US3864093A - High-temperature, wear-resistant coating - Google Patents
High-temperature, wear-resistant coating Download PDFInfo
- Publication number
- US3864093A US3864093A US307345A US30734572A US3864093A US 3864093 A US3864093 A US 3864093A US 307345 A US307345 A US 307345A US 30734572 A US30734572 A US 30734572A US 3864093 A US3864093 A US 3864093A
- Authority
- US
- United States
- Prior art keywords
- metal
- base alloys
- oxide
- group
- wear
- 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
- 238000000576 coating method Methods 0.000 title description 25
- 239000011248 coating agent Substances 0.000 title description 24
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 51
- 239000000956 alloy Substances 0.000 claims abstract description 51
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 34
- 239000000758 substrate Substances 0.000 claims abstract description 28
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000002245 particle Substances 0.000 claims abstract description 19
- 229910044991 metal oxide Inorganic materials 0.000 claims abstract description 18
- 150000004706 metal oxides Chemical class 0.000 claims abstract description 18
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 17
- 239000010941 cobalt Substances 0.000 claims abstract description 17
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 17
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 17
- 229910001092 metal group alloy Inorganic materials 0.000 claims abstract description 15
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 13
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 13
- 239000011651 chromium Substances 0.000 claims abstract description 13
- 229910052742 iron Inorganic materials 0.000 claims abstract description 13
- 239000003870 refractory metal Substances 0.000 claims description 6
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims description 5
- 229910001928 zirconium oxide Inorganic materials 0.000 claims description 5
- WGLPBDUCMAPZCE-UHFFFAOYSA-N Trioxochromium Chemical compound O=[Cr](=O)=O WGLPBDUCMAPZCE-UHFFFAOYSA-N 0.000 claims description 4
- 229910000423 chromium oxide Inorganic materials 0.000 claims description 4
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 229910052751 metal Inorganic materials 0.000 abstract description 29
- 239000002184 metal Substances 0.000 abstract description 29
- 239000011159 matrix material Substances 0.000 abstract description 15
- 238000000034 method Methods 0.000 abstract description 8
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 abstract description 6
- 229910052782 aluminium Inorganic materials 0.000 abstract description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 6
- 229910052710 silicon Inorganic materials 0.000 abstract description 6
- 239000010703 silicon Substances 0.000 abstract description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 abstract 1
- 229910052593 corundum Inorganic materials 0.000 abstract 1
- 229910001845 yogo sapphire Inorganic materials 0.000 abstract 1
- 239000000463 material Substances 0.000 description 13
- 239000000203 mixture Substances 0.000 description 6
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 238000005474 detonation Methods 0.000 description 4
- 206010037660 Pyrexia Diseases 0.000 description 3
- 239000008199 coating composition Substances 0.000 description 3
- 229910000449 hafnium oxide Inorganic materials 0.000 description 3
- WIHZLLGSGQNAGK-UHFFFAOYSA-N hafnium(4+);oxygen(2-) Chemical compound [O-2].[O-2].[Hf+4] WIHZLLGSGQNAGK-UHFFFAOYSA-N 0.000 description 3
- 239000000395 magnesium oxide Substances 0.000 description 3
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 3
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 3
- 239000010955 niobium Substances 0.000 description 3
- SIWVEOZUMHYXCS-UHFFFAOYSA-N oxo(oxoyttriooxy)yttrium Chemical compound O=[Y]O[Y]=O SIWVEOZUMHYXCS-UHFFFAOYSA-N 0.000 description 3
- BPUBBGLMJRNUCC-UHFFFAOYSA-N oxygen(2-);tantalum(5+) Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[Ta+5].[Ta+5] BPUBBGLMJRNUCC-UHFFFAOYSA-N 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 229910001404 rare earth metal oxide Inorganic materials 0.000 description 3
- 229910052596 spinel Inorganic materials 0.000 description 3
- 239000011029 spinel Substances 0.000 description 3
- 229910001936 tantalum oxide Inorganic materials 0.000 description 3
- ZCUFMDLYAMJYST-UHFFFAOYSA-N thorium dioxide Chemical compound O=[Th]=O ZCUFMDLYAMJYST-UHFFFAOYSA-N 0.000 description 3
- 229910003452 thorium oxide Inorganic materials 0.000 description 3
- FRWYFWZENXDZMU-UHFFFAOYSA-N 2-iodoquinoline Chemical compound C1=CC=CC2=NC(I)=CC=C21 FRWYFWZENXDZMU-UHFFFAOYSA-N 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- LTPBRCUWZOMYOC-UHFFFAOYSA-N beryllium oxide Inorganic materials O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 2
- 239000000292 calcium oxide Substances 0.000 description 2
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 238000007750 plasma spraying Methods 0.000 description 2
- 231100000241 scar Toxicity 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 235000012239 silicon dioxide Nutrition 0.000 description 2
- 229910000601 superalloy Inorganic materials 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 208000032544 Cicatrix Diseases 0.000 description 1
- LFVLUOAHQIVABZ-UHFFFAOYSA-N Iodofenphos Chemical compound COP(=S)(OC)OC1=CC(Cl)=C(I)C=C1Cl LFVLUOAHQIVABZ-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910017709 Ni Co Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000010953 base metal Substances 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000010285 flame spraying Methods 0.000 description 1
- 229910000856 hastalloy Inorganic materials 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 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
- 230000013011 mating Effects 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 239000000376 reactant Substances 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 1
- 230000037387 scars Effects 0.000 description 1
- 229910052814 silicon oxide Inorganic materials 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000004901 spalling Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 1
- 229910001247 waspaloy Inorganic materials 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 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
- C23C4/04—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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
- Y10S428/924—Composite
- Y10S428/926—Thickness of individual layer specified
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12063—Nonparticulate metal component
- Y10T428/12139—Nonmetal particles in particulate 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.]
