US3393089A - Method of forming improved zinc-aluminum coating on ferrous surfaces - Google Patents
Method of forming improved zinc-aluminum coating on ferrous surfaces Download PDFInfo
- Publication number
- US3393089A US3393089A US627207A US62720767A US3393089A US 3393089 A US3393089 A US 3393089A US 627207 A US627207 A US 627207A US 62720767 A US62720767 A US 62720767A US 3393089 A US3393089 A US 3393089A
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- aluminum
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- bath
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- 238000000576 coating method Methods 0.000 title description 70
- 239000011248 coating agent Substances 0.000 title description 54
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 title description 25
- 238000000034 method Methods 0.000 title description 20
- 229910000611 Zinc aluminium Inorganic materials 0.000 title description 10
- HXFVOUUOTHJFPX-UHFFFAOYSA-N alumane;zinc Chemical compound [AlH3].[Zn] HXFVOUUOTHJFPX-UHFFFAOYSA-N 0.000 title description 9
- 229910052782 aluminium Inorganic materials 0.000 description 37
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 37
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 18
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 16
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 15
- 229910052710 silicon Inorganic materials 0.000 description 15
- 239000010703 silicon Substances 0.000 description 15
- 229910052725 zinc Inorganic materials 0.000 description 15
- 239000011701 zinc Substances 0.000 description 15
- 229910052751 metal Inorganic materials 0.000 description 13
- 239000002184 metal Substances 0.000 description 13
- 229910000831 Steel Inorganic materials 0.000 description 9
- 229910052742 iron Inorganic materials 0.000 description 9
- 239000010959 steel Substances 0.000 description 9
- 238000005260 corrosion Methods 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 8
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 239000001996 bearing alloy Substances 0.000 description 5
- 238000007654 immersion Methods 0.000 description 5
- 239000000243 solution Substances 0.000 description 5
- 230000001464 adherent effect Effects 0.000 description 4
- 239000010953 base metal Substances 0.000 description 4
- 238000004140 cleaning Methods 0.000 description 4
- 150000002739 metals Chemical class 0.000 description 4
- 238000005275 alloying Methods 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000011253 protective coating Substances 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 150000003839 salts Chemical class 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 2
- 239000007864 aqueous solution Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910052793 cadmium Inorganic materials 0.000 description 2
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- XFRVVPUIAFSTFO-UHFFFAOYSA-N 1-Tridecanol Chemical compound CCCCCCCCCCCCCO XFRVVPUIAFSTFO-UHFFFAOYSA-N 0.000 description 1
- BMYNFMYTOJXKLE-UHFFFAOYSA-N 3-azaniumyl-2-hydroxypropanoate Chemical compound NCC(O)C(O)=O BMYNFMYTOJXKLE-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000906 Bronze Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 description 1
- 229910001327 Rimmed steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- VQLYBLABXAHUDN-UHFFFAOYSA-N bis(4-fluorophenyl)-methyl-(1,2,4-triazol-1-ylmethyl)silane;methyl n-(1h-benzimidazol-2-yl)carbamate Chemical compound C1=CC=C2NC(NC(=O)OC)=NC2=C1.C=1C=C(F)C=CC=1[Si](C=1C=CC(F)=CC=1)(C)CN1C=NC=N1 VQLYBLABXAHUDN-UHFFFAOYSA-N 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000005246 galvanizing Methods 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 229910052708 sodium Inorganic materials 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 238000004381 surface treatment Methods 0.000 description 1
- 229910000648 terne Inorganic materials 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 229940087291 tridecyl alcohol Drugs 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
-
- 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
-
- 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
- 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
- C23C2/34—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the shape of the material to be treated
- C23C2/36—Elongated material
- C23C2/38—Wires; Tubes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
Definitions
- ABSTRACT OF THE DISCLOSURE A method of coating steel sheet or strip in which the base metal is passed through a molten metal bath consisting of 25% to 70% aluminum, silicon in an amount not less than 0.5% of the aluminum content, balance zinc.
- This invention relates to zinc-aluminum coatings on ferrous surfaces, and more particularly to zinc-aluminum protective coatings on steel surfaces which coatings are ductile, corrosion resistant and tightly adherent to said surfaces.
- metals have been used in the past as a protective coating for ferrous surfaces, such metals including tin, zinc, terne metal, nickel, chromium, cadmium, copper, aluminum, bronze and lead.
- One of the most commonly used coating metals is zinc, partly because of its relatively low cost, and partly because of its higher position in the electromotive series relative to iron.
