to make 1.0 gallon.
- the protective coating obtained was a uniform iridescent brassy color, and was free of any gray powdery material. No sparking was observed when the workpiece was subjected to wire brushing and grinding operations.
- Example 2 A pressure die-casting of DowmetalK (a magnesium-base alloy containing 10.0 per cent alumi-; num, 0.5 per cent silicon, and 0.1 per cent man-.
- DowmetalK a magnesium-base alloy containing 10.0 per cent alumi-; num, 0.5 per cent silicon, and 0.1 per cent man-.
- the die-casting was coated by immersing it for one minute at room temperature in a bath having the following com position:
- Nitric acid (sp. gr. 1.42) pints..' 0.9
- a ma ne sium-base alloy containing at least per cent by weight of magnesium and from 4 to 12 per cent -,of aluminum, wherein a magnesium-aluminum,-
- intermetallic compound is. present as a discrete phase in 'the metal, the step of immersingthe article in anaqueous solution, the dissolved conj stituents of which consist of at least 2 per cent 1 ,by weight of a coating substance selected-from the class consisting of chromicacidand water ⁇ - soluble salts thereof, a strong mineralacid infa coating on the surface of articles formed ofmag of the solution below about 2.0, and a substance selected from the class consisting of hydrofluoric acid and water-soluble salts thereof in a concentration corresponding to between about 0.23 and about 0.67 per cent by weight of combined fluorine in the solution, for a time to form a coating on the article.
- a coating substance selected-from the class consisting of chromicacidand water ⁇ - soluble salts thereof, a strong mineralacid infa coating on the surface of articles formed ofmag of the solution below about 2.0
- An aqueous solution for producing protective coatings on the surface of magnesium-base alloys the dissolved constituents of which consists of at least 2 per cent by weight of a substance selected from the class consisting of chromic acid and water-soluble salts thereof, nitric acid in a proportion sufficient to maintain the pH value of the solution below about 2.0, and a substance selected from the class consisting of hydrofluoric acid and water-soluble salts thereof in a concentration corresponding to between about 0.06 and about 1.7 per cent by weight of combined fluorine in the solution.
Description
Patented Oct. 7, 1947 UNITED STATE s PATENT OFFICE SURFACE TREATMENT OF MAGNESIUM ALLO No Drawing. Application August 19, 1944,
' Serial No. 550,314
8 Claims.-
This invention relates to an improved method of producing a protective coating on the surface of aluminum-containing magnesium-base alloys.
Articles of magnesium-base alloys are conventionally protected against corrosion during shipment, storage, and machining, and provided with a paint base by applying to the surface thereof some type of chemical finish, of which the socalled chrome-pickle, produced by immersing the article in an aqueous solution of chromic acid or a soluble chromate and a strong mineral acid, usually nitric acid, is by far the most common. It has been observed, however, that when the chrome-pickle treatment is applied to certain aluminum-containing magnesium-base alloys, there is sometimes obtained, instead of the expected uniform iridescent brass-colored finish ordinarily produced, a coating consisting in part of a loose deposit of a heavy dark gray powder. This powder, which has been identified as an intermetallic compound of magnesium and a-luminum (probably MgsAlz OI"Mg'4A13)', not, only seriously detracts from the appearance of the treated article but also constitutes a distinct fire hazard, since, in addition to being easily ignited, it produces sparks on the application of slight frictional forces. Unless precautions are taken, simple wire-brushing or grinding of powdercoated parts may cause minor fires in accumulated dust, and even the striking together of two coated articles results in serious sparking. The occasional occurrence of this powder, then, is a serious practical disadvantage in the application of the chrome-pickle treatment to magnesiumbase alloys of all types.
Extended investigation of the "chrome-pickle procedure has shown that the dark gray powdery deposit of magnesium-aluminum compoundis obtained principally in the treatment of articles formed of magnesium-base alloys containing at least 85 per cent by weightof magnesium and from 4 to 12 per cent of aluminum, especially when these alloys are in a metallurgical state such that a magnesium-aluminum intermetallic compound is present as a discrete phase in the solid metal, as is the usual case with articles' which have been pressure die-cast or have beenheat-treated and aged. Incoating such articles;
the chrome-pickle solution appears to etch ormains on the surface of the treated article and gives rise to the non-uniform appearance and sparking hazard mentioned.
