US2982019A - Method of protecting magnesium with a coating of titanium or zirconium - Google Patents
Method of protecting magnesium with a coating of titanium or zirconium Download PDFInfo
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- US2982019A US2982019A US528271A US52827155A US2982019A US 2982019 A US2982019 A US 2982019A US 528271 A US528271 A US 528271A US 52827155 A US52827155 A US 52827155A US 2982019 A US2982019 A US 2982019A
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- magnesium
- titanium
- coating
- alloy
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- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 title claims description 49
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims description 25
- 229910052719 titanium Inorganic materials 0.000 title claims description 24
- 239000010936 titanium Substances 0.000 title claims description 24
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 title claims description 15
- 238000000034 method Methods 0.000 title claims description 15
- 229910052726 zirconium Inorganic materials 0.000 title claims description 12
- 229910052749 magnesium Inorganic materials 0.000 title description 23
- 239000011777 magnesium Substances 0.000 title description 23
- 239000011248 coating agent Substances 0.000 title description 21
- 238000000576 coating method Methods 0.000 title description 21
- 229910052751 metal Inorganic materials 0.000 claims description 93
- 239000002184 metal Substances 0.000 claims description 93
- 229910045601 alloy Inorganic materials 0.000 claims description 28
- 239000000956 alloy Substances 0.000 claims description 28
- 230000007797 corrosion Effects 0.000 claims description 19
- 238000005260 corrosion Methods 0.000 claims description 19
- 239000000463 material Substances 0.000 claims description 12
- 239000002131 composite material Substances 0.000 claims description 10
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 8
- 229910052725 zinc Inorganic materials 0.000 claims description 8
- 239000011701 zinc Substances 0.000 claims description 8
- 229910052793 cadmium Inorganic materials 0.000 claims description 4
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 3
- 239000010953 base metal Substances 0.000 description 19
- 150000002739 metals Chemical class 0.000 description 17
- 239000010410 layer Substances 0.000 description 13
- 229910000861 Mg alloy Inorganic materials 0.000 description 10
- 239000002585 base Substances 0.000 description 10
- 229910001069 Ti alloy Inorganic materials 0.000 description 5
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 238000005507 spraying Methods 0.000 description 4
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 3
- 229910052776 Thorium Inorganic materials 0.000 description 3
- 239000000470 constituent Substances 0.000 description 3
- 229910052735 hafnium Inorganic materials 0.000 description 3
- 230000000737 periodic effect Effects 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 description 2
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229940075397 calomel Drugs 0.000 description 2
- ZOMNIUBKTOKEHS-UHFFFAOYSA-L dimercury dichloride Chemical compound Cl[Hg][Hg]Cl ZOMNIUBKTOKEHS-UHFFFAOYSA-L 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 239000002923 metal particle Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910001029 Hf alloy Inorganic materials 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910001264 Th alloy Inorganic materials 0.000 description 1
- 229910001093 Zr alloy Inorganic materials 0.000 description 1
- KPZUWETZTXCDED-UHFFFAOYSA-N [V].[Cu] Chemical compound [V].[Cu] KPZUWETZTXCDED-UHFFFAOYSA-N 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 229910052783 alkali metal Inorganic materials 0.000 description 1
- 229910001515 alkali metal fluoride Inorganic materials 0.000 description 1
- 150000001340 alkali metals Chemical class 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 125000002915 carbonyl group Chemical group [*:2]C([*:1])=O 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000008199 coating composition Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005868 electrolysis reaction Methods 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 150000004673 fluoride salts Chemical class 0.000 description 1
- 150000002222 fluorine compounds Chemical class 0.000 description 1
- 238000001640 fractional crystallisation Methods 0.000 description 1
- 150000004820 halides Chemical class 0.000 description 1
- 150000004678 hydrides Chemical class 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- -1 jnickel Chemical compound 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000001465 metallisation Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000007747 plating Methods 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 230000003334 potential effect Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000011780 sodium chloride Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- WEQHQGJDZLDFID-UHFFFAOYSA-J thorium(iv) chloride Chemical compound Cl[Th](Cl)(Cl)Cl WEQHQGJDZLDFID-UHFFFAOYSA-J 0.000 description 1
