US3136632A - Aluminum base alloy - Google Patents
Aluminum base alloy Download PDFInfo
- Publication number
- US3136632A US3136632A US153710A US15371061A US3136632A US 3136632 A US3136632 A US 3136632A US 153710 A US153710 A US 153710A US 15371061 A US15371061 A US 15371061A US 3136632 A US3136632 A US 3136632A
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- aluminum
- coating
- alloy
- aluminum base
- magnesium
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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
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/12—Aluminium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
Definitions
- This invention relates to a method for producing composite metal articles having a ferrous metal base portion coated with aluminum or aluminum base alloys, the composite article produced thereby and the aluminum base coating alloys. More particularly this invention relates to a method for coating a ferrous metal base with aluminum or aluminum alloys which provides a coating characterized by a lustrous smooth appearance free from the presence of stains, the composite articles produced thereby and the aluminum base coating alloys.
- Coatings of aluminum on ferrous metal products are highly desirable since the composites resulting in effect embody superior properties resident in each metal.
- the aluminum coating adds the more salient properties of resistance to corrosion and oxidation at both atmospheric and somewhat elevated temperatures, enhanced electrical conductivity, improvement in the brazing of aluminum to steel and a more attractive appearance.
- the appearance of the a coating In the production of aluminum coated ferrous metal articles one of the primary factors in regard to commercially acceptable results is the appearance of the a coating.
- a lustrous smooth appearance similar to the color and texture of cast aluminum is a desirable characteristic in such aluminum coatings.
- the coatings may display a brown or tan stain, particularly if the ferrous article is quenched in Water while the coating is still molten.
- many aluminizing alloys may not be productive of satisfactory results.
- beryllium has been added to aluminizing alloys to provide a clean bath surface and to prevent staining of the coating during air cooling.
- beryllium is very expensive and while the amount of beryllium added to the aluminizing alloy may be small, a continual replacement is required to maintain bright coatings.
- the use of beryllium in aluminizing alloys is expensive.
- Examples of prior art aluminum metal baths for coating ferrous base metal are commercially pure aluminum, aluminum-silicon alloys and an alloy consisting essentially of by weight from 1 to 6% silicon, at least one element selected from the group consisting of chromium, molybdenum and tungsten in amount from about 0.1 to 0.4%, the total not exceeding about 0.5 at least one element selected from the group consisting of boron, titanium, vanadium and zirconium in amount from about 0.02 to about 0.20% boron and titanium, and from about 0.1 to about 0.25% vanadium and zirconium, the total of these last named elements not exceeding about 0.5%, 0.001 to 0.10% sodium, balance substantially all aluminum and impurities in normal amounts.
- magnesium from about 0.05 to 0.45% by Weight are productive of satisfactory results wherein the production of an attractive relatively smooth stain free coating is the primary factor with regard to the intended purpose of the composite article.
- amounts of magnesium from about 0.1 to 0.2% by 0.05% by weight magnesium do not provide sufiicient resistance to staining.
- the ferrous articles to be coated are first thoroughly cleaned by a suitable method, such as acid pickling, to remove oxide film or scale. They may then be rinsed, dried and immersed in the coating bath with or without the use of a conventional flux. For large sections the use of flux may be used for further cleaning before immersion in the alloy bath.
- the articles with or without pickling depending on the nature of the surface, may be pretreated by bright annealing in suitable apparatus in an inert or reducing atmosphere and then directly immersed in the molten coating bath Without exposure to the atmosphere. 7
- the bath temperature is maintained suificiently high so that the alloys employed are completely molten.
- the particular bath temperature depends upon the coating alloy composition and the composition and nature of the ferrous article and, in regard to the alloys herein disclosed, temperatures generally of from 1280 to 1375 F. are recommended.
- j V 7 Since thickness of the Fe-Al interfacial layer increases with bath temperature,'it is recommended that the lowest operating temperature consistent with good coating results be used to minimize cracking and spalling' molten bath.
- the immersion time and also. the bath temperature may be regulated to produce a composition suitable for the intended application. Extending the time of immersion tends to increase the thickness of the FeAl layer and, accordingly, the shortest immersion time consistent with satisfactory coverage is usually recommended.