In an effort to eliminate formation of the powdery deposit, the prior art has suggested solution heat-treating the articles before chromepickling so as to dissolve the discrete intermetallic compound" into the body of the magnesiumbase alloy matrix. This process, while effective, is inapplicable in many instances since the heattreating operation alters the physical properties of the metal. In addition, even where such alteration may be tolerated, the metal frequently tends to blister at the high temperatures involved, and must often be refinished before the chemical coating is applied. In so'far as is known, no satisfactory solution of the powder formation problem has heretofore been available.
An object of the invention, therefore, is to provide a ooatingmethod' for magnesium-base alloys which retains the advantages of the chromepic'kle process and at the same time eliminates formation of the powdery gray deposit Without altering the physicalcharacteristics of the articles treated.
This object is realized in the process of the invention, which consists essentially in subjecting the article to be treated to the action of a solution of the chrome-pickle type to which has been added a small proportion of a fluoride.
The presence of this latter ingredient injs'ure's dissolution of any" magnesium-aluminum intermetallic compound present in the metal being treated without otherwise appreciably altering the course of the treatment; The uniform pleasing iridescent brassy finish characteristic of the chrome-pickle is invariably obtained, and no formation of dark gray powdery deposit is observed.
The treating solution used in the process is an aqueous solution containing as the effective ingredients chromic acid or a water-soluble salt thereof, a strong mineral acid, and hydrofluoric acid or a water-soluble salt thereof. The chromate constituent is ordinarily added in the form of chromic anhydride (0103) or an alkali metal or ammonium chromate or bichromate, sodium bichromate' being'convenient'. Concentrations of chromic acid or soluble chromate of at least 2 per cent by weight of the solution are ordinarily added in a proportion sufficient to maintain the pH value of the solution below about 2.0, preferably about 0.3 to 1.0.
. or alkaline cleaning.
Nitric acid is most satisfactory in producing a coating useful as an adherent paint base. The fluoride ingredient is conveniently aqueous hydrofluoric acid or a solid alkali metal or ammonium fluoride or bifluoride, such as sodium fluoride or ammonium bifluoride (NHiHFz), although other simple fluorides are: operable. Complex fluo-acids and their salts are not effective. The hydrofluoric acid or fluoride should be added in a proportion corresponding to between about 0.06 and about 1.7 per cent by weight of combined fluorine in the solution, values of 0.23 to 0.67 per cent being most ad. vantageous. If concentrations below about 0.06 per cent are used the efiectiveness of the solu:
tion is impaired, whereas at fluoride concentrations much above 1.3 to 1.7 per cent the solu-' .tion no longer produces chromate-type coatings but tends to form non-adherent deposits of mottled appearance.
In'practicing the invention, the magnesiumbase alloy article to be coated is first cleaned by' conventional methods such as solvent degreasing The article is then immersed in the coating bath as described above for a time sufficient to produce a satisfactory finish, usually for 0.2 minute or more, usually about one minute, after which it is withdrawn from the bath, allowed to drain free of solution, washed, and dried. The temperature of the coating bath is not critical, room temperature being-customary.
The coatings produced in the manner described are of a uniform color, usually brass-like, are extremely adherent to the base metal, and afford protection against corrosion at least equal to that of the standard chrome-pickle. They provide an excellent base for subsequent siccative coatings, such as paints or enamels.
The process of the invention, while effective in producing chromate-type finishes on magnesium-v base alloys of all types, is particularly advan'-' tageous in treating alloys containing at least 85 per cent magnesium and from 4 to 12 per cent of aluminum, with or without lesser proportions of other minor alloying elements such as manganese, zinc, silver, and silicon, since these alloys are the ones which, in certain states of heat treatment, ordinarily contain amagnesium-aluminum intermetallic compound. With such compound containing alloys, the new method is essential in' securing a useful coating. Even in treating ar-" ticles of alloys of this range of compositions in which an intermetallic compound has not been intentionally precipitated in the metal'or is not known to be present, it is advantageous, asa practical measure, to use the process of the invention at all times in place of the conventional chrome-pickle, since the possibility of gray I powder formation due to the unexpected presence of intermetallic compounds is eliminated.
