US3818566A - Aluminum alloy products and surface treatment - Google Patents

Aluminum alloy products and surface treatment Download PDF

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Publication number
US3818566A
US3818566A US00263767A US26376772A US3818566A US 3818566 A US3818566 A US 3818566A US 00263767 A US00263767 A US 00263767A US 26376772 A US26376772 A US 26376772A US 3818566 A US3818566 A US 3818566A
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US
United States
Prior art keywords
percent
aluminum
beige color
alloy
coating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00263767A
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English (en)
Inventor
W Anderson
E Franz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Alcoa Corp
Original Assignee
Aluminum Company of America
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR7117602A priority Critical patent/FR2091651A5/fr
Priority to DE19712124107 priority patent/DE2124107A1/de
Application filed by Aluminum Company of America filed Critical Aluminum Company of America
Priority to US00263767A priority patent/US3818566A/en
Application granted granted Critical
Publication of US3818566A publication Critical patent/US3818566A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/04Anodisation of aluminium or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/04Anodisation of aluminium or alloys based thereon
    • C25D11/06Anodisation of aluminium or alloys based thereon characterised by the electrolytes used
    • C25D11/08Anodisation of aluminium or alloys based thereon characterised by the electrolytes used containing inorganic acids
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D11/00Electrolytic coating by surface reaction, i.e. forming conversion layers
    • C25D11/02Anodisation
    • C25D11/04Anodisation of aluminium or alloys based thereon
    • C25D11/14Producing integrally coloured layers
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/923Physical dimension
    • Y10S428/924Composite
    • Y10S428/926Thickness of individual layer specified
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9265Special properties
    • Y10S428/927Decorative informative
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12583Component contains compound of adjacent metal
    • Y10T428/1259Oxide
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component