- Panels of mild steel measuring 4 X 6" X .035 were degreased by furnace bluing then pickled in a 20 HCl solution at 170 F. for from 30 to 120 seconds. This was followed by dipping in an aqueous solution of Na SiF plus ZrCl Each specimen was then dipped for from 4 to seconds in a molten bath of aluminum base alloy maintained at 1300 F. The compositions of the bath employed are indicated below. The coated specimens were then withdrawn and tapped lightly while in countered in continued operation, 1.7% by weight iron was added to the melt. The amounts of magnesium as indicated in Table I below were then incrementally added to the melt and specimens immersed in each alloy. Table V I indicates the appearance of these specimens.
- Another'aluminum base alloy bath was made up from approximately 10 pounds of an aluminum-5% by weight silicon alloy which was melted in an induction furnace and to which 1.7 by weightiron was added for reasons Do. Rough and wrinkled;
- Another aluminum base alloy bath was made up from approximately 10 pounds of an aluminum base alloy consisting essentially of, by weight, 2.50% silicon, 0.10% chromium, 0.10% molybdenum, 0.05% titanium, 0.002% sodium, balance substantially all aluminum and impurities in normal amounts, which was melted in an induction furnace and to which 1.7 by weight iron was added for reasons given above.
- the amounts of magnesium as indicated in Table IV below were then incrementally added to the melt and specimens immersed in each alloy. Table IV indicates the appearance of these specimens.
- aluminurnfv is meant to cover high purity aluminum, commercial purity aluminum and aluminum base alloys.
- An aluminum base alloy for coating ferrous metal wherein the coated surface is characterized by smoothness and freedom from staining, consisting essentially of from about I to 6% silicon, at least one element selected from the group consisting of. chromium, molybdenum and tungsten in amount from about 0.1 to about 0.4%,
- the total not exceeding about 0.5% at least one element selected from the group consisting of boron, titanium, vanadium and zirconium in amount from about 0.02 to about 0.20% boron and titanium, and from about 0.1 to about 0.25% vanadium and zirconium, the total of these last named elements not exceeding about 0.5%, 0.001 to 0.10% sodium, 0.05 to 0.45% magnesium, balance substantially all aluminum and impurities in normal amounts.
- An aluminum base alloy for coating ferrous metal wherein the coated surface is characterized by smoothness and freedom from staining, consisting essentially of 6 about 2.50% silicon, 0.10% chromium, 0.10% molybdenum, 0.05% titanium, 0.002% sodium, 0.1 to 0.2% magnesium, balance substantially all aluminum and impurities in normal amounts.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Coating With Molten Metal (AREA)
Description
United States Patent 3,136,632 ALUMINUM BASE ALLOY John D. Sprowl, Spokane, Wash, assignor to Kaiser Aluminum & Chemical Corporation, Oakland, Calif, a corporation of Delaware No Drawing. Original application May 26, 1958, Ser. No. 737,485, now Patent No'. 3,055,771, dated Sept. 25, 1962. Divided and this application Nov. 20, 1961, Ser. No. 153,710
2 Claims. (Cl. 75-147) This invention relates to a method for producing composite metal articles having a ferrous metal base portion coated with aluminum or aluminum base alloys, the composite article produced thereby and the aluminum base coating alloys. More particularly this invention relates to a method for coating a ferrous metal base with aluminum or aluminum alloys which provides a coating characterized by a lustrous smooth appearance free from the presence of stains, the composite articles produced thereby and the aluminum base coating alloys.
This application is a divisional application of my copending application Serial Number 737,485, filed May 26, 1958, now issued as United States Patent 3,055,771.
Coatings of aluminum on ferrous metal products are highly desirable since the composites resulting in effect embody superior properties resident in each metal. To the strength and other desirable characteristics of the iron or steel core, the aluminum coating adds the more salient properties of resistance to corrosion and oxidation at both atmospheric and somewhat elevated temperatures, enhanced electrical conductivity, improvement in the brazing of aluminum to steel and a more attractive appearance.
In the production of aluminum coated ferrous metal articles one of the primary factors in regard to commercially acceptable results is the appearance of the a coating. A lustrous smooth appearance similar to the color and texture of cast aluminum is a desirable characteristic in such aluminum coatings. When utilizing many aluminizing alloys the coatings may display a brown or tan stain, particularly if the ferrous article is quenched in Water while the coating is still molten. Where the aluminum coated ferrous article is intended for ornamental purposes or for some other reason a stain free surface is desired, many aluminizing alloys may not be productive of satisfactory results.