- XJDNKRIXUMDJCW-UHFFFAOYSA-J titanium tetrachloride Chemical compound Cl[Ti](Cl)(Cl)Cl XJDNKRIXUMDJCW-UHFFFAOYSA-J 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
Images
Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L15/00—Devices or apparatus for measuring two or more fluid pressure values simultaneously
-
- 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
- B23K20/16—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating with interposition of special material to facilitate connection of the parts, e.g. material for absorbing or producing gas
-
- 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
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/001—Interlayers, transition pieces for metallurgical bonding of workpieces
- B23K35/002—Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of light metal
-
- 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
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/16—Composite materials, e.g. fibre reinforced
-
- 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
- Y10S428/937—Sprayed metal
-
- 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
- Y10S428/938—Vapor deposition or gas diffusion
-
- 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
- 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
-
- 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
-
- 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
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
Definitions
- This invention relates to duplex metal articles, and more particularly is concerned with the production of a duplex metal sheet or the like comprising a base of magnesium metal, or a magnesium alloy, having a layer of corrosion-resista t met l or metal alloy thereover which is highly resistant to corrosiqn,
- This application is a division of my copending application Serial No. 356,697, now US. Letters Patent No. 2,746,134.
- magnesium alloy sheets comprising a core of magnesium or magnesium alloy provided with a coating consisting of p re magnesium or a magnesium alloy which is more resistant to corrosive attack than the core metal.
- duplex metals have not been generally satisfactory be- ;,cause they possess the disadvantage that at any point where the core or base metal is exposed in contact with ,,th e coating metal, as, for example, along a cut edge of the sheet, or where the coating has been perforated, an ,electrolytic type of corrosion is set up which causes a preferential attack on the base metal resulting in an impairment of its structural properties.
- the preferred metal or alloy used is titanium, zirconium or alloys thereof wherein titanium or zirconium, or both, are the chief constituents.
- Other metals of group IV of the periodic table of elements e.g., hafnium, thorium, etc. may be substituted for all or a part of the titanium or zirconium, the high melting point metals of group IVA being preferred.
- the A subgroup of group IV comprises the elements titanium, zirconium, hafnium and thorium.
- Another object of the invention is to provide a duplex metal article in which the core or base metal is magnesium or magnesium alloy which is enclosed in a protective outer casing of a corrosion-resistant metal or suitable alloy thereof, the same being preferably welded or gas plated, or otherwise secured to the base metal so as to form a unitary laminated metal product.
- Another object is to provide a corrosion-resistant duplex metal article in which magnesium or various mag- .ne.si1 1m alloys may be. used .as the base, or core metal, and
- a magnesium sheet or article having improved corrosion-resistant properties over magnesium metal or its alloys.
- the invention comprises a composite metal body, which may be in the form of a sheet, tube or'rod or the like wherein the base metal or core comprises magnesium metal or a suitable alloy thereof and the sheath or covering layer of a corrosion-resistant metal as its principal constituent.
- the sheath or covering layer may constitute from about 8% to 60% ofthe weight 'of the composite metal sheet, rod or bar, but for most 'pur ⁇ poses the preferred proportion is about 10 to 25% or less of the weight of the composite product.
- One method of making a bonded composite sheet or rod is by coating the surface of the magnesium surface to be sheathed with molten metal, e.g. spraying molten metal such as zinc, cadmium, or alloys thereoffand then applying thereto a sheet or layer of titanium or zirconium metal.
- molten metal such as zinc, cadmium, or alloys thereoffand
- the magnesium sheet and corrosion-resistant sheet being superimposed one upon the other with the sprayed molten metal film at the interface, the superimposed sheets being heated to a temperature of about 600 to 700 F. or above, but below the melting point of the interface bonding metal.
- the superimposed sheets while still hot are passed one or more times between rolls adjusted to produce a substantial reduction in the thickness of the composite sheet. There results a magnesium base sheet hay.- ing a sheath of corrosion-resistant metal strongly bonded thereto.
