US2937435A - Clad metal body and method of making the same - Google Patents

Clad metal body and method of making the same Download PDF

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US2937435A
US2937435A US677224A US67722457A US2937435A US 2937435 A US2937435 A US 2937435A US 677224 A US677224 A US 677224A US 67722457 A US67722457 A US 67722457A US 2937435 A US2937435 A US 2937435A
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aluminum
high purity
sheet
clad metal
magnesium
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US677224A
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Brenner Paul
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Vereinigte Leichtmetallwerke GmbH
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22—Non-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
    • B23K20/227—Non-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
    • B23K20/2275—Non-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
    • 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
    • B32B15/012—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 aluminium or an aluminium alloy
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/922—Static electricity metal bleed-off metallic stock
    • Y10S428/923—Physical dimension
    • Y10S428/924—Composite
    • Y10S428/926—Thickness of individual layer specified
    • 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
    • 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
    • Y10T428/12764—Next to Al-base component

Definitions

  • the present invention relates to a clad metal body and method of making the same, and more particularly, the present invention relates to a clad metal body having an aluminum or aluminum-alloy face the aluminum of which is of high purity.
  • iron bodies or iron alloy bodies such as steel sheets with aluminum in order to combine the mechanical strength properties of the ironcontaining metal (the term metal throughout the present specification is to be understood as including alloys as well as elementary metals) with the high corrosion resistance of the aluminum, particularly in order to prevent rusting of the iron-containing surface. It is also desirable,
  • the present invention mainly consists in a clad metal body, comprising in combination, a base body containing iron, an outer facing sheet composed ofan anodizable, high purity aluminum-containing metal,-the aluminum of the metal having a'purity of .at least 99.9%, and an intermediate layer between'the base body and the facing sheet, the layer consisting essentially of an aluminum alloy of such composition as not to react with iron under formation of an iron aluminide when heatedto the temperatures required for hot rolling and soft annealing of the clad metal body. 7
  • the present invention contemplates a clad metal sheet body of predetermined thickness comprising, in combination, a base sheet body made of steel,,a facing sheet composed of a. substance belonging to the group consisting of highpurity aluminum having a purityof at least 99.9%,- alloys of the high purity aluminum and up to 5% magnesium, alloys of the high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of the high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium, the facing sheet having a thickness of about 10%,of the predetermined thickness, and an intermediate layer, consisting essentially of an.
  • the intermediateflayer having a thickness of between 0.05 mm. and 0.5mm. so as to prevent diffusion of iron from the base body to the facing sheet, whereby formation of iron aluminides during hot rolling and soft annealing of the clad metal sheet body is prevented due to the interposition of thealuminum-silicon alloy layer between the base sheet body'and the facing sheet.
  • the present invention also includes a method of forming a clad metalbody including a facing sheet member composed of an anodizable, high-purity aluminumcontaining metal, the aluminum of the metal having a' purity of at least 99.9%, and also including an iron-containing base body member, comprising the steps of adhering to one of the members an intermediate layer consisting ,essentially of an aluminum alloy ofsuch composition as not to react with iron under formation of an iron aluminide when heated to the temperatures'required for hot rolling and soft annealing of the cladmetal body, and adhering to the free face of the intermediate layer the other of the members, whereby a clad metal body free of iron aluminides is formed ,due to the' interposition of the intermediate layer between the. members.
  • an intermediate layer is placed between the iron-containing base body such as a steel sheet and the cladding or plating sheet which consists of high purity aluminum, i.e. of
  • the intermediate layer is composed'of an aluminum alloy which preferably contains between 0.5 and 2% silicon.
  • the aluminum of the aluminum alloy of which the intermediate layer is formed need not be of such high purity as The'high purity of the aluminum of the facing layer is required in order to achieve the desired degree of corrosion-resistant and/or gloss. This does not apply to the intermediate la'yer s'o that thealuminum of thealuminum-silicon alloy of the intermediate layer may be' commercial aluminum hav ing a plurality of for instance between 99.0 and 99.8%.
  • the minimum purity of the high purity aluminum of-the facing layer should Ive-99.9% and pref- 3. erably, the purity of the alumin-containing facing layer should be between 99.99% and 99.995%.
  • the intermediate layer is preferably composed of an aluminum alloy containing between 0.5 and 2% silicon, the balance being commercial aluminum. It is also possible to use for the intermediate layer an aluminum-silicon alloy containing more than 2% of silicon since all aluminum-silicon alloys below the eutectic composition will prevent the formation of iron aluminides at the relatively low temperature of hot rolling and soft annealing of the clad metal body. However, increasing the silicon content of the aluminum alloy of the intermediate layer beyond 2% will not further improve the ability of the intermediate layer to prevent the formation of iron aluminides, While aluminum alloys containing larger percentages of silicon show progressively decreasing rolling properties. Thus, it is preferred to limit the silicon content of the aluminum alloy of the intermediate layer to between 0.5 and 2% of silicon.