- Y10T428/1266—O, S, or organic compound in metal component
- Y10T428/12667—Oxide of transition metal or Al
-
- 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.]
- Y10T428/12674—Ge- or Si-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
- Y10T428/12743—Next to refractory [Group IVB, VB, or VIB] 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
- Y10T428/1275—Next to Group VIII or IB 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
- Y10T428/1275—Next to Group VIII or IB metal-base component
- Y10T428/12757—Fe
Definitions
- This invention relates to a high-temperature, wearresistant coated article, and a process for producing it, wherein the coated layer comprises metal oxide particles dispersed in a metal alloy matrix, said allo'y matrix comprising essentially at least one first metal selected from the group consisting of iron, cobalt and nickel and at least one second metal selected from the group consisting of aluminum, silicon and chromium, with the aggregate of the first metal being at least 40% by weight and the aggregate of the second metal being between about and about 40% by weight.
- coatings available for pro viding a metal alloy substrate with a surface having specific characteristics suitable for a particular end use application.
- the coating' may be applied to increase the wear-resistant characteristics of the substrate, decrease the contact-friction characteristics of the substrate, electrically or thermally insulate the substrate, or protect it from oxidation or othercorrosive attack.
- various types of coating materials can be ap plied on substrates by use of detonation guns, plasma are devices and the like, for improving the wear resistance of the substrates.
- wearresistant coating materials can be used for hightemperature service, above 1000F, since the physical properties and/or coefficient of thermal expansion characteristics of most of the available coating materials are not compatible with the substrates used in hightemperature environments.
- Complex metal alloys containing tungsten, chromium or the like, are currently being used as wear-resistant coating materials for the surfaces of superalloy turbine blades.
- the composition of the coating is such that the coating will form carbide phases (WC, W C, CI'ggCs) during solidification. It is these hard refractory carbides that are primarily responsible for the wear resistance of the coated surfaces. However, at high temperatures in oxygen-containing environments, the hard refractory carbide surface is consumed by oxidation. Changing the alloy composition to increase corrosion resistance is not the solution since the change usually results in decreasing the wear resistance of the coating.
- cermets Another class of wear-resistant materials that is presently used is known as cermets, and includes materials consisting of a high volume fraction (usually greater than 80%) of hard particles such as oxides, or carbides and a metallic binder. Even though the metallic binder may be relatively corrosion resistant, these materials are unsatisfactory because they lack impact and fatigue resistance. Thus a problem plaguing the industry today is combining oxidation resistance and wear resistance in a useful coating.
- the present invention overcomes the above drawbacks and limitations by being directed to a coating for a substrate whereby said coating comprises a relatively low volume fraction of metal oxide particles uniformly dispersed in an oxidation-resistant metal alloy matrix.
- this invention is directed to a hightemperature, wear-resistant coated article, and process for producing it, comprising a substrate with a coated layer, said layer composed of particles of at least one metal oxide substantially uniformly dispersed in a metal alloy matrix, said alloy matarix comprising essentially at least one first metal selected from the group consisting of iron, cobalt, and nickel, and at least one second metal selected from the group consisting of aluminum, silicon and chromium, and wherein the aggregate of the first metal is at least about 40% by weight of the alloy to provide sufficient strength and ductility and the aggregate of the second metal is between about 10% and about 40% by weight of the alloy to provide sufficient corrosion resistance.
- the coating composition of this invention in a particulate form can be deposited on a suitable solid structural substrate by conventional plasma-spraying techniques as disclosed in U.S. Pat. Nos. 2,858,4ll and 3,016,447, or by Detonation Gun techniques as disclosed in U.S. Pats. Nos. 2,714,563, 2,950,867 and 2,964,420 or by flame spraying techniques as disclosed in U.S. Pat. No. 2,861,900.
- the unique wear-resistant material so deposited will consist of a lamellar structure of interlocking and overlapping microscopic leaves me chanically bonded to each other and to said substrate without substantial alloying at the interface thereof, and be composed of metal oxide particles intentionally added to the oxidation-resistant metal matrix.
- the metal oxide particles for use in this invention are selected from at least one of the group consisting of aluminum oxide, chromium oxide, beryllium oxide, titanium dioxide, silicon dioxide, thorium oxide, zirconium oxide, tantalum oxide, calcium oxide, magnesium oxide, hafnium oxide, yttrium oxide, the rare earth oxides and spinel combinations of the above such as MgO-Al O NiO-Al O and CoO'Al O
- the size of the metal oxide particles can very between about 0.05 micron and about 74 microns, preferably between about 1 micron and 44 microns, and be present in a volume fraction of between about 2% and about 50%. preferably between about 5% and about 25%.
- Particle sizes below 0.05 micron are too small to add useful wear resistance, while sizes greater than 74 microns cause excessive wear of the mating surface. Volume fractions less than 2% do not provide sufficient wear resistance, but if the fraction is greater than 50%, the material has insufficient ductility, impact resistance and resistance to thermal fatigue.
- the particles, dispersed in the matrix as discrete components, must be stable in the intended high temperature operating atmosphere and substantially non-reactant with both the alloy of the matrix and the material of the substrate.
- the metal alloy matrix of this invention comprises essentially at least one first metal selected from the group consisting of iron, cobalt and nickel, and at least one second metal selected from the group consisting of aluminum, silicon and chromium.
