GB2276887A - Metal coated with tin-zinc alloy coating - Google Patents
Metal coated with tin-zinc alloy coating Download PDFInfo
- Publication number
- GB2276887A GB2276887A GB9405510A GB9405510A GB2276887A GB 2276887 A GB2276887 A GB 2276887A GB 9405510 A GB9405510 A GB 9405510A GB 9405510 A GB9405510 A GB 9405510A GB 2276887 A GB2276887 A GB 2276887A
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- United Kingdom
- Prior art keywords
- coating
- tin
- zinc
- weight percent
- metal
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Classifications
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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
- C23C2/08—Tin or alloys based thereon
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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
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/024—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by cleaning or etching
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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
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/026—Deposition of sublayers, e.g. adhesion layers or pre-applied alloying elements or corrosion protection
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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
- C23C2/06—Zinc or cadmium or alloys based thereon
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
- C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/627—Electroplating characterised by the visual appearance of the layers, e.g. colour, brightness or mat appearance
Abstract
A metal substrate such as steel, for use as architectural sheet material, is coated with a low reflecting, high corrosion-resistant, two-phase tin-zinc metallic coating comprising at least 15 weight percent tin and at least 7 weight percent zinc. The coating is applied by passing the sheet through a molten bath of metal comprising less than 0.01% lead, at least 7% zinc, and at least 15% tin until at least 0.01 to 0.05 inch of coating is on said strip. Alternatively the coating may be applied by electroplating. A barrier of nickel, applied by electroplating, may be applied prior to coating with the tin-zinc coating.
Description
Coated Metal
The present invention relates to coated metal, and, more particularly, to coated metal suitable as an architectural sheet material that is environmentally friendly while providing long life and desired colorisation.
As background material, so that the specification need not specify in detail what is known in the art, U.S. Patents 4987716 and 4934120 (incorporated herein by reference) illustrate metal roofing of the type to which this invention can be used.
GB-A-2265389, which describes a process of hot-dip coating roofing materials, is also incorporated herein by reference.
Over the years, architectural materials, such as metal roofing systems and metal siding (guttering) systems, made of pliable metals in various sheet gauge thicknesses have been used.
Metals such as carbon steel, stainless steel, copper and aluminium are the most popular types of metal. These architectural metal materials are commonly treated with corrosion-resistant coatings to prevent rapid oxidation of the metal surface, thereby extending the life of the materials. A popular corrosion-resistant coating for carbon steel and stainless steel is a terne coating. Terne coating has been the predominant and most popular coating for roofing materials due to its relatively low cost, ease of application, excellent corrosion-resistant properties and desirable colorisation during weathering. The terne coating is an alloy typically containing about 80% lead and the remainder tin. The coating is generally applied to-the architectural materials by a hot-dip process wherein the material is immersed into a molten bath of terne metal.Although terne coated sheet metals have exhibited excellent resistant properties and have been used in a variety of applications, the terne coating has been questioned in relation to its impact on the environment. Environmental and public safety laws have been recently proposed and/or passed prohibiting the use of materials containing lead. Because the terne alloy contains a very high percentage of lead, materials coated with terne have been prohibited in various types of usages or applications such as aquifer roofing systems. The concern of lead possibly leaching from the terne coating has made such coated materials inadequate and/or undesirable for several types of building applications. The terne alloy has a further disadvantage in that the newly applied terne is very shiny and highly reflective.As a result, the highlyreflective coating cannot be used on buildings or roofing systems such as at airports and military establishments.
The terne coating eventually loses its highly-reflective properties as the components within the terne coating are reduced (weathered); however, the desired amount of reduction takes approximately 1-1/2 to 2 years when the terne coating is exposed to the atmosphere, thus requiring the terne metals to be stored over long periods of time prior to being used in these special areas. The storage time is significantly prolonged if the terne-coated materials are stored in rolls and the rolls are protected from the atmosphere.