  • the intermediate layer may also contain such other alloying elements as will not interfere with the prevention of the formation of iron aluminides. For instance, the aluminum-silicon alloy of the intermediate layer may also contain manganese.
  • the thickness of the intermediate layer of aluminumsilicon alloy should be at least 0.05 mm. and will preferably be between 0.2 and 0.5 mm. Generally, increase in the thickness of the intermediate layer relative to the thickness of the iron-containing base body such as a steel sheet, will increase the difliculties of cladding by rolling. Thus, the thickness of the intermediate layer is preferably so chosen as to be just sufiicient to prevent diffusion of iron from the base body through the intermediate layer into the face layer of high purity aluminum or high purity aluminum alloys.
  • the face layer of the clad metal body according to the present invention may be composed of aluminum having a purity of'at least 99.9%, preferably of 99.99% or even higher such as 99.995%, or of aluminum alloys, the aluminum component of which has a purity of at least 99.9% or preferably a purity of 99.99%, which alloys may also contain up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium.
  • the following table contains a list of several compositions of the facing sheet of the clad metal body according to the present invention, the specific compositions however, given as illustrative only without limiting the present invention to the specific details given in the following table.
  • the thickness of the facing layer of. the clad metal body according to the present invention is preferably between 5 and 15% of the entire thickness of the clad metal sheet, in any event, the thickness of the facing layer is to be at least about 0.2 mm.
  • the clad metal body according to the present invention may for instance be produced by first plating sheet iron in conventional manner with an alloy consisting of high purity aluminum and 1% silicon, and then plating in a second st p ont t e free the aluminum-silicon alloy a sheet composed for instance of high purity alu-. minum and 1% magnesium.
  • a clad metal consisting of a layer of an aluminum-silicon alloy and of a layer consisting for instance of high purity aluminum or of an alloy of high purity aluminum and magnesium, and to plate onto the free face of the aluminum-silicon alloy layer in a second step the sheet iron or steel sheet.
  • a clad metal consisting of a layer of an aluminum-silicon alloy and of a layer consisting for instance of high purity aluminum or of an alloy of high purity aluminum and magnesium
  • the cladding of the various metal layers is performed in conventional manner preferably by hot rolling.
  • the high purity aluminum face of the clad metal body is then anodically oxidized or otherwise brightened and improved in its light reflectivity in conventional manner.
  • the sheet of high purity aluminum is first plated onto the intermediate layer of aluminum-silicon alloy, and the thus formed clad metal is then rolled onto a steel band.
  • the finished clad sheet is to have a thickness of the high purity aluminum layer of 0.3 mm., a thickness of the intermediate layer of aluminum-silicon alloy of 0.2 mm., and a thickness of the steel band of 2.5 mm.
  • the starting material is a band of high purity aluminum having a purity of 99.995% and a thickness of 30 mm., and a band of aluminum-silicon alloy containing 0.7% silicon, the balance aluminum having a purity of 99.8%.
  • the thickness of the aluminum-silicon alloy band is 10 mm.
  • Both bands are first brushed on their plating faces and then pickled in 10% sodium hydroxide at a temperature of 30 C. and for a period of 7 minutes. Thereafter, the bands are neutralized with 10% sulfuric acid at room temperature and washed with water. Then both bands are heated to 500 C.
  • the preferred hot rolling temperature for the subsequent plating is 400 0., since, however, the bands cool during the rolling process, in fact the entire rolling takes place within the temperature range of between 500 and 300 C.
  • the bands are rolled down in one pass to the extent of 40%.
  • the thus formed intermediary clad metal sheet is then further cold rolled in any desired number of passes and with any desired degree of reduction per pass.
  • the sheets maybe annealed if this becomes necessary due to cold work hardening.
  • the clad metal sheet consisting of the high purity aluminum sheet and the aluminum-silicon alloy sheet is rolled down to a thickness of 1 mm. It is essential that in case of an intermediate annealing, the reduction in thickness after the annealing has to amount to at least 40% in order to prevent coarse grain formation in the high purity aluminum layer which would make the same unsuitable for subsequent chemical brightening.
  • the thickness relationship of the high purity aluminum layer and the aluminum-silicon alloy layer thus now no longer corresponds to the relationship of the thicknesses of the original sheets since the softer high purity aluminum sheet has been deformed to a higher degree than the aluminumsilicon alloy layer.
  • the high purity aluminum layer accounts for 0.7 mm. and the aluminum-silicon alloy layer for 0.3 mm.
  • a soft annealed steel band of Thomas steel having an initial thickness of 4 mm. is now brushed on its plating face and heated to 400 C.
  • the intermediary clad metal sheet of high purity aluminum and aluminumsilicon alloy is heated to the same temperature.