- crushed sponge titanium metal which is cheaper than titanium alloy metals
- a suitable bonding agent such as molten metal may be employed to form the composite
- crushed and screened titanium sponge metal 300 mesh or finer
- titanium alloy particles which have a sufficiently low sintering temperature
- the same may be united to the magnesium metal surface by sintering.
- Titanium metal in a pure state has a melting point of aroundv 1800 F., so that the lower melting point of titanium alloy, as aforementioned, is preferably used for sintering purposes.
- Zirconium metal as produced by electrolysis of fits double alkali metal fluoride salt, or by reduction of the oxide with calcium metal, may be used.
- Hafnium is used associated with zirconium from which, if desired, it
- Thorium metal may be prepared by the action of alkali metal on the halide, e.g., thorium chloride.
- the corrosion-resistant metals are amphoteric and possess the common characteristic of raising the electrode potential of the magnesium with which they are alloyed. The reason why this particular group should exhibit this effect is not entirely clear, but probably has some relationship to their relative position in the periodic table. These metals raise the electrode potential of the magnesium in varying degree, depending, first, upon the particular metal or metals used and, second, upon' the particular amounts which may be added to the magnesium.
- the choice of the proper magnesium alloy to be used as the coating material in combination with any given magnesium metal base depends upon a predetermined knowledge of the electrode potential of the base metal in question. I
- the coating magnesium alloys containing one or more of the class of metals above described should have an electrode potential greater than that of the base metal. These different potentials are readily measured in accordance with methods long known in the art against a standard electrode. If the potential of the base metal is electro-negative with respect to the standard electrode, it is not necessary that the coating metal be eleetro-positive with respect to the standard electrode, but only that it be less electro-negative than the base metal in order to be satisfactory for the purpose of my invention. Therefore, throughout this specification and claims, where it is said that the electrode potentialof the coating metal should be higher than that of the base metal, it is meant that the coating metal should be more. electro-positive with respect to the standard electrode than is the base metal.
- a convenient standard electrode for measuring the po tential difference mentioned may be readily selected from those now in regular use for similar measurements.
- a calomel electrode has been selected as a standard.
- the magnesium metal to be tested is made one element of an electrolytic cell; the calomel is made the other element.
- the electrolyte is a normal solution of sodium chloride containing 0.3 percent by weight of hydrogen peroxide.
- the circuit is closed and the potential difference of the elements is measured on a potentiometer.
- Titanium metal powder useful in practicing this invention may be obtained from any suitable source and produced by different processes.
- One method of producing titanium metal is by the reduction of titanium tetrachloride with magnesium.
- the resultant titanium metal is recovered in the form of aspongy mass which is crushed to produce metal particles of'suitable size for incorporating into the coating composition.
- titanium alloy of aluminum and chromium is set out in an example illustrating the invention, it will 'be understood that other alloys of'titanium maybe employed. Titanium alloyed with up to of other metals, e.g. molybdenum, tungsten, jnickel, vanadium copper or iron, are illustrative of alloys which may also be used.
- corrosion-resistant metals as used in the specification and claims, in intended to include the metals and their alloys of the IV group of the periodic table and mixtures of metal particles wherein the metals of this group constitute the major constituent.
- the addition of one or more of the elements above described to the corrosion-resistant metal for the purpose of forming the protective coating or alloy may be made and in any suitable amount necessary to attain the desired electrode potential so long as other desirable properties of the magnesium itself are not materially impaired; and, likewise, other elements not deleteriously affecting the desired potential properties and other desirable characteristics of-the magnesium may be added.
- the following amounts of the metals of the 'class above described best serve the general purposes of this invention in producing the electrode potential desiredwithout materially impairing other desirable properties of the magnesium metal.
- mediate heatingincident-to such forming operations tends may be any magnesium metal having the properties which it is desired to obtain in the finished article.
- Various known alloys possessing known combination of properties may be used, such as a magnesium-base alloy comprising 6 to 7% aluminum, and less than 1% zinc, the remainder being magnesium.