The invention may be further understoodfby. reference to the following examples, which, it will be appreciated, are illustrative'ratherthan lirni tative,
7 Example 1 A sand-cast workpiece of Dowmetal C (a magnesium-base alloy containing 9.0 per cent alumi'e jnum, 2.0 per cent zinc, and 0.1 per cent'maltgae crete phase in the metal, was coated according to the invention. The article was first cleaned of dirt and oily matter by alkaline cleaning, and was then immersed for one minute at room temperature in a solution having the following composition: a V
Sodiumbichromate (NazCr'zOmZHzO) pounds 1.5 Nitric acid (sp. gr. 1.42) pints 1.5
Vlfater, to make 1.0 gallon.
-After, immersion the article was drained to remove solution and then washed in water. .15.
The protective coating obtained was a uniform iridescent brassy color, and was free of any gray powdery material. No sparking was observed when the workpiece was subjected to wire brushing and grinding operations.
Example 2 A pressure die-casting of DowmetalK (a magnesium-base alloy containing 10.0 per cent alumi-; num, 0.5 per cent silicon, and 0.1 per cent man-.
tion. After alkaline cleaning, the die-casting was coated by immersing it for one minute at room temperature in a bath having the following com position:
Chromic anhydride (crop pounds 1.0
Nitric acid (sp. gr. 1.42) pints..' 0.9
Water, to make 1.0 gallon.
After immersion, th idie casting was drained,
rinsed in water, and dried. 'It exhibited aprotective coating similar to that described in Example 1, and free of any gray powdery inclusions.
This application is a. contiriuation-in-part of my copending application Serial No. 429,132, filed. 'January 31, 1942. Y Q p 7 I claim: 7 1. In a method of providing a protective nesium-base alloys, the step of subjecting the article to the action of an aqueous solution, the. dissolved constituents of which consist of a sub-' stance selected from the'class consisting of chro- 1 mic acid and water-soluble salts thereof, a strong mineral-acid in aproportion sufficient to maintain the pH value of the solution. below about;
5a ""sisting of hydrofluoric acid and water-soluble 2.0, and a substance selected'from the class con-1 salts thereof, in a concentration corresponding to between. about 0.06 and-about. 1.7 per cent rby' 7 2;. A method according to claim 1 wherein the strong mineral acid is nitric acid.
nese, the balance being magnesium), which had 11 been solution heat treated and aged in conven-, tional manner to improve the strength and hardness, and which therefore contained a magnesium-aluminum'intermetallic compound as a dis;
3. In a method of providing a protective coat: I
ing on the surface of articles formed of; a ma ne sium-base alloy containing at least per cent by weight of magnesium and from 4 to 12 per cent -,of aluminum, wherein a magnesium-aluminum,-
intermetallic compound is. present as a discrete phase in 'the metal, the step of immersingthe article in anaqueous solution, the dissolved conj stituents of which consist of at least 2 per cent 1 ,by weight of a coating substance selected-from the class consisting of chromicacidand water{- soluble salts thereof, a strong mineralacid infa coating on the surface of articles formed ofmag of the solution below about 2.0, and a substance selected from the class consisting of hydrofluoric acid and water-soluble salts thereof in a concentration corresponding to between about 0.23 and about 0.67 per cent by weight of combined fluorine in the solution, for a time to form a coating on the article.
4. A method according to claim 3 wherein the strong mineral acid is nitric acid.
5. A method according to claim 3 wherein the coating substance is sodium bichromate and the strong mineral acid is nitric acid.
6. A method according to claim 3 wherein the coating substance is chromic acid and the strong mineral acid is nitric acid.
7. In a process of providing a protective coating on the surface of articles formed of aluminum-containing magnesium-base alloys in which a magnesium-aluminum intermetallic compound is present a a discrete phase in the metal, wherein the article is subjected to the action of an aqueous solution, the dissolved constituents of which consist of chromic acid or a water-soluble salt thereof and a strong mineral acid in a proportion sufficient to maintain the pH value of the solution below about 2.0, the method of insuring dissolution of theaforesaid intermetallic compound during treatment which comprises maintaining dissolved in the treating solution a substance selected from the class consisting of hydrofluoric acid and water-soluble salts thereof in a concentration corresponding to 6 between about 0.06 and about 1.7 per cent by weight of combined fluorine in the solution.