- the aggregate of the first metal should be at least 40% by weight and the aggregate of the second metal should be between about 10% and about 40% by weight.
- the balance of the metal alloy can be composed of one or more adventitious elements, and/or one or more elements or compounds added to impart mechanical strength and/or corrosion resistance at high temperatures; for example, tungsten, molybdenum, vanadium, manganese, carbon, rhenium, yttrium, lanthanum, boron, niobium, titanium, tantalum, zirconium and the like.
- the metal alloy should be of the particulate form and sized 200 Tyler mesh and finer so that it can be mixed with the metal oxide particles prior to deposition on a suitable substrate.
- the metal oxide particles and the components alloy powder; said alloy comprising essentially at least one first metal selected from the group consisting of iron, cobalt and nickel, and at least one second metal selected from the group consisting of aluminum, silicon of the metal alloy matrix material should be selected so and chromium, the aggregate of said first metal being that the metal oxide particles will not effectively react at least about 40% by weight and the aggregate of said with the alloy and thereby remain substantially dissecond metal being between about and about 40% persed in the alloy matrix as discrete stable particles.
- the final wear-resistant coating should have a tween about 0.05 micron and 74 microns and present Vickers Hardness Number (VHN) of greater than 500 10 in a volume fraction of between about 2% and about as determined in accordance with ASTM Test Method 50%; and wherein said alloy powder being sized about E92-67 using a 300 gram test load.
- VHN Vickers Hardness Number
- Examples of admi- 200 Tyler mesh and finer; and rably suited alloys for the matrix Of this invention are I depositing said mixture of particles and powders Show" in Table onto a substrate by a technique selected from the group
- Some examples of substrate materials used in various i ti of detonation gun means, plasma spraying corrosive environments and admirably suited as submeans d fl Spraying means so as to dh i l strates for the coating Of this invention include, but are coat Said substrate a high-temperature wearnot limited Steel, Stainless Steel, iron base alloys resistant coating having a surface hardness of at least nickel, nickel base alloys, cobalt, cobalt base alloys, about 500 VHN chromium, chromium base alloys, refractory metals, EXAMPLE and refractory-metal base alloys.
- the specific coating composition selected for a substrate intended for a par- A base alloy F havmg the composltlon ticular end use environment should be selected so that shownm m n slzed Tyler mesh and finer it will adhere to the substrate without substantially was mfxed 3o'mlcron and Smaller Chromfum spalling or peeling while neither the metal oxide parti- Oxide Varlous Volume fractlons and deposlted cles nor the metal alloy matrix therein will effectively JT3D turbine blades using a detonation gun under react with the substrate in its intended environment.
- the metal particles mium oxide mixture until a 0.008 to 0.010 inch thick should be stable in the alloy matrix and the overall layer was established.
- the coated blades were then high-temperature,wear-resistant coating should be statested in an engine simulator wear-test device that ble on the substrate in its intended end-use environcauses thermal stress and impact and sliding wear damment. Usually a coating of about 0.003 inch or thicker age similar to an actual engine by rubbing two blade Z- would be suitable for most applications. notch sections against each other.
- the temperature in As used herein, metal base alloy shall mean alloys the simulator during the test was recorded at ]650F wherein (899C).
- the base metal is present in the largest proportion by faces of two blades, a wear scar was embedded in the weight.
- High temperature shall mean l00OF or higher. coated test surfaces.
- the depth of the wear scars in the Therefore substrates to be coated according to this invarious coating compositions tested is shown in Table vention should be such that they substantially maintain Ill.
- the additheir integrity at high temperatures. tion of metal oxide particles, in various volume frac- The process of this invention entails the following tions, to the coating will substantially increase the wear steps: resistance of the coating without degrading its good oxa. preparing a mixture of at least one metal oxide seidation resistance.
- the surface hardness of said Ma new 1 coated layer bein at least 500 VHN as determined 2 g using a 300 gram test load and the coated layer having aggregate of Gm metal in chains 48.65% a microstructure consisting of a thin lamel lar structure "aggregate of second metal in coating 29 a 10 of interlocking and overlapping microscopic leaves me- TABLE III Duration Material Depth of Wear of Test LlOl alloy 1 X 10' inch l2 hours LlOl alloy 6 v/o cl'gog less than l X 10 inch l2 hours LlOl alloy 4 W0 C503 4 X 10 inch 12 hours LlOl alloy 2 v/o C1203 2 X l0" inch 12 hours thorium oxide, zirconium oxide, tantalum oxide, siliconoxide, magnesium oxide, hafnium oxide, yt
- coated article of claim 1 wherein said substrate is selected from the group consisting of steel, stainless steel, iron base alloys, cobalt, cobalt base alloys, nickel, nickel base alloys, chromium, chromium base alloys, refractory metals and refractory-metal base alloys.
- metal oxide particles are selected from a group consisting of aluminum oxide, stabilized zirconium oxide and chromium oxide; said metal alloy is selected from a group consisting of nickel base alloys, iron base alloys and cobalt base alloys, and said substrate is selected from a group consisting of nickel base alloys, cobalt base alloys and iron base alloys.