  • the two bands are then superposed and rolled down in one path to the extent of 40% of their original combined tively soft aluminum-silicon layer and even more the high purity aluminum layer are considerably more reduced in thickness during this rolling operation than the steel sheet so that the three layers of the clad metal sheet now have the following thicknesses: steel layer 2.5 mm., aluminum-silicon alloy 0.2 mm., high purity aluminum facing layer 0.3 mm.
  • the thus formed clad metal sheet is soft annealed at a temperature of 560 C. since the steel layer of the composite sheet has suffered certain degree of cold hardening during the rolling at a temperature of 400 C.
  • the intermediate layer of aluminum-silicon alloy is .first rolled onto the soft annealed steel band. This is done in the same manner as described in Example 1 for the rolling of the intermediate clad metal sheet consisting of high purity aluminum and aluminum-silicon alloy onto the steel band. During subsequent rolling of the high purity aluminum layer onto the free face of the aluminum-silicon alloy layer of the intermediate clad metal sheet consisting of the steel layer and the aluminum-silicon alloy layer, a lower degree of rolling down of about 30% is chosen. Apart from the lesser percentage ofreduction in the overall thickness, the rolling of the high purity aluminum layer onto the intermediary composite sheet is carried out in the manner as described in Example 1 for the rolling of the high purity aluminum layer onto the aluminum-silicon alloy.
  • a clad metal body comprising, in combination, a base body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, alloys of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of said high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base body, said intermediate layer having a thickness of at least about 0.05 mm.
  • a clad metal body comprising, in combination, a base body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, 'alloys 'of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base body, said intermediate layer having a thickness of between 0.05 mm. and 0.5 mm.
  • a clad metal body comprising, in combination, a base body made of steel; a facing sheet composed of a. substance belonging to the group consisting of high purity aluminum having a purity of at least 99.99%, alloys of said high purity aluminum and between 0.5% and 2% magnesium, alloys of said high'purity aluminum, between 0.5% and 2% magnesium and between 4% and 6% zinc, and alloys of said high purity aluminum, between 0.5% and 2% magnesium, between 4% and 6% 'zinc and between 0.1% and 0.5% beryllium; and an intermediate layer consisting essentially of an aluminumsilicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base body, said intermediate layer having a thickness of between 0.05 mm. and 0.5 mm. so as to prevent diffusion of iron from said base body to said facing sheet,
  • a clad metal sheet body comprising, in combination, a base sheet body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, alloys of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of said high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium, said facing sheet having a thickness of at least 0.2 mm.; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base sheet body, said intermediate layer having a thick- 7 ness of between 0.05 mm.
  • a clad metal sheet body of predetermined thickness comprising, in combination, a base sheet body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, alloys of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of said high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium, said facing sheet having a thickness of between 5% and 15% of said predetermined thickness; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base sheet body, said intermediate layer having a thickness of between 0.05 mm.
  • a clad metal sheet body of predetermined thickness comprising, in combination, a base sheet body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.99%, alloys of said high purity aluminum and between 0.5% and 2% magnesium, alloys of said high purity aluminum, between 0.5% and 2% magnesium and between 4% and 6% zinc, and alloys of said high purity aluminum, between 0.5% and 2% magnesium, between 4% and 6% zinc and between 0.1% and 0.5% beryllium, said facing sheet having a thickness of about 10% of said predetermined thickness; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base sheet body, said intermediate layer having a thickness of between 0.05 mm.

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Description

tion.
CLAD METAL BODY AND METHOD OF MAKING THE SAME Paul Brenner, Bad Godesberg, Germany, assignor to Vereinigte Leichtmetall-Werke G.m.b.H., Bonn, Germany No Drawing. Filed Aug. 9, 1957, Ser. No. 677,224
Claims priority, application Germany Aug. 11, 1956 7 Claims. c1. 29-19 1 The present invention relates to a clad metal body and method of making the same, and more particularly, the present invention relates to a clad metal body having an aluminum or aluminum-alloy face the aluminum of which is of high purity.
It is frequently desirable to plate iron bodies or iron alloy bodies such as steel sheets with aluminum in order to combine the mechanical strength properties of the ironcontaining metal (the term metal throughout the present specification is to be understood as including alloys as well as elementary metals) with the high corrosion resistance of the aluminum, particularly in order to prevent rusting of the iron-containing surface. It is also desirable,
to plate'iron-containing metal bodies with aluminum .of high purity such as a purity of at least 99.9% .or with certain aluminum alloys the aluminum of which is of such high purity. This is particularly desirable when the formation upon subsequent deformation of the clad metal .body; Formation of these iron aluminides can be prevented by alloying the aluminum-containing face layer with silicon in the amount of about 1%.
