US2588421A - Application of sprayed metal coatings to solid objects - Google Patents
Application of sprayed metal coatings to solid objects Download PDFInfo
- Publication number
- US2588421A US2588421A US792835A US79283547A US2588421A US 2588421 A US2588421 A US 2588421A US 792835 A US792835 A US 792835A US 79283547 A US79283547 A US 79283547A US 2588421 A US2588421 A US 2588421A
- Authority
- US
- United States
- Prior art keywords
- metal
- molybdenum
- sprayed
- coating
- spray
- 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
- 229910052751 metal Inorganic materials 0.000 title claims description 154
- 239000002184 metal Substances 0.000 title claims description 154
- 238000000576 coating method Methods 0.000 title claims description 76
- 239000007787 solid Substances 0.000 title description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 82
- 239000011733 molybdenum Substances 0.000 claims description 78
- 229910052750 molybdenum Inorganic materials 0.000 claims description 78
- 239000007921 spray Substances 0.000 claims description 70
- 239000011248 coating agent Substances 0.000 claims description 63
- 238000005507 spraying Methods 0.000 claims description 47
- 238000000034 method Methods 0.000 claims description 46
- 230000006872 improvement Effects 0.000 claims description 14
- 230000003750 conditioning effect Effects 0.000 claims description 12
- 239000011521 glass Substances 0.000 description 16
- 238000007788 roughening Methods 0.000 description 12
- 239000010959 steel Substances 0.000 description 12
- 229910000831 Steel Inorganic materials 0.000 description 11
- 150000002739 metals Chemical class 0.000 description 11
- 229910000897 Babbitt (metal) Inorganic materials 0.000 description 10
- 229910052782 aluminium Inorganic materials 0.000 description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 10
- 238000010438 heat treatment Methods 0.000 description 10
- 238000000227 grinding Methods 0.000 description 9
- 239000000203 mixture Substances 0.000 description 9
- 238000002360 preparation method Methods 0.000 description 9
- 229910045601 alloy Inorganic materials 0.000 description 8
- 239000000956 alloy Substances 0.000 description 8
- 229910000677 High-carbon steel Inorganic materials 0.000 description 7
- 238000003754 machining Methods 0.000 description 7
- 229910000906 Bronze Inorganic materials 0.000 description 6
- 229910001182 Mo alloy Inorganic materials 0.000 description 6
- 238000005422 blasting Methods 0.000 description 6
- 239000010974 bronze Substances 0.000 description 6
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 6
- 229910052755 nonmetal Inorganic materials 0.000 description 6
- 239000004576 sand Substances 0.000 description 6
- 238000012360 testing method Methods 0.000 description 6
- 229910000975 Carbon steel Inorganic materials 0.000 description 5
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 5
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 5
- 239000010953 base metal Substances 0.000 description 5
- 239000000919 ceramic Substances 0.000 description 5
- 238000010291 electrical method Methods 0.000 description 5
- 239000002245 particle Substances 0.000 description 5
- 239000011135 tin Substances 0.000 description 5
- 229910052718 tin Inorganic materials 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 239000010962 carbon steel Substances 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 230000001788 irregular Effects 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 229910052709 silver Inorganic materials 0.000 description 4
- 239000004332 silver Substances 0.000 description 4
- -1 Ineonel and the like Inorganic materials 0.000 description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- 229910000861 Mg alloy Inorganic materials 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 210000003746 feather Anatomy 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 238000005488 sandblasting Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 229910001220 stainless steel Inorganic materials 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 229910000851 Alloy steel Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000002826 coolant Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005530 etching Methods 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 239000011133 lead Substances 0.000 description 2
- 239000000314 lubricant Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- MGRWKWACZDFZJT-UHFFFAOYSA-N molybdenum tungsten Chemical compound [Mo].[W] MGRWKWACZDFZJT-UHFFFAOYSA-N 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 229910052573 porcelain Inorganic materials 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000009877 rendering Methods 0.000 description 2
- 238000010008 shearing Methods 0.000 description 2
- 238000013517 stratification Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910000792 Monel Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 241001275902 Parabramis pekinensis Species 0.000 description 1