Tin coating of carbon steel is a well-known process for use in the food industry. However, in the specialized art of architectural materials, a tin coating for architectural materials has not been used until done by the present inventors. The most popular process for applying a tin coating to carbon steel for use in the food industry is by an electrolysis process. In an electrolysis process, the coating thickness is very thin and typically ranges between 3.8sox 10 4 to 20.7 X low 4 mm (1.5 X 10 5 to 8.15 X low in.). Furthermore, the equipment and materials needed to properly electroplate the metal materials are very expensive and relatively complex to use. The expense of applying an electroplated-tin coating and the limited obtainable thicknesses of the tin coating are a disadvantage. for using such a process for building and roofing materials.A hotdip process for applying the tin coating may be used; however, if the architectural materials are not properly prepared and the coating is not properly applied to the roofing materials, minute areas of discontinuity in the tin coating may occur resulting in non-uniform corrosion protection. This is especially a problem when the tin is applied to stainless steel materials by a hot-dip process. Tin is not electroprotective to steel under oxidizing conditions.
Consequently, discontinuities in the tin coating result in the corrosion of the exposed metal. Tin coatings have the further disadvantage of having a highly-reflective surface.
As a result, architectural materials coated with a tin coating cannot be used in an environment where highlyreflective materials are undesirable until the coated materials are further treated (i.e. painted) or the tin is allowed time to oxidize.
Coating architectural materials with zinc metal, commonly known as galvanization, is another popular metal treatment to inhibit corrosion. Zinc is a highly desirable metal to coat architectural materials with because of its relatively low cost, ease of application (i.e. hot-dip application) and excellent corrosion resistance. Zinc is also electroprotective to steel under oxidizing conditions and prevents the exposed metal, due to discontinuities in the zinc coating, from corroding. This electrolytic protection extends away from the zinc coating over exposed metal surfaces for a sufficient distance to protect the exposed metal at cut edges, scratches, and other coating discontinuities. With all of the advantages of using zinc, zinc coatings have several disadvantages that make it undesirable for many types of building applications.
Although zinc coatings will bond to many types of metals, the formed bond is not strong and can result in the zinc coating flaking off the building materials. Zinc is also a very rigid and brittle metal and tends to crack and/or flake off when the building materials are formed on site, i.e.
press fitting of roofing materials.
Due to the various environmental concerns and problems associated with corrosion-resistant coatings applied to metal architectural materials, there has been a demand for a coating which can be easily and successfully applied to materials that protect the materials from corrosion, does not have a highly-reflective surface subsequent to application and allows the materials to be formed at the building site.
Summary of The Invention
The present invention relates to a corrosion-resistant coating formulation for use on architectural materials wherein the coating is environmentally friendly, has a low lead content and quickly weathers to a non highly-reflective desirable surface.
In accordance with the principal feature of the invention, there is provided an architectural material typically of stainless steel or carbon steel coated with a tin-zinc alloy. The tin-zinc coating is a two-phase metal coating comprising a large weight percentage of zinc and a relatively large weight percentage of tin. The tin content of the two-phase coating is less than 35 weight percent and the zinc content is at least 65 weight percent. The unique tin-zinc combination provides for both a corrosion-resistant coating that protects the surface of the architectural material from oxidation and also forms a gray surface, which is very similar to weathered terne, and which is also not highly reflective.
In accordance with another aspect of the present invention, the tin-zinc coating is applied to the metal roofing materials by a hot-dip process. If the tin-zinc coating is to be applied to stainless steel architectural materials, the coating is preferably applied to the roofing materials in similar fashion to that disclosed in GB-A-2265389 referred to above.
"Stainless steel" in the application means a large variety of alloy metals containing chromium and iron. The alloy may also contain other elements such as nickel, carbon, molybdenum, silicon, manganese, titanium, boron, copper, aluminium, nitrogen and various other metals or compounds. Elements such as nickel can be flashed (electroplated) onto the surface of the chromiumiron alloy or directly incorporated into the chromium-alloy.
The hot dip process disclosed in GB-A-2265389 must be slightly modified to accommodate the higher temperatures necessary to hot-dip coat the tin-zinc coating. Tin melts at 2320C (4500F) and lead melts at 3280C (6220F). In the hot-dip process of GB-A-2265389, the coating metal has a large amount of tin thus causing the melting temperature of the coating to be close to 232"C (4500F). In the present invention, the zinc component of the metal coating is the largest component. Zinc melts at 420"C (7880F). As a result, the melting point of the tin-zinc coating approaches 420"C which is a significantly higher temperature than which was used in the process disclosed in GB-A2265389. To accommodate for the higher temperatures, the coating vat may have to be made of a material which can withstand the higher temperatures.Furthermore, the time for cooling the tin-zinc coating may have to be increased. Other than these modifications, the process disclosed in GB-A-2265389 is used to coat the tin-zinc coating onto stainless steel. The hot-dip process disclosed in GB-A-2265389 can be used to coat architectural materials made of metals other than stainless steel such as carbon steel, aluminium, copper, bronze, etc.