In accordance with the prior art, beryllium has been added to aluminizing alloys to provide a clean bath surface and to prevent staining of the coating during air cooling. However, beryllium is very expensive and while the amount of beryllium added to the aluminizing alloy may be small, a continual replacement is required to maintain bright coatings. Thus the use of beryllium in aluminizing alloys is expensive.
Accordingly, it is an object of the present invention to provide a method of coating ferrous base metal to produce composite articles wherein the coating is characterized by a smooth appearance free or essentially free from any presence of staining.
It is a further object of this invention to provide an aluminum base alloy for coating ferrous base metal articles which provides a coating in the solid state or ascoated condition eminently suitable for ornamental or other purposes due to a lustrous smooth appearance and freedom from the presence of stains.
It is a still further object of the invention to provide aluminum alloy coated composite articles characterized by a lustrous smooth appearance and freedom from stains and relatively inexpensive aluminum base alloys for production thereof wherein conventional methods of hot dip coating may be employed.
FF W
. Other objects and advantages of the invention will be apparent from the following detailed description thereof.
It has been discovered that the maintenance of a small but effective amount of magnesium in a molten coating bath of aluminum results in a coating exhibiting an appearance characterized by freedom from staining. When compared to the appearance of prior art commercially pure aluminum and aluminum alloy coatings, the freedom from staining of the coatings of the present invention is unique. Examples of prior art aluminum metal baths for coating ferrous base metal are commercially pure aluminum, aluminum-silicon alloys and an alloy consisting essentially of by weight from 1 to 6% silicon, at least one element selected from the group consisting of chromium, molybdenum and tungsten in amount from about 0.1 to 0.4%, the total not exceeding about 0.5 at least one element selected from the group consisting of boron, titanium, vanadium and zirconium in amount from about 0.02 to about 0.20% boron and titanium, and from about 0.1 to about 0.25% vanadium and zirconium, the total of these last named elements not exceeding about 0.5%, 0.001 to 0.10% sodium, balance substantially all aluminum and impurities in normal amounts.
In general it has been found that amounts of magnesium from about 0.05 to 0.45% by Weight are productive of satisfactory results wherein the production of an attractive relatively smooth stain free coating is the primary factor with regard to the intended purpose of the composite article. However, optimum results in regard to smoothness and freedom from staining are realized by amounts of magnesium from about 0.1 to 0.2% by 0.05% by weight magnesium do not provide sufiicient resistance to staining.
Although the addition of magnesium to the aluminum alloy in accordance with this invention is primarily suited for ornamental purposes due to the freedom from staining obtained, it was found that there was a lack of any substantial adverse effect upon the ductility of the composites produced.
In accordance with this invention, the ferrous articles to be coated are first thoroughly cleaned by a suitable method, such as acid pickling, to remove oxide film or scale. They may then be rinsed, dried and immersed in the coating bath with or without the use of a conventional flux. For large sections the use of flux may be used for further cleaning before immersion in the alloy bath. On the other hand, the articles with or without pickling, depending on the nature of the surface, may be pretreated by bright annealing in suitable apparatus in an inert or reducing atmosphere and then directly immersed in the molten coating bath Without exposure to the atmosphere. 7
The bath temperature is maintained suificiently high so that the alloys employed are completely molten. Of course, the particular bath temperature depends upon the coating alloy composition and the composition and nature of the ferrous article and, in regard to the alloys herein disclosed, temperatures generally of from 1280 to 1375 F. are recommended. j V 7 Since thickness of the Fe-Al interfacial layer increases with bath temperature,'it is recommended that the lowest operating temperature consistent with good coating results be used to minimize cracking and spalling' molten bath. The immersion time and also. the bath temperature may be regulated to produce a composition suitable for the intended application. Extending the time of immersion tends to increase the thickness of the FeAl layer and, accordingly, the shortest immersion time consistent with satisfactory coverage is usually recommended.