- 229910000978 Pb alloy Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- IUWCPXJTIPQGTE-UHFFFAOYSA-N chromium cobalt Chemical compound [Cr].[Co].[Co].[Co] IUWCPXJTIPQGTE-UHFFFAOYSA-N 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 229910010272 inorganic material Inorganic materials 0.000 description 1
- 239000011147 inorganic material Substances 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- LQBJWKCYZGMFEV-UHFFFAOYSA-N lead tin Chemical compound [Sn].[Pb] LQBJWKCYZGMFEV-UHFFFAOYSA-N 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000002203 pretreatment Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 229910000679 solder Inorganic materials 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 229910001256 stainless steel alloy Inorganic materials 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
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/08—Metallic material containing only metal elements
-
- 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
- Y10S384/00—Bearings
- Y10S384/90—Cooling or heating
- Y10S384/912—Metallic
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49643—Rotary bearing
- Y10T29/49647—Plain bearing
- Y10T29/49668—Sleeve or bushing making
- Y10T29/49677—Sleeve or bushing making having liner
-
- 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
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49705—Coating or 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49709—Specific metallic composition
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
-
- 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
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/266—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension of base or substrate
Definitions
- This invention relates to new and useful improvements in the application of sprayed metal coatings to solid objects.
- metal spraying is carried out with the use of metal spray guns, 1. e., devices in which the metal is fed to a heating zone from which zone metal particles, at least some of which are molten or in a heat plastic condition, are propelled against the surface to be sprayed. The propulsion may be effected either by centrifugal means or by means of a blast of air or other gas.
- metal spray guns 1. e., devices in which the metal is fed to a heating zone from which zone metal particles, at least some of which are molten or in a heat plastic condition, are propelled against the surface to be sprayed. The propulsion may be effected either by centrifugal means or by means of a blast of air or other gas.
- One of the most widely used forms of spraying device is a metal spray 'gun utilizing the metal to be sprayed in the form of a rod or wire which is fed by a suitable feed mechanism into a heating zone" which is produced by the combustion of a combustible and a combustion supporting gas.
- Such rod or wire may be a relatively solid rod or wire of such metal, or alternatively it may be composed of particles of such metal bonded together by a suitable binder such as a plastic material.
- a suitable binder such as a plastic material.
- the binder is usually of the kind which will volatilize as the result of the applied 1 heat of the spray gun.
- sprayed metal is carried out for a variety of purposes, as for example to protect a surface, such as a shaft or sleeve surface against corrosion, to provide a coating of the desired ornamental or bearing characteristics or to build up worn sections of parts.
- the surface to which the spray metal is to be applied is as a rule suitable pre-conditioned.
- pro-conditioning treatment has been generally of two kindsroughening and heating.
- Roughening has been carried out by me hanical roughenspray metal must be of a type involving the formation of a multiple number of closely spaced cavities with peened and splayed edges and interspaces forming a multitude of key ways.
- the most common method of procuring such type surfaces has been by sand or grit blasting.
- Sand or grit blasting is in many cases unsatisfactory and will often not yield a surface capable of bonding applied spray metal with a satisfactory degree of bond.
- Spray metal has a tendency to shrink and in many cases a sand or grit blasted surface does not provide a sufficient bonding surface to prevent the separation of the applied metal coating from the base particularly under working conditions.
- many machine parts or the like due to their configuration or their structural relation to other parts, are unsuitable for sand or grit blasting.
- One of the basic disadvantages of the sand or grit blasting procedure is due to the fact that the blasting causes compressive stresses in the blasted surface which frequently results in warpage of the object blasted, particularly where such object has a relatively thin section.
- An alternative form of mechanical surface roughening for spray metal bonding purposes is that of machine roughening a surface to be sprayed in a particular manner designed to procure the above mentioned surface characteristics essential for spray metal bonding.