However, when it is desired to clad iron-containing U ite S at P en Tree metal bodies with high purity aluminum or with alloys I consisting of high purity aluminum and of limited quantities of for instance magnesium, zinc and beryllium, i.e. with aluminum 'or aluminum alloys which are particularly well-suited to be brightened by a chemical or electro chemical method or to be anodically oxidized, then the alloying of the same with silicon in order to prevent formation of the brittle iron aluminide zone will interfere with brightening or anodically oxidizing the aluminum surface layer. r
i It is therefore an object of the present invention to overcome the difficulties in making clad metal bodies com prising an iron-containing base body and a facing sheet of high purity aluminum or high purity aluminum alloys capable of being so-treated as to achieve high light reflectivity.
It is another object of the present invention to provide a clad metal body comprising an-iron-containing base body and a facing sheet including high purity aluminum,
which clad body can be deformed Without rack forma- It is another object of the present invention to adhere manner as to obtain a clad metal sheet free of iron aluminides. l
the aluminumof the facing layer.
Other objects and advantages of thepresent invention will become apparent froma further reading of the description and of the appended claims.
With the above and other objects in view, the present invention mainly consists in a clad metal body, comprising in combination, a base body containing iron, an outer facing sheet composed ofan anodizable, high purity aluminum-containing metal,-the aluminum of the metal having a'purity of .at least 99.9%, and an intermediate layer between'the base body and the facing sheet, the layer consisting essentially of an aluminum alloy of such composition as not to react with iron under formation of an iron aluminide when heatedto the temperatures required for hot rolling and soft annealing of the clad metal body. 7
According to a preferred embodiment, the present invention contemplates a clad metal sheet body of predetermined thickness comprising, in combination, a base sheet body made of steel,,a facing sheet composed of a. substance belonging to the group consisting of highpurity aluminum having a purityof at least 99.9%,- alloys of the high purity aluminum and up to 5% magnesium, alloys of the high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of the high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium, the facing sheet having a thickness of about 10%,of the predetermined thickness, and an intermediate layer, consisting essentially of an. aluminumsilicon alloy containing between 0.5 and 2.0% silicon, firmly adhering to one face of the facing sheet and to the base sheet body, the intermediateflayer having a thickness of between 0.05 mm. and 0.5mm. so as to prevent diffusion of iron from the base body to the facing sheet, whereby formation of iron aluminides during hot rolling and soft annealing of the clad metal sheet body is prevented due to the interposition of thealuminum-silicon alloy layer between the base sheet body'and the facing sheet. The present invention also includes a method of forming a clad metalbody including a facing sheet member composed of an anodizable, high-purity aluminumcontaining metal, the aluminum of the metal having a' purity of at least 99.9%, and also including an iron-containing base body member, comprising the steps of adhering to one of the members an intermediate layer consisting ,essentially of an aluminum alloy ofsuch composition as not to react with iron under formation of an iron aluminide when heated to the temperatures'required for hot rolling and soft annealing of the cladmetal body, and adhering to the free face of the intermediate layer the other of the members, whereby a clad metal body free of iron aluminides is formed ,due to the' interposition of the intermediate layer between the. members. I Thus, according to the present invention, an intermediate layer is placed between the iron-containing base body such as a steel sheet and the cladding or plating sheet which consists of high purity aluminum, i.e. of
aluminum having a purity of at least 99.9% or of a suitable alloy of high purity aluminum. The intermediate layer is composed'of an aluminum alloy which preferably contains between 0.5 and 2% silicon. The aluminum of the aluminum alloy of which the intermediate layer is formed need not be of such high purity as The'high purity of the aluminum of the facing layer is required in order to achieve the desired degree of corrosion-resistant and/or gloss. This does not apply to the intermediate la'yer s'o that thealuminum of thealuminum-silicon alloy of the intermediate layer may be' commercial aluminum hav ing a plurality of for instance between 99.0 and 99.8%. In contrast thereto, the minimum purity of the high purity aluminum of-the facing layer should Ive-99.9% and pref- 3. erably, the purity of the alumin-containing facing layer should be between 99.99% and 99.995%.
The intermediate layer is preferably composed of an aluminum alloy containing between 0.5 and 2% silicon, the balance being commercial aluminum. It is also possible to use for the intermediate layer an aluminum-silicon alloy containing more than 2% of silicon since all aluminum-silicon alloys below the eutectic composition will prevent the formation of iron aluminides at the relatively low temperature of hot rolling and soft annealing of the clad metal body. However, increasing the silicon content of the aluminum alloy of the intermediate layer beyond 2% will not further improve the ability of the intermediate layer to prevent the formation of iron aluminides, While aluminum alloys containing larger percentages of silicon show progressively decreasing rolling properties. Thus, it is preferred to limit the silicon content of the aluminum alloy of the intermediate layer to between 0.5 and 2% of silicon. The intermediate layer may also contain such other alloying elements as will not interfere with the prevention of the formation of iron aluminides. For instance, the aluminum-silicon alloy of the intermediate layer may also contain manganese.