In accordance with another aspect of the invention, bismuth and antimony may be added to the tin-zinc coating to inhibit the crystallization of the tin in cold weather. When tin crystallizes, the bonding of the tin-zinc coating to the roofing materials may weaken resulting in flaking of the coating. The addition of small amounts of bismuth and/or antimony prevents such crystallization of the tin. Bismuth or zinc may be added in larger quantities to also enhance the hardness and strength of the tin-zinc coating to increase the resistance to wear of the coating.
In accordance with another feature of the present invention, the tin-zinc coating is essentially lead free. The lead content is maintained at extremely low levels not exceeding 0.05 weight percent. Preferably, the lead content is maintained at much lower weight percentage levels so as to dispense with any environmental concerns associated with the tin-zinc coating.
In accordance with yet another feature of the present invention, the tin-zinc coating composition is such that the coating provides excellent corrosion resistance and the coated materials can be formed on site without the tin-zinc coating cracking and/or flaking off. The amount of zinc in the tin-zinc coating is controlled such that the coating does not become too rigid and brittle.
In accordance with still another aspect of the present invention, the metallic roofing materials are plated with a nickel barrier prior to applying the tin-zinc coating to provide additional corrosion resistance, especially against halogens such as chlorine. The nickel barrier is applied to the metal building materials at a thin layer. Although the tin-zinc coating provides excellent protection against most of these corrosion-producing elements and compounds, compounds such as chlorine have the ability to eventually penetrate the tin-zinc coating and attack and oxidize the surface of the metallic building materials thereby weakening the bond between the roofing material and the tin-zinc coating. The nickel barrier has been found to provide an almost impenetrable barrier to these elements and/or compounds which in fact penetrate the tin-zinc coating.Due to the very small amount of these compounds penetrating the tinzinc coating, the thickness of the nickel barrier can be maintained at thin thicknesses while still maintaining the ability to prevent these components from attacking the metal roofing material. The tin-zinc coating and thin nickel coating effectively complement one another to provide superior corrosion resistance.
The primary object of the present invention is the provision of an architectural material coated with a metallic coating which is highly corrosive resistant.
Another object of the present invention is the provision of an architectural material treated with a metallic coating that is not highly reflective.
Yet another object of the present invention is a metallic coating, as defined above, which is a two-phase system comprised of tin and zinc.
Yet another object of the present invention is the provision of a roofing material having a tin-zinc metallic coating which is essentially lead free.
Still yet another object of the present invention is to provide a two-phase, tin-zinc metallic coating applied to a base metal sheet which coated sheet can be formed and sheared to form various building and roofing components that can be subsequently assembled on site without the metallic coating flaking off, chipping, and/or cracking.
Still another object of the present invention is the provision of providing a tin-zinc coated roofing material which can be preformed into roof pans and subsequently seamed on site either by pressed seams or soldered seams into waterproof joints.
Another object of the present invention is the provision of applying a thin nickel barrier to the surface of the roofing material prior to applying the tin-zinc coating.
These and other objects and advantages will become apparent to those skilled in the art upon reading -of the detailed description of the invention set forth below.
Description of The Preferred Embodiment
The tin-zinc coating is a two-phase metallic coating which, when applied to stainless steel or low carbon steel materials, forms a highly corrosion-resistant coating that reduces the corrosion of the materials when exposed to the atmosphere. The tin-zinc coating contains a large weight percentage of zinc and essentially the balance of tin. It has been discovered that by adding zinc in the amounts of at least 65 weight percent of the tin-zinc alloy, the corrosion resistance of the two-phase metallic coating is significantly increased as compared to a protective coating essentially composed of tin. Although the exact reasons for this physical phenomenon of increased corrosion resistance due to the addition of zinc to tin is unknown to the inventors, it has been found that by adding zinc to tin, the two-phase metallic coating exhibits corrosive-resistant properties which exceed that of tin coatings and, in some environments, that of a terne coating. The tin-zinc coating is electroprotective under oxidizing conditions which inhibits oxidation of exposed metal near the tin-zinc coating. As a result, minor discontinuities in the tin-zinc coating do not result in oxidation of the exposed metal, a contrary result if only a tin coating is used.The tin-zinc coating may contain small amounts of other metals to modify the physical properties of the tin-zinc, two-phase metallic coating; however, these secondary metal components contribute primarily to the strength of the coating and not to the corrosion-resistant properties of the coating. The tin-zinc coating can be applied to both stainless steel and carbon steel materials by preferably using a conventional hot-dipping process; however, the coating may be applied by other means such as by electroplating, an airknife process, etc. The tin-zinc coating is not limited to only the protection of stainless steel and carbon steel and may also be applied to other metals such as copper, bronze, tin, titanium, etc.