- This surface roughening method is such that it has the same inherent limitations and drawbacks as the ones involving sand or grit blasting.
- This limitation re ,beproperly surface-conditioned by mechanical roughening procedures, such as grit or sand blasting or rough machining. Though partly hardened mechanical parts have been prepared by grit or sand blasting, using very hard grit such as aluminum oxide abrasive, nevertheless the bond obtained is usually very unsatisfactory.
- Such heating frequently causes localized changes in the metal structure of the base which materially reduces the fatigue strength of the base metal.
- Another disadvantage of the electrical method of fusing or welding electrode metal to a base metal to produce a roughened surface is due to the fact that such electrical method tends to produce tensile stress in the surface of the object treated and such stresses frequently cause warpage, particularly on an object that has a relatively thin section.
- the heating method of surface conditioning a metallic base to bond thereto applied spray metal involves the heating of the surface to a relatively high temperature and thereafter spraying the hot surface with metal.
- This method is not widely used and requires, as a general rule, considerable skill and elaborate equipment and is relatively expensive.
- the temperature to which the surface or base must be heated is so high that it tends to warp or otherwise destroy the article e to which the metal spray is to be applied.
- a further limitation in the method of heating to produce bonding resides in the fact that most metals oxidize to an objectionable degree when heated in air.
- Another limitation inherent in the heating method is the fact that it is not feasible for use on most hardened metal articles as they will soften and thus lose their hardness if they are heated to the temperatures necessary to secure the desired degree of bonding to the spray metal applied thereto.
- One object of the invention comprises, inter alia, a method for applying spray metal to surfaces of inorganic materials including surfaces of metal and non-metal, and of the latter preferably vitreous surfaces such as glass or ceramic, which method is substantially free from the aforementioned limitations inherent in hitherto known practices.
- Another object of this invention is to provide a method for bonding spray metal to surfaces and particularly to surfaces of metal and nonmetal vitreous surfaces such as glass and other vitreous surfaces including ceramics, which does not materially affect more than a thin skin of the surface to which the spray metal is applied.
- a further object of the invention is the novel spray metal coated articles inwhich the spray metal adheres to the base surface in a novel manner and with a high degree of bond.
- the invention is essentially an improvement in the method for aplying spray metal to an inorganic surface, particularly a surface of metal or of non-metal vitreous material, with a high degree of bond, which comprises conditioning such surface for spray metal bonding by spraying at least a flash coating of molybdenum thereon and thereafter spraying metal onto the thusly coated surface.
- the invention is'particularly applicable to surfaces which are usually not adapted to receive and retain applied spray metal with a desired degree of bond, such as for example relatively smooth surfaces. No other conditions or heating treatment need be applied.
- the molybdenum sprayed onto the surface, to be thereafter coated with spray metal maybe applied to any desired thickness.
- a flash coating of the molybdenum suffices, i. e., a relatively thin coating as may be obtained, for instance, by a relatively rapid once-or-twiceover application of the molybdenum spraying gun and not necessarily presenting a continuous coating.
- the inven tion at least .0005 inch and preferably .002 inch of substantially continuous molybdenum coating is recommended.
- the upper limit of the molybdenum coating is only dictated by practical and economical considerations. Once a coating thickness of the desired bonding characteristics is applied, any additional thickness will not further substantially improve the bonding characteristics of the molybdenum layer.
- the metal spraying is preferably carried. out by use of a metal spray gun, using wire or rod as a source of metal.
- the molybdenum that I may use in accordance with my invention may be pure molybdenum or a molybdenum alloy or composition. In the latter case I prefer a relatively high molybdenum content, such as an alloy or composition having or more molybdenum. I may, however, use any alloy of molybdenum having 40% or greater molybdenum content and alloyedwith any other metals which are known to alloy with molybdenum. I
- molybdenum is used herein, it is intended to designate thereby substantially pure molybdenum as well as alloys or compositions containing at least 40% molybdenum.
- a molybdenum composition I mean thereby a composition containing finely divided metallic molybdenum in combination with not necessarily alloyed therewith.
