US2100257A - Composite body of magnesium and aluminum, and method of making same - Google Patents
Composite body of magnesium and aluminum, and method of making same Download PDFInfo
- Publication number
- US2100257A US2100257A US63031A US6303136A US2100257A US 2100257 A US2100257 A US 2100257A US 63031 A US63031 A US 63031A US 6303136 A US6303136 A US 6303136A US 2100257 A US2100257 A US 2100257A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- magnesium
- alloy
- envelope
- zinc
- 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
Links
- 229910052782 aluminium Inorganic materials 0.000 title description 111
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title description 111
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 title description 98
- 229910052749 magnesium Inorganic materials 0.000 title description 89
- 239000011777 magnesium Substances 0.000 title description 89
- 239000002131 composite material Substances 0.000 title description 13
- 238000004519 manufacturing process Methods 0.000 title description 4
- 229910045601 alloy Inorganic materials 0.000 description 60
- 239000000956 alloy Substances 0.000 description 60
- 229910052751 metal Inorganic materials 0.000 description 35
- 239000002184 metal Substances 0.000 description 35
- 238000000034 method Methods 0.000 description 26
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 22
- 239000011701 zinc Substances 0.000 description 22
- 229910052725 zinc Inorganic materials 0.000 description 20
- 239000011248 coating agent Substances 0.000 description 18
- 238000000576 coating method Methods 0.000 description 18
- 239000011162 core material Substances 0.000 description 18
- 150000002739 metals Chemical class 0.000 description 12
- 238000005266 casting Methods 0.000 description 9
- 229910000611 Zinc aluminium Inorganic materials 0.000 description 8
- HXFVOUUOTHJFPX-UHFFFAOYSA-N alumane;zinc Chemical compound [AlH3].[Zn] HXFVOUUOTHJFPX-UHFFFAOYSA-N 0.000 description 8
- 238000003475 lamination Methods 0.000 description 8
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 6
- 229910000861 Mg alloy Inorganic materials 0.000 description 5
- 229910001297 Zn alloy Inorganic materials 0.000 description 4
- 238000005275 alloying Methods 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 230000035515 penetration Effects 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 239000011888 foil Substances 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 150000002680 magnesium Chemical class 0.000 description 2
- -1 magnesium-zinc-aluminum Chemical compound 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- JIAARYAFYJHUJI-UHFFFAOYSA-L zinc dichloride Chemical compound [Cl-].[Cl-].[Zn+2] JIAARYAFYJHUJI-UHFFFAOYSA-L 0.000 description 2
- 230000001464 adherent effect Effects 0.000 description 1
- FJMNNXLGOUYVHO-UHFFFAOYSA-N aluminum zinc Chemical compound [Al].[Zn] FJMNNXLGOUYVHO-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000002310 reflectometry Methods 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000011592 zinc chloride Substances 0.000 description 1
- 235000005074 zinc chloride Nutrition 0.000 description 1
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
- B32B15/017—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of aluminium or an aluminium alloy, another layer being formed of an alloy based on a non ferrous metal other than aluminium
-
- 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
- Y10S428/9335—Product by special process
- Y10S428/939—Molten or fused coating
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49982—Coating
- Y10T29/49984—Coating and casting
-
- 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.]
- Y10T428/12729—Group IIA metal-base component
-
- 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
-
- 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.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12785—Group IIB metal-base component
- Y10T428/12792—Zn-base component
Definitions
- magnesium is a highly desirable body material, but noentirely satisfactory way for protecting magnesium from corrosion has so far been suggested; while both metals are strong and have very similar melting temperatures, coeflicients of expansion and contraction, etc., aluminum has higher electrical and thermal conductivity, greater reflectivity, is more resistant to abrasion, chemical reaction, corrosion, etc.
- Another object of this invention is to provide a method whereby magnesium may be suitably protected against corrosion.
- Another object ofthis invention is to produce laminated magnesium and aluminum by a procedure which assures a substantially uniform alloy bond throughout the contiguous surfaces of the laminations'.
- Another object of this invention is to provide a method for producing laminated bodies of aluminum and magnesium wherein the depth of the alloy bond connecting the laminations may be controlled so as to secure a predetermined depth as well as a substantially uniform character of bond.
- Another object of this invention is to provide a method of the type characterized which is of such character that it may be efficiently and economically performed in large-scale commercial operations.
- Another object of this invention is to produce a billet, ingot, block, or other body composed of a magnesium core and a coating lamina of aluminum on one or more faces thereof with a substantially uniform alloy bond between the magnesium and aluminum throughout the contiguous surfaces thereof.
- Another object of this invention is to produce rolled plates, sheets, foils, etc., of aluminum coated magnesium wherein the laminations are united by a. substantially uniform alloy bond throughout the contiguous surfaces thereof and in which at the same time are preserved the desirable characteristics of the magnesium as a core metal and of the aluminum as a surfacing metal.
- Another object of this invention is to provide a magnesium body which is completely and permanently coated with a corrosion-preventing envelope and which ,can therefore be widely used where decreased weight or increased strength or stiffness or decreased cost per unit of cross sectional weight are desirable.