The large zinc content of the two-phase metallic tinzinc coating has not been previously used, especially on architectural materials such as metallic building and roofing materials. The bonding of the tin-zinc coating to carbon steel and stainless steel roofing materials is surprisingly strong and forms a durable protective coating which is not easily removable, thereby resisting flaking of the coating. The surfaces of the metallic roofing and building materials may be pretreated prior to the coating to improve the bonding between the tin-zinc coating and the surface of the metallic roofing material. For stainless steel materials, pickling the surface of the stainless steel provides for significantly greater bonding of the coating.
Preferably, the pickling process disclosed in GB-A-2265389 is used to maximize the bonding of the tin-zinc coating to the stainless steel materials.
The life of the architectural material is significantly extended by coating the material with the tin-zinc metallic coating. The tin-zinc coating acts as a barrier to the atmosphere which prevents the metallic coating from ozidizing and/or reducing in the presence of oxygen, carbon dioxide or other reducing agents in the environment. Although the tinzinc coating oxidizes in the presence of various reducing agents in the atmosphere, the rate of oxidation is significantly slower than that of the architectural materials. Furthermore, the tin and zinc oxide which forms on the coating surface provides corrosion resistance to the tin-zinc coating itself which further enhances the corrosion protection provided by the tin-zinc coating. The tin-zinc oxides also reduce the reflectivity of the tin-zinc coating and color the tin-zinc coating.
Terne coated materials have become very popular since terne coated materials eventually weather and turn a grey, earth tone color. The inventors discovered that the novel tinzinc formulations forms a colored coating which closely matches the popular grey, earth tone color of weathered terne. Furthermore, by coating the building materials with the tin-zinc coating, the usable life of the materials is extended typically beyond the life of the structure the coated materials are used on due to the corrosion-resistance of the tin-zinc coating.
The tin-zinc coating is primarily composed of tin and zinc and contains little, if any, lead thus making the coating essentially lead free and environmentally friendly. The lead content, if any, is maintained at extremely low levels within the metallic coating. The amount of lead in the tinzinc coating is maintained such that no more than 0.05 weight percent is present in the coating. Preferably, the lead content in the coating is maintained at levels less than 0.01 weight percent. The limiting of lead content in the metallic coating eliminates any concerns associated with the leaching of the lead from the metallic coating and the environmental concerns associated with products containing lead.
The tin-zinc metallic coating is a two-phase system which contains a large weight percentage of zinc. Preferably, the zinc weight percentage is at least 65% and can be as much as 85% of the tin-zinc coating. The tin content within the metallic coating essentially makes up the balance of the metallic coating. The zinc content ranges between 15-35 weight percent of the tin-zinc metallic coating.
Preferably, the metallic coating includes 20 weight percent tin. The tin-zinc system forms a two-phase metallic coating. A two-phase system is defined as a metal alloy comprising two primary components. Surprisingly, the inventors have found that the tin-zinc coating provides a protective coating with a higher corrosion resistance as compared to a tin coating primarily made up of tin. The amount of zinc within the metallic coating is maintained so as not to exceed 85% so that the metallic coating remains relatively pliable for use in a press-fit roofing system.