- Other magnesium-base alloys commercially available which may be used besides magnesium are alloys containing tin (5%), zinc (4%) and manganese (1%), remainder magnesium. Also magnesium metal containing 1 to 3% manganese, with or without tin.
- Figure 1 is a perspective view of a duplex article or sheet having a core 10 of magnesium metal and an outer covering or layer 11 of titanium metal or alloy.
- Figure 2 is a view in cross-section, illustrating a duplex metal article in the form of a tube, and comprising a base metal 12 of iron, magnesium or the like with an inner layer or liner 13 consisting of titanium metal or alloy containing chiefly titanium.
- Figure 3 is a cross-sectional view of showing two sheets of metal 14 and 15 being rolled and reduced in thickness while bonding the pair of metal sheets together, one of the sheets as at 14 being designated as magnesium and reference character 15 representing titanium, zirconium or the like metal.
- Figure 4 illustrates in perspective and sectioned, a solid rod having a core 16 of magnesium having an outer'protective layer 17 of a suitable corrosion-resistant metal.
- Figure 5 is an enlarged cross-sectional view of a magnesium-base alloy sheet 18 having a layer 19 of titanium, zirconium or the like metal, which may be applied by spraying the metal thereon.
- the same may be deposited by gaseous metal deposition. This may be accomplished by employing a heat-decomposable carbonyl or hydride or an equivalent gaseous compound of the metal to be deposited and effecting the deposition as described in the U.S. patents to F. E. Drummond, see for example Nos. 2,332,309 and 2,344,138.
- duplex article of my invention any of the known methods of forming such duplex metal articles may be used.
- One method which ha's'been found particularly useful is to roll together the coating alloy and the base' alloy in sheet or slab form as illustrated in Figure 3. It is satisfactory to cast the base alloy in an ingot mold lined with the coating alloy.
- the article may then, if desired, be mechanically worked, as for example, by rolling or drawing or other suitable operation to form the particular type of duplexarticle desired, such as sheet,
- Duplex material may also be produced by spraying, gas plating or the like so as to provide the magnesium metal with an adherent coating of corrosionresistant metal or alloy. This method may be used to advantage where irregular shapes such as castings are to be coated.
- duplex articles of the invention may be provided on any one or all exposed surfaces with the protective coatingalloy, as for example are shown in Figures 1 and 2 of the drawing.
- Figure 1 shows a duplex article comprising a base 1 of a magnesium metal provided on its top and bottom surfaces with a magnesium alloy coating.
- a duplex metal article in tubular form comprising a base metal having an inner layer or coating of titanium metal. This type of material is useful, for example, in the manufacture of pipes used to conduct a material to magnesium metal.
- a method of protecting magnesium metal surfaces against corrosion which comprises-applying onsaidmagnesium metal moltenmetal selected frorn thegroup .con-
- a method of protecting magnesium metal surfaces against corrosion which comprises spraying on said magnesium metal molten metal selected from the group consisting of zinc, cadmium and alloys thereof, applying thereover a sheet of metal, selected from the group consisting of titanium and zirconium, heating the resultant sheet material to a temperature of about 600-700 F. and passing the heated sheet material through rolls under the application of pressure to produce a composite metal body of magnesium metal having a corrosion resistant outer surface metal layer.
- a method of protecting magnesium metal surfaces against corrosion which comprises applying on said magesium metal a molten layer of zinc, applying over said zinc metal a sheet of titanium metal, heating the resultant sheet material to a temperature of approximately 600- 700 F. and then passing the resultant metal product betvveen rolls while the same is heated to produce a composite metal body of magnesium metal having a corrosiou resistant outer surface metal layer.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Laminated Bodies (AREA)
Description
y 1961 F. E. DRUMMOND 2,982,019
METHOD OF PROTECTING MAGNESIUM WITH A COATING OF TITANIUM OF ZIRCONIUM Original Filed May 22, 1953 IN VEN TOR.