Landscapes
- Chemical & Material Sciences (AREA)
- 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)
- Other Surface Treatments For Metallic Materials (AREA)
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US307345A US3864093A (en) | 1972-11-17 | 1972-11-17 | High-temperature, wear-resistant coating |
CA183,291A CA1000126A (en) | 1972-11-17 | 1973-10-12 | High-temperature, wear-resistant coating and a process for making it |
DE2356617A DE2356617C3 (de) | 1972-11-17 | 1973-11-13 | Verfahren zum Aufbringen eines gegenüber hohen Temperaturen und Abrieb beständigen Überzugs auf Metallgegenständen |
JP12838073A JPS5634632B2 (enrdf_load_stackoverflow) | 1972-11-17 | 1973-11-16 | |
CH1611373A CH587353A5 (enrdf_load_stackoverflow) | 1972-11-17 | 1973-11-16 | |
GB5325673A GB1448256A (en) | 1972-11-17 | 1973-11-16 | High-temperature wear resistant coating and a process for making it |
FR7340984A FR2207027B1 (enrdf_load_stackoverflow) | 1972-11-17 | 1973-11-16 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US307345A US3864093A (en) | 1972-11-17 | 1972-11-17 | High-temperature, wear-resistant coating |
Publications (1)
Publication Number | Publication Date |
---|---|
US3864093A true US3864093A (en) | 1975-02-04 |
Family
ID=23189330
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US307345A Expired - Lifetime US3864093A (en) | 1972-11-17 | 1972-11-17 | High-temperature, wear-resistant coating |
Country Status (7)
Country | Link |
---|---|
US (1) | US3864093A (enrdf_load_stackoverflow) |
JP (1) | JPS5634632B2 (enrdf_load_stackoverflow) |
CA (1) | CA1000126A (enrdf_load_stackoverflow) |
CH (1) | CH587353A5 (enrdf_load_stackoverflow) |
DE (1) | DE2356617C3 (enrdf_load_stackoverflow) |
FR (1) | FR2207027B1 (enrdf_load_stackoverflow) |
GB (1) | GB1448256A (enrdf_load_stackoverflow) |
Cited By (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4101713A (en) * | 1977-01-14 | 1978-07-18 | General Electric Company | Flame spray oxidation and corrosion resistant superalloys |
US4124737A (en) * | 1976-12-30 | 1978-11-07 | Union Carbide Corporation | High temperature wear resistant coating composition |
US4217151A (en) * | 1978-01-27 | 1980-08-12 | Victor Company Of Japan, Limited | Cermet type magnetic material |
US4404263A (en) * | 1978-12-13 | 1983-09-13 | Glyco-Metall-Werke Daelen & Loos Gmbh | Laminated bearing material and process for making the same |
US4446199A (en) * | 1982-07-30 | 1984-05-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Overlay metallic-cermet alloy coating systems |
US4451496A (en) * | 1982-07-30 | 1984-05-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Coating with overlay metallic-cermet alloy systems |
US4578114A (en) * | 1984-04-05 | 1986-03-25 | Metco Inc. | Aluminum and yttrium oxide coated thermal spray powder |
US4639399A (en) * | 1985-11-26 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Navy | Nickel oxide, ceramic insulated, high temperature coating |
US4740428A (en) * | 1985-04-24 | 1988-04-26 | Honda Giken Kogyo Kabushiki Kaisha | Fiber-reinforced metallic member |
US4822689A (en) * | 1985-10-18 | 1989-04-18 | Union Carbide Corporation | High volume fraction refractory oxide, thermal shock resistant coatings |
US5120350A (en) * | 1990-07-03 | 1992-06-09 | The Standard Oil Company | Fused yttria reinforced metal matrix composites and method |
US5277936A (en) * | 1987-11-19 | 1994-01-11 | United Technologies Corporation | Oxide containing MCrAlY-type overlay coatings |
US5436047A (en) * | 1991-09-24 | 1995-07-25 | International Business Machines Corporation | Thin film magnetic recording disk comprising a metallic disk blank, a substantially non-magnetic Ni-Cr-O film having a textured surface and a magnetic film |
US5612090A (en) * | 1992-11-20 | 1997-03-18 | Nisshin Steel Co., Ltd. | Iron-based material having excellent oxidation resistance at elevated temperatures and process for the production thereof |
US5670213A (en) * | 1995-03-14 | 1997-09-23 | Hilite Industries, Inc. | Process for increasing torque generated by a clutch |
US5712050A (en) * | 1991-09-09 | 1998-01-27 | General Electric Company | Superalloy component with dispersion-containing protective coating |
US5721061A (en) * | 1996-11-15 | 1998-02-24 | General Electric Company | Oxidation-resistant coating for niobium-base alloys |
US5795659A (en) * | 1992-09-05 | 1998-08-18 | International Inc. | Aluminide-silicide coatings coated products |
WO1998041346A1 (en) * | 1997-03-17 | 1998-09-24 | Levinski, Leonid | Powder mixture for thermal diffusion coating |
US5942333A (en) * | 1995-03-27 | 1999-08-24 | Texas Research Institute | Non-conductive coatings for underwater connector backshells |
US6302318B1 (en) * | 1999-06-29 | 2001-10-16 | General Electric Company | Method of providing wear-resistant coatings, and related articles |