- Another object of this invention is to produce aluminum coated' magnesium which can be readily drawn, rolled, pressed, shaped and otherwise worked, and therefore fabricated into a wide variety of articles and applied to a wide variety of uses, but with assurance that the alloy bond between the laminations will not be destroyed.
- Another object of this invention is to produce aluminum coated magnesium which while preserving the desirable characteristics of the magnesium as a core metal and the aluminum as a surfacing metal also secures various advantages to be derived from their association in laminations, the character and thickness of the alloy bond between the laminations being such as not to interfere with or detract from the characteristics to be desirably obtained from the associ- 2 ation of these two metals into a laminated structure.
- the thickness of the. alloy bond may be controlled and predetermined.
- the coating metal substantially coextensive with the outer face of the ultimate product, but it is within the contemplation of the present invention to provide an aluminum coating on one face only, or on less than all of the faces of billets, ingots, blocks, or other bodies where such is suflicient, and therefore the term envelope as herein used is to be interpreted as embracing a covering on one or more faces of the magnesium core.
- the magnesium in an aluminum envelope which will produce composite metal in the form of a billet, ingot, block, or the like, it is to be expressly understood that the invention is not restricted thereto.
- the composite metal may be formed incon formity with the present invention in other shapes, including tubes, bars, etc., or in fact in any suitable form that is appropriate for the ultimate product to be produced, and therefore the invention is not restricted to the formation of billets,
- the term billet as used herein is to be construed as a term generic to any suitable form in which the aluminum is united to a magnesium core as herein explained.
- the composite metal body is to be formed as a billet or the like with a coating of aluminum that is coextensive with opposed faces thereof.
- the preferred procedure is, as follows:--Aluminum in a form to provide a suitable envelope is first provided.
- the thickness of said envelope may be varied within relatively wide limits depending upon the -use to which the composite' metal is to be put, the desired characteristics in the ultimate product, etc.
- the envelope may be relatively thick. The envelope must not be so thin,1in comparison with the volume of. mag
- the relative heat capacities of the two metals aresuch as to aluminum to magnesium desired in the ultimate product, which will vary with the use to which the composite metal is to be put and the characteristics desired.
- the aluminum envelope is preferably formed from hot rolled sheets, as this provides an envelope which is well annealed and has a relatively clean surface.
- cold rolled aluminum sheets may be employed if preferred, provided the sheets are sufliciently annealed and the surface thereof is properly cleaned to enable the carrying out of the process as herein described.
- the face of the sheet or sheets which, when the envelope is assembled or formed, isto be united to the magnesium is then provided with a substantially uniform layer of zinc aluminum alloy of predetermined depth.
- the preferred procedure is to heat the aluminum sheet to a temperature at least as high as the eutectic melting point of the aluminum zinc binary system.
- Zinc is then applied to that face of the aluminum sheet which is to be united with the core in such a way as to assure a uniform break down and detachment of the aluminum oxide film on the aluminum sheet and to obtain the desired depth of alloy.
- the aluminum sheet may first be treated with a zinc chloride or any other suitable flux that will break down the aluminum oxide, but I prefer to use abrasion of the aluminum surface, as with any suitable wire brush, after the molten zinc, which may be melted by the temperature of the aluminum plate, has been spread over the surface of the aluminum so that it is applied uniformly thereover, working the brush through the coating of molten zinc to break down the oxide film while the zinc coating pro"- tects the aluminum surface from contact with the oxygen of the air.
- This procedure also avoids the presence of foreign material that may have to be removed to avoid formation of gas or other interference with the establishment of a uniform bond between the core and envelope when magnesium is cast into said envelope as hereinafter explained.
- the depth of the alloy formed can be varied depending upon the temperature of the aluminum and the time and character of the mechanical or chemical work which are used in breaking down the aluminum oxide film and assuring a penetration of the zinc. into the aluminum. Ordinarily, a relatively thin layer of alloy is desired, deep penetration of the zinc into the aluminum being undesirable because the alloy is less ductile than either the aluminum or magnesium.
- the molten zinc goes into solution with the aluminum and establishes a zinc aluminum alloy, and this alloy when formed as heretofore described is substantially uniform in thickness and of controlled thickness throughout the surface. of the aluminum sheet.
- I preferably form the envelope by bending the sheet into U form with the alloy layer on the inside, so that the parallel legs thereof are spaced at the distance predetermined for the thickness of the magne- ;ium core, the connection between said legs helping to maintain said legs at the predetermined spacing, and Where the. envelope is sumciently stiff supporting and retaining the side sheets at that-spacing.
- the envelope is mounted in any suitable mold, bywhich term is to be understood.
- any suitable form' which will properly retain the envelope in a position for a casting operation and, where necessary,*complete the cavity between the elementsof the envelope for reception ii the molten magnesium;
- Magnesium is thencast into the cavity of the mold at any suitable temperature.
- the usual pouring temperature employed in the casting of magnesium billets may be used, but higher degrees of superheat may be employed depending upon the depth of alloy bond desired.
- the molten magnesium melts the zinc aluminum alloy' upon contact therewith, producing surface fusion of the alloy and forming a fused bond between said alloy and the magnesium, which bond is composed of an alloy of magnesium, zinc and aluminum.
- the depth of alloy bond may be increased over that established by the initial formation of the alloy during the preceding step, and the depth of this bond may thus be widely varied and accurately controlled.