F OLSOM E DRUMMO/VD Ariorneys United States Patent 9 METHOD OF PROTECTING MAGNESIUM WITH A COATING F TITANIUM'OR ZIRCONIUM :Folsom .E. Qrummond, Washington, D.C., assignor, by n1esne assignments, to Union Carbide Corporation, New York, N.Y., a corporation of New York .3 Claims. (Cl. 29-492) This invention relates to duplex metal articles, and more particularly is concerned with the production of a duplex metal sheet or the like comprising a base of magnesium metal, or a magnesium alloy, having a layer of corrosion-resista t met l or metal alloy thereover which is highly resistant to corrosiqn, This application is a division of my copending application Serial No. 356,697, now US. Letters Patent No. 2,746,134.
a It has been proposed heretofore to produce magnesium alloy sheets comprising a core of magnesium or magnesium alloy provided with a coating consisting of p re magnesium or a magnesium alloy which is more resistant to corrosive attack than the core metal. Such duplex metals, however, have not been generally satisfactory be- ;,cause they possess the disadvantage that at any point where the core or base metal is exposed in contact with ,,th e coating metal, as, for example, along a cut edge of the sheet, or where the coating has been perforated, an ,electrolytic type of corrosion is set up which causes a preferential attack on the base metal resulting in an impairment of its structural properties. 7
This preferential or selective corrosive attack on the ,core metal will occur when the core metal has an elec- ;trode potential greater than that of the outer metal. Under these conditions a voltaic action may be set up be- ,tween the two metals in contact with the corroding mec lium and the resultant electrolytic action tends to dissolve the core metal. This type of corrosive action seriously restricts the use of magnesium and certain of the magnesium alloys as a core or base metal in the fabrication of duplex metal articles.
The preferred metal or alloy used is titanium, zirconium or alloys thereof wherein titanium or zirconium, or both, are the chief constituents. Other metals of group IV of the periodic table of elements, e.g., hafnium, thorium, etc. may be substituted for all or a part of the titanium or zirconium, the high melting point metals of group IVA being preferred. The A subgroup of group IV comprises the elements titanium, zirconium, hafnium and thorium.
It is an object of this invention to provide a duplex metal article consisting of a metal or alloy which corrodes readily (cg. when subjected to boiling glacial (99.5%) acetic acid), and which isprotected against this corrosive action by being provided with a sheath coating or covering of the metals or alloys of titanium, zirconium, hafnium and thorium.
Another object of the invention is to provide a duplex metal article in which the core or base metal is magnesium or magnesium alloy which is enclosed in a protective outer casing of a corrosion-resistant metal or suitable alloy thereof, the same being preferably welded or gas plated, or otherwise secured to the base metal so as to form a unitary laminated metal product.
Another object is to provide a corrosion-resistant duplex metal article in which magnesium or various mag- .ne.si1 1m alloys may be. used .as the base, or core metal, and
I product.
wherein the surfaces of the core metal are protected by a sheath comprising said corrosion-resistant metal or metal alloy, and wherein there is provided a lightweight metal article having the structural properties of the combined metals or alloys. A magnesium sheet or article is thus provided having improved corrosion-resistant properties over magnesium metal or its alloys.
Briefly, the invention comprises a composite metal body, which may be in the form of a sheet, tube or'rod or the like wherein the base metal or core comprises magnesium metal or a suitable alloy thereof and the sheath or covering layer of a corrosion-resistant metal as its principal constituent. The sheath or covering layer may constitute from about 8% to 60% ofthe weight 'of the composite metal sheet, rod or bar, but for most 'pur} poses the preferred proportion is about 10 to 25% or less of the weight of the composite product.
One method of making a bonded composite sheet or rod is by coating the surface of the magnesium surface to be sheathed with molten metal, e.g. spraying molten metal such as zinc, cadmium, or alloys thereoffand then applying thereto a sheet or layer of titanium or zirconium metal. The magnesium sheet and corrosion-resistant sheet being superimposed one upon the other with the sprayed molten metal film at the interface, the superimposed sheets being heated to a temperature of about 600 to 700 F. or above, but below the melting point of the interface bonding metal. The superimposed sheets while still hot are passed one or more times between rolls adjusted to produce a substantial reduction in the thickness of the composite sheet. There results a magnesium base sheet hay.- ing a sheath of corrosion-resistant metal strongly bonded thereto.