- the surface of the object to be metal sprayed may be perfectly smooth andno roughening or other conditioning treatment other than cleaning (if necessary) is required.
- the surface to be sprayed upon with molybdenum should, however, be a clean surface. Cleaning may be accomplished satisfactorily in numerous ways, such as by abrasion, light sand blasting, acid etching, and the like procedures. These are particularly to be used with metals when there is any danger of oxides being present on the surface. If the surface is relatively clean of oxides and is merely to be freed from dirt particles or greasy matter, it may sufiice if the same is cleaned with a suit able solvent or the like.
- the degree of adhesion of the applied spray metal to the base may be further enhanced, if desired, if the glass surface is slightly abraded or frosted as by etching, light grinding or the like. This may be particularly advantageous when spraying onto a relatively cool glass surface to counteract or ameliorate the effects of possible heat shock.
- Any metal which is capable of being sprayed may then be sprayed directly onto the molybdenum sprayed surface.
- the final metal to be sprayed is selected according to its characteristics to meet the requirements of the particular job being done.
- the journal of a rotating shaft may require a hard, dense metal to operate in a journal bearing.
- a common metal to use would be high carbon steel.
- the journal would first be sufficiently un- 1-.
- a suitable molybdenum would then be metal sprayed onto the undercut surface of the shaft to a thickness of, for instance, .001 inch to .003 inch, and thereafter the high carbon steel would be metal sprayed onto the journal section to a sufficient thickness to permit machining or grinding of the metal sprayed surface to a desired final journal size.
- the preheating tends to reduce the stress in the final sprayed-on coating and is carried out at relativel low temperatures (as compared with temperatures required by heat bonding methods).
- the preheating temperatures are of the order of magnitude of about 300 F.
- mild preheating may sometimes be advantageous to reduce the effect of heat shock on the glass. Heat shock sometimes results, when spraying on glass, at localized points where particles of hot sprayed metal strike .the cold glass and cause strains which may subsequently become the focal points of localized fractures.
- grooves and ridges or other forms of an irregular contour on the surface of the base are also at times of advantage.
- Such grooves or other irregular contours have several advantageous functions although they are not a necessary requirement of the bonding procedure set forth in this invention.
- One of the advantageous functions of grooves Or other irregular contours of the base is the increase in surface area which such contours provide, which results in an increase bond to the sprayed metal due to such increased area. of bonding.
- Another advantageous function of such contours is the beneficial effect on the structure of the sprayed metal layer. Such beneficial effect is due to the folding of the stratification layers of such sprayed metal structure. Sprayed metal structures resulting from spraying onto a surface with an irregular contour are generally stronger due to the folding of stratifications or laminations than the structures resulting from the spraying of the same metal onto a substantially even surface.
- One of the primary commercial advantages of this invention resides not only in the cost saving that results from the elimination of the previously required surface preparation step but frequently also in the saving of the spraying of the additional metal necessary to fill the intricacies and other spaces provided by roughening methods of surface preparation and also the saving in the additional time and expense required in machining or grinding the final sprayed metal. surface.
- roughening methods are used, the rough contours of the base are partially reproduced on the final surface and must be removed by machining or otherwise if an even surface is to result.
- molybdenum or a. molybdenum alloy or composition for the first coating applied to the surface of the object, but also to use the same or a different molybdenum or molybdenum alloy or composition for the subsequently applied spray metal coating.
- the entire coating could be of the same molybdenum or molybdenum alloy.
- molybdenum for the subsequent- 1y applied sprayed metal layer is particularly advantageous for thin coatings such as could be used for restoring worn pressed fit areas of a shaft which is pressed into a hub. In such cases, it is unnecessary to undercut the shaft by machining or grinding in the usual manner since no additional minimum space is required for the sprayed metal.
- the worn areas are sprayed with molybdenum and thereafter ground to size. This practice produces very thin coatings with feather edges as they approach the ends of the worn area. This cannot be satisfactorily done with previously known methods of spray metal bonding by surface preparation.