US6436202B1 (en) | 2000-09-12 | 2002-08-20 | Nova Chemicals (International) S.A. | Process of treating a stainless steel matrix |
US20020160189A1 (en) * | 2001-03-08 | 2002-10-31 | Kazuhiro Wataya | Thermal spray spherical particles, and sprayed components |
US6670049B1 (en) * | 1995-05-05 | 2003-12-30 | General Electric Company | Metal/ceramic composite protective coating and its application |
US6824883B1 (en) | 2000-09-12 | 2004-11-30 | Nova Chemicals (International) S.A. | Surface on a stainless steel matrix |
US20050013993A1 (en) * | 2003-07-16 | 2005-01-20 | Honeywell International Inc. | Environmental & thermal barrier coating |
EP1618224A1 (en) * | 2003-04-28 | 2006-01-25 | Coppe/Ufrj - Coordenacao Dos Programas De Pos Graduacao De Engenharia Da Universidade Federal Do Rio De Janeiro | Use of thermal spraying with niobium oxides and niobium alloys during the production process of rolled steel plates |
US20060137486A1 (en) * | 2003-05-20 | 2006-06-29 | Bangaru Narasimha-Rao V | Advanced erosion resistant oxide cermets |
US20060254418A1 (en) * | 2005-04-07 | 2006-11-16 | Sulzer Metco Ag | Material and process for thermal coating, surface layer and also compressor with a surface layer of the material |
US20060261311A1 (en) * | 2003-07-15 | 2006-11-23 | Dacral | Use of yttrium, zirconium, lanthanum, cerium, praseodymium and/or neodymium as reinforcing agent for an anticorrosion coating composition |
JP2007505210A (ja) * | 2003-06-24 | 2007-03-08 | ノバ ケミカルズ(インターナショナル)ソシエテ アノニム | 鋼基板上の複合材料表面 |
US20070116973A1 (en) * | 2005-11-21 | 2007-05-24 | Pareek Vinod K | Process for coating articles and articles made therefrom |
US20070116884A1 (en) * | 2005-11-21 | 2007-05-24 | Pareek Vinod K | Process for coating articles and articles made therefrom |
US20070131054A1 (en) * | 2003-05-20 | 2007-06-14 | Bangaru Narasimha-Rao V | Multi-scale cermets for high temperature erosion-corrosion service |
US20080245445A1 (en) * | 2007-04-04 | 2008-10-09 | David Andrew Helmick | Process for forming a chromium diffusion portion and articles made therefrom |
US20090214888A1 (en) * | 2003-08-18 | 2009-08-27 | Upchurch Charles J | Method and apparatus for producing alloyed iron article |
US7635515B1 (en) * | 2004-04-08 | 2009-12-22 | Powdermet, Inc | Heterogeneous composite bodies with isolated lenticular shaped cermet regions |
US20100172789A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Method of coating with cryo-milled nano-grained particles |
WO2013056289A1 (de) | 2011-10-20 | 2013-04-25 | Isiqiri Interface Technolgies Gmbh | ECHTZEITMESSUNG VON RELATIVEN POSITIONSDATEN UND/ODER VON GEOMETRISCHEN MAßEN EINES BEWEGTEN KÖRPERS UNTER VERWENDUNG OPTISCHER MESSMITTEL |
US8544769B2 (en) | 2011-07-26 | 2013-10-01 | General Electric Company | Multi-nozzle spray gun |
US8697250B1 (en) | 2013-02-14 | 2014-04-15 | Praxair S.T. Technology, Inc. | Selective oxidation of a modified MCrAlY composition loaded with high levels of ceramic acting as a barrier to specific oxide formations |
US9581030B2 (en) | 2011-01-21 | 2017-02-28 | Lockheed Martin Corporation | Ultra high temperature environmental protection coating |
EP2574545A3 (en) * | 2011-09-30 | 2017-10-11 | Rolls-Royce plc | Wear Resistant Coating and Use Thereof |
WO2019069183A1 (en) | 2017-10-04 | 2019-04-11 | Nova Chemicals Corporation | PERFECTED PROTECTIVE SURFACE ON STAINLESS STEEL |
US10605013B2 (en) | 2015-10-23 | 2020-03-31 | Halliburton Energy Services, Inc. | Casing string assembly with composite pre-milled window |
US10781319B2 (en) | 2011-01-21 | 2020-09-22 | Lockheed Martin Corporation | Ultra high temperature environmental protection coating |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS4998409A (enrdf_load_stackoverflow) * | 1973-01-11 | 1974-09-18 | ||
JPS56156753A (en) * | 1980-05-06 | 1981-12-03 | Mitsubishi Heavy Ind Ltd | Composite material |
JPS5925333U (ja) * | 1982-08-10 | 1984-02-16 | 株式会社東芝 | 送り装置 |
GB2199849B (en) * | 1987-01-16 | 1991-05-15 | Rolls Royce Plc | Superalloy surface treatment against vapourisation |
JPS63230860A (ja) * | 1987-03-20 | 1988-09-27 | Riken Corp | 耐摩耗表面層 |
EP0331519B1 (en) * | 1988-03-04 | 1992-07-01 | Alcan International Limited | Production of aluminum matrix composite coatings of metal structures |
FI88935C (fi) * | 1990-09-04 | 1993-07-26 | Tampella Telatek Oy | Foerfarande foer belaeggande av en aongturbin och daertill anslutna staolytor |
US5455119A (en) * | 1993-11-08 | 1995-10-03 | Praxair S.T. Technology, Inc. | Coating composition having good corrosion and oxidation resistance |
JP2001020055A (ja) * | 1999-07-06 | 2001-01-23 | Praxair St Technol Inc | 硼化クロムコーティング |
JP2006505694A (ja) * | 2002-11-04 | 2006-02-16 | ドンカスターズ リミテッド | 高温合金 |
JP7001444B2 (ja) * | 2017-11-29 | 2022-01-19 | 花王株式会社 | 吸収性物品 |