Using crushed sponge titanium metal, which is cheaper than titanium alloy metals, a suitable bonding agent such as molten metal may be employed to form the composite In this method crushed and screened titanium sponge metal (300 mesh or finer) is distributed as a powdered layer over the cleaned surface of the magnesium or magnesium alloy sheet and bonded therewith by the use of molten zinc, cadmium or a suitable alloy thereof, as described above. Where titanium alloy particles are used which have a sufficiently low sintering temperature, the same may be united to the magnesium metal surface by sintering. Titanium metal in a pure state has a melting point of aroundv 1800 F., so that the lower melting point of titanium alloy, as aforementioned, is preferably used for sintering purposes.
Zirconium metal, as produced by electrolysis of fits double alkali metal fluoride salt, or by reduction of the oxide with calcium metal, may be used. Hafnium is used associated with zirconium from which, if desired, it
. may be separated by fractional crystallization of the complex fluorides. Thorium metal may be prepared by the action of alkali metal on the halide, e.g., thorium chloride. The corrosion-resistant metals are amphoteric and possess the common characteristic of raising the electrode potential of the magnesium with which they are alloyed. The reason why this particular group should exhibit this effect is not entirely clear, but probably has some relationship to their relative position in the periodic table. These metals raise the electrode potential of the magnesium in varying degree, depending, first, upon the particular metal or metals used and, second, upon' the particular amounts which may be added to the magnesium. The choice of the proper magnesium alloy to be used as the coating material in combination with any given magnesium metal base depends upon a predetermined knowledge of the electrode potential of the base metal in question. I
The coating magnesium alloys containing one or more of the class of metals above described should have an electrode potential greater than that of the base metal. These different potentials are readily measured in accordance with methods long known in the art against a standard electrode. If the potential of the base metal is electro-negative with respect to the standard electrode, it is not necessary that the coating metal be eleetro-positive with respect to the standard electrode, but only that it be less electro-negative than the base metal in order to be satisfactory for the purpose of my invention. Therefore, throughout this specification and claims, where it is said that the electrode potentialof the coating metal should be higher than that of the base metal, it is meant that the coating metal should be more. electro-positive with respect to the standard electrode than is the base metal. While 'no fixed potential difference is required between the electrode potential of the base metal and that of the coating metal, a substantial protection may be given any base metal by a coating metal of higher electrode potential. It is generally desirable that there be a relatively wide difference inthe electrode potential of the two metals, since it has been found that with greater differences in potential there usually occurs less attack on the base metal, and by suitable adjustment of the potential difference it is possible to afford the base metal complete protection for all practical purposes.
A convenient standard electrode for measuring the po tential difference mentioned may be readily selected from those now in regular use for similar measurements. For the purpose of this description of the invention, a calomel electrode has been selected as a standard. In measuring the electrode potential in question, the magnesium metal to be tested is made one element of an electrolytic cell; the calomel is made the other element. The electrolyte is a normal solution of sodium chloride containing 0.3 percent by weight of hydrogen peroxide. The circuit is closed and the potential difference of the elements is measured on a potentiometer.
Titanium metal powder useful in practicing this invention may be obtained from any suitable source and produced by different processes. One method of producing titanium metal is by the reduction of titanium tetrachloride with magnesium. The resultant titanium metal is recovered in the form of aspongy mass which is crushed to produce metal particles of'suitable size for incorporating into the coating composition.
Although a titanium alloy of aluminum and chromium is set out in an example illustrating the invention, it will 'be understood that other alloys of'titanium maybe employed. Titanium alloyed with up to of other metals, e.g. molybdenum, tungsten, jnickel, vanadium copper or iron, are illustrative of alloys which may also be used.
The term corrosion-resistant metals, as used in the specification and claims, in intended to include the metals and their alloys of the IV group of the periodic table and mixtures of metal particles wherein the metals of this group constitute the major constituent.