The inventors have discovered that the use of large weight percentages of zinc in the tin-zinc alloy does not cause the coating to be too rigid or brittle thus preventing the coated material to be formed or bent which results in a cracked coating. In Application Serial No. 042,649, the inventors, when first developing the novel tin-zinc coating, believed that zinc weight percentages above 30 weight percent would make the coating rigid and brittle which would result in the cracking of the tin-zinc coating when the coated material was bent or formed. Shortly after the filing of Application Serial No. 042,649, extensive experimentation was performed on tin-zinc coatings having a zinc content above 50 weight percent.Surprisingly, the inventors discovered that a tin-zinc coating containing 6585 weight percent zinc and the balance tin produced an acceptably malleable metallic coating which -- resisted cracking when bent or formed. The inventors are of the belief that the unique characteristics of the two-phase metallic tin-zinc system somehow modifies the rigid characteristics of zinc to allow the tin-zinc coating to be malleable. In addition to the surprising malleability of the tin-zinc coating, the inventors discovered that the coating provides comparable corrosion resistance to tin-zinc coatings containing larger amounts of tin. Finally, the inventors discovered that the tin-zinc coating containing 65-85 weight percent zinc produced a colored coating which closely matched the gray, earth tone color of weathered terne.Besides terne coatings providing corrosion resistance, terne weathers over time and changes color to a gray, earth tone color. This color has become very popular with consumers; however, the color has been almost impossible until now to match unless the material was painted. The inventors have discovered that the high zinc tin-zinc coating changes to a color which very closely resembles the popular grey, earth tone color. The tin-zinc system of Application Serial No. 042,649 does change to a grey color; however, the grey shade is much different from the popular grey, earth tone which is associated with terne coatings.
The tin-zinc metallic coating may also contain small amounts of other metallic components which can be used to slightly modify the physical properties of the metallic coating. The metallic coating may contain bismuth and antimony to increase the strength of the metallic coating and also to inhibit the crystallization of the tin at lower temperatures. The amount of bismuth in the metallic coating may range between 0-1.7 weight percent and the amount of antimony may range between 0-7.5 weight percent of the coating. Preferably, antimony and/or bismuth are added to the metallic coating in an amount between 0.01- - 0.5 weight percent of the coating. This weight percentage amount is sufficient to prevent the tin from crystallizing at low temperatures which may result in the metallic coating flaking off the metallic roofing materials. It is believed that the high levels of zinc also help stabilize the tin within the coating. Antimony and/or bismuth in weight percentages greater than 0.5% are primarily added to harden and/or strengthen the metallic coating. Small amounts of other metals, such as iron or copper, may be added to the metallic coating to strengthen and/or increase the pliability of the metallic coating. These other types of metals typically constitute very small weight percentages within the metallic coating and generally do not exceed more than 2% of the metallic coating and preferably are less than 1% of the metallic coating.
The tin-zinc coating quickly forms a grey, earth tone color which closely resembles the color associated with weathered terne coatings. The grey surface is much less reflective than that of coatings of tin and/or non-weathered terne. The reduced reflective surface of the tin-zinc coating is important in that the coated building materials can be immediately used on facilities that require materials not to be highly reflective. Prior coatings such as tin and/or terne had to be weathered and/or additionally treated before such coated building materials could be used on facilities which prohibit the use of highly-reflective materials.
The tin-zinc coating can be applied to many types of metals. The two most popular metals are carbon steel and stainless steel. These two metals are preferably pretreated before coating to clean the material surface and remove oxides from the surface so that a strong bond is formed between the material and the tin-zinc coating.
Stainless steel is a metal alloy containing iron and chromium. Stainless steel may also include nickel which can be impregnated within the stainless steel and/or flashed on the stainless steel surface, usually by electroplating.
Carbon steel and other types of metals used as architectural material usually do not contain nickel. The inventors have discovered that if the architectural material is plated with a thin nickel layer prior to coating the material which the tin-zinc coating, the material exhibits improved corrosion resistance in acidic environments. If a nickel layer is to be applied, the nickel layer is preferably plated to the metallic building material by an electrolysis process. The thickness of the layer is maintained such that it preferably is not more than 3 microns (0.0003 in.) thick and preferably has a thickness which ranges between 1-3 microns. The bond between the tin-zinc coating and the nickel layer is surprisingly strong and durable and thereby inhibits the tin-zinc coating from flaking especially when the building materials are preformed or formed during installation.The plating of the building materials with the nickel layer is very desirable when the building materials are used in an environment which has high concentrations of fluorine, chlorine and other halogens. Although the tin-zinc coating significantly reduces the corrosive effects of halogens on the metallic building materials, the inventors have found that by placing a thin layer of plated nickel between the metallic building material and the tin-zinc coating, the corrosive effects of the halogens are even further reduced.