KR102485518B1 (ko) * | 2020-03-31 | 2023-01-06 | 주식회사 엘 앤 에프 | 활물질 제조용 소성로의 코팅 물질 및 이를 포함하는 소성로 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3705791A (en) * | 1970-09-18 | 1972-12-12 | Wall Colmonoy Corp | Cermet alloy composition |
US3719519A (en) * | 1965-08-06 | 1973-03-06 | G Perugini | Process of forming protective coatings on metallic surfaces by spraying a combination of powders of a metal alloy,chromium and a ceramic oxide |
US3718962A (en) * | 1970-09-28 | 1973-03-06 | Gen Electric | High temperature metallic diffusion coating |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2775531A (en) * | 1949-05-10 | 1956-12-25 | Univ Ohio State Res Found | Method of coating a metal surface |
US3279939A (en) * | 1963-02-26 | 1966-10-18 | Union Carbide Corp | Nichrome-chromia coating |
US3436511A (en) * | 1965-01-18 | 1969-04-01 | Union Carbide Corp | Coating composition and method of applying |
NL6616433A (enrdf_load_stackoverflow) * | 1965-11-29 | 1967-05-30 | ||
FR2130209B1 (enrdf_load_stackoverflow) * | 1971-03-25 | 1974-06-28 | Goetzewerke |
-
1972
- 1972-11-17 US US307345A patent/US3864093A/en not_active Expired - Lifetime
-
1973
- 1973-10-12 CA CA183,291A patent/CA1000126A/en not_active Expired
- 1973-11-13 DE DE2356617A patent/DE2356617C3/de not_active Expired
- 1973-11-16 GB GB5325673A patent/GB1448256A/en not_active Expired
- 1973-11-16 CH CH1611373A patent/CH587353A5/xx not_active IP Right Cessation
- 1973-11-16 JP JP12838073A patent/JPS5634632B2/ja not_active Expired
- 1973-11-16 FR FR7340984A patent/FR2207027B1/fr not_active Expired
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3719519A (en) * | 1965-08-06 | 1973-03-06 | G Perugini | Process of forming protective coatings on metallic surfaces by spraying a combination of powders of a metal alloy,chromium and a ceramic oxide |
US3705791A (en) * | 1970-09-18 | 1972-12-12 | Wall Colmonoy Corp | Cermet alloy composition |
US3718962A (en) * | 1970-09-28 | 1973-03-06 | Gen Electric | High temperature metallic diffusion coating |
Cited By (73)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4124737A (en) * | 1976-12-30 | 1978-11-07 | Union Carbide Corporation | High temperature wear resistant coating composition |
DE2801016A1 (de) * | 1977-01-14 | 1978-07-20 | Gen Electric | Gegenstand aus einer superlegierung, der durch flammspritzen mit einem oxidations- und korrosionsbestaendigen ueberzug versehen ist sowie verfahren zu dessen herstellung |
US4101713A (en) * | 1977-01-14 | 1978-07-18 | General Electric Company | Flame spray oxidation and corrosion resistant superalloys |
US4217151A (en) * | 1978-01-27 | 1980-08-12 | Victor Company Of Japan, Limited | Cermet type magnetic material |
US4404263A (en) * | 1978-12-13 | 1983-09-13 | Glyco-Metall-Werke Daelen & Loos Gmbh | Laminated bearing material and process for making the same |
US4446199A (en) * | 1982-07-30 | 1984-05-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Overlay metallic-cermet alloy coating systems |
US4451496A (en) * | 1982-07-30 | 1984-05-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Coating with overlay metallic-cermet alloy systems |
US4578114A (en) * | 1984-04-05 | 1986-03-25 | Metco Inc. | Aluminum and yttrium oxide coated thermal spray powder |
US4740428A (en) * | 1985-04-24 | 1988-04-26 | Honda Giken Kogyo Kabushiki Kaisha | Fiber-reinforced metallic member |
US4822689A (en) * | 1985-10-18 | 1989-04-18 | Union Carbide Corporation | High volume fraction refractory oxide, thermal shock resistant coatings |
US4639399A (en) * | 1985-11-26 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Navy | Nickel oxide, ceramic insulated, high temperature coating |
US5277936A (en) * | 1987-11-19 | 1994-01-11 | United Technologies Corporation | Oxide containing MCrAlY-type overlay coatings |
US5120350A (en) * | 1990-07-03 | 1992-06-09 | The Standard Oil Company | Fused yttria reinforced metal matrix composites and method |
US5712050A (en) * | 1991-09-09 | 1998-01-27 | General Electric Company | Superalloy component with dispersion-containing protective coating |
US5436047A (en) * | 1991-09-24 | 1995-07-25 | International Business Machines Corporation | Thin film magnetic recording disk comprising a metallic disk blank, a substantially non-magnetic Ni-Cr-O film having a textured surface and a magnetic film |
US5795659A (en) * | 1992-09-05 | 1998-08-18 | International Inc. | Aluminide-silicide coatings coated products |
US5612090A (en) * | 1992-11-20 | 1997-03-18 | Nisshin Steel Co., Ltd. | Iron-based material having excellent oxidation resistance at elevated temperatures and process for the production thereof |
US5631090A (en) * | 1992-11-20 | 1997-05-20 | Nisshin Steel Co., Ltd. | Iron-based material having excellent oxidation resistance at elevated temperatures and process for the production thereof |