The thickness of the intermediate layer of aluminumsilicon alloy should be at least 0.05 mm. and will preferably be between 0.2 and 0.5 mm. Generally, increase in the thickness of the intermediate layer relative to the thickness of the iron-containing base body such as a steel sheet, will increase the difliculties of cladding by rolling. Thus, the thickness of the intermediate layer is preferably so chosen as to be just sufiicient to prevent diffusion of iron from the base body through the intermediate layer into the face layer of high purity aluminum or high purity aluminum alloys.
The face layer of the clad metal body according to the present invention may be composed of aluminum having a purity of'at least 99.9%, preferably of 99.99% or even higher such as 99.995%, or of aluminum alloys, the aluminum component of which has a purity of at least 99.9% or preferably a purity of 99.99%, which alloys may also contain up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium.
The following table contains a list of several compositions of the facing sheet of the clad metal body according to the present invention, the specific compositions however, given as illustrative only without limiting the present invention to the specific details given in the following table.
TABLE 1 Composition of facing sheet (a) aluminum 99.9% pure (b) aluminum 99.99% pure (c) aluminum 99.995% pure (d) aluminum 99.99% pure plus 0.5% magnesium (e) aluminum 99.99% pure plus 1% magnesium (1) aluminum 99.99% pure plus 1.5 %-2% magnesium (g) aluminum 99.99% pure plus 12% magnesium plus 4-6% Zinc (h) aluminum 99.99% pure plus 12% magnesium plus 4-6% zinc plus 0.1-0.5 beryllium (i) aluminum 99.9% pure plus up to 5% magnesium, up
to 6% zinc, up to 0.5% beryllium (j) aluminum 99.995% pure plus up to 5% magnesium.
The thickness of the facing layer of. the clad metal body according to the present invention is preferably between 5 and 15% of the entire thickness of the clad metal sheet, in any event, the thickness of the facing layer is to be at least about 0.2 mm.
The clad metal body according to the present invention may for instance be produced by first plating sheet iron in conventional manner with an alloy consisting of high purity aluminum and 1% silicon, and then plating in a second st p ont t e free the aluminum-silicon alloy a sheet composed for instance of high purity alu-. minum and 1% magnesium.
However, it is also possible according to the present invention to form in a first step a clad metal consisting of a layer of an aluminum-silicon alloy and of a layer consisting for instance of high purity aluminum or of an alloy of high purity aluminum and magnesium, and to plate onto the free face of the aluminum-silicon alloy layer in a second step the sheet iron or steel sheet. Thus, in any event an intermediate layer consisting of the aluminum-silicon alloy is formed.
The cladding of the various metal layers is performed in conventional manner preferably by hot rolling.
The high purity aluminum face of the clad metal body is then anodically oxidized or otherwise brightened and improved in its light reflectivity in conventional manner.
The following examples are given as illustrative only of the present invention, the invention however not being limited to the specific details of the examples.
EXAMPLE 1 According to the present example, the sheet of high purity aluminum is first plated onto the intermediate layer of aluminum-silicon alloy, and the thus formed clad metal is then rolled onto a steel band. The finished clad sheet is to have a thickness of the high purity aluminum layer of 0.3 mm., a thickness of the intermediate layer of aluminum-silicon alloy of 0.2 mm., and a thickness of the steel band of 2.5 mm.
The starting material is a band of high purity aluminum having a purity of 99.995% and a thickness of 30 mm., and a band of aluminum-silicon alloy containing 0.7% silicon, the balance aluminum having a purity of 99.8%. The thickness of the aluminum-silicon alloy band is 10 mm. Both bands are first brushed on their plating faces and then pickled in 10% sodium hydroxide at a temperature of 30 C. and for a period of 7 minutes. Thereafter, the bands are neutralized with 10% sulfuric acid at room temperature and washed with water. Then both bands are heated to 500 C. The preferred hot rolling temperature for the subsequent plating is 400 0., since, however, the bands cool during the rolling process, in fact the entire rolling takes place within the temperature range of between 500 and 300 C. In order to obtain faultless bonding during the roll-plating process, the bands are rolled down in one pass to the extent of 40%. The thus formed intermediary clad metal sheet is then further cold rolled in any desired number of passes and with any desired degree of reduction per pass. Between individual cold rolling steps, the sheets maybe annealed if this becomes necessary due to cold work hardening. According to the present example, the clad metal sheet consisting of the high purity aluminum sheet and the aluminum-silicon alloy sheet is rolled down to a thickness of 1 mm. It is essential that in case of an intermediate annealing, the reduction in thickness after the annealing has to amount to at least 40% in order to prevent coarse grain formation in the high purity aluminum layer which would make the same unsuitable for subsequent chemical brightening. The thickness relationship of the high purity aluminum layer and the aluminum-silicon alloy layer thus now no longer corresponds to the relationship of the thicknesses of the original sheets since the softer high purity aluminum sheet has been deformed to a higher degree than the aluminumsilicon alloy layer. Of the now-obtained total sheet thickness of 1 mm., the high purity aluminum layer accounts for 0.7 mm. and the aluminum-silicon alloy layer for 0.3 mm.