- zinc coatings do not have adequate resistance to corrosion. The search for metallic coatings which will combine high protective power, ductility, adherence, good appearance and low cost is a continuing one.
- Another object of this invention is to provide metallic coatings on ferrous base stock, which coatings are metallurgically bonded to the base stock.
- Another object of this invention is to provide a ferrous base which has a metallic coating thereon and in which the iron-bearing alloy layer at the interface between coating and base metal is thin and uniform.
- a further object is to provide a ferrous base having a metallic coating thereon characterized by good appearance and formability.
- An additional object is to provide a ferrous base with -a metallic coating which is ductible and firmly adherent.
- Another object is to provide a method for producing said coated product.
- Our product is characterized by the fact that the ironbearing alloy layer at the interface of the ferrous base and the coating is thin and uniform.
- the method by which our new product is obtained broadly comprises applying to a ferrous base, such as strip, the surface of which is substantially free from oxides and other contaminants, a coating consisting essentially of 25% to 70% aluminum, balance zinc, the coating being applied in such a manner as to result in a thin and uniform iron-bearing alloy layer at the interface between the base and the coating.
- a ferrous base such as strip
- a coating consisting essentially of 25% to 70% aluminum, balance zinc
- the bath in which this coating is applied should contain a small amount of silicon, for the reasons hereinafter set forth.
- This invention has particular applicability for the coating of steel strip and wire.
- Heavy alloying at the interface of steel strip and a non-ferrous protective coating metal promotes cracks in the coating upon subsequent deformation of the coated product.
- heavy alloying of coating metal with iron of the strip results in a large proportionate loss of base metal, thus weakening the base metal itself. Then too, heavy alloying at the interface at times results in an uneven coating, the surface appearance of which leaves much to be desired.
- the drawing is a diagrammatic side elevation of a preferred embodiment of apparatus for producing the product of this invention.
- a preferred method of coating a ferrous base is as follows.
- the strip is first passed through a cleaning solution which removes grease and dirt from the surface thereof.
- the cleaned strip is then introduced into a furnace and heated to a temperature approximately that of the coating bath.
- the strip is then passed through a protective atmosphere directly into a bath of molten metal consisting essentially of 25% to 70% aluminum, balance zinc.
- the temperature of the bath is maintained slightly above the melting point of the metal, the exact temperature depending, of course, upon the relative amounts of aluminum and zinc in the bath.
- Strip speeds and bath immersion times are similar to those used in continuous galvanizing.
- the cleaning solution was maintained at a temperature of approximately 200 F.
- the cleaned strip was scrubbed at scrubbers 5, and rinsed in tank 6 with water rinse 7. From the rinse tank 6, the strip was led through rubber squeegee rolls 8, over rolls 9 and downwardly through a furnace 10, where the strip was heated to a temperature of approximately l200 F.
- the furnace was heated by the products of combustion of natural gas and air in the ratio of 1 to 8. From the furnace, the strip was led around positioning roll 11, through a holding chamber 12 where its temperature fell to approximately 800 F. An atmosphere of 99% hydrogen was maintained in the holding chamber 12 to protect the strip from oxidation prior to its entry into the coating pot 13. After entering pot 13, the strip was passed through a molten bath 14, by
- This bath was maintained at a temperature of 1060 F.
- the strip was passed between a pair of smooth low carbon steel exit rolls 16.
- An air-blast 17 was used to chill the coating as the strip passed vertically to roll 18, and then take-up reel 19.
- the speed of the strip was approximately 45 feet per minute and the time of immersion in the coating bath was about 4 seconds.
- the total coating thickness which includes the coating on the two sides of the thus-coated strip, averaged 0.00197 inch.
- the zinc employed for the molten mixture had a specified zinc purity of better than 99.99%.
- Silicon was added to the bath in the form of an aluminum alloy. This material analyzed as follows:
- thin iron-bearing alloy layer is meant a layer at the interface having an average thickness not greater than about 0.25 mil, excluding localized projections.
- our invention in its broad aspects, is not limited to an alloy layer of this thinness, for in some applications it may be possible to tolerate a layer of greater thickness.
- uniform a layer surface which is substantially flat (for a flat substrate) but which may include localized projections into the zinc-aluminum coat-
- the operating temperature of the molten coating bath will ordinarily range from about 975 F. to 1220 F., depending on the amount of aluminum in the alloy, the temperature increasing with increasing aluminum content.
- Coatings made as above described are metallurgically bonded to the ferrous base.
- the coated products of this invention show an advantage over continuously galvanized products in the salt spray test of the order of approximately 3 to 1, up to 8 to l.