- Excessive penetration of the zinc and magnesium into the aluminum is undesirable, and therefore the temperature relationship between thealuminum envelope and the magnesium cast therein, with respect to the relative heat capacities of the two, must be predetermined to avoid undue penetration ofthe zinc and magnesium into the aluminum.
- the mold may be water cooled if desired, such being ordinarily desirable where'the molds are to be used at frequent intervalsand it is desirable to withdraw therefrom at least some of the heat resulting from the previous casting operation.
- the billet may be passed to the rolls as soon as it has cooled to a suitable rolling temperature. I prefer to roll the billet hot, to avoid drastic strain hardening of the composite metal.
- Thetemperature at which the composite metal is rolled may vary within relatively wide'limits, depending upon the desired characteristics of the ultimate product. Ordinarily, the temperature should not be so high as to cause substantial dispersion of one metal into the other and thereby unduly increase the depth of the alloy bond, but a temperature which gives a considerable degree .of plasticity to the aluminum and magnesium is usually desirable.
- the break down passes are preferably carried out at a temperature between 550 F. and 900 F., but thereafter the further rolling operations may be carried out at any suitable temperature, depending upon the characteristics desired in the ultimate product.
- Aluminlmi coated magnesium plates or sheets of suitable thickness may thereby 'be formed for fabricationinto a wideyariety of articles, and
- the composite metal so provided possesses the advantages derived from the use of the lighter weight magnesium as a body or corematerial
- the envelope may be composed of pure alumi-' num or a .wide variety of aluminum base alloys depending upon the character of coating desired, and thec'ore may be composed of pure magnesium or any suitable magnesium alloy.”
- the core is preferably a magnesium base alloy with a small percentage of aluminum therein, the presence ,of the aluminum also giving desirable characteristics to the core metal. Therefore, it is to be expressly understood that when aluminum or magnesium are referred to herein it is intended to embrace within such terms any suitable alloy of aluminum for the coating metal and any suitable alloy of magnesium for the core metal.
- the present invention therefore provides billets and other bodies of aluminum coated magnesium wherein the magnesium and aluminum are united throughout their contiguous surfaces by a substantially uniform alloy bond of predetermined depth.
- the composite metal is possessed of the various desirable characteristics inherent in the use of aluminum as a coating metal and mag-' as produced by the method disclosed, may be put to a wide variety of uses, and a wide variety of objects may be made therefrom, without destroying the alloy bond between the laminations. Therefore the composite metal of this invention can be applied to many uses in the electrical, mechanical and chemical arts where the light weight of the magnesium makes use thereof desirable.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of substantially destroying the oxide film at the surface of the aluminum to be united to the magnesium by forming an alloy of zinc and aluminum at the inner face of an aluminum envelope, and casting magnesium into said envelope into direct contact with said alloy to form therewith a "substantially continuous alloy bond between said magnesium and aluminum.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming acoating sheet of aluminum, substantially destroying the oxide film at the surface thereof to be united to the magnesium while alloying zinc therewith, and uniting a magnesium core thereto by establishing a substantially uniform aluminum .zinc magnesium alloy bond between the contiguous surfaces of the magnesium and aluminum.
- the method of forming bodies of corrosionreslstant magnesium which includes the steps of forming a coating sheet of aluminum, substantially destroying the oxide film at the surface thereof to be united to the magnesium while alloying zinc therewith, and fusing the alloyed face of said coating sheet to a magnesium core by a substantially uniform alloy bond which is substantially continuous and co-extensive with the contiguous faces thereof.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum which has a substantially continuous predetermined layer of zinc aluminum alloy adherent to the inner face of said envelope with substantial uniformity, and fusing to said layer a core of magnesium to establish a substantially uniform alloy bond between said metals.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming a. sheet of aluminum, forming an alloy layer at the face of said sheet which/is to be united to the magnesium, and fusing to said alloy layer a magnesium core to form an alloy bond of substantially uniform character and predetermined depth throughout the contiguous surfaces of said metals.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of substantially destroying the oxide film at thesurface of the aluminum to be united-to the magnesium by alloying zinc to said face of the aluminum to provide a relatively thin alloy layer, and fusing to saidlayer a core of magnesium.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of substantially destroying the oxide film at the surface of the aluminum tobe united to the magnesium by alloying zinc to said face of the aluminum to provide a relatively thin alloy layer, and casting molten magnesium into contact with said layer to form a fused bond with said alloy layer.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the-steps oi substantially destroying the oxide film at the surface of the aluminum to be united to the magnesium by forming an alloy of zinc andaluminum at the inner face of an envelope uheet oi aluminum and uniting said alloyed face of said aluminum envelope sheet to a fused magnesium core by forming a substantially uniform alloy bond therebetween while 'controlling the relative temperatures of said metals to predctermine the depth of the bond so oxide fllmon said aluminum to form a predetermined layer of zinc aluminum alloy, forming the aluminum into an envelope, and then fusing a core of magnesium to said alloy within said envelope.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of applying molten zinc to aluminum while breaking down the aluminum oxide film on said aluminum to form a predetermined layer of zinc aluminum alloy, forming the" aluminum into an envelope, and then casting into said envelope a core of molten magnesium to fuse the surface of said alloy and establish a substantially uniform alloy bond between the aluminum and magnesium.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of applying molten zinc to aluminum while breaking down the aluminum oxide film on-said aluminum to form a predetermined layer of zinc aluminum alloy, forming the aluminum into an envelope, and then casting into said envelope a core of molten magnesium to fuse the surface of said alloy and establish a substantially uniform alloy bond between the aluminum and magnesium while controlling the relative temperatures of said aluminum and magnesium with respect to their relative heat capacities so as to predetermine the depth of alloy bond so formed.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum having alloyed to the inner face of said envelope a thin coating of zinc, and then fusing a core of magnesium to said thin coating to unite said magnesium to said aluminum by a magnesium-zinc-aluminum alloy.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum having alloyed to the inner face of said envelope a thin coating of zinc, and then casting a core of molten magnesium into said envelope to form a fused bond with said thin coating and unite said magnesium to said aluminum by a magnesium-zinc-aluminum alloy.