A soft annealed steel band of Thomas steel having an initial thickness of 4 mm. is now brushed on its plating face and heated to 400 C. The intermediary clad metal sheet of high purity aluminum and aluminumsilicon alloy is heated to the same temperature. The two bands are then superposed and rolled down in one path to the extent of 40% of their original combined tively soft aluminum-silicon layer and even more the high purity aluminum layer are considerably more reduced in thickness during this rolling operation than the steel sheet so that the three layers of the clad metal sheet now have the following thicknesses: steel layer 2.5 mm., aluminum-silicon alloy 0.2 mm., high purity aluminum facing layer 0.3 mm.
Finally, the thus formed clad metal sheet is soft annealed at a temperature of 560 C. since the steel layer of the composite sheet has suffered certain degree of cold hardening during the rolling at a temperature of 400 C.
7 EXAMPLE 2 The intermediate layer of aluminum-silicon alloy is .first rolled onto the soft annealed steel band. This is done in the same manner as described in Example 1 for the rolling of the intermediate clad metal sheet consisting of high purity aluminum and aluminum-silicon alloy onto the steel band. During subsequent rolling of the high purity aluminum layer onto the free face of the aluminum-silicon alloy layer of the intermediate clad metal sheet consisting of the steel layer and the aluminum-silicon alloy layer, a lower degree of rolling down of about 30% is chosen. Apart from the lesser percentage ofreduction in the overall thickness, the rolling of the high purity aluminum layer onto the intermediary composite sheet is carried out in the manner as described in Example 1 for the rolling of the high purity aluminum layer onto the aluminum-silicon alloy.
It will be understood that each of the elements described above, or two or more together, may also find a useful application in other types of clad metal bodies differing from the types described above.
While the invention has been illustrated and described as embodied in a clad metal sheet having a high purity aluminum face layer, it is not intended to be limited to the details shown, since various modifications and structural changes may be made without departing in any way from the spirit of the present invention.
Without further analysis, the foregoing will so fully reveal the gist of the present invention that others can by applying current knowledge readily adapt it for various applications without omitting features that, from the standpoint of prior art, fairly constitute essential characteristics of the generic or specific aspects of this invention and, therefore, such adaptations should and are intended to be comprehended within the meaning and range of equivalence of the following claims.
What is claimed as new and desired to be secured by Letters Patent is:
1. A clad metal body comprising, in combination, a base body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, alloys of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of said high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base body, said intermediate layer having a thickness of at least about 0.05 mm. so as to prevent diffusion of iron from said base body to said facing sheet, whereby formation of iron aluminides during hot rolling and soft annealing of said clad metal body is prevented due to the interposition of said aluminum-silicon alloy layer between said basebody and said facing sheet.
2. A clad metal body comprising, in combination, a base body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, 'alloys 'of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base body, said intermediate layer having a thickness of between 0.05 mm. and 0.5 mm. so as to prevent diffusion of iron from said base body to said facing sheet, whereby formation of'iron aluminides during hot rolling and soft annealing of said clad metal body is prevented due to the interposition of said aluminum-silicon alloy layer between said base body and said facing sheet.
3. A clad metal body comprising, in combination, a base body made of steel; a facing sheet composed of a. substance belonging to the group consisting of high purity aluminum having a purity of at least 99.99%, alloys of said high purity aluminum and between 0.5% and 2% magnesium, alloys of said high'purity aluminum, between 0.5% and 2% magnesium and between 4% and 6% zinc, and alloys of said high purity aluminum, between 0.5% and 2% magnesium, between 4% and 6% 'zinc and between 0.1% and 0.5% beryllium; and an intermediate layer consisting essentially of an aluminumsilicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base body, said intermediate layer having a thickness of between 0.05 mm. and 0.5 mm. so as to prevent diffusion of iron from said base body to said facing sheet,
whereby formation of iron aluminides during hot rolling and soft annealing of said clad metal body is prevented due to the interposition of said aluminum-silicon alloy layer between said base body and said facing sheet.
4. A clad metal sheet body comprising, in combination, a base sheet body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, alloys of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of said high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium, said facing sheet having a thickness of at least 0.2 mm.; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base sheet body, said intermediate layer having a thick- 7 ness of between 0.05 mm. and 0.5 mm. so as to prevent diffusion of iron from said base body to said facing sheet, whereby formation of iron aluminides during hot rolling and soft annealing of said clad metal sheet body is prevented due to the interposition of said aluminum- -silicon alloy layer between said base sheet body and said facing sheet.