- Example 1 A carbon steel shaft having a carbon content of .45% is first mounted in a lathe and the area to be built up with sprayed metal is first reduced in diameter by a cutting tool to a diameter such as to leave sufficient space for the desired thickness of the thereafter-to-beapplied sprayed metal coating.
- the desired coating is to be approximately .030 inch thick and it is desired that the finished sprayed metal coating be flush with the original diameter of the shaft. Therefore the original diameter of the shaft is undercut to .060 inch smaller in diameter than the original throughout the area to be sprayed.
- the cutting with the tool in the lathe is done dry without use of lubricant or coolants so as to avoid contamination of the metal surface.
- a flash coating in this case approximately .091 inch diameter sintered and drawn molybdenum wire.
- the gun nozzle is held at a distance of about 5 inches from the surface of the shaft.
- the gun is adjusted so as not to have an excessively oxidizing type flame.
- the shaft is rotated in the lathe and the gun is moved so as to cause the spray to rapidly traverse the surface of the shaft in order to apply the desired thickness of molybdenum in about two passes of the spray.
- a sprayed metal coating of an 18-8 type stainless steel is applied.
- This coating is applied using the same metallizing gun, a /8" diameter wire of stainless steel being utilized in the gun and employing a standard spraying procedure by moving the spraying gun back and forth over the rotating shaft sufiiciently rapidly to produce layers of approximately .005 inch thick with each pass of the gun.
- the gun is held with its nozzle approximately 6 inches distant from the surface of the shaft.
- the spraying is continued until the coating has been built up to a diameter approximately .015 inch larger than the original shaft diameter.
- the sprayed stainless steel coating is ground to the original shaft diameter, utilizing conventional grinding equipment for the purpose.
- Example 2 .003 inch thick, of molybdenum is then applied by spraying onto the clean surface of the plate.
- the spraying is done by the use of a conventional spray gun of the wire feed type and molybdenum wire approximately .091 inch in diameter is used.
- the coating is applied by moving the gun so as to cause the spray to traverse the plate at a rate to apply the molybdenum coating in about five passes, holding the gun at a distance of approximately 6 inches.
- High carbon steel containing approximately .80% carbon is then sprayed onto the sprayed metal surface on the plate using the same metal spray gun and a /8 inch steel wire.
- the gun is operated in a conventional manner and a coating is applied by moving the gun so as to cause the spray to traverse the work at a rate such as to deposit between about .003 inch and .005 inch steel at a pass.
- the spraying is continued until a thickness of approximately /8 inch of spray metal coating is obtained on the plate.
- Example 3 A plate similar to the one prepared in Example 2 is prepared in the same manner and sprayed with a molybdenum layer in the same manner as set forth in Example 2. After the spraying of the molybdenum layer, a coating of aluminum bronze (approximately 9% aluminum) is applied, using the same metal spray gun and applying it in the same manner as described above in Example 2 for the application of high carbon steel. The aluminum bronze is applied to the same final thickness of approximately /8 inch.
- aluminum bronze approximately 9% aluminum
- Example 4 As a means of evaluating the bond strength between the applied spray metal coatings and the base, the following test is conducted:
- Plates are prepared, as set forth above in Examples 2 and 3. These plates consist of mild steel plates with thin coatings of sprayed molybdentun and coatings approximately A; inch of high carbon steel and aluminum bronze respectively. One end of each plate is smoothed so as to expose the boundary between the sprayed metal and the base. Pieces of these coatings are removed from the steel plates by placing the sharp point of a chisel at the edge of the ground surface of the plate at the boundary between the sprayed metal coating and the base and driving the chisel. Both the removed pieces of coating and the exposed surface of the base are then examined.
- the pieces of sprayed high carbon steel show continuous coatings of sprayed molybdenum on the side of the piece adjacent the plate, and the plate to which they were bonded also shows a continuous coating of molybdenum.