- the method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum having alloyed to the inner face of said envelope a thin coating of zinc, and. then casting a core of molten magnesium into said envelope to form a fused bond'with said thin coating and unite said magnesium to said aluminum by a magnesiumzinc-aluminum alloy while controllingthe relative temperatures of the aluminum and magnesium with respect to their relative heat capacities to predetermine the depth of alloy bond formed between said aluminum an magnesium.
- a malleable ductile aluminum coatedmagnesium body composed of airelatively thin aluminum coating sheet having a zinc aluminum alloy layer at its inner face united to a magnesium core by a. substantially continuous bond of controlled thickness, said bond being composed of a relatively thin layer of aluminum, zinc and magnesium alloy substantially coextensive with the contiguous surfaces of the magnesium and aluminum and uniformly bonded to both of said metals.
Landscapes
- Laminated Bodies (AREA)
Description
Patented Nov. 23, 1937 UNITED STATES PATENT OFFICE COMPOSITE BODY OF MAGNESIUM AND ALUMINUM, AND METHOD OF MAKING SAME Clayton E. Larson, Louisville, Ky assignor to Reynolds Metals Comany, New York, N. Y., a corporation of Delaware No Drawing. Application February 8, 1936,
Serial No. 63,031
15 Claims.
lower specific gravity than aluminum, and there-' fore where lighter weight per unit of cross sectional area or greater stiffness and strength per unit of cross sectional weight are desirable; as in the saving 'of weight, lowering of costs, reduction in dead load of moving parts and structures, etc, magnesium is a highly desirable body material, but noentirely satisfactory way for protecting magnesium from corrosion has so far been suggested; while both metals are strong and have very similar melting temperatures, coeflicients of expansion and contraction, etc., aluminum has higher electrical and thermal conductivity, greater reflectivity, is more resistant to abrasion, chemical reaction, corrosion, etc.
The bonding of magnesium to aluminum has heretofore presented grave practical difficulties. The high surface tension, tenacity and resistance to rupture of the aluminum oxide illm and the magnesium oxide film, existing on aluminum and magnesium in the presence of air, render diflicult the adhesion of magnesium to aluminum, even though an effort be made to roll the two together under relatively high pressure and at an elevated temperature, because of the difficulty of breaking through the tenacious oxide films. Therefore, so far as I am aware, no commercially feasible pro-' cedure has heretofore been suggested for producing laminated magnesium and aluminum because of the absence of a method which will assure a substantially uniform bond between the laminations of the diverse metals.
It is an object of this invention to provide a method whereby magnesium may be satisfactorily used for the fabrication of a wide variety of articles where weight is important.
Another object of this invention is to provide a method whereby magnesium may be suitably protected against corrosion.
Another object ofthis invention is to produce laminated magnesium and aluminum by a procedure which assures a substantially uniform alloy bond throughout the contiguous surfaces of the laminations'.
Another object of this invention is to provide a method for producing laminated bodies of aluminum and magnesium wherein the depth of the alloy bond connecting the laminations may be controlled so as to secure a predetermined depth as well as a substantially uniform character of bond.
Another object of this invention is to provide a method of the type characterized which is of such character that it may be efficiently and economically performed in large-scale commercial operations.
Another object of this invention is to produce a billet, ingot, block, or other body composed of a magnesium core and a coating lamina of aluminum on one or more faces thereof with a substantially uniform alloy bond between the magnesium and aluminum throughout the contiguous surfaces thereof.
Another object of this invention is to produce rolled plates, sheets, foils, etc., of aluminum coated magnesium wherein the laminations are united by a. substantially uniform alloy bond throughout the contiguous surfaces thereof and in which at the same time are preserved the desirable characteristics of the magnesium as a core metal and of the aluminum as a surfacing metal.
Another object of this invention is to provide a magnesium body which is completely and permanently coated with a corrosion-preventing envelope and which ,can therefore be widely used where decreased weight or increased strength or stiffness or decreased cost per unit of cross sectional weight are desirable.
Another object of this invention is to produce aluminum coated' magnesium which can be readily drawn, rolled, pressed, shaped and otherwise worked, and therefore fabricated into a wide variety of articles and applied to a wide variety of uses, but with assurance that the alloy bond between the laminations will not be destroyed.