5. A clad metal sheet body of predetermined thickness comprising, in combination, a base sheet body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.9%, alloys of said high purity aluminum and up to 5% magnesium, alloys of said high purity aluminum, up to 5% magnesium and up to 6% zinc, and alloys of said high purity aluminum, up to 5% magnesium, up to 6% zinc and up to 0.5% beryllium, said facing sheet having a thickness of between 5% and 15% of said predetermined thickness; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base sheet body, said intermediate layer having a thickness of between 0.05 mm. and 0.5 mm. so as to prevent diffusion of iron from said base body to said facing sheet, whereby formation of iron aluminides during hot rolling and soft annealing of said clad metal sheet body is prevented due to the interposition of said aluminum-silicon alloy layer between said base sheet body and said facing sheet.
6. A clad metal sheet body of predetermined thickness comprising, in combination, a base sheet body made of steel; a facing sheet composed of a substance belonging to the group consisting of high purity aluminum having a purity of at least 99.99%, alloys of said high purity aluminum and between 0.5% and 2% magnesium, alloys of said high purity aluminum, between 0.5% and 2% magnesium and between 4% and 6% zinc, and alloys of said high purity aluminum, between 0.5% and 2% magnesium, between 4% and 6% zinc and between 0.1% and 0.5% beryllium, said facing sheet having a thickness of about 10% of said predetermined thickness; and an intermediate layer consisting essentially of an aluminum-silicon alloy containing between 0.5% and 2.0% silicon, firmly adhering to one face of said facing sheet and to said base sheet body, said intermediate layer having a thickness of between 0.05 mm. and 0.5 mm. so as to prevent diffusion of iron from said base body to said facing sheet, whereby formation of iron aluminides during hot rolling and sofe annealing of said clad metal sheet body is prevented due to the interposition of said aluminum-silicon alloy layer between said base sheet body and said facing sheet.
7. A method of forming a clad metal sheet body inlcludinga facing sheet member composed of a substance belonging to the group consisting of high purity aluminum having a purity of at'least 99.9%, alloys of said high purity, aluminum and magnesium, alloys of said high purity aluminum, magnesium and zinc, and alloys of said high purity aluminum, magnesium, zinc and beryllium, and also including an iron-containing base sheet member, comprising the steps of rolling onto one face of one of said sheet members an intermediate layer consisting essentially of an aluminum-silicon alloy and having a thickness greater than 0.05 mm.; rolling onto the free face of said intermediate layer one face of the other of said sheet members thereby forming a composite body comprising said facing sheet member, said base sheet member and said intermediate layer between said members; and subjecting said composite body to reduction rolling so as to reduce the thickness of said intermediate layer to a value being at least equal to 0.05 mm., whereby a clad metal sheet body free of iron aluminides is formed due to the interposition of said intermediate layer between said sheet members.
References Cited in the file of this patent UNITED STATES PATENTS 1,805,448 Frary May 12, 1931 2,565,768 Gittings Aug. 28, 1951 2,708,304 Lundin May 17, 1955 2,735,170 Moifatt Feb. 21, 1956

Claims (1)

1. A CLAD METAL BODY COMPRISING, IN COMBINATION, A BASE BODY MADE OF STEEL, A FACING SHEET COMPOSED OF A SUBSTANCE BELONGING TO THE GROUP CONSISTING OF HIGH PURITY ALUMINUM HAVING A PURITY OF AT LEAST 99.9%, ALLOYS OF SAID HIGH PURITY ALUMINUM AND UP TO 5% MAGNESIUM, ALLOYS OF SAID HIGH PURITY ALUMINUM, UP TO 5% MAGNESIUM AND UP TO 6% ZINC, AND ALLOYS OF SAID HIGH PURITY ALUMINUM, UP TO 5% MAGNESIUM, UP TO 6% ZINC AND UP TO 0.5% BERYLLIUM, AND AN INTERMEDIATE LAYER CONSISTING ESSENTIALLY OF AN ALUMINUM-SILICON ALLOY CONTAINING BETWEEN 0.5% AND 2.0% SILICON, FIRMLY ADHERING TO ONE FACE OF SAID FACING SHEET AND TO SAID BASE BODY, SAID INTERMEDIATE LAYER HAVING A THICKNESS OF AT LEAST ABOUT 0.05 MM. SO AS TO PREVENT DIFFUSION OF IRON FROM SAID BASE BODY TO SAID FACING SHEET, WHEREBY FORMATION OF IRON ALUMINIDES DURING HOT ROLLING AND SOFT ANNEALING OF SAID CLAD METAL BODY IS PREVENTED DUE TO THE INTERPOSITION OF SAID ALUMINUM-SILICON ALLOY LAYER BETWEEN SAID BASE BODY AND SAID FACING SHEET.