- the coated products of the invention exhibit a small spangle. This property is highly desirable in many operations, where additional surface treatment, such as the application of paint, is required. In the coating range of from about 25 to 45% aluminum content the surface of the product has an exceptionally smooth, white lustre.
- the corrosion resistance of the products of our invention within the coating range of 25% to 70% aluminum content, is far and above that which can be met with galvanized products.
- the mufiier test referred to is that known as Muffler Condensate Test.
- coated specimens 2 inches by 4 inches, are dipped into an aqueous solution of 0.05 normal sulfuric acid and 0.01 normal hydrobromic acid for 8 seconds at a solution temperature of F.
- the specimens are removed at the end of the 8 second immersion period, and suspended in the vapors of the immersion solution for the remainder of one hour.
- the procedure is repeated every hour for 20 hours, after which the specimens are heated in a laboratory furnace for 2 hours at 500 F. to complete what is referred to as a one-day cycle.
- Specimens are examined visually after each one-day cycle for start of rusting (disregarding the rusting of the sheared edges of the specimens).
- the complete test comprises -13 one-day cycles.
- the products of our invention in the entire range from 25 to 70% aluminum in the coating, meet A.S.T.M. Specification No. A93-59T for bend test requirements. Further, in the demanding flat lockseam test, the products of our invention showed no flaking at any aluminum concentration in the coating of from 25 to 45 The 70% aluminum coating showed slight localized flaking.
- the ductility and adherence of the coatings of the products of our invention, over the entire range of aluminum content (25 to 70% aluminum) are such that the said products can withstand commercial forming such as corrugating, bending, etc. without significant cracking or flakmg.
- Our improved coating may also be applied by what may be referred to as a roll-bonding procedure.
- a roll-bonding procedure As an example of this method, the surface of a low carbon steel sheet was roughened by acid etching. A thin layer of tridecyl alcohol was applied to the surface of the sheet. The sheet was then coated with a mixture comprising zinc powder (75 and aluminum powder (25% the alcohol serving to promote initial adherence of the powder to the sheet. The sheet, with the powder coating thereon, was passed through pressure rolls to compact the powder on the sheet, and was then heated at 750 F. for a period of about five minutes to bond the coating to the sheet.
- This method is described more fully in an application by Edward H. Mayer and Milton N. Rahn, which was filed as application Serial No. 382,659, July 14, 1964, now abandoned, and continuation-in-part application Serial. No. 451,328, filed April 27, 1965, now Patent No. 3,325,282.
- silicon is required in producing the product of our invention by the hot dip process.
- the presence of silicon in the bath promotes the formation of an adherent coating, suppresses the formation of an iron-bearing alloy layer at the interface between the strip and the coating, and assures that the alloy layer which is formed is thin and uniform.
- the silicon content of the bath should be not less than 0.5 and preferably about 3%, of the aluminum content. More silicon may be used if desired. Silicon will also be present in the coating. However, the silicon content of the coating does not, so far as we can determine, have any effect on the corrosion resistance of the coated product. Silicon is not essential to the roll bonding process.
- Examples of articles, other than steel strip, for which the above-described zinc-aluminum coatings would find ready application are steel wire, hardware and structural shapes.
- the coatings of the products of our invention consist essentially of the metals zinc and aluminum, other substances which do not materially detract from the novel and basic properties of our invention may be present either as impurities or as deliberate additions.
- the coating may contain up to 0.3% chromium for control of intergranular corrosion.
- a method of forming a zinc-aluminum coating on a ferrous base which comprises passing a ferrous base through a molten coating bath consisting essentially of from 25% to aluminum, and from to 30% zinc, and to which has been added a small quantity of silicon in an amount not less than 0.5% of the aluminum content.
- a method of forming a zinc-aluminum coating on a ferrous base which comprises removing oxides from the surface of the base, passing the ferrous base with its oxidefree surface through a molten coating bath consisting essentially of from 25 to 70% aluminum, and from 75 to 30% zinc, and to which has been added a small quantity of silicon in an amount not less than 0.5% of the aluminum content.