Another object of this invention is to produce aluminum coated magnesium which while preserving the desirable characteristics of the magnesium as a core metal and the aluminum as a surfacing metal also secures various advantages to be derived from their association in laminations, the character and thickness of the alloy bond between the laminations being such as not to interfere with or detract from the characteristics to be desirably obtained from the associ- 2 ation of these two metals into a laminated structure.
Other objects will appear as the description of the invention'proceeds.
'In conformity with the present invention a composite metal body of aluminum and mag-' nesium. Then magnesium is fused to said alloy,
establishing an alloy bond of zinc, magnesium and aluminum between the magnesium and aluminum. Thereby are avoided the discontinuities and irregularities of bond which would exist if the metals were rolled or otherwise pressed together. By suitably controlling the relative temperatures of the magnesium and aluminum, with regard to the heat capacities of the volumes of the respective metals employed, the thickness of the. alloy bond may be controlled and predetermined. By this procedure a substantially uniform alloy bond between the magnesium and aluminum is established throughout the contiguous surfaces thereof, and as the depth of said bond may be nicely controlled, the laminated body can be given the desired characteristics suitable for the use to which the laminated metal is to be put.
For most purposes it is preferable to have the coating metal substantially coextensive with the outer face of the ultimate product, but it is within the contemplation of the present invention to provide an aluminum coating on one face only, or on less than all of the faces of billets, ingots, blocks, or other bodies where such is suflicient, and therefore the term envelope as herein used is to be interpreted as embracing a covering on one or more faces of the magnesium core. Furthermore, while it is preferred to cast the magnesium in an aluminum envelope which will produce composite metal in the form of a billet, ingot, block, or the like, it is to be expressly understood that the invention is not restricted thereto.
as the composite metal may be formed incon formity with the present invention in other shapes, including tubes, bars, etc., or in fact in any suitable form that is appropriate for the ultimate product to be produced, and therefore the invention is not restricted to the formation of billets,
ingots, blocks, etc., but the term billet as used herein is to be construed as a term generic to any suitable form in which the aluminum is united to a magnesium core as herein explained. For purposes of illustrating the invention, however, it will be assumed that the composite metal body is to be formed as a billet or the like with a coating of aluminum that is coextensive with opposed faces thereof.
.The preferred procedure is, as follows:--Aluminum in a form to provide a suitable envelope is first provided. The thickness of said envelope may be varied within relatively wide limits depending upon the -use to which the composite' metal is to be put, the desired characteristics in the ultimate product, etc. As aluminum and magnesium have closely'similar melting temperatures and like rolling temperatures, the envelope may be relatively thick. The envelope must not be so thin,1in comparison with the volume of. mag
nesium to be used in the core, that the relative heat capacities of the two metals aresuch as to aluminum to magnesium desired in the ultimate product, which will vary with the use to which the composite metal is to be put and the characteristics desired.
The aluminum envelope is preferably formed from hot rolled sheets, as this provides an envelope which is well annealed and has a relatively clean surface. However, cold rolled aluminum sheets may be employed if preferred, provided the sheets are sufliciently annealed and the surface thereof is properly cleaned to enable the carrying out of the process as herein described.
The face of the sheet or sheets which, when the envelope is assembled or formed, isto be united to the magnesium is then provided with a substantially uniform layer of zinc aluminum alloy of predetermined depth. The preferred procedure is to heat the aluminum sheet to a temperature at least as high as the eutectic melting point of the aluminum zinc binary system. Zinc is then applied to that face of the aluminum sheet which is to be united with the core in such a way as to assure a uniform break down and detachment of the aluminum oxide film on the aluminum sheet and to obtain the desired depth of alloy. To this end the aluminum sheet may first be treated with a zinc chloride or any other suitable flux that will break down the aluminum oxide, but I prefer to use abrasion of the aluminum surface, as with any suitable wire brush, after the molten zinc, which may be melted by the temperature of the aluminum plate, has been spread over the surface of the aluminum so that it is applied uniformly thereover, working the brush through the coating of molten zinc to break down the oxide film while the zinc coating pro"- tects the aluminum surface from contact with the oxygen of the air. This procedure also avoids the presence of foreign material that may have to be removed to avoid formation of gas or other interference with the establishment of a uniform bond between the core and envelope when magnesium is cast into said envelope as hereinafter explained.
The depth of the alloy formed can be varied depending upon the temperature of the aluminum and the time and character of the mechanical or chemical work which are used in breaking down the aluminum oxide film and assuring a penetration of the zinc. into the aluminum. Ordinarily, a relatively thin layer of alloy is desired, deep penetration of the zinc into the aluminum being undesirable because the alloy is less ductile than either the aluminum or magnesium. The molten zinc goes into solution with the aluminum and establishes a zinc aluminum alloy, and this alloy when formed as heretofore described is substantially uniform in thickness and of controlled thickness throughout the surface. of the aluminum sheet.