US5670213A (en) * | 1995-03-14 | 1997-09-23 | Hilite Industries, Inc. | Process for increasing torque generated by a clutch |
US5942333A (en) * | 1995-03-27 | 1999-08-24 | Texas Research Institute | Non-conductive coatings for underwater connector backshells |
US6670049B1 (en) * | 1995-05-05 | 2003-12-30 | General Electric Company | Metal/ceramic composite protective coating and its application |
US5721061A (en) * | 1996-11-15 | 1998-02-24 | General Electric Company | Oxidation-resistant coating for niobium-base alloys |
WO1998041346A1 (en) * | 1997-03-17 | 1998-09-24 | Levinski, Leonid | Powder mixture for thermal diffusion coating |
US6171359B1 (en) | 1997-03-17 | 2001-01-09 | Leonid Levinski | Powder mixture for thermal diffusion coating |
US6302318B1 (en) * | 1999-06-29 | 2001-10-16 | General Electric Company | Method of providing wear-resistant coatings, and related articles |
US6398103B2 (en) | 1999-06-29 | 2002-06-04 | General Electric Company | Method of providing wear-resistant coatings, and related articles |
US6436202B1 (en) | 2000-09-12 | 2002-08-20 | Nova Chemicals (International) S.A. | Process of treating a stainless steel matrix |
US6824883B1 (en) | 2000-09-12 | 2004-11-30 | Nova Chemicals (International) S.A. | Surface on a stainless steel matrix |
US7156979B2 (en) | 2000-09-12 | 2007-01-02 | Nova Chemicals (International) S.A. | Thermal cracking process using tubes, pipes, and coils made of novel stainless steel matrix |
US20050077210A1 (en) * | 2000-09-12 | 2005-04-14 | Benum Leslie Wilfred | Surface on a stainless steel matrix |
US20020160189A1 (en) * | 2001-03-08 | 2002-10-31 | Kazuhiro Wataya | Thermal spray spherical particles, and sprayed components |
EP1239055A3 (en) * | 2001-03-08 | 2004-01-07 | Shin-Etsu Chemical Co., Ltd. | Thermal spray spherical particles, and sprayed components |
US6916534B2 (en) | 2001-03-08 | 2005-07-12 | Shin-Etsu Chemical Co., Ltd. | Thermal spray spherical particles, and sprayed components |
EP1618224A1 (en) * | 2003-04-28 | 2006-01-25 | Coppe/Ufrj - Coordenacao Dos Programas De Pos Graduacao De Engenharia Da Universidade Federal Do Rio De Janeiro | Use of thermal spraying with niobium oxides and niobium alloys during the production process of rolled steel plates |
US20060280874A1 (en) * | 2003-04-28 | 2006-12-14 | Coppe/Ufrj Coordenacao Dos Programas De Pos Graduacao De Engenharia Da Universidade | Use of thermal spraying with niobium oxides and niobium alloys during the production process of rolled steel plates |
US20060137486A1 (en) * | 2003-05-20 | 2006-06-29 | Bangaru Narasimha-Rao V | Advanced erosion resistant oxide cermets |
US7501090B2 (en) * | 2003-05-20 | 2009-03-10 | Exxonmobil Research And Engineering Company | Method for protecting metal surfaces utilizing erosion resistant oxide cermets |
US20070131054A1 (en) * | 2003-05-20 | 2007-06-14 | Bangaru Narasimha-Rao V | Multi-scale cermets for high temperature erosion-corrosion service |
US7153338B2 (en) * | 2003-05-20 | 2006-12-26 | Exxonmobil Research And Engineering Company | Advanced erosion resistant oxide cermets |
US20120177933A1 (en) * | 2003-05-20 | 2012-07-12 | Narasimha-Rao Venkata Bangaru | Multi-scale cermets for high temperature erosion-corrosion service |
US20080245183A1 (en) * | 2003-05-20 | 2008-10-09 | Narasimha-Rao Venkata Bangaru | Advanced erosion resistant oxide cermets |
US7316724B2 (en) * | 2003-05-20 | 2008-01-08 | Exxonmobil Research And Engineering Company | Multi-scale cermets for high temperature erosion-corrosion service |
JP2007505210A (ja) * | 2003-06-24 | 2007-03-08 | ノバ ケミカルズ(インターナショナル)ソシエテ アノニム | 鋼基板上の複合材料表面 |
US20060261311A1 (en) * | 2003-07-15 | 2006-11-23 | Dacral | Use of yttrium, zirconium, lanthanum, cerium, praseodymium and/or neodymium as reinforcing agent for an anticorrosion coating composition |
US8641925B2 (en) | 2003-07-15 | 2014-02-04 | Nof Metal Coatings Europe | Use of yttrium, zirconium, lanthanum, cerium, praseodymium and/or neodymium as reinforcing agent for an anticorrosion coating composition |
US8080176B2 (en) | 2003-07-15 | 2011-12-20 | Nof Metal Coatings Europe | Use of yttrium, zirconium, lanthanum, cerium, praseodymium and/or neodymium as reinforcing agent for an anticorrosion coating composition |
US20050013993A1 (en) * | 2003-07-16 | 2005-01-20 | Honeywell International Inc. | Environmental & thermal barrier coating |
US8137765B2 (en) | 2003-08-18 | 2012-03-20 | Upchurch Charles J | Method of producing alloyed iron article |
US20090214888A1 (en) * | 2003-08-18 | 2009-08-27 | Upchurch Charles J | Method and apparatus for producing alloyed iron article |
US7635515B1 (en) * | 2004-04-08 | 2009-12-22 | Powdermet, Inc | Heterogeneous composite bodies with isolated lenticular shaped cermet regions |