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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating With Molten Metal (AREA)
- Laminated Bodies (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Description
July 16, 1968 BORZILLO ET AL 3,393,089
METHOD OF FORMING IMPROVED ZINC-ALUMINUM COATING ON FERROUS SURFACES Original Filed July 14, 1964 IN VE N TORS Angela R. Borz/l/o James B. Horton United States Patent 3,393,089 METHOD OF FORMING IMPROVED ZINC-ALUMI- NUM COATING 0N FERROUS SURFACES Angelo R. Borzillo, Bethlehem, and James B. Horton,
Allentown, Pa., assignors to Bethlehem Steel Corporation, a corporation of Delaware Original application July 14, 1964, Ser. No. 382,595, now Patent No. 3,343,930, dated Sept. 26, 1967. Divided and this application Mar. 30, 1967, Ser No. 627,207
2 Claims. (Cl. 117-114) ABSTRACT OF THE DISCLOSURE A method of coating steel sheet or strip in which the base metal is passed through a molten metal bath consisting of 25% to 70% aluminum, silicon in an amount not less than 0.5% of the aluminum content, balance zinc.
This application is a division of application Ser. No. 382,595, filed July 14, 1964, for Non-Ferrous Metal- Coated Product and Method Therefor, now Patent No. 3,343,930.
Background of the invention This invention relates to zinc-aluminum coatings on ferrous surfaces, and more particularly to zinc-aluminum protective coatings on steel surfaces which coatings are ductile, corrosion resistant and tightly adherent to said surfaces.
In the protection of ferrous surfaces from corrosive media it is common practice to coat the ferrous metal surface with a non-ferrous metal, by immersion in a molten bath of the coating metal or by other methods. These coatings should not only be protective, but they should be ductile and tightly adherent as well, and should have a smooth, pleasing appearance.
Many metals have been used in the past as a protective coating for ferrous surfaces, such metals including tin, zinc, terne metal, nickel, chromium, cadmium, copper, aluminum, bronze and lead. One of the most commonly used coating metals is zinc, partly because of its relatively low cost, and partly because of its higher position in the electromotive series relative to iron. However, for many applications, zinc coatings do not have adequate resistance to corrosion. The search for metallic coatings which will combine high protective power, ductility, adherence, good appearance and low cost is a continuing one.
Summary of the invention Accordingly it is an object of this invention to provide a ferrous base having thereon a metallic coating which is highly corrosion-resistant.
Another object of this invention is to provide metallic coatings on ferrous base stock, which coatings are metallurgically bonded to the base stock.
Another object of this invention is to provide a ferrous base which has a metallic coating thereon and in which the iron-bearing alloy layer at the interface between coating and base metal is thin and uniform.
A further object is to provide a ferrous base having a metallic coating thereon characterized by good appearance and formability.
An additional object is to provide a ferrous base with -a metallic coating which is ductible and firmly adherent.
Another object is to provide a method for producing said coated product.
We have discovered that the foregoing objects can be attained by providing a ferrous base which has metallurgically bonded thereto a coating consisting essentially of from 25% to 70% aluminum, with the balance substantially zinc.
Our product is characterized by the fact that the ironbearing alloy layer at the interface of the ferrous base and the coating is thin and uniform.
Briefly, the method by which our new product is obtained broadly comprises applying to a ferrous base, such as strip, the surface of which is substantially free from oxides and other contaminants, a coating consisting essentially of 25% to 70% aluminum, balance zinc, the coating being applied in such a manner as to result in a thin and uniform iron-bearing alloy layer at the interface between the base and the coating. The bath in which this coating is applied should contain a small amount of silicon, for the reasons hereinafter set forth.
This invention has particular applicability for the coating of steel strip and wire. Heavy alloying at the interface of steel strip and a non-ferrous protective coating metal promotes cracks in the coating upon subsequent deformation of the coated product. In addition, with strip of thin gages, heavy alloying of coating metal with iron of the strip results in a large proportionate loss of base metal, thus weakening the base metal itself. Then too, heavy alloying at the interface at times results in an uneven coating, the surface appearance of which leaves much to be desired.
Brief description of the drawing The drawing is a diagrammatic side elevation of a preferred embodiment of apparatus for producing the product of this invention.
Detailed description The coated product of our invention and a preferred method, by which the coating may be applied to a ferrous base, will be described with reference to the drawing.
A preferred method of coating a ferrous base, e.g., steel strip, is as follows. The strip is first passed through a cleaning solution which removes grease and dirt from the surface thereof. The cleaned strip is then introduced into a furnace and heated to a temperature approximately that of the coating bath. The strip is then passed through a protective atmosphere directly into a bath of molten metal consisting essentially of 25% to 70% aluminum, balance zinc. The temperature of the bath is maintained slightly above the melting point of the metal, the exact temperature depending, of course, upon the relative amounts of aluminum and zinc in the bath.
Strip speeds and bath immersion times are similar to those used in continuous galvanizing.
Following is a specific example of our preferred method.