:hin sheets, foils, and the like, I preferably form the envelope by bending the sheet into U form with the alloy layer on the inside, so that the parallel legs thereof are spaced at the distance predetermined for the thickness of the magne- ;ium core, the connection between said legs helping to maintain said legs at the predetermined spacing, and Where the. envelope is sumciently stiff supporting and retaining the side sheets at that-spacing. The envelope is mounted in any suitable mold, bywhich term is to be understood.
any suitable form'which will properly retain the envelope in a position for a casting operation and, where necessary,*complete the cavity between the elementsof the envelope for reception ii the molten magnesium;
Magnesium is thencast into the cavity of the mold at any suitable temperature. Ordinarily, the usual pouring temperature employed in the casting of magnesium billets may be used, but higher degrees of superheat may be employed depending upon the depth of alloy bond desired. The molten magnesium melts the zinc aluminum alloy' upon contact therewith, producing surface fusion of the alloy and forming a fused bond between said alloy and the magnesium, which bond is composed of an alloy of magnesium, zinc and aluminum. By suitably controlling the temperatures of the two metals with respect to the heat capacities of their respective, volumes, the depth of alloy bond may be nicely controlled. Thus by heating the aluminum or by having such heat capacities due to the volume of magnesium present, the depth of alloy bond may be increased over that established by the initial formation of the alloy during the preceding step, and the depth of this bond may thus be widely varied and accurately controlled. Excessive penetration of the zinc and magnesium into the aluminum is undesirable, and therefore the temperature relationship between thealuminum envelope and the magnesium cast therein, with respect to the relative heat capacities of the two, must be predetermined to avoid undue penetration ofthe zinc and magnesium into the aluminum. To this end the mold may be water cooled if desired, such being ordinarily desirable where'the molds are to be used at frequent intervalsand it is desirable to withdraw therefrom at least some of the heat resulting from the previous casting operation.
Assuming that the billet is to be rolled into plates,'sheets-, or foils, the billet may be passed to the rolls as soon as it has cooled to a suitable rolling temperature. I prefer to roll the billet hot, to avoid drastic strain hardening of the composite metal. Thetemperature at which the composite metal is rolled, however, may vary within relatively wide'limits, depending upon the desired characteristics of the ultimate product. Ordinarily, the temperature should not be so high as to cause substantial dispersion of one metal into the other and thereby unduly increase the depth of the alloy bond, but a temperature which gives a considerable degree .of plasticity to the aluminum and magnesium is usually desirable. The break down passes are preferably carried out at a temperature between 550 F. and 900 F., but thereafter the further rolling operations may be carried out at any suitable temperature, depending upon the characteristics desired in the ultimate product.
Aluminlmi coated magnesium plates or sheets of suitable thickness may thereby 'be formed for fabricationinto a wideyariety of articles, and
'the composite metal so provided possesses the advantages derived from the use of the lighter weight magnesium as a body or corematerial,
while the magnesium is properly encased and protected by the corrosion-resistant aluminum.
The envelope may be composed of pure alumi-' num or a .wide variety of aluminum base alloys depending upon the character of coating desired, and thec'ore may be composed of pure magnesium or any suitable magnesium alloy." Ordinarily, for economy in the use of scrap, the core is preferably a magnesium base alloy with a small percentage of aluminum therein, the presence ,of the aluminum also giving desirable characteristics to the core metal. Therefore, it is to be expressly understood that when aluminum or magnesium are referred to herein it is intended to embrace within such terms any suitable alloy of aluminum for the coating metal and any suitable alloy of magnesium for the core metal.
The present invention therefore provides billets and other bodies of aluminum coated magnesium wherein the magnesium and aluminum are united throughout their contiguous surfaces by a substantially uniform alloy bond of predetermined depth. The composite metal is possessed of the various desirable characteristics inherent in the use of aluminum as a coating metal and mag-' as produced by the method disclosed, may be put to a wide variety of uses, and a wide variety of objects may be made therefrom, without destroying the alloy bond between the laminations. Therefore the composite metal of this invention can be applied to many uses in the electrical, mechanical and chemical arts where the light weight of the magnesium makes use thereof desirable.
While the preferred procedure has been described with considerable particularity, it is to be expressly understood that the invention is not restricted thereto, as various departures therefrom will now suggest themselves to those skilled in the art. Other methods of securing the alloy layer or of fusing the magnesium core to the alloy layer may be used for example, and any other suitable metal may be used for effecting the alloy layer, provided an alloy bond as herein disclosed is established between the magnesium and the aluminum. Reference is therefore to be had to the claims hereto appended for a definition of the limits of the invention.
What is claimed is:
l. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of substantially destroying the oxide film at the surface of the aluminum to be united to the magnesium by forming an alloy of zinc and aluminum at the inner face of an aluminum envelope, and casting magnesium into said envelope into direct contact with said alloy to form therewith a "substantially continuous alloy bond between said magnesium and aluminum.
2. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming acoating sheet of aluminum, substantially destroying the oxide film at the surface thereof to be united to the magnesium while alloying zinc therewith, and uniting a magnesium core thereto by establishing a substantially uniform aluminum .zinc magnesium alloy bond between the contiguous surfaces of the magnesium and aluminum.
3. The method of forming bodies of corrosionreslstant magnesium which includes the steps of forming a coating sheet of aluminum, substantially destroying the oxide film at the surface thereof to be united to the magnesium while alloying zinc therewith, and fusing the alloyed face of said coating sheet to a magnesium core by a substantially uniform alloy bond which is substantially continuous and co-extensive with the contiguous faces thereof.
4. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum which has a substantially continuous predetermined layer of zinc aluminum alloy adherent to the inner face of said envelope with substantial uniformity, and fusing to said layer a core of magnesium to establish a substantially uniform alloy bond between said metals.
5. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming a. sheet of aluminum, forming an alloy layer at the face of said sheet which/is to be united to the magnesium, and fusing to said alloy layer a magnesium core to form an alloy bond of substantially uniform character and predetermined depth throughout the contiguous surfaces of said metals.
6. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of substantially destroying the oxide film at thesurface of the aluminum to be united-to the magnesium by alloying zinc to said face of the aluminum to provide a relatively thin alloy layer, and fusing to saidlayer a core of magnesium.
'7. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of substantially destroying the oxide film at the surface of the aluminum tobe united to the magnesium by alloying zinc to said face of the aluminum to provide a relatively thin alloy layer, and casting molten magnesium into contact with said layer to form a fused bond with said alloy layer.
8. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the-steps oi substantially destroying the oxide film at the surface of the aluminum to be united to the magnesium by forming an alloy of zinc andaluminum at the inner face of an envelope uheet oi aluminum and uniting said alloyed face of said aluminum envelope sheet to a fused magnesium core by forming a substantially uniform alloy bond therebetween while 'controlling the relative temperatures of said metals to predctermine the depth of the bond so oxide fllmon said aluminum to form a predetermined layer of zinc aluminum alloy, forming the aluminum into an envelope, and then fusing a core of magnesium to said alloy within said envelope.
10. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of applying molten zinc to aluminum while breaking down the aluminum oxide film on said aluminum to form a predetermined layer of zinc aluminum alloy, forming the" aluminum into an envelope, and then casting into said envelope a core of molten magnesium to fuse the surface of said alloy and establish a substantially uniform alloy bond between the aluminum and magnesium.
11. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of applying molten zinc to aluminum while breaking down the aluminum oxide film on-said aluminum to form a predetermined layer of zinc aluminum alloy, forming the aluminum into an envelope, and then casting into said envelope a core of molten magnesium to fuse the surface of said alloy and establish a substantially uniform alloy bond between the aluminum and magnesium while controlling the relative temperatures of said aluminum and magnesium with respect to their relative heat capacities so as to predetermine the depth of alloy bond so formed. I
12. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum having alloyed to the inner face of said envelope a thin coating of zinc, and then fusing a core of magnesium to said thin coating to unite said magnesium to said aluminum by a magnesium-zinc-aluminum alloy.
13. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum having alloyed to the inner face of said envelope a thin coating of zinc, and then casting a core of molten magnesium into said envelope to form a fused bond with said thin coating and unite said magnesium to said aluminum by a magnesium-zinc-aluminum alloy.
14. The method of forming laminated billets and other bodies of aluminum coated magnesium which includes the steps of forming an envelope of aluminum having alloyed to the inner face of said envelope a thin coating of zinc, and. then casting a core of molten magnesium into said envelope to form a fused bond'with said thin coating and unite said magnesium to said aluminum by a magnesiumzinc-aluminum alloy while controllingthe relative temperatures of the aluminum and magnesium with respect to their relative heat capacities to predetermine the depth of alloy bond formed between said aluminum an magnesium. I l
15. A malleable ductile aluminum coatedmagnesium body composed of airelatively thin aluminum coating sheet having a zinc aluminum alloy layer at its inner face united to a magnesium core by a. substantially continuous bond of controlled thickness, said bond being composed of a relatively thin layer of aluminum, zinc and magnesium alloy substantially coextensive with the contiguous surfaces of the magnesium and aluminum and uniformly bonded to both of said metals.