US7357068B2 (en) * | 2005-04-07 | 2008-04-15 | Sulzer Metco Ag | Material and process for thermal coating, surface layer and also compressor with a surface layer of the material |
US20060254418A1 (en) * | 2005-04-07 | 2006-11-16 | Sulzer Metco Ag | Material and process for thermal coating, surface layer and also compressor with a surface layer of the material |
US20070116809A1 (en) * | 2005-11-21 | 2007-05-24 | General Electric Company | Process for coating articles and articles made therefrom |
US20070116973A1 (en) * | 2005-11-21 | 2007-05-24 | Pareek Vinod K | Process for coating articles and articles made therefrom |
US7601431B2 (en) * | 2005-11-21 | 2009-10-13 | General Electric Company | Process for coating articles and articles made therefrom |
US20070116884A1 (en) * | 2005-11-21 | 2007-05-24 | Pareek Vinod K | Process for coating articles and articles made therefrom |
US8262812B2 (en) | 2007-04-04 | 2012-09-11 | General Electric Company | Process for forming a chromium diffusion portion and articles made therefrom |
US20080245445A1 (en) * | 2007-04-04 | 2008-10-09 | David Andrew Helmick | Process for forming a chromium diffusion portion and articles made therefrom |
US9222164B2 (en) | 2007-04-04 | 2015-12-29 | General Electric Company | Process for forming a chromium diffusion portion and articles made therefrom |
CN106077677A (zh) * | 2009-01-08 | 2016-11-09 | 通用电气公司 | 用冷冻研磨纳米粒状颗粒涂覆的方法 |
US20100172789A1 (en) * | 2009-01-08 | 2010-07-08 | General Electric Company | Method of coating with cryo-milled nano-grained particles |
US8268237B2 (en) * | 2009-01-08 | 2012-09-18 | General Electric Company | Method of coating with cryo-milled nano-grained particles |
CN101851721A (zh) * | 2009-01-08 | 2010-10-06 | 通用电气公司 | 用冷冻研磨纳米粒状颗粒涂覆的方法 |
US10781319B2 (en) | 2011-01-21 | 2020-09-22 | Lockheed Martin Corporation | Ultra high temperature environmental protection coating |
US9581030B2 (en) | 2011-01-21 | 2017-02-28 | Lockheed Martin Corporation | Ultra high temperature environmental protection coating |
US8544769B2 (en) | 2011-07-26 | 2013-10-01 | General Electric Company | Multi-nozzle spray gun |
EP2574545A3 (en) * | 2011-09-30 | 2017-10-11 | Rolls-Royce plc | Wear Resistant Coating and Use Thereof |
WO2013056289A1 (de) | 2011-10-20 | 2013-04-25 | Isiqiri Interface Technolgies Gmbh | ECHTZEITMESSUNG VON RELATIVEN POSITIONSDATEN UND/ODER VON GEOMETRISCHEN MAßEN EINES BEWEGTEN KÖRPERS UNTER VERWENDUNG OPTISCHER MESSMITTEL |
US8697250B1 (en) | 2013-02-14 | 2014-04-15 | Praxair S.T. Technology, Inc. | Selective oxidation of a modified MCrAlY composition loaded with high levels of ceramic acting as a barrier to specific oxide formations |
US10605013B2 (en) | 2015-10-23 | 2020-03-31 | Halliburton Energy Services, Inc. | Casing string assembly with composite pre-milled window |
WO2019069183A1 (en) | 2017-10-04 | 2019-04-11 | Nova Chemicals Corporation | PERFECTED PROTECTIVE SURFACE ON STAINLESS STEEL |
US11035031B2 (en) | 2017-10-04 | 2021-06-15 | Nova Chemicals (International) S.A. | Protective surface on stainless steel |
US11859291B2 (en) | 2017-10-04 | 2024-01-02 | Nova Chemicals (International) S.A. | Protective surface on stainless steel |
Also Published As
Publication number | Publication date |
---|---|
DE2356617B2 (de) | 1977-04-21 |
DE2356617A1 (de) | 1974-05-22 |
JPS4981236A (enrdf_load_stackoverflow) | 1974-08-06 |
FR2207027B1 (enrdf_load_stackoverflow) | 1976-05-07 |
JPS5634632B2 (enrdf_load_stackoverflow) | 1981-08-11 |
FR2207027A1 (enrdf_load_stackoverflow) | 1974-06-14 |
CA1000126A (en) | 1976-11-23 |
CH587353A5 (enrdf_load_stackoverflow) | 1977-04-29 |
DE2356617C3 (de) | 1985-01-24 |
GB1448256A (en) | 1976-09-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3864093A (en) | High-temperature, wear-resistant coating | |
US4124737A (en) | High temperature wear resistant coating composition | |
US3313633A (en) | High temperature flame spray powder | |
US4966820A (en) | Ceramics-coated heat resisting alloy member | |
US4249913A (en) | Alumina coated silicon carbide abrasive | |
US4313760A (en) | Superalloy coating composition | |
US4339509A (en) | Superalloy coating composition with oxidation and/or sulfidation resistance | |
US4447503A (en) | Superalloy coating composition with high temperature oxidation resistance | |
US4198442A (en) | Method for producing elevated temperature corrosion resistant articles | |
US3150938A (en) | Coating composition, method of application, and product thereof | |
US4275090A (en) | Process for carbon bearing MCrAlY coating | |
US5682596A (en) | High temperature anti-fretting wear coating combination | |
US5141821A (en) | High temperature mcral(y) composite material containing carbide particle inclusions | |
US4615864A (en) | Superalloy coating composition with oxidation and/or sulfidation resistance | |
JPH08505439A (ja) | 硬化肉盛り用スプレーパウダーと硬化肉