Referring to the drawing, a strip 1 of 28 gage rimmed steel, having a carbon content of 0.06%, a manganese content of 0.31%, and other elements customarily found in rimmed strip steel, was fed from pay-off reel 2 to cleaning tank 3 containing an aqueous solution 4 (approximately 4 oz./gal.) of Pennsalt No. 30, a standard alkaline cleaning solution for steel strip. The cleaning solution was maintained at a temperature of approximately 200 F. The cleaned strip was scrubbed at scrubbers 5, and rinsed in tank 6 with water rinse 7. From the rinse tank 6, the strip was led through rubber squeegee rolls 8, over rolls 9 and downwardly through a furnace 10, where the strip was heated to a temperature of approximately l200 F. The furnace was heated by the products of combustion of natural gas and air in the ratio of 1 to 8. From the furnace, the strip was led around positioning roll 11, through a holding chamber 12 where its temperature fell to approximately 800 F. An atmosphere of 99% hydrogen was maintained in the holding chamber 12 to protect the strip from oxidation prior to its entry into the coating pot 13. After entering pot 13, the strip was passed through a molten bath 14, by
way of sinker rolls and 15. This bath was maintained at a temperature of 1060 F. Upon leaving the bath, the strip was passed between a pair of smooth low carbon steel exit rolls 16. An air-blast 17 was used to chill the coating as the strip passed vertically to roll 18, and then take-up reel 19. The speed of the strip was approximately 45 feet per minute and the time of immersion in the coating bath was about 4 seconds. The total coating thickness, which includes the coating on the two sides of the thus-coated strip, averaged 0.00197 inch.
In preparing the molten bath, 99.50% minimum A1 grade aluminum was used. This material had the following analysis:
Percent Aluminum a- 99.65
Iron 0. l9
Silicon 0. l 3
Manganese 0.01 Zinc 0.01
Vanadium 0.01
Cadmium 0.02
Sodium 0.001
The zinc employed for the molten mixture had a specified zinc purity of better than 99.99%.
Silicon was added to the bath in the form of an aluminum alloy. This material analyzed as follows:
Percent Silicon 12.00 Iron 0.33 Aluminum Balance These ingredients were combined in such proportions that the bath analyzed approximately 35% aluminum, 64% zinc, and 1% silicon.
As the aluminum content in the coating is increased,
above 35%, there is evidence of a small amount of interfacial alloy layer. But even when the aluminum represents 70% of the alloy coating, the iron-bearing alloy at the interface is uniform and thin.
By thin iron-bearing alloy layer is meant a layer at the interface having an average thickness not greater than about 0.25 mil, excluding localized projections. However, our invention, in its broad aspects, is not limited to an alloy layer of this thinness, for in some applications it may be possible to tolerate a layer of greater thickness.
By uniform is meant a layer surface which is substantially flat (for a flat substrate) but which may include localized projections into the zinc-aluminum coat- The operating temperature of the molten coating bath will ordinarily range from about 975 F. to 1220 F., depending on the amount of aluminum in the alloy, the temperature increasing with increasing aluminum content.
Specific examples of preferred bath temperatures for varying aluminum contents are set forth in the following examples:
Approximate bath Aluminum percent temperature F.)
Coatings made as above described are metallurgically bonded to the ferrous base.
Our coated products have many favorable properties, as will be apparent from the following data based on coatings produced by the method above described.
In the entire coating range of 25% to 70% aluminum, the coated products of this invention show an advantage over continuously galvanized products in the salt spray test of the order of approximately 3 to 1, up to 8 to l.
4 The salt spray test is performed according to A.S.T.M. Method B117-62.
Typical results (average of four 4" x 6" test specimens with protected edges) for salt spray tests are set Same as (2) with 70% Al *Tests not completed.
Appearance-Wise, the coated products of the invention exhibit a small spangle. This property is highly desirable in many operations, where additional surface treatment, such as the application of paint, is required. In the coating range of from about 25 to 45% aluminum content the surface of the product has an exceptionally smooth, white lustre.
In the so-called muflier test, the corrosion resistance of the products of our invention, within the coating range of 25% to 70% aluminum content, is far and above that which can be met with galvanized products.
The mufiier test referred to is that known as Muffler Condensate Test. In the test, coated specimens, 2 inches by 4 inches, are dipped into an aqueous solution of 0.05 normal sulfuric acid and 0.01 normal hydrobromic acid for 8 seconds at a solution temperature of F. The specimens are removed at the end of the 8 second immersion period, and suspended in the vapors of the immersion solution for the remainder of one hour. The procedure is repeated every hour for 20 hours, after which the specimens are heated in a laboratory furnace for 2 hours at 500 F. to complete what is referred to as a one-day cycle. Specimens are examined visually after each one-day cycle for start of rusting (disregarding the rusting of the sheared edges of the specimens). The complete test comprises -13 one-day cycles.