Examples of the tin-zinc, two-phase metallic coating which have exhibited the desired characteristics as mentioned above are set forth as follows:
Alloy
Ingredients A B C
Tin 15 20 30
Antimony < 7.5 < 7.5 < 7.5
Bismuth < 1.7 < 1.7 < 1.7
Iron < 0.1 < 0.1 < 0.1
Copper < 2.0 < 2.0 < 2.0
Lead < 0.05 < 0.05 - < 0.05 Zinc Bal. Bal. Bal.
Generally, the formulations of the tin-zinc metallic coating include in weight percentage amounts; 65-85% zinc, 0-0.5% antimony, 0-0.58 bismuth, 15-35t tin and less than 0.01 lead.
The thickness of the tin-zinc coating may be varied depending upon the environment in which the architectural materials are to be used. The tin-zinc coating exhibits superior corrosive-resistant properties as compared to tin coatings. The metallic coating may be applied in a thickness between 0.001-0.05 in. Preferably, the coating thickness is applied by a hot-dip process and ranges between 0.001-0.002 in. Such a coating thickness has been found to be adequate to prevent and/or significantly reduce the corrosion of the metallic architectural materials in virtually all types of environments. Coatings having thicknesses greater than 0.002 can be used in harsh environments to provide added corrosion protection.
The tin-zinc coating can be welded with standard lead solders and no-lead solders. Preferably, no-lead solders are used to avoid concerns associated with the use of lead.
The invention has been described with reference to the preferred and alternate embodiments. Modifications and alterations will become apparent to those skilled in the art upon the reading and understanding of the details discussed in the detailed discussion of the invention provided for herein. This invention is intended to include all such modifications and alterations insofar as they come within the scope of the present invention.
Claims (16)
1. Coated metal comprising a metal substrate coated with a low
reflecting, highly corrosion-resistant, two-phase tin-zinc
metallic coating, said coating comprising at least 15
weight percent tin and at least 7 weight percent zinc.
2. Coated metal according toz claim 1, wherein said zinc
constitutes at least 65 weight percent of said coating.
3. Coated metal according to claim 1 or 2, wherein said tin
constitutes 15-35 weight percent of said coating.
4. Coated metal according to any of claims 1 to 3, wherein
said coating comprises
Tin 15.0 - 35. 0%
Zinc 65.0 - 85. 0%
Bismuth 0.0 - 1. 7%
Antimony 0.0 - 7. 5%
Iron 0.0 - 0. 1%
Lead 0.0 - 0.05%
5. Coated metal according to any of claims 1 to 6, wherein
said metallic coating includes at least 0.01 weight percent
metallic stabilizer.
6. Coated metal according to any of claims 1 to 5, wherein
said lead is less than 0.01 weight percent of said coating.
7. Coated metal according to any of claims 1 to 6, wherein
said metal substrate comprises carbon steel, stainless
steel or copper.
8. Coated metal according to any of claims 1 to 7, wherein
said coating has a thickness of 0.001 to 0.05 inch.
9. Coated metal according to any of claims 1 to 8, wherein the
surface of said metal material is plated with a thin nickel
layer prior to applying said two-phase metallic coating.
10. Coated metal according to claim 11, wherein said nickel
layer thickness does not exceed three microns.
11. Coated metal according to claim 11 or 12, wherein said
nickel layer is electroplated onto said steel sheet.
12. A method of producing a corrosion-resistant coated sheet
material, which comprises passing a sheet of metal through
a molten bath of metal comprising less than 0.01% lead, at
least 7% zinc, and at least 15% tin until at least 0.01 to
0.05 inch of coating is on said strip.
13. A method according to claim 12, wherein said tin
constitutes 15 to 35 weight percent of said coating and
said zinc constitutes 65 to 85 weight percent of said
coating.
14. A method according to claim 13, wherein said tin
constitutes 70 to 93 weight percent of said coating and
said zinc constitutes 7 to 30 weight percent of said
coating.
15. A method according to any of claims 12 to 14, including an
initial step of applying a thin barrier of nickel onto said
metal sheet prior to passing said metal sheet through said
molten bath.