The addition of one or more of the elements above described to the corrosion-resistant metal for the purpose of forming the protective coating or alloy may be made and in any suitable amount necessary to attain the desired electrode potential so long as other desirable properties of the magnesium itself are not materially impaired; and, likewise, other elements not deleteriously affecting the desired potential properties and other desirable characteristics of-the magnesium may be added. In general, the following amounts of the metals of the 'class above described best serve the general purposes of this invention in producing the electrode potential desiredwithout materially impairing other desirable properties of the magnesium metal.
"my' invention derives its principal structural properties,
'rodorother form of material.
mediate heatingincident-to such forming operations tends may be any magnesium metal having the properties which it is desired to obtain in the finished article. Various known alloys possessing known combination of properties may be used, such as a magnesium-base alloy comprising 6 to 7% aluminum, and less than 1% zinc, the remainder being magnesium. Other magnesium-base alloys commercially available which may be used besides magnesium are alloys containing tin (5%), zinc (4%) and manganese (1%), remainder magnesium. Also magnesium metal containing 1 to 3% manganese, with or without tin.
In the drawing:
Figure 1 is a perspective view of a duplex article or sheet having a core 10 of magnesium metal and an outer covering or layer 11 of titanium metal or alloy.
Figure 2 is a view in cross-section, illustrating a duplex metal article in the form of a tube, and comprising a base metal 12 of iron, magnesium or the like with an inner layer or liner 13 consisting of titanium metal or alloy containing chiefly titanium.
Figure 3 is a cross-sectional view of showing two sheets of metal 14 and 15 being rolled and reduced in thickness while bonding the pair of metal sheets together, one of the sheets as at 14 being designated as magnesium and reference character 15 representing titanium, zirconium or the like metal.
Figure 4 illustrates in perspective and sectioned, a solid rod having a core 16 of magnesium having an outer'protective layer 17 of a suitable corrosion-resistant metal.
Figure 5 is an enlarged cross-sectional view of a magnesium-base alloy sheet 18 having a layer 19 of titanium, zirconium or the like metal, which may be applied by spraying the metal thereon.
As an alternative method of applying the corrosionresistant metal over magnesium metal surfaces, the same may be deposited by gaseous metal deposition. This may be accomplished by employing a heat-decomposable carbonyl or hydride or an equivalent gaseous compound of the metal to be deposited and effecting the deposition as described in the U.S. patents to F. E. Drummond, see for example Nos. 2,332,309 and 2,344,138.
In forming the duplex article of my invention, any of the known methods of forming such duplex metal articles may be used. One method which ha's'been found particularly useful is to roll together the coating alloy and the base' alloy in sheet or slab form as illustrated in Figure 3. It is satisfactory to cast the base alloy in an ingot mold lined with the coating alloy. The article may then, if desired, be mechanically worked, as for example, by rolling or drawing or other suitable operation to form the particular type of duplexarticle desired, such as sheet,
' The working with interto improve the bond between the coating metal and the base metal. Duplex material may also be produced by spraying, gas plating or the like so as to provide the magnesium metal with an adherent coating of corrosionresistant metal or alloy. This method may be used to advantage where irregular shapes such as castings are to be coated.
The duplex articles of the invention may be provided on any one or all exposed surfaces with the protective coatingalloy, as for example are shown in Figures 1 and 2 of the drawing. Figure 1 shows a duplex article comprising a base 1 of a magnesium metal provided on its top and bottom surfaces with a magnesium alloy coating. In Figure 2, a duplex metal article in tubular form comprising a base metal having an inner layer or coating of titanium metal. This type of material is useful, for example, in the manufacture of pipes used to conduct a material to magnesium metal.
What is claimed is:
l. A method of protecting magnesium metal surfaces against corrosion, which comprises-applying onsaidmagnesium metal moltenmetal selected frorn thegroup .con-
sheet material to a temperature of about GOO-700 F.
and passing the heated sheet material through rolls under.
the application of pressure to produce a composite metal body of magnesium metal having a corrosion resistant outer surface metal layer.