*Rusting of sheared edges of specimens disregarded.
The products of our invention in the entire range from 25 to 70% aluminum in the coating, meet A.S.T.M. Specification No. A93-59T for bend test requirements. Further, in the demanding flat lockseam test, the products of our invention showed no flaking at any aluminum concentration in the coating of from 25 to 45 The 70% aluminum coating showed slight localized flaking.
Furthermore, the products of our invention having coatings in the range between 25 and 45 aluminum showed only slight cracking when bent 180 flat on themselves.
The ductility and adherence of the coatings of the products of our invention, over the entire range of aluminum content (25 to 70% aluminum) are such that the said products can withstand commercial forming such as corrugating, bending, etc. without significant cracking or flakmg.
Our improved coating may also be applied by what may be referred to as a roll-bonding procedure. As an example of this method, the surface of a low carbon steel sheet was roughened by acid etching. A thin layer of tridecyl alcohol was applied to the surface of the sheet. The sheet was then coated with a mixture comprising zinc powder (75 and aluminum powder (25% the alcohol serving to promote initial adherence of the powder to the sheet. The sheet, with the powder coating thereon, was passed through pressure rolls to compact the powder on the sheet, and was then heated at 750 F. for a period of about five minutes to bond the coating to the sheet. This method is described more fully in an application by Edward H. Mayer and Milton N. Rahn, which was filed as application Serial No. 382,659, July 14, 1964, now abandoned, and continuation-in-part application Serial. No. 451,328, filed April 27, 1965, now Patent No. 3,325,282.
As far as is presently known, silicon is required in producing the product of our invention by the hot dip process. We have found that the presence of silicon in the bath promotes the formation of an adherent coating, suppresses the formation of an iron-bearing alloy layer at the interface between the strip and the coating, and assures that the alloy layer which is formed is thin and uniform. We have further found that the silicon content of the bath should be not less than 0.5 and preferably about 3%, of the aluminum content. More silicon may be used if desired. Silicon will also be present in the coating. However, the silicon content of the coating does not, so far as we can determine, have any effect on the corrosion resistance of the coated product. Silicon is not essential to the roll bonding process.
To recapitulate, we have found that our zinc-aluminum coated ferrous products, wherein the aluminum content represents from 25% to 70% of the total coating, exhibit corrosion resistance properties superior to those of continuously galvanized products. Within this broad range, coatings having an aluminum content between 25 and 45% of the total coating are characterized by their ductility and freedom from flaking, when subjected to severe forming operations; while coatings having an aluminum content between 40% and 60% of the total coating are characterized by their remarkable corrosion resistance, which is far superior to that of galvanized coatings a1- through at some slight loss of formability at the high end of the aluminum ranges.
Examples of articles, other than steel strip, for which the above-described zinc-aluminum coatings would find ready application, are steel wire, hardware and structural shapes.
While the coatings of the products of our invention consist essentially of the metals zinc and aluminum, other substances which do not materially detract from the novel and basic properties of our invention may be present either as impurities or as deliberate additions. For example, the coating may contain up to 0.3% chromium for control of intergranular corrosion.
By the term consisting essentially of we do not wish to exclude the presence of such substances.
All percentages shown herein, which relate to bath or coating components, represent weight percent.
We claim:
1. A method of forming a zinc-aluminum coating on a ferrous base which comprises passing a ferrous base through a molten coating bath consisting essentially of from 25% to aluminum, and from to 30% zinc, and to which has been added a small quantity of silicon in an amount not less than 0.5% of the aluminum content.
2. A method of forming a zinc-aluminum coating on a ferrous base which comprises removing oxides from the surface of the base, passing the ferrous base with its oxidefree surface through a molten coating bath consisting essentially of from 25 to 70% aluminum, and from 75 to 30% zinc, and to which has been added a small quantity of silicon in an amount not less than 0.5% of the aluminum content.
References Cited UNITED STATES PATENTS 781,300 1/1905 Prescott 75178.6 2,196,034 4/1940 Schulze 75178.6 2,782,493 2/1957 Russell 29196.2 2,870,008 1/1959 Neu 75146 FOREIGN PATENTS 553,873 3/1958 Canada.
723,480 2/ 1955 Great Britain.