16. A method of producing a coloured architectural material
comprising the steps of coating the surface of a metal
architectural material with a tin-zinc metallic coating
comprising at least 7% zinc and at least 15% tin; and
oxidising the surface of said tin-zinc metallic coating.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US4264993A | 1993-04-05 | 1993-04-05 | |
| US08/175,523 US5401586A (en) | 1993-04-05 | 1993-12-30 | Architectural material coating |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB9405510D0 GB9405510D0 (en) | 1994-05-04 |
| GB2276887A true GB2276887A (en) | 1994-10-12 |
| GB2276887B GB2276887B (en) | 1997-12-10 |
Family
ID=26719484
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB9405510A Expired - Fee Related GB2276887B (en) | 1993-04-05 | 1994-03-21 | Coated metal |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2276887B (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2284618A (en) * | 1993-12-10 | 1995-06-14 | Berkman Louis Co | Steel having a corrosion resistant intermetallic surface layer |
| US5455122A (en) * | 1993-04-05 | 1995-10-03 | The Louis Berkman Company | Environmental gasoline tank |
| US5470667A (en) * | 1993-04-05 | 1995-11-28 | The Louis Berkman Company | Coated metal strip |
| FR2721327A1 (en) * | 1994-06-15 | 1995-12-22 | Berkman Cy Louis | Lead-free, tin@-zinc@ alloy coating for metallic architectural materials |
| US5480731A (en) * | 1992-03-27 | 1996-01-02 | The Louis Berkman Company | Hot dip terne coated roofing material |
| US5489490A (en) * | 1993-04-05 | 1996-02-06 | The Louis Berkman Company | Coated metal strip |
| US5491036A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated strip |
| US5491035A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated metal strip |
| US5597656A (en) * | 1993-04-05 | 1997-01-28 | The Louis Berkman Company | Coated metal strip |
| GB2289691B (en) * | 1994-03-14 | 1999-09-29 | Berkman Louis Co | Coated metal |
| GB2337057A (en) * | 1993-12-10 | 1999-11-10 | Berkman Louis Co | Coated Substrate |
| GB2360231A (en) * | 2000-03-15 | 2001-09-19 | Marley Alutec Ltd | Guttering |
| EP1477582A2 (en) * | 1995-03-28 | 2004-11-17 | Nippon Steel Corporation | Rust-proofing steel sheet for fuel tanks and production method thereof |
| EP1734144A2 (en) * | 2005-06-15 | 2006-12-20 | Heinz Lutta | Hot dip galvanisation of iron or steel parts |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6794060B2 (en) | 1992-03-27 | 2004-09-21 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| US6080497A (en) | 1992-03-27 | 2000-06-27 | The Louis Berkman Company | Corrosion-resistant coated copper metal and method for making the same |
| US6652990B2 (en) | 1992-03-27 | 2003-11-25 | The Louis Berkman Company | Corrosion-resistant coated metal and method for making the same |
| EP3872231A1 (en) * | 2020-02-28 | 2021-09-01 | voestalpine Stahl GmbH | Method for conditioning the surface of a metal strip coated with a zinc alloy corrosion protection layer |
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| US3962501A (en) * | 1972-12-15 | 1976-06-08 | Nippon Steel Corporation | Method for coating of corrosion-resistant molten alloy |
| US3966564A (en) * | 1974-01-07 | 1976-06-29 | Whyco Chromium Company Inc. | Method of electrodepositing an alloy of tin, cobalt and a third metal and electrolyte therefor |
| US4049481A (en) * | 1975-12-17 | 1977-09-20 | Mitsui-Anaconda Electro Copper Sheet Co. Ltd. | Surface treatment method of copperfoil |
| GB1517454A (en) * | 1975-04-02 | 1978-07-12 | Garphytte Bruk Ab | Hot dipping process for the preparation of rope and spring wire of carbon steel with corrosion resistance |
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| US4814049A (en) * | 1983-06-24 | 1989-03-21 | Tektronic, Inc. | Plating bath composition for copper-tin-zinc alloy |
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| GB1040916A (en) * | 1964-08-14 | 1966-09-01 | Richard Thomas & Baldwins Ltd | Treatment of galvanized sheets |
| DE1627741C3 (en) * | 1966-09-30 | 1974-06-20 | Nippon Steel Corp., Tokio | Solid lubricant layer applied to sheet steel to be formed and process for their manufacture |