- the pieces of aluminum bronze show no evidence of molybdenum on the surface adjacent the plate, and the plate from which they were removed shows a continuous coating of aluminum bronze covering the sprayed molybdenum coating.
- the test shows that the strength of the molybdenum layer in a direction perpendicular to the plate is stronger than the internal strength of the sprayed aluminum bronze in the'same direction but weaker than the strength of the sprayed high carbon steel in this direction.
- Example 5 The following further shows the strength with 9 through the center of the rod.
- a cold finished mild steel rod substantially closely but slidably fitting the bar, is then inserted to project slightly beyond the first end and leaving a handle portion at the second end.
- the rod is then secured in this position in the axial bore and is ground flush with the first end to a smooth finish.
- a .003 inch application of sprayed molybdenum is made on the ground surface covering the entire first end including the flush end of the rod.
- the rod is then pulled back, thereby shearing with a relatively sharply defined edge, the coating over the rod end from the coating over the first end of the bar.
- the rod After removal of any surface burrs the rod is replaced to its original position with the molybdenum surfaces fiush with each other. .10% carbon steel is then sprayed, in the manner set forth in Example 2, to a thickness of about /8 inch.
- the thusly prepared test piece is then placed in a testing device in which measurable pull is exerted on the handle portion of the rod and the amount of pull in pounds is observed which is required to break the rod from the applied spray metal. In this case the total pull required divided by the area of the sprayed end of the rod gives the tensile strength in pounds per square inch of the bond between the rod surface and applied spray metal. strength in tension is about 2000 pounds per square inch. Failure takes place within the molybdenum coating.
- the metal spray gun of the wire feed type used in the above described examples is one having a normal capacity for spraying about 10 pounds of a inch .10% carbon steel wire per hour. Guns of different capacity or other metal sprayingdevices of different type may be used, in which case the particular operating conditions are to be adapted to those regulating the normal spraying procedure of the particular equipment used, and if necessary with the additional provision of appropriate safeguards or adjustment to avoid excessive oxidizing conditions.
- any number of bases in combination with any number of applied spray metals may be prepared in accordance with the invention.
- Test pieces of various combinations which were prepared utilizing the equipment and procedures set forth in the preceding examples, showed in each case satisfactory adhesion of the applied spray metal to the base, failure usually occurring by fracture in either the molybdenum or the superim- In this case the bond Other posed spray metal.
- suitable base metals for instance include steel, carbon steel and other steel and iron alloys either in the soft or hardened condition, including cast iron, nickel and the various nickel alloys such as Monel, Ineonel and the like, copper and various copper alloys including brass, zinc, lead, tin, aluminum and aluminum alloys, magnesium and magnesium alloys, chromium cobalt and/or tungsten compositions or alloys.
- the following spray metals may be applied to these bases: aluminum and aluminum alloys, copper and copper alloys, including bronzes and brasses, steel, steel alloys including various carbon steels and also including stainless steel alloys, iron, zinc, lead and lead alloys including babbitt, tin and various other metals conventionally used for metal spraying.
- the same has proven useful for a variety of purposes, particularly in such cases as the repair of cylinder cracks, cracks across valve seats, filling cracks, defects or blow-holes in castings, etc.
- the products obtained in accordance with the invention show a relatively high resistance to corrosive influence upon the surface of the base. They are further characterized by relatively high shear strength, i. e., resistance to shearing forces exerted in a direction parallel to the surface direction of the base.
- the molybdenum is applied in essentially the same manner as specified in the hereinabove enumerated examples, using essentially the same spraying technique and equipment.
- the ultimately applied spray metal adheres to the base with a high degree of bond and no surface preparation of pre-treatment other than cleaning is necessary.
- Example 6 The surface of a glass-lined steel tank from which a portion of the glass had been accidently chipped is desired to be repaired.
- the crack should be enlarged sufficiently to permit easy application of the metal spray by means of a small portable grinder.
- the edges of the glass should be ground to a taper and an area surrounding the defect should be ground slightly.