ALFRED L. LEAVITT, Primary Examiner.
J. R. BATTEN, JR., Assistant Examiner.
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB22715/65A GB1115673A (en) | 1964-07-14 | 1965-05-28 | Zinc-aluminum coated products and methods therefor |
| SE7130/65A SE315460B (en) | 1964-07-14 | 1965-06-01 | |
| DE19651796353 DE1796353C2 (en) | 1964-07-14 | 1965-07-09 | Ferrous metal article with a zinc-aluminum alloy coating and method for its manufacture |
| DE19651521148 DE1521148C3 (en) | 1964-07-14 | 1965-07-09 | Ferrous metal article with an aluminum-zinc alloy coating and method for its manufacture |
| LU49050D LU49050A1 (en) | 1964-07-14 | 1965-07-12 | |
| FR24793A FR1441918A (en) | 1964-07-14 | 1965-07-15 | Zinc and aluminum coatings and their application process |
| US627207A US3393089A (en) | 1964-07-14 | 1967-03-30 | Method of forming improved zinc-aluminum coating on ferrous surfaces |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US382595A US3343930A (en) | 1964-07-14 | 1964-07-14 | Ferrous metal article coated with an aluminum zinc alloy |
| US627207A US3393089A (en) | 1964-07-14 | 1967-03-30 | Method of forming improved zinc-aluminum coating on ferrous surfaces |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3393089A true US3393089A (en) | 1968-07-16 |
Family
ID=27009843
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US627207A Expired - Lifetime US3393089A (en) | 1964-07-14 | 1967-03-30 | Method of forming improved zinc-aluminum coating on ferrous surfaces |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3393089A (en) |
| GB (1) | GB1115673A (en) |
| LU (1) | LU49050A1 (en) |
| SE (1) | SE315460B (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3928657A (en) * | 1971-04-15 | 1975-12-23 | British Steel Corp | Strip shape correction on galvanising line |
| US3958994A (en) * | 1974-08-26 | 1976-05-25 | American Hoechst Corporation | Photosensitive diazo steel lithoplate structure |
| WO1981002748A1 (en) * | 1980-03-25 | 1981-10-01 | S Radtke | Zinc-aluminum alloys and coatings |
| US4358887A (en) * | 1980-04-04 | 1982-11-16 | Creps John A | Method for galvanizing and plastic coating steel |
| US4389463A (en) * | 1981-07-23 | 1983-06-21 | United Technologies Corporation | Zinc-aluminum hot dip coated ferrous article |
| US4390377A (en) * | 1981-01-12 | 1983-06-28 | Hogg James W | Novel continuous, high speed method of galvanizing and annealing a continuously travelling low carbon ferrous wire |
| US4456663A (en) * | 1981-12-02 | 1984-06-26 | United States Steel Corporation | Hot-dip aluminum-zinc coating method and product |
| US4462533A (en) * | 1982-06-24 | 1984-07-31 | Bethlehem Steel Corp. | Method of reconditioning welded joints |
| EP0037143B1 (en) * | 1980-03-25 | 1985-03-20 | CENTRE DE RECHERCHES METALLURGIQUES CENTRUM VOOR RESEARCH IN DE METALLURGIE Association sans but lucratif | Hot dip coating process |
| US4605598A (en) * | 1983-06-28 | 1986-08-12 | Fils Et Cables D'acier De Lens (Fical) | Steel wire having superposed coatings resisting corrosion |
| US4721656A (en) * | 1984-09-17 | 1988-01-26 | Eltech Systems Corporation | Electroplating aluminum alloys from organic solvent baths and articles coated therewith |
| US6468674B2 (en) | 1999-10-07 | 2002-10-22 | Bethlehem Steel Corporation | Coating composition for steel—product, a coated steel product, and a steel product coating method |
| US6610422B1 (en) | 2001-01-31 | 2003-08-26 | Nkk Corporation | Coated steel sheet and method for manufacturing the same |
| US20070119715A1 (en) * | 2005-11-25 | 2007-05-31 | Sacks Abraham J | Corrosion Resistant Wire Products and Method of Making Same |
| CN119040870A (en) * | 2024-07-12 | 2024-11-29 | 常州大学 | Preparation method and application of Al-Zn-Mg composite coating |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US781300A (en) * | 1904-02-02 | 1905-01-31 | Thomas Prescott | Manufacture of metallic alloys. |