8. An aqueous solution for producing protective coatings on the surface of magnesium-base alloys, the dissolved constituents of which consists of at least 2 per cent by weight of a substance selected from the class consisting of chromic acid and water-soluble salts thereof, nitric acid in a proportion sufficient to maintain the pH value of the solution below about 2.0, and a substance selected from the class consisting of hydrofluoric acid and water-soluble salts thereof in a concentration corresponding to between about 0.06 and about 1.7 per cent by weight of combined fluorine in the solution.
HERBERT K. DE LONG.
REFERENCES CITED 'The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,172,041 Urban Sept. 5, 1939 2,269,435 Buzzard Jan. 13, 1942 2,313,755 Loose Mar. 16, 1943 2,322,205 De Long June 22, 1943 FOREIGN PATENTS Number Country Date 136,060 Switzerland Dec. 16, 1929
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US550314A US2428749A (en) | 1944-08-19 | 1944-08-19 | Surface treatment of magnesium alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US550314A US2428749A (en) | 1944-08-19 | 1944-08-19 | Surface treatment of magnesium alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2428749A true US2428749A (en) | 1947-10-07 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US550314A Expired - Lifetime US2428749A (en) | 1944-08-19 | 1944-08-19 | Surface treatment of magnesium alloys |
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Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2507956A (en) * | 1947-11-01 | 1950-05-16 | Lithographic Technical Foundat | Process of coating aluminum |
| US2613165A (en) * | 1950-07-03 | 1952-10-07 | Aluminum Co Of America | Surface treatment of magnesium and magnesium alloy articles |
| US2620265A (en) * | 1950-09-28 | 1952-12-02 | Kaiser Aluminium Chem Corp | Composition for treating aluminum and aluminum alloys |
| US2674523A (en) * | 1953-04-24 | 1954-04-06 | Kelite Products Inc | Process and composition for treatment of magnesium prior to spot welding |
| US2727841A (en) * | 1950-11-30 | 1955-12-20 | Poor & Co | Method and composition for improving corrosion resistance of zinc |
| US2798829A (en) * | 1953-08-04 | 1957-07-09 | American Chem Paint Co | Process for enhancing the corrosion resistance of certain coated aluminum surfaces |
| US2808542A (en) * | 1953-12-28 | 1957-10-01 | Gen Electric | Foil for electrolytic condensers and process |
| US2847371A (en) * | 1955-06-28 | 1958-08-12 | Tiarco Corp | Chromium plating on aluminum |
| US2854371A (en) * | 1956-02-01 | 1958-09-30 | Shwayder Bros Inc | Method and solution for treatment of magnesium articles |
| US2859144A (en) * | 1954-08-27 | 1958-11-04 | Poor & Co | Process and composition for protectively coating aluminum and aluminum alloys |
| US2864730A (en) * | 1953-12-17 | 1958-12-16 | Allied Res Products Inc | Method for protecting magnesium and magnesium alloys from corrosion |
| US2883311A (en) * | 1956-10-01 | 1959-04-21 | Vertol Aircraft Corp | Method and composition for treating aluminum and aluminum alloys |
| US2946728A (en) * | 1955-06-23 | 1960-07-26 | Cleveland Pneumatic Ind Inc | Adherent electroplating on titanium |
| US2961358A (en) * | 1957-03-08 | 1960-11-22 | Amchem Prod | Method of forming a chromate conversion coating on magnesium |
| US2983634A (en) * | 1958-05-13 | 1961-05-09 | Gen Am Transport | Chemical nickel plating of magnesium and its alloys |
| US3039909A (en) * | 1956-07-09 | 1962-06-19 | Dow Chemical Co | Method of uniformly reducing the dimensions of magnesium shapes |
| US3345276A (en) * | 1963-12-23 | 1967-10-03 | Ibm | Surface treatment for magnesiumlithium alloys |
| US3367799A (en) * | 1963-10-08 | 1968-02-06 | Army Usa | Process for cleaning aluminum |
| US3411958A (en) * | 1965-05-03 | 1968-11-19 | Mc Donnell Douglas Corp | Treatment of steel parts |