The improved results obtained by the practice of this invention are more fully illustrated with reference to' the examples below:
Panels of mild steel measuring 4 X 6" X .035 were degreased by furnace bluing then pickled in a 20 HCl solution at 170 F. for from 30 to 120 seconds. This was followed by dipping in an aqueous solution of Na SiF plus ZrCl Each specimen was then dipped for from 4 to seconds in a molten bath of aluminum base alloy maintained at 1300 F. The compositions of the bath employed are indicated below. The coated specimens were then withdrawn and tapped lightly while in countered in continued operation, 1.7% by weight iron was added to the melt. The amounts of magnesium as indicated in Table I below were then incrementally added to the melt and specimens immersed in each alloy. Table V I indicates the appearance of these specimens.
TABLE I Appearance of Aluminized Steel Panels Color Luster Surface texture Light tan Very light tan...
Li ht.
Slightly rough.
Do. Do. Smooth.
Do. Do.
Fairly bright do Dull Wrinkled. Very wrinkled.
TABLE II Appearance of Aluminized Steel Panels Percent Color Luster Surface texture Mg by wt.
0.00 Brown spotted Smooth. 0.05. Light- Do. 0.10. Do. 0.20 Do. 0.30 Do. 0.40 Slightly wrinkled. 0 50 do Wrinkled. 1.00 do Wrinkled, rough.
Another'aluminum base alloy bath was made up from approximately 10 pounds of an aluminum-5% by weight silicon alloy which was melted in an induction furnace and to which 1.7 by weightiron was added for reasons Do. Rough and wrinkled;
unsatisfactory.
4 given above. The amounts of magnesium as indicated in Table III below were then incrementally added to the melt and specimens immersed in each alloy. Table III indicated the appearance of these specimens.
TABLE. III
Appearance of Alaminized Steel Panels Percent Mg by wt.
Surface texture Color i Luster Slightly rough.
Rough, wrinkled.
Very rough,
wrinkled.
Another aluminum base alloy bath was made up from approximately 10 pounds of an aluminum base alloy consisting essentially of, by weight, 2.50% silicon, 0.10% chromium, 0.10% molybdenum, 0.05% titanium, 0.002% sodium, balance substantially all aluminum and impurities in normal amounts, which was melted in an induction furnace and to which 1.7 by weight iron was added for reasons given above. The amounts of magnesium as indicated in Table IV below were then incrementally added to the melt and specimens immersed in each alloy. Table IV indicates the appearance of these specimens.
It is readily seen from the results indicated above that the surfaces of the aluminized articles employing the principles of this invention were superior to those produced outside the teachings of this invention. More specifically, it will be noted that those coating baths containing magnesium in amounts above about 0.45% resulted in coatings which were wrinkled and, accordingly,
Those coating baths containing magnesium contents below about 0.05% resulted in coatings characterized by tan or brown stain and thus were also unsatisfactory. While some of the samples having magnesium contents within the broad range of the invention exhibited slight wrinkling or slight roughness, the coatings produced were satisfactory from an appearance standpoint for many purposes.
As used herein the term aluminurnfv is meant to cover high purity aluminum, commercial purity aluminum and aluminum base alloys.
It will be understood that various changes, omissions and additions may be made to this invention without departing from the spirit and scope thereof as set forth in the appended claims.
All percentages in the claims are by Weight of the total coating bath.
What is claimed is:
1 An aluminum base alloy for coating ferrous metal wherein the coated surface is characterized by smoothness and freedom from staining, consisting essentially of from about I to 6% silicon, at least one element selected from the group consisting of. chromium, molybdenum and tungsten in amount from about 0.1 to about 0.4%,
the total not exceeding about 0.5%, at least one element selected from the group consisting of boron, titanium, vanadium and zirconium in amount from about 0.02 to about 0.20% boron and titanium, and from about 0.1 to about 0.25% vanadium and zirconium, the total of these last named elements not exceeding about 0.5%, 0.001 to 0.10% sodium, 0.05 to 0.45% magnesium, balance substantially all aluminum and impurities in normal amounts.
2. An aluminum base alloy for coating ferrous metal wherein the coated surface is characterized by smoothness and freedom from staining, consisting essentially of 6 about 2.50% silicon, 0.10% chromium, 0.10% molybdenum, 0.05% titanium, 0.002% sodium, 0.1 to 0.2% magnesium, balance substantially all aluminum and impurities in normal amounts.