2. A method of protecting magnesium metal surfaces against corrosion which comprises spraying on said magnesium metal molten metal selected from the group consisting of zinc, cadmium and alloys thereof, applying thereover a sheet of metal, selected from the group consisting of titanium and zirconium, heating the resultant sheet material to a temperature of about 600-700 F. and passing the heated sheet material through rolls under the application of pressure to produce a composite metal body of magnesium metal having a corrosion resistant outer surface metal layer.
3. A method of protecting magnesium metal surfaces against corrosion, which comprises applying on said magesium metal a molten layer of zinc, applying over said zinc metal a sheet of titanium metal, heating the resultant sheet material to a temperature of approximately 600- 700 F. and then passing the resultant metal product betvveen rolls while the same is heated to produce a composite metal body of magnesium metal having a corrosiou resistant outer surface metal layer.
References Cited in the file of this patent UNITED STATES PATENTS 1,709,781 DeBoer et al Apr. 16, 1929 1,733,813 Marden etal. Oct. 29, 1929 2,100,258 Larson Nov. 23, 1937 2,301,332 Scheller Nov. 10, 1942 2,366,168 Bakarian Jan. 2, 1945 2,463,010 Almen Mar. 1, 1949 2,477,279 Anderson July 26, 1949 2,491,284 Sears Dec. 13, 1949 2,536,673 Widell Jan. 2, 1951 2,588,421 Shepard Mar. 11, 1952 2,682,702 Fink July 6, 1954 2,685,124 Toulmin Aug. 3, 1954 2,704,727 Pawlyk Mar. 22, 1955 2,706,153 Glasser Apr." 12, 1955 2,713,196 Brown July 19, 1955 2,746,888 Ross May 22, 1956 2,772,985 Wainer Dec. 4, 1956
Claims (1)
1. A METHOD OF PROTECTING MAGNESIUM METAL SURFACES AGAINST CORROSION, WHICH COMPRISES APPLYING ON SAID MAGNESIUM METAL MOLTEN METAL SELECTED FROM THE GROUP CONSISTING OF ZINC, CADMIUM AND ALLOYS THEREOF, APPLYING THEREOVER A SHEET OF METAL, SELECTED FROM THE GROUP CONSISTING OF TITANIUM AND ZIRCONIUM, HEATING THE RESULTANT SHEET MATERIAL TO A TEMPERATURE OF ABOUT 600-700*F. AND PASSING THE HEATED SHEET MATERIAL THROUGH ROLLS UNDER THE APPLICATION OF PRESSURE TO PRODUCE A COMPOSITE METAL BODY OF MAGNESIUM METAL HAVING A CORROSION RESISTANT OUTER SURFACE METAL LAYER.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US528271A US2982019A (en) | 1953-05-22 | 1955-08-15 | Method of protecting magnesium with a coating of titanium or zirconium |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US356697A US2746134A (en) | 1953-05-22 | 1953-05-22 | Duplex metal sheet or article |
| US528271A US2982019A (en) | 1953-05-22 | 1955-08-15 | Method of protecting magnesium with a coating of titanium or zirconium |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2982019A true US2982019A (en) | 1961-05-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US528271A Expired - Lifetime US2982019A (en) | 1953-05-22 | 1955-08-15 | Method of protecting magnesium with a coating of titanium or zirconium |
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| Country | Link |
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| US (1) | US2982019A (en) |
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| US3256072A (en) * | 1961-10-03 | 1966-06-14 | United States Borax Chem | Abrasion resistant materials |
| US3293009A (en) * | 1962-05-08 | 1966-12-20 | Nat Res Corp | Niobium stannide superconductor product |
| US3295935A (en) * | 1958-07-22 | 1967-01-03 | Texas Instruments Inc | Composite stock comprising a plurality of layers of alloying constituents, each layerbeing less than 0.001 inch in thickness |
| US3479730A (en) * | 1964-03-25 | 1969-11-25 | Linde Ag | Method of and assembly for the joining of elements of different materials |
| US3991929A (en) * | 1972-09-22 | 1976-11-16 | Imperial Chemical Industries Limited | Coating and bonding of metals |
| US5943772A (en) * | 1997-08-19 | 1999-08-31 | Brazeway, Inc. | Method of cladding tubing and manufacturing condensor cores |
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