CLAYTON E. LARSON.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US63031A US2100257A (en) | 1936-02-08 | 1936-02-08 | Composite body of magnesium and aluminum, and method of making same |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US63031A US2100257A (en) | 1936-02-08 | 1936-02-08 | Composite body of magnesium and aluminum, and method of making same |
Publications (1)
Publication Number | Publication Date |
---|---|
US2100257A true US2100257A (en) | 1937-11-23 |
Family
ID=22046454
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US63031A Expired - Lifetime US2100257A (en) | 1936-02-08 | 1936-02-08 | Composite body of magnesium and aluminum, and method of making same |
Country Status (1)
Country | Link |
---|---|
US (1) | US2100257A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2418265A (en) * | 1939-09-22 | 1947-04-01 | Sherka Chemical Co Inc | Process for providing aluminum and aluminum alloys with metal coatings |
US2735163A (en) * | 1956-02-21 | Composite magnesium-iron articles | ||
US2837207A (en) * | 1954-12-29 | 1958-06-03 | Rca Corp | Getter structure |
US2872028A (en) * | 1954-12-29 | 1959-02-03 | Rca Corp | Getter structure |
US2881514A (en) * | 1955-04-12 | 1959-04-14 | Ohio Commw Eng Co | Aluminized magnesium products and method of making |
US2987816A (en) * | 1956-12-10 | 1961-06-13 | Robert A Noland | Bonding aluminum metals |
US3133796A (en) * | 1961-07-19 | 1964-05-19 | Reynolds Metals Co | Composite aluminum material |
US3179504A (en) * | 1964-03-27 | 1965-04-20 | Dow Chemical Co | Composite body of magnesium and aluminum and method of making same |
US3841386A (en) * | 1971-04-01 | 1974-10-15 | I Niimi | Method of joining a beryllium workpiece to light metals |
US20080078521A1 (en) * | 2006-09-28 | 2008-04-03 | Gm Global Technology Operations, Inc. | Galvanic corrosion protection for magnesium components using cast-in-place isolators |
US20100015469A1 (en) * | 2008-07-16 | 2010-01-21 | Romanowski Christopher A | Method for twin roll casting of aluminum clad magnesium |
CN102441627A (en) * | 2010-10-12 | 2012-05-09 | 通用汽车环球科技运作有限责任公司 | Bimetallic forging forming method |
-
1936
- 1936-02-08 US US63031A patent/US2100257A/en not_active Expired - Lifetime
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2735163A (en) * | 1956-02-21 | Composite magnesium-iron articles | ||
US2418265A (en) * | 1939-09-22 | 1947-04-01 | Sherka Chemical Co Inc | Process for providing aluminum and aluminum alloys with metal coatings |
US2837207A (en) * | 1954-12-29 | 1958-06-03 | Rca Corp | Getter structure |
US2872028A (en) * | 1954-12-29 | 1959-02-03 | Rca Corp | Getter structure |
US2881514A (en) * | 1955-04-12 | 1959-04-14 | Ohio Commw Eng Co | Aluminized magnesium products and method of making |
US2987816A (en) * | 1956-12-10 | 1961-06-13 | Robert A Noland | Bonding aluminum metals |
US3133796A (en) * | 1961-07-19 | 1964-05-19 | Reynolds Metals Co | Composite aluminum material |
US3179504A (en) * | 1964-03-27 | 1965-04-20 | Dow Chemical Co | Composite body of magnesium and aluminum and method of making same |
US3841386A (en) * | 1971-04-01 | 1974-10-15 | I Niimi | Method of joining a beryllium workpiece to light metals |
US20080078521A1 (en) * | 2006-09-28 | 2008-04-03 | Gm Global Technology Operations, Inc. | Galvanic corrosion protection for magnesium components using cast-in-place isolators |
US7845388B2 (en) * | 2006-09-28 | 2010-12-07 | Gm Global Technology Operations, Inc. | Galvanic corrosion protection for magnesium components using cast-in-place isolators |
DE102007045818B4 (en) * | 2006-09-28 | 2018-11-15 | GM Global Technology Operations LLC (n. d. Ges. d. Staates Delaware) | A method of providing protection against galvanic corrosion for a magnesium or magnesium alloy component and a magnesium or magnesium alloy component prepared by the method |
US20100015469A1 (en) * | 2008-07-16 | 2010-01-21 | Romanowski Christopher A | Method for twin roll casting of aluminum clad magnesium |
US8122940B2 (en) | 2008-07-16 | 2012-02-28 | Fata Hunter, Inc. | Method for twin roll casting of aluminum clad magnesium |
CN102441627A (en) * | 2010-10-12 | 2012-05-09 | 通用汽车环球科技运作有限责任公司 | Bimetallic forging forming method |
US8980439B2 (en) * | 2010-10-12 | 2015-03-17 | GM Global Technology Operations LLC | Bimetallic forging and method |
CN102441627B (en) * | 2010-10-12 | 2015-05-13 | 通用汽车环球科技运作有限责任公司 | Bimetallic forging forming method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2100258A (en) | Composite body of copper and aluminum or copper and magnesium, and method of making same | |
US2100257A (en) | Composite body of magnesium and aluminum, and method of making same | |
US2908073A (en) | Method of bonding aluminous metal to dissimilar metal | |
US2301332A (en) | Aluminum clad magnesium and method of making same | |
JP2000073152A (en) | Production of superfine structure high strength metallic sheet by repeated lap joint rolling | |
US3206808A (en) | Composite-ingot casting system | |
US20110127003A1 (en) | Method for producing light alloy vehicle wheel | |
US2100255A (en) | Method of making composite bodies of zinc and aluminum | |
US2707323A (en) | Method of producing copper clad steel | |
US1865089A (en) | Corrosion-resistant aluminum alloy articles and method of making the same | |
US2993269A (en) | Methods for producing titanium-clad metal | |
US2166510A (en) | Method for coating metal with aluminum or the like | |
US3204917A (en) | Layered mold | |
US1001669A (en) | Compound metal body and process of making the same. | |
US2102394A (en) | Method of making composite ferrous metal articles | |
US3469301A (en) | Process for the production of bonded metal structures | |
US3046640A (en) | Process and product of zinc and aluminum lamination | |
US1043576A (en) | Clad metals and process of making same. | |
US2191470A (en) | Manufacture of veneered articles | |
US2100256A (en) | Method of making composite bodies of zinc and aluminum | |
US1757790A (en) | Process of making reenforced noncorrosive steel | |
US2195613A (en) | Means for producing composite metal products | |
US1359719A (en) | Method of making compound metallic articles | |
US2193246A (en) | Composite metal product | |
US1826860A (en) | Process of making products with welded faces of stable surface alloy |