| US3416975A (en) * | 1965-05-04 | 1968-12-17 | Nasa | Etching of aluminum for bonding |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH136060A (en) * | 1928-02-21 | 1929-10-31 | Sprenger Patentverwertung Otto | Process for the production of coatings on metals. |
| US2172041A (en) * | 1937-10-07 | 1939-09-05 | Stephen F Urban | Pickling solution |
| US2269435A (en) * | 1940-11-27 | 1942-01-13 | Robert W Buzzard | Treatment for coated magnesium and its alloys |
| US2313755A (en) * | 1938-12-02 | 1943-03-16 | Dow Chemical Co | Method of producing protective coatings upon magnesium and its alloys |
| US2322205A (en) * | 1939-05-01 | 1943-06-22 | Dow Chemical Co | Method of treating magnesium and its alloys |
-
1944
- 1944-08-19 US US550314A patent/US2428749A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH136060A (en) * | 1928-02-21 | 1929-10-31 | Sprenger Patentverwertung Otto | Process for the production of coatings on metals. |
| US2172041A (en) * | 1937-10-07 | 1939-09-05 | Stephen F Urban | Pickling solution |
| US2313755A (en) * | 1938-12-02 | 1943-03-16 | Dow Chemical Co | Method of producing protective coatings upon magnesium and its alloys |
| US2322205A (en) * | 1939-05-01 | 1943-06-22 | Dow Chemical Co | Method of treating magnesium and its alloys |
| US2269435A (en) * | 1940-11-27 | 1942-01-13 | Robert W Buzzard | Treatment for coated magnesium and its alloys |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2507956A (en) * | 1947-11-01 | 1950-05-16 | Lithographic Technical Foundat | Process of coating aluminum |
| US2613165A (en) * | 1950-07-03 | 1952-10-07 | Aluminum Co Of America | Surface treatment of magnesium and magnesium alloy articles |
| US2620265A (en) * | 1950-09-28 | 1952-12-02 | Kaiser Aluminium Chem Corp | Composition for treating aluminum and aluminum alloys |
| US2727841A (en) * | 1950-11-30 | 1955-12-20 | Poor & Co | Method and composition for improving corrosion resistance of zinc |
| US2674523A (en) * | 1953-04-24 | 1954-04-06 | Kelite Products Inc | Process and composition for treatment of magnesium prior to spot welding |
| US2798829A (en) * | 1953-08-04 | 1957-07-09 | American Chem Paint Co | Process for enhancing the corrosion resistance of certain coated aluminum surfaces |
| US2864730A (en) * | 1953-12-17 | 1958-12-16 | Allied Res Products Inc | Method for protecting magnesium and magnesium alloys from corrosion |
| US2808542A (en) * | 1953-12-28 | 1957-10-01 | Gen Electric | Foil for electrolytic condensers and process |
| US2859144A (en) * | 1954-08-27 | 1958-11-04 | Poor & Co | Process and composition for protectively coating aluminum and aluminum alloys |
| US2946728A (en) * | 1955-06-23 | 1960-07-26 | Cleveland Pneumatic Ind Inc | Adherent electroplating on titanium |
| US2847371A (en) * | 1955-06-28 | 1958-08-12 | Tiarco Corp | Chromium plating on aluminum |
| US2854371A (en) * | 1956-02-01 | 1958-09-30 | Shwayder Bros Inc | Method and solution for treatment of magnesium articles |
| US3039909A (en) * | 1956-07-09 | 1962-06-19 | Dow Chemical Co | Method of uniformly reducing the dimensions of magnesium shapes |
| US2883311A (en) * | 1956-10-01 | 1959-04-21 | Vertol Aircraft Corp | Method and composition for treating aluminum and aluminum alloys |
| US2961358A (en) * | 1957-03-08 | 1960-11-22 | Amchem Prod | Method of forming a chromate conversion coating on magnesium |
| US2983634A (en) * | 1958-05-13 | 1961-05-09 | Gen Am Transport | Chemical nickel plating of magnesium and its alloys |
| US3367799A (en) * | 1963-10-08 | 1968-02-06 | Army Usa | Process for cleaning aluminum |
| US3345276A (en) * | 1963-12-23 | 1967-10-03 | Ibm | Surface treatment for magnesiumlithium alloys |
| US3411958A (en) * | 1965-05-03 | 1968-11-19 | Mc Donnell Douglas Corp | Treatment of steel parts |
| US3416975A (en) * | 1965-05-04 | 1968-12-17 | Nasa | Etching of aluminum for bonding |
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