References Cited in the file of this patent UNITED STATES PATENTS 1,932,835 Weber Oct. 31, 1933 2,076,578 Kempf et a1 Apr. 13, 1937 2,076,579 Kempf et al Apr. 13, 1937 2,908,566 Cron et al Oct. 13, 1959
Claims (1)
1. AN ALUMINUM BASE ALLOY FOR COATING FERROUS METAL WHEREIN THE COATED SURFACE IS CHARACTERIZED BY SMOOTHNESS AND FREEDOM FROM STAINING, CONSISTING ESSENTIALLY OF FROM ABOUT 1 TO 6% SILICON, AT LEAST ONE ELEMENT SELECTED FROM THE GROUP CONSISTING OD CHROMIUM, MOLYBDENUM AND TUNGSTEN IN AMOUNT FROM ABOUT 0.1 TO ABOUT 0.4%, THE TOTAL NOT EXCEEDING ABOUT 0.5%, AT LEAST ONE ELEMENT SELECTED FROM THE GROUP CONSISTING OF BORON, TITANIUM, VANADIUM AND ZIRCONIUM IN AMOUNT FROM ABOUT 0.02 TO ABOUT 0.20% BORON AND TITANIUM, AND FROM ABOUT 0.1 TO ABOUT 0.25% VANADIUM AND ZIRCONIUM, THE TOTAL OF THESE LAST NAMED ELEMENS NOT EXCEEDING ABOUT 0.5%, 0.001 TO 0.10% SODIUM, 0.05 TO 0.45% MAGNESIUM, BALANCE SUBSTANTIALLY ALL ALUMINUM AND IMPURITIES IN NORMAL AMOUNTS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US153710A US3136632A (en) | 1958-05-26 | 1961-11-20 | Aluminum base alloy |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US737485A US3055771A (en) | 1958-05-26 | 1958-05-26 | Method of coating a ferrous base with aluminum |
US153710A US3136632A (en) | 1958-05-26 | 1961-11-20 | Aluminum base alloy |
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US3136632A true US3136632A (en) | 1964-06-09 |
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US153710A Expired - Lifetime US3136632A (en) | 1958-05-26 | 1961-11-20 | Aluminum base alloy |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2660937A1 (en) * | 1990-04-13 | 1991-10-18 | Centre Rech Metallurgique | PROCESS FOR THE TEMPERED COATING OF A CONTINUOUS STEEL STRIP. |
BE1004077A3 (en) * | 1990-04-13 | 1992-09-22 | Centre Rech Metallurgique | Continuous dip coating method for a steel strip |
US20180021893A1 (en) * | 2015-03-20 | 2018-01-25 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Brazing filler material and brazing sheet |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1932835A (en) * | 1932-09-21 | 1933-10-31 | Aluminum Co Of America | Aluminum alloys |
US2076579A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloy |
US2076578A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloys |
US2908566A (en) * | 1956-06-01 | 1959-10-13 | North American Avation Inc | Aluminum base alloy |
-
1961
- 1961-11-20 US US153710A patent/US3136632A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1932835A (en) * | 1932-09-21 | 1933-10-31 | Aluminum Co Of America | Aluminum alloys |
US2076579A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloy |
US2076578A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloys |
US2908566A (en) * | 1956-06-01 | 1959-10-13 | North American Avation Inc | Aluminum base alloy |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2660937A1 (en) * | 1990-04-13 | 1991-10-18 | Centre Rech Metallurgique | PROCESS FOR THE TEMPERED COATING OF A CONTINUOUS STEEL STRIP. |
BE1004077A3 (en) * | 1990-04-13 | 1992-09-22 | Centre Rech Metallurgique | Continuous dip coating method for a steel strip |
US5279903A (en) * | 1990-04-13 | 1994-01-18 | Centre De Recherches Metallurgiques - Centrum Voor Research In De Metallurgie | Steel product having a coating based on a hypereutectic zinc-aluminum alloy |
US20180021893A1 (en) * | 2015-03-20 | 2018-01-25 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Brazing filler material and brazing sheet |
US10478925B2 (en) * | 2015-03-20 | 2019-11-19 | Kobe Steel, Ltd. | Brazing filler material and brazing sheet |
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