- a flash coating of molybdenum just thick enough to completely cover the surface of the defect is applied by metal spraying in a manner using the equipment set forth in the preceding examples.
- the nozzle is set at a distance of approximately 12 inches away from the glass surface in order to avoid heatshock to the glass giving rise to an impairment of its strength.
- Pure tin is then sprayed onto the molybdenumcoated defective area, using conventional metal spraying equipment and technique, to a sufiicient thickness to permit of finishing to the original surface contour of the glass tank.
- the surface of the tin is then finished by grinding with a portable grinding tool, to as nearly as possible conform to the original contour of the glass-lined tank. If desired, the tin surface may be hand polished, such as by use of a line abrasive cloth.
- Example 7 of copper is metal sprayed in the conventional manner, as for instance set forth in the preceding examples, onto the surface covered by the molybdenum.
- the sprayed copper coating firmly adheres to the porcelain and may then be soldered by using lead-tin solder in the conventional manner.
- Magnesium or aluminum alloy can be substi tuted for the porcelain in the above example, thereby making available for the first time an effective method for the satisfactory soldering to these metals and their alloys.
- the surface to which the spray is to be Prior to metal spraying should be one which does not tend to decomposition at the temperature to which the surface sprayed becomes heated.
- adhesion of the applied spray metal to the base is of a high order, tests showing failure to occur in the vitreous material.
- the vitreous surface may be pre-heated and in some cases it may be desirable to resort to a combination of preheating and spraying at a greater distance from the base. In all cases, however, the distance should not be so great that the spraying efficiency is interfered with by over-cooling of the propelled metal spray before it reaches the base surface to which it is applied.
- Another advantageous application of the in vention by way of preferred embodiment thereof is the manufacture of thin bearing shells.
- it has not been practical to apply the bearing metal to such thin shells because the methods of preparation for bonding sprayed metal have been destructive to such shells by causing severe war-page.
- any method of preparation used leave a relatively smooth surface because of the very thin amount of bearing metal applied.
- Example 8 A thin bearing shell for use for the backing of a bearing metal for an aircraft engine connecting rod bearing is to be surfaced with a suitable bear ing metal.
- the shell in this case consists of a strip of steel 1" wide and thick which has been formed into the shape of a semi-circle 2 /2" in diameter.
- the inner surface of the shell is to be coated with silver with a final thickness after finishing of .005 inch.
- the clean metal shell is coated with a flash coating of molybdenum by metal spraying just thick enough to completely cover the inner surface.
- the spraying of the molybdenum in this case is carried out the same a described in connection with Example 1.
- the molybdenum coated inner surface of the shell is then sprayed with silver using the same metal spray gun and .391 inch diameter silver wire to a thickness of .007 inch.
- the shell is then machined to a smooth surface about .002 inch of silver being removed to produce the desired finish and diameter.
- any bearing metal may be applied in accordance with the invention to any relatively thin shell of a relatively hard backing metal.
- the sprayed bearing metal is applied onto a molybdenum sprayed hard metal backing shell substantially not exceeding thickness.
- the novel spray metal coated article in accordance with the invention thus broadly comprises an article having a substantially inorganic surface, such as a metal or non-metal surface, a layer of spray metal and intermediate said inorganic surface and said layer of spray metal, in surface-to-surface bond therewith, a layer of sprayed molybdenum of at least flash coating thickness.
- the improvement which comprises conditioning such surface for spray metal bonding by Spraying from substantially molten condition at least a flash coating of molybdenum thereon and thereafter spraying from substantially molten condition metal onto the thusly coated surface.
- the improvement which comprises conditioning such surface for spray metal bonding by spraying from substantially molten condition a coating of molybdenum of at least about .0005 inch thickness thereon.