| US2196034A (en) * | 1938-03-24 | 1940-04-02 | Gen Electric | High melting point solder |
| GB723480A (en) * | 1952-09-26 | 1955-02-09 | Reynolds Metals Co | Improvements in or relating to aluminum coating of steel |
| US2782493A (en) * | 1952-01-02 | 1957-02-26 | Kaiser Aluminium Chem Corp | Aluminum coated ferrous article |
| CA553873A (en) * | 1958-03-04 | Industrial Development Co. (Establishment) | Zinc aluminium alloy | |
| US2870008A (en) * | 1954-11-18 | 1959-01-20 | Main Alloy Company Establishme | Zinc-aluminium alloys and the method for producing same |
-
1965
- 1965-05-28 GB GB22715/65A patent/GB1115673A/en not_active Expired
- 1965-06-01 SE SE7130/65A patent/SE315460B/xx unknown
- 1965-07-12 LU LU49050D patent/LU49050A1/xx unknown
-
1967
- 1967-03-30 US US627207A patent/US3393089A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA553873A (en) * | 1958-03-04 | Industrial Development Co. (Establishment) | Zinc aluminium alloy | |
| US781300A (en) * | 1904-02-02 | 1905-01-31 | Thomas Prescott | Manufacture of metallic alloys. |
| US2196034A (en) * | 1938-03-24 | 1940-04-02 | Gen Electric | High melting point solder |
| US2782493A (en) * | 1952-01-02 | 1957-02-26 | Kaiser Aluminium Chem Corp | Aluminum coated ferrous article |
| GB723480A (en) * | 1952-09-26 | 1955-02-09 | Reynolds Metals Co | Improvements in or relating to aluminum coating of steel |
| US2870008A (en) * | 1954-11-18 | 1959-01-20 | Main Alloy Company Establishme | Zinc-aluminium alloys and the method for producing same |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3928657A (en) * | 1971-04-15 | 1975-12-23 | British Steel Corp | Strip shape correction on galvanising line |
| US3958994A (en) * | 1974-08-26 | 1976-05-25 | American Hoechst Corporation | Photosensitive diazo steel lithoplate structure |
| EP0037143B1 (en) * | 1980-03-25 | 1985-03-20 | CENTRE DE RECHERCHES METALLURGIQUES CENTRUM VOOR RESEARCH IN DE METALLURGIE Association sans but lucratif | Hot dip coating process |
| WO1981002748A1 (en) * | 1980-03-25 | 1981-10-01 | S Radtke | Zinc-aluminum alloys and coatings |
| US4358887A (en) * | 1980-04-04 | 1982-11-16 | Creps John A | Method for galvanizing and plastic coating steel |
| US4390377A (en) * | 1981-01-12 | 1983-06-28 | Hogg James W | Novel continuous, high speed method of galvanizing and annealing a continuously travelling low carbon ferrous wire |
| US4389463A (en) * | 1981-07-23 | 1983-06-21 | United Technologies Corporation | Zinc-aluminum hot dip coated ferrous article |
| US4456663A (en) * | 1981-12-02 | 1984-06-26 | United States Steel Corporation | Hot-dip aluminum-zinc coating method and product |
| US4462533A (en) * | 1982-06-24 | 1984-07-31 | Bethlehem Steel Corp. | Method of reconditioning welded joints |
| US4605598A (en) * | 1983-06-28 | 1986-08-12 | Fils Et Cables D'acier De Lens (Fical) | Steel wire having superposed coatings resisting corrosion |
| US4721656A (en) * | 1984-09-17 | 1988-01-26 | Eltech Systems Corporation | Electroplating aluminum alloys from organic solvent baths and articles coated therewith |
| US6468674B2 (en) | 1999-10-07 | 2002-10-22 | Bethlehem Steel Corporation | Coating composition for steel—product, a coated steel product, and a steel product coating method |
| US6610422B1 (en) | 2001-01-31 | 2003-08-26 | Nkk Corporation | Coated steel sheet and method for manufacturing the same |
| US20070119715A1 (en) * | 2005-11-25 | 2007-05-31 | Sacks Abraham J | Corrosion Resistant Wire Products and Method of Making Same |
| CN119040870A (en) * | 2024-07-12 | 2024-11-29 | 常州大学 | Preparation method and application of Al-Zn-Mg composite coating |
Also Published As
| Publication number | Publication date |
|---|---|
| LU49050A1 (en) | 1966-11-22 |
| DE1796353B1 (en) | 1977-04-28 |
| GB1115673A (en) | 1968-05-29 |
| DE1521148B2 (en) | 1975-09-18 |
| DE1521148A1 (en) | 1969-08-07 |
| SE315460B (en) | 1969-09-29 |
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