US3865560A - Process for manufacturing decorative products of aluminum and alloys of aluminum - Google Patents

Process for manufacturing decorative products of aluminum and alloys of aluminum Download PDF

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Publication number
US3865560A
US3865560A US028061A US2806170A US3865560A US 3865560 A US3865560 A US 3865560A US 028061 A US028061 A US 028061A US 2806170 A US2806170 A US 2806170A US 3865560 A US3865560 A US 3865560A
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US
United States
Prior art keywords
aluminum
composite sheet
sheet
thickness
alloy
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
US028061A
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English (en)
Inventor
Leon Sabetay
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.)
Cegedur GP
Original Assignee
Cegedur GP
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
Application filed by Cegedur GP filed Critical Cegedur GP
Application granted granted Critical
Publication of US3865560A publication Critical patent/US3865560A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • B23K20/227Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded with ferrous layer
    • B23K20/2275Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded with ferrous layer the other layer being aluminium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/01Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/016Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of aluminium or aluminium alloys
    • 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
    • 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
    • Y10T428/12764Next to Al-base component

Definitions

  • This invention relates to the manufacture of decorative products of aluminum and alloys of aluminum.
  • tint of the oxide layer of an anodized aluminum or alloy of aluminum depends somewhat on the chemical composition of the metal at the surface.
  • This property has been used in the manufacture of decorative products having an oxide layer of various colors by anodizing the parts in which the chemical composition at the surface varies locally, depending somewhat upon the design.
  • the welding seams appear as different colors from that of the sheet.
  • a sheet of aluminum alloy is plated with a layer of another alloy of aluminum. Thereafter, the external layer is locally heated in order to cause diffusion of the two alloys into one another with the formation of zones having different chemical compositions which develop different colors upon anodization.
  • the colors of the final outside layer, as well as other properties of the sheet, such as mechanical resistance, stability for stamping, etc. depend primarily on the chemical composition of the composite, this may result in conflict between the desired colors and the desired properties of the final product.
  • lt is an object of this invention to produce and to provide a method for producing composite sheets having surface designs of local chemical heterogeneities whereby the inconveniences heretofore described can be overcome for producing colors which differ in the surface of the metal.
  • a composite sheet known as a covering sheet, which is relatively thin and has on the surface zones of various chemical compositions corresponding to the tints desired in the final oxide layer.
  • the sheet is joined, as by welding or by hot rolling, with the heterogeneous phase outermost onto a relatively thick plate, hereinafter referred to as the support plate, the chemical composition of the support plate corresponding to the mechanical or physical properties desired for the final product and in which the ratio of thickness between the support and the cover sheet is at least equal to 5.
  • the assembly comprising the support plate and cover sheet joined one to the other, is then rolled to the desired final thickness, which should be at most equal to H15 and preferably in the range of l/30 to H500 of the initial thickness.
  • an elongate strip formed of the composite sheet which has designs on the surface in the form of elongated veins, of which the chemical compositions can vary progressively from one vein to the other and which are capable of producing, by anodization, a decorative design with tint variations in which the overall appearance is reproduced throughout the length of the strip.
  • the mechanical properties of the composite will correspond to those of a simple sheet formed solely of the support plate.
  • the composite sheet can, for example, be subjected to a mechani cal forming treatment and/or to a heat treatment which may be adapted to impart high mechanical characteristics.
  • the cover sheet is selected to have a thickness within the range of a few millimeters to several tens of millimeters, such as up to millimeters, before application while the support has a thickness which may be within the range of 6 to 20 times the thickness of the cover sheet.
  • cover sheet For manufacturing the cover sheet, use is made of a sheet having a thickness of 20 millimeters, a length of 3 meters and a width of 1.5 meters, formed of an A-Ml alloy containing approximately 1.2 percent by weight manganese and 98.8 percent by weight of aluminum with the usual impurities.
  • A-Ml alloy containing approximately 1.2 percent by weight manganese and 98.8 percent by weight of aluminum with the usual impurities.
  • One face of the sheet is plated beforehand with a layer having a thickness of 2 millimeters of A-Sl2 alloy containing about 12 percent by weight silicon and 88 percent by weight aluminum, plus impurities.
  • the surface layer of A-Sl2 alloy and the underlying layer of A-Ml alloy are locally melted in accordance with a design in the form of zig-zag lines, as by the use of a torch or an arc welding head of the known TlG type.
  • the two alloys A-Sl2 and A-Ml become partially intermixed in a more or less regular manner.
  • the two alloys A-Sl2 and A-Ml mutually diffuse in the solid state one into another.
  • This cover sheet is then plated by hot rolling onto a support having a thickness of 200 millimeters, a length of 3 meters and a width of 1.5 meters.
  • the support consists of A-MIG alloy containing about 1.3 percent by weight manganese, 1.1 percent by weight magnesium and 97.6 percent by weight aluminum plus impurities.
  • the cover sheet is positioned with the surface of A-S l 2 facing outwardly.
  • the assembly comprising the support and cover sheet is rolled to a thickness of about 4 millimeters.
  • the original motif of heterogeneities in the cover sheet will be extended more than 50-fold.
  • the composite strip having a thickness of 4 millimeters, is subjected to surface pickling to a depth of about 2/l00 millimeters, followed by anodization in an aqueous sulphuric acid solution, in accordance with known procedures.
  • the anodized strip has a deep grey surface decorated with more or less elongated light veins, suggesting the appearance of the surface of certain natural rocks.
  • the composite product of this invention can he employed in such fields as architecture, furniture, household articles, automobile bodies and various articles for decorative and/or structural purposes.
  • a process for manufacturing composite sheets including a face sheet of aluminum or an alloy of aluminum having on the surface local chemical heterogeneities capable of causing variation in tint in response to anodization comprising positioning a relatively thin composite sheet having local surface heterogeneities of a composition corresponding to the tints desired for the final anodized oxide layer to cover the entire surface of a relatively thick support plate consisting of a metal having the mechanical and/or physical properties desired for the final product, the ratio between the thickness of the support and the composite sheet being at least equal to 5, rolling the composite sheet and support for reduction in combined thickness by an amount at least equal to l/l5 of the initial thickness.
  • a decorative product obtained by anodizing the composite sheet ma nufactufed the process of claim 1.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Metal Rolling (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
US028061A 1969-04-16 1970-04-13 Process for manufacturing decorative products of aluminum and alloys of aluminum Expired - Lifetime US3865560A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR6911760A FR2040876A5 (no) 1969-04-16 1969-04-16