| US4202921A (en) * | 1976-02-24 | 1980-05-13 | Aktiebolaget Garphytte Bruk | Process for the preparation of rope and spring wire of carbon steel with an improved corrosion resistance |
| CA1129804A (en) * | 1977-11-11 | 1982-08-17 | Masayoshi Usui | Anticorrosive overlap-coated iron or steel material |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1008316A (en) * | 1962-06-06 | 1965-10-27 | Budavox Budapesti Hiradastechn | Pretinning of aluminium or aluminium alloys |
| US3962501A (en) * | 1972-12-15 | 1976-06-08 | Nippon Steel Corporation | Method for coating of corrosion-resistant molten alloy |
| US3966564A (en) * | 1974-01-07 | 1976-06-29 | Whyco Chromium Company Inc. | Method of electrodepositing an alloy of tin, cobalt and a third metal and electrolyte therefor |
| GB1517454A (en) * | 1975-04-02 | 1978-07-12 | Garphytte Bruk Ab | Hot dipping process for the preparation of rope and spring wire of carbon steel with corrosion resistance |
| US4049481A (en) * | 1975-12-17 | 1977-09-20 | Mitsui-Anaconda Electro Copper Sheet Co. Ltd. | Surface treatment method of copperfoil |
| US4184928A (en) * | 1977-09-15 | 1980-01-22 | HH-Produkter, Magnusson & Co. | Method of preparing a steel surface for painting or enamelling |
| US4814049A (en) * | 1983-06-24 | 1989-03-21 | Tektronic, Inc. | Plating bath composition for copper-tin-zinc alloy |
Cited By (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5491036A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated strip |
| US5667849A (en) | 1992-03-27 | 1997-09-16 | The Louis Berkman Company | Method for coating a metal strip |
| US5616424A (en) | 1992-03-27 | 1997-04-01 | The Louis Berkman Company | Corrosion-resistant coated metal strip |
| US5520964A (en) * | 1992-03-27 | 1996-05-28 | The Louis Berkman Company | Method of coating a metal strip |
| US5480731A (en) * | 1992-03-27 | 1996-01-02 | The Louis Berkman Company | Hot dip terne coated roofing material |
| US5491035A (en) * | 1992-03-27 | 1996-02-13 | The Louis Berkman Company | Coated metal strip |
| US5597656A (en) * | 1993-04-05 | 1997-01-28 | The Louis Berkman Company | Coated metal strip |
| US5455122A (en) * | 1993-04-05 | 1995-10-03 | The Louis Berkman Company | Environmental gasoline tank |
| US5492772A (en) * | 1993-04-05 | 1996-02-20 | The Louis Berkman Company | Building material coating |
| US5489490A (en) * | 1993-04-05 | 1996-02-06 | The Louis Berkman Company | Coated metal strip |
| US5695822A (en) | 1993-04-05 | 1997-12-09 | The Louis Berkman Company | Method for coating a metal strip |
| US5470667A (en) * | 1993-04-05 | 1995-11-28 | The Louis Berkman Company | Coated metal strip |
| GB2337057A (en) * | 1993-12-10 | 1999-11-10 | Berkman Louis Co | Coated Substrate |
| GB2284618A (en) * | 1993-12-10 | 1995-06-14 | Berkman Louis Co | Steel having a corrosion resistant intermetallic surface layer |
| GB2337057B (en) * | 1993-12-10 | 1999-12-15 | Berkman Louis Co | Coated substrate |
| GB2284618B (en) * | 1993-12-10 | 1999-12-15 | Berkman Louis Co | Coated substrate |
| GB2289691B (en) * | 1994-03-14 | 1999-09-29 | Berkman Louis Co | Coated metal |
| FR2721327A1 (en) * | 1994-06-15 | 1995-12-22 | Berkman Cy Louis | Lead-free, tin@-zinc@ alloy coating for metallic architectural materials |
| EP1477582A2 (en) * | 1995-03-28 | 2004-11-17 | Nippon Steel Corporation | Rust-proofing steel sheet for fuel tanks and production method thereof |
| EP1477582A3 (en) * | 1995-03-28 | 2005-05-18 | Nippon Steel Corporation | Rust-proofing steel sheet for fuel tanks and production method thereof |
| GB2360231A (en) * | 2000-03-15 | 2001-09-19 | Marley Alutec Ltd | Guttering |
| EP1734144A2 (en) * | 2005-06-15 | 2006-12-20 | Heinz Lutta | Hot dip galvanisation of iron or steel parts |
| EP1734144A3 (en) * | 2005-06-15 | 2007-01-03 | Heinz Lutta | Hot dip galvanisation of iron or steel parts |
Also Published As
| Publication number | Publication date |
|---|---|
| GB9405510D0 (en) | 1994-05-04 |
| GB2276887B (en) | 1997-12-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20130321 |