Definitions

  • This invention relates to aluminum alloy products, especially sheet products, which can develop unique color response when properly anodized. Especially unique is the ability to develop a very pleasing beige tone which is quite attractive.
  • Aluminum alloys have found wide acceptance in architectural applications because of their durability and attractiveness together with the ease with which a building can be covered, trimmed or decorated with such.
  • One popular practice contemplates employing an alloy which, upon anodic oxidation of the surface, yields a colored oxide coating. This practice offers advantages in ease of application and color durability.
  • the variety of these integral colors together with the uniformity of a given color has been limited.
  • the anodic coating should be about 0.7 mil (0.0007 inch) and often more in thickness so as to provide a sufficiently durable oxide coating.
  • ln coatings of this thickness present technology readily enables achieving rich or dark colors. For instance, shades of gold, bronze, gray and even black are achieved without great effort.
  • the delicate or subtle colors and shades are quite elusive especially in the thick architectural coatings.
  • a special alloy composition which, when properly anodized, provides an integral beige colored oxide coating which is quite delicate and exhibits an attractive metallic hue.
  • the beige color is extremely attractive when viewed in the form of a large surface such as would appear on a large building.
  • the improved material can also develop the richer bronze or black colors thus making it a multipurpose alloy which can relieve fabricators of the burden of stocking large numbers of alloy materials.
  • Another advantage of the improved material is its ease of fabrication. It can be readily rolled as a sheet product. It can also be applied as a cladding to a sheet core material. In addition, it can be extruded, forged or otherwise worked into a desired product.
  • the improved alloy consists essentially of, by weight, 0.05 to 0.15 percent Cu, 0.5 to 0.7 percent Fe, 0.15 to 0.3 percent Si, 0.3 to 0.6 percent Mn, the balance being aluminum and incidental elements and impurities.
  • a preferred composition contains 0.35 to 0.5 percent Mn.
  • the alloy may include small amounts of incidental elements such as up to 0.01 percent B and 0.05 percent Ti which may be added in casting for grain refining purposes.
  • the alloy may also contain the usual impurities associated with aluminum. Zinc is an innocuous impurity and can be present up to about 0.5 percent.
  • the alloy is especially easy to roll, extrude or otherwise shape into an article.
  • the alloy is cast as by continuous casting to provide stock for the subsequent fabrication procedures. This stock is homogenized by heating to a temperature of at least 950F for a period of time sufficient to dissolve the soluble constituents. a typical time being 24 hours. At this point the stock is hot rolled to provide a plate-like product. Some reheating may be employed if necessary or convenient. The plate is then cold rolled to produce a sheet product having moderate strength. Ease of fabrication is an attractive feature of the present invention in that rolling and other fabrication problems are minimized.
  • the material may be fabricated using essentially the same practices as those used in producing the economical strain hardening aluminum alloys known commercially as l l00 and 3003.
  • the strength of the alloy is not especially striking.
  • Cold rolled sheet typically exhibits tensile property levels of 15 to 30 ksi. While this strength level is not very high it is adequate for architectural applications such .as curtain walls for large buildings.
  • the improved alloy can be provided as a cladding on a core layer of a different alloy.
  • This practice is common in several applications where the strength or some other desirable quality of a core material can be utilized while still obtaining the advantages in appearance, corrosion protection, etc., of a given clad material.
  • the improved material can be hot roll bonded to a core material to provide a laminate plate which is then fabricated into sheet as described above.
  • a typical core material might be alloy 3003 which contains, nominally, 1.2 percent Mn, 0.12 percent Cu, with the balance aluminum and impurities.
  • Other core materials may also be employed where they offer special advantages.
  • the improved sheet or other product can be annealed, stabilized or otherwise thermally treated without impairing its color response to the subsequent anodic coating application.
  • the improved alloy is applied as a cladding on a heat treatable core the composite can be heat treated to develop the properties in the core. This, itself, is significant since many previous alloys are sensitive to thermal treatment in their color response.
  • the alloy product is next anodized to develop an integrally bonded oxide coating using acidic electrolytes of the type generally known in the anodizing art.
  • acidic electrolytes of the type generally known in the anodizing art.
  • Several sheets of the improved alloy containing about 0.] percent Cu, 0.6 percent Fe, 0.2 percent Si and 0.4 percent Mn approximately 0.08 inch in thickness have been anodically anodized in an aqueous bath containing about 15 percent sulfuric acid.
  • the bath is maintained at F and the anodizing is performed at a constant current density of 24 amperes per square foot for a period of time of about 33 minutes. This produces an oxide coating ranging from about 1.0 mil in thickness.
  • the coating exhibits an integral beige color with a metallic luster.
  • the color is to refer to the Munsell value which is a recognized system of color description which is described in ASTM Designation: Dl535-68; ASTM STANDARDS PART II 1969 p. 285.
  • the Munsell values for this beige color were approximately Y for hue, 7.05 for value and 0.90 for chroma.
  • the beige color can be varied from this level as by increasing the Mn content slightly or altering the anodizing conditions whereby the temperature is lowered and time increased to develop richer colors. Reversing these results in a move toward pale colors.
  • the beige color for the improved alloy can be varied such that typical Munsell values would range between 2Y to 8Y for hue, 6.5 to 7.2 for value and /0.65 to H2 for chroma for lighter to darker beige tones.
  • Typical coating thickness can be 1 to L2 mil and still exhibit the delicate beige color.
  • the anodizing conditions can be varied fairly widely.
  • the aqueous bath can contain 130 to 200 grams per liter H 50
  • the temperature may vary from 70 to 90F and the current density can vary from 6 to 36 amperes per square foot.
  • the time can vary from about 20 to 60 minutes and the coating from 0.7 to 1.2 mils in thickness.
  • the improved material can readily develop anodic oxide coatings exhibiting an integral beige color.
  • anodic coating it is usually desirable to seal the anodic coating in the conventional manner, for example by immersing in hot (210F) water or other suitable solutions.
  • the coloration and texture developed by the anodic treatment can be modified by treatment of the surface of the metal product prior to anodic oxidation.
  • the surface can be chemically brightened by washing with a solution of phosphoric and nitric acids or electrochemical means. Mechanical treatments such as buffing, polishing, sand blasting, and the like, can also be employed to alter the texture of the surface.
  • a method of producing a product exhibiting a beige color having a metallic luster comprising 1. providing a shaped body composed of an aluminum base alloy consisting essentially of 0.05 to 0. percent Cu, 0.5 to 0.7 percent Fe, 0.15 to 0.3 percent Si, 0.3 to 0.6 percent Mn, the balance being aluminum and incidental elements and impurities, and
  • an aluminum architectural shaped body exhibiting an integrally developed anodic oxide coating having a beige color of metallic luster the improvement wherein said shaped body is provided in an aluminum base alloy consisting essentially of 0.05 to 0.15 percent Cu, 0.5 to 0.7 percent Fe, 0.15 to 0.3 percent Si, 0.3 to 0.6 percent Mn, the balance being aluminum and incidental elements and impurities, said improvement enabling the development of an anodic oxidation coating 1.0 to 1.2 mil in thickness having an integral beige color characterized by Munsell values of 2Y to 8Y for hue, 6.5 to 7.5 for value and /0.65 to 1.2 for chroma.
  • anodic oxidation coating 1.0 to 1.2 mil in thickness having an integral beige color characterized by Munsell values of 2Y to 8Y for hue, 6.5 to 7.5 for value and /0.65 to 1.2 for chroma.
  • An architectural sheet product composed of an alloy consisting essentially of 0.05 to 0.15 percent Cu, 0.5 to 0.7 percent Fe, 0. 15 to 0.3 percent Si, 0.3 to 0.6 percent Mn, the balance being aluminum and incidental elements and impurities, said product having an integrally bonded oxide coating 10 to 1.2 mil in thickness and having an integral beige color characterized by Munsell values of 2Y to 8Y for hue, 6.5 to 7.5 for value and /0.65 to 1.2 for chroma.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Mechanical Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Laminated Bodies (AREA)
US00263767A 1970-05-14 1972-06-19 Aluminum alloy products and surface treatment Expired - Lifetime US3818566A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR7117602A FR2091651A5 (enrdf_load_stackoverflow) 1970-05-14 1971-05-14
DE19712124107 DE2124107A1 (de) 1970-05-14 1971-05-14 Herstellung gefärbter anodisierter Teile
US00263767A US3818566A (en) 1970-05-14 1972-06-19 Aluminum alloy products and surface treatment