Publications (1)

Publication Number Publication Date
US3865560A true US3865560A (en) 1975-02-11

Family

ID=9032481

Family Applications (1)

Application Number Title Priority Date Filing Date
US028061A Expired - Lifetime US3865560A (en) 1969-04-16 1970-04-13 Process for manufacturing decorative products of aluminum and alloys of aluminum

Country Status (10)

Country Link
US (1) US3865560A (no)
AT (1) AT298952B (no)
BE (1) BE748975A (no)
CA (1) CA948359A (no)
CH (1) CH513990A (no)
ES (1) ES378612A1 (no)
FR (1) FR2040876A5 (no)
GB (1) GB1311970A (no)
NL (1) NL7005389A (no)
NO (1) NO126781B (no)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2823767A1 (fr) * 2001-04-24 2002-10-25 Pechiney Rhenalu Blocs metalliques de forte epaisseur destines a l'usinage
US20060013986A1 (en) * 2001-10-02 2006-01-19 Dolan Shawn E Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to organic or inorganic coating
US20090098373A1 (en) * 2001-10-02 2009-04-16 Henkelstrasse 67 Anodized coating over aluminum and aluminum alloy coated substrates and coated articles
US20090258242A1 (en) * 2001-10-02 2009-10-15 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to polytetrafluoroethylene or silicone coating
US20100000870A1 (en) * 2001-10-02 2010-01-07 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating aluminum and/or titanium with ceramic oxides
WO2012076467A3 (en) * 2010-12-06 2013-07-18 Bang & Olufsen A/S A method to obtain a radiation scattering surface finish on an object
WO2013113867A1 (en) * 2012-02-01 2013-08-08 Bang & Olufsen A/S A method for manufacturing a multilayer structure of different metals and alloys
US9701177B2 (en) 2009-04-02 2017-07-11 Henkel Ag & Co. Kgaa Ceramic coated automotive heat exchanger components

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941282A (en) * 1955-01-21 1960-06-21 Howard A Fromson Decorative aluminum product
US3076706A (en) * 1958-10-21 1963-02-05 Reynolds Metals Co Method of forming wrought aluminous metal
US3290145A (en) * 1962-03-09 1966-12-06 Reynolds Metals Co Method of producing multitextural flat stock
US3400057A (en) * 1964-06-03 1968-09-03 Reynolds Metals Co Alloy and finishing system
US3475167A (en) * 1965-11-04 1969-10-28 Kaiser Aluminium Chem Corp Aluminum alloy for color anodizing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941282A (en) * 1955-01-21 1960-06-21 Howard A Fromson Decorative aluminum product
US3076706A (en) * 1958-10-21 1963-02-05 Reynolds Metals Co Method of forming wrought aluminous metal
US3290145A (en) * 1962-03-09 1966-12-06 Reynolds Metals Co Method of producing multitextural flat stock
US3400057A (en) * 1964-06-03 1968-09-03 Reynolds Metals Co Alloy and finishing system
US3475167A (en) * 1965-11-04 1969-10-28 Kaiser Aluminium Chem Corp Aluminum alloy for color anodizing

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2823767A1 (fr) * 2001-04-24 2002-10-25 Pechiney Rhenalu Blocs metalliques de forte epaisseur destines a l'usinage
WO2002085615A1 (en) * 2001-04-24 2002-10-31 Pechiney Rhenalu Metal blocks suitable for machining applications
US6777106B2 (en) 2001-04-24 2004-08-17 Pechiney Rhenalu Metal blocks suitable for machining applications
US20100000870A1 (en) * 2001-10-02 2010-01-07 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating aluminum and/or titanium with ceramic oxides
US20090098373A1 (en) * 2001-10-02 2009-04-16 Henkelstrasse 67 Anodized coating over aluminum and aluminum alloy coated substrates and coated articles
US20090258242A1 (en) * 2001-10-02 2009-10-15 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to polytetrafluoroethylene or silicone coating
US20060013986A1 (en) * 2001-10-02 2006-01-19 Dolan Shawn E Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to organic or inorganic coating
US7820300B2 (en) 2001-10-02 2010-10-26 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to organic or inorganic coating
US8361630B2 (en) 2001-10-02 2013-01-29 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating an aluminum substrate with ceramic oxides prior to polytetrafluoroethylene or silicone coating
US8663807B2 (en) 2001-10-02 2014-03-04 Henkel Ag & Co. Kgaa Article of manufacture and process for anodically coating aluminum and/or titanium with ceramic oxides
US9023481B2 (en) * 2001-10-02 2015-05-05 Henkel Ag & Co. Kgaa Anodized coating over aluminum and aluminum alloy coated substrates and coated articles
US9701177B2 (en) 2009-04-02 2017-07-11 Henkel Ag & Co. Kgaa Ceramic coated automotive heat exchanger components
WO2012076467A3 (en) * 2010-12-06 2013-07-18 Bang & Olufsen A/S A method to obtain a radiation scattering surface finish on an object
WO2013113867A1 (en) * 2012-02-01 2013-08-08 Bang & Olufsen A/S A method for manufacturing a multilayer structure of different metals and alloys

Also Published As

Publication number Publication date
DE2018026B2 (no) 1973-01-04
CA948359A (en) 1974-06-04
NL7005389A (no) 1970-10-20
CH513990A (fr) 1971-10-15
NO126781B (no) 1973-03-26
DE2018026A1 (de) 1970-10-22
FR2040876A5 (no) 1971-01-22
BE748975A (fr) 1970-10-15
ES378612A1 (es) 1973-02-01
GB1311970A (en) 1973-03-28
AT298952B (de) 1972-05-25

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