- Method for preparing thin bearing shells which comprises conditioning the bearing surface of a relatively thin shell of relatively hard backing metal for spray metal bonding by spraying from substantially molten condition at least a flash coating of molybdenum thereon, and thereafter spraying bearing metal onto the thu'sly coated surface.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US792835A US2588421A (en) | 1947-12-19 | 1947-12-19 | Application of sprayed metal coatings to solid objects |
BE485463A BE485463A (enrdf_load_stackoverflow) | 1947-12-19 | 1948-10-25 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US792835A US2588421A (en) | 1947-12-19 | 1947-12-19 | Application of sprayed metal coatings to solid objects |
Publications (1)
Publication Number | Publication Date |
---|---|
US2588421A true US2588421A (en) | 1952-03-11 |
Family
ID=25158217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US792835A Expired - Lifetime US2588421A (en) | 1947-12-19 | 1947-12-19 | Application of sprayed metal coatings to solid objects |
Country Status (2)
Country | Link |
---|---|
US (1) | US2588421A (enrdf_load_stackoverflow) |
BE (1) | BE485463A (enrdf_load_stackoverflow) |
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US2988807A (en) * | 1959-05-29 | 1961-06-20 | Gen Motors Corp | Method of aluminizing cobalt base alloys and article resulting therefrom |
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US3082516A (en) * | 1957-12-03 | 1963-03-26 | Union Carbide Corp | Fabrication of metal shapes |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2763920A (en) * | 1951-03-06 | 1956-09-25 | Thompson Prod Inc | Corrosion and impact-resistant article |
US2752268A (en) * | 1951-08-04 | 1956-06-26 | Whitfield & Sheshunoff Inc | Process of making alluminum coated ferrous bodies |
US2800707A (en) * | 1951-08-04 | 1957-07-30 | Whitfield & Sheshunoff Inc | Aluminum coated ferrous bodies and processes of making them |
US2772985A (en) * | 1951-08-08 | 1956-12-04 | Thompson Prod Inc | Coating of molybdenum with binary coatings containing aluminum |
US2857297A (en) * | 1951-10-25 | 1958-10-21 | Nat Res Corp | Process of coating molybdenum |
US2706692A (en) * | 1951-12-07 | 1955-04-19 | Poor & Co | Method of bonding vitreous enamels and articles produced thereby |
US2927371A (en) * | 1953-01-23 | 1960-03-08 | Armco Steel Corp | Method of continuously forming welded coated steel tubing |
US2965513A (en) * | 1953-01-30 | 1960-12-20 | Helen E Brennan | Formation of metal strip under controlled pressure |
US2982019A (en) * | 1953-05-22 | 1961-05-02 | Union Carbide Corp | Method of protecting magnesium with a coating of titanium or zirconium |
US2982017A (en) * | 1953-05-22 | 1961-05-02 | Union Carbide Corp | Method of protecting magnesium with a coating of titanium |
US2833668A (en) * | 1954-06-10 | 1958-05-06 | John Altorfer | Method of bonding aluminum to a metal |
US2833603A (en) * | 1954-06-10 | 1958-05-06 | Joseph J Dailey | Article of manufacture |
US3044156A (en) * | 1954-06-23 | 1962-07-17 | Marshall G Whitfield | Temperature resistant body |
US2839292A (en) * | 1954-08-09 | 1958-06-17 | Harry T Bellamy | Refractory reservoir for aluminum |
US2873219A (en) * | 1954-12-20 | 1959-02-10 | Joseph B Brennan | Metal-coated batt and method and apparatus for producing same |
US3038563A (en) * | 1956-10-30 | 1962-06-12 | Gen Motors Corp | Brakes |
US2996791A (en) * | 1956-11-23 | 1961-08-22 | Hughes Aircraft Co | Method of manufacturing a composite rotor |
US2950149A (en) * | 1957-01-29 | 1960-08-23 | John B Thomson | Relatively reciprocable shaft and bearing |
US3082516A (en) * | 1957-12-03 | 1963-03-26 | Union Carbide Corp | Fabrication of metal shapes |
US3017689A (en) * | 1958-03-27 | 1962-01-23 | United States Steel Corp | Anti-skid tread plate |
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Also Published As
Publication number | Publication date |
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BE485463A (enrdf_load_stackoverflow) | 1948-11-13 |
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