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US3733970A 1970-05-14 1970-05-14
US00263767A US3818566A (en) 1970-05-14 1972-06-19 Aluminum alloy products and surface treatment

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US3818566A true US3818566A (en) 1974-06-25

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US (1) US3818566A (enrdf_load_stackoverflow)
DE (1) DE2124107A1 (enrdf_load_stackoverflow)
FR (1) FR2091651A5 (enrdf_load_stackoverflow)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4163665A (en) * 1978-06-19 1979-08-07 Alumax Mill Products, Inc. Aluminum alloy containing manganese and copper and products made therefrom
US4571368A (en) * 1983-01-17 1986-02-18 Atlantic Richfield Company Aluminum and zinc sacrificial alloy
DE3917188A1 (de) * 1989-05-26 1990-11-29 Happich Gmbh Gebr Verfahren zur erzeugung farbiger oberflaechen auf teilen aus aluminium oder aluminium-legierungen
US5503689A (en) * 1994-04-08 1996-04-02 Reynolds Metals Company General purpose aluminum alloy sheet composition, method of making and products therefrom
US5820015A (en) * 1996-04-02 1998-10-13 Kaiser Aluminum & Chemical Corporation Process for improving the fillet-forming capability of brazeable aluminum articles
US6350532B1 (en) * 1997-04-04 2002-02-26 Alcan International Ltd. Aluminum alloy composition and method of manufacture

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3616725A1 (de) * 1986-05-14 1987-11-19 Alusuisse Herstellung von aluminiumlegierungs-erzeugnissen mit gleichmaessig grauer lichtechter oberflaeche
EP0362127B1 (de) * 1988-09-27 1993-10-06 Alusuisse-Lonza Services Ag Kathodenfolie für Elektrolytkondensatoren

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3227639A (en) * 1961-10-24 1966-01-04 Aluminum Co Of America Method of anodizing aluminum with electrolyte containing sulfophthalic acid

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3227639A (en) * 1961-10-24 1966-01-04 Aluminum Co Of America Method of anodizing aluminum with electrolyte containing sulfophthalic acid

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Appearence Control of Architectural Anodized Finishes by Buskey et al., Kaiser Aluminum & Chemical Corp., 1968, pgs. 6 7. *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4163665A (en) * 1978-06-19 1979-08-07 Alumax Mill Products, Inc. Aluminum alloy containing manganese and copper and products made therefrom
US4571368A (en) * 1983-01-17 1986-02-18 Atlantic Richfield Company Aluminum and zinc sacrificial alloy
DE3917188A1 (de) * 1989-05-26 1990-11-29 Happich Gmbh Gebr Verfahren zur erzeugung farbiger oberflaechen auf teilen aus aluminium oder aluminium-legierungen
US5102508A (en) * 1989-05-26 1992-04-07 Gebr. Happich Gmbh Method of producing colored surfaces on parts of aluminum or aluminum alloy
US5503689A (en) * 1994-04-08 1996-04-02 Reynolds Metals Company General purpose aluminum alloy sheet composition, method of making and products therefrom
US5820015A (en) * 1996-04-02 1998-10-13 Kaiser Aluminum & Chemical Corporation Process for improving the fillet-forming capability of brazeable aluminum articles
US6350532B1 (en) * 1997-04-04 2002-02-26 Alcan International Ltd. Aluminum alloy composition and method of manufacture

Also Published As

Publication number Publication date
FR2091651A5 (enrdf_load_stackoverflow) 1972-01-14
DE2124107A1 (de) 1972-01-27

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