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Cited By (15)

* Cited by examiner, † Cited by third party
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US3093459A (en) * 1958-08-02 1963-06-11 Aluminium Ind Ag Method for manufacturing highly polishable sheets of aluminum
US3173202A (en) * 1961-08-10 1965-03-16 S W Farber Inc Aluminum cladding
US3400450A (en) * 1965-11-10 1968-09-10 Aluminum Co Of America Method of forming ferrous sheet faced with aluminum
US3436804A (en) * 1968-04-23 1969-04-08 Olin Mathieson Process for forming composite aluminum alloy
US3648353A (en) * 1970-01-02 1972-03-14 Texas Instruments Inc Method of making automotive trim
US3811177A (en) * 1969-12-15 1974-05-21 Vaw Ver Aluminium Werke Ag Process for brazing workpieces of aluminum containing material
US3831263A (en) * 1972-08-11 1974-08-27 Aluminum Co Of America Method of soldering
US3905780A (en) * 1973-06-25 1975-09-16 Armco Steel Corp Oxidation-resistant low alloy steel with Al coating
US4046304A (en) * 1973-09-12 1977-09-06 Teikoku Piston Ring Co., Ltd. Process for producing metal composite material
FR2374093A1 (en) * 1976-12-17 1978-07-13 Univ College Cardiff Cuic PROCESS FOR APPLYING AT LEAST ONE COATING LAYER ON A SUBSTRATE
US4150179A (en) * 1977-12-19 1979-04-17 University College Cardiff Hot dip aluminizing of steel strip
FR2530536A1 (en) * 1982-07-26 1984-01-27 Nisshin Steel Co Ltd Aluminium-coated steel sheet and process for its production.
US4526103A (en) * 1982-04-01 1985-07-02 Nisshin Steel Co., Ltd. Aluminum coated steel support for planographic plate
EP0761369A2 (en) * 1995-08-31 1997-03-12 Philip C. Lewis Method for low temperature bimetallic formation of ductile single material with two metal layers
US20100276001A1 (en) * 2009-05-01 2010-11-04 Fujifilm Corporation Metal composite substrate and method of producing the same

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US1805448A (en) * 1929-11-30 1931-05-12 Aluminum Co Of America Corrosion-resistant aluminum alloy article
US2565768A (en) * 1948-04-02 1951-08-28 United States Steel Corp Aluminum coating of ferrous metal and resulting product
US2708304A (en) * 1952-06-27 1955-05-17 Lundin Helen Marie Aluminum coated articles
US2735170A (en) * 1956-02-21 Method-of producing a multilayer strep

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US2735170A (en) * 1956-02-21 Method-of producing a multilayer strep
US1805448A (en) * 1929-11-30 1931-05-12 Aluminum Co Of America Corrosion-resistant aluminum alloy article
US2565768A (en) * 1948-04-02 1951-08-28 United States Steel Corp Aluminum coating of ferrous metal and resulting product
US2708304A (en) * 1952-06-27 1955-05-17 Lundin Helen Marie Aluminum coated articles

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3093459A (en) * 1958-08-02 1963-06-11 Aluminium Ind Ag Method for manufacturing highly polishable sheets of aluminum
US3173202A (en) * 1961-08-10 1965-03-16 S W Farber Inc Aluminum cladding
US3400450A (en) * 1965-11-10 1968-09-10 Aluminum Co Of America Method of forming ferrous sheet faced with aluminum
US3436804A (en) * 1968-04-23 1969-04-08 Olin Mathieson Process for forming composite aluminum alloy
US3811177A (en) * 1969-12-15 1974-05-21 Vaw Ver Aluminium Werke Ag Process for brazing workpieces of aluminum containing material
US3648353A (en) * 1970-01-02 1972-03-14 Texas Instruments Inc Method of making automotive trim
US3831263A (en) * 1972-08-11 1974-08-27 Aluminum Co Of America Method of soldering
US3905780A (en) * 1973-06-25 1975-09-16 Armco Steel Corp Oxidation-resistant low alloy steel with Al coating
US4046304A (en) * 1973-09-12 1977-09-06 Teikoku Piston Ring Co., Ltd. Process for producing metal composite material
FR2374093A1 (en) * 1976-12-17 1978-07-13 Univ College Cardiff Cuic PROCESS FOR APPLYING AT LEAST ONE COATING LAYER ON A SUBSTRATE
US4150179A (en) * 1977-12-19 1979-04-17 University College Cardiff Hot dip aluminizing of steel strip
US4526103A (en) * 1982-04-01 1985-07-02 Nisshin Steel Co., Ltd. Aluminum coated steel support for planographic plate
FR2530536A1 (en) * 1982-07-26 1984-01-27 Nisshin Steel Co Ltd Aluminium-coated steel sheet and process for its production.
EP0761369A2 (en) * 1995-08-31 1997-03-12 Philip C. Lewis Method for low temperature bimetallic formation of ductile single material with two metal layers
EP0761369A3 (en) * 1995-08-31 1997-09-03 Philip C Lewis Method for low temperature bimetallic formation of ductile single material with two metal layers
US20100276001A1 (en) * 2009-05-01 2010-11-04 Fujifilm Corporation Metal composite substrate and method of producing the same
EP2248662A1 (en) * 2009-05-01 2010-11-10 Fujifilm Corporation Metal composite substrate and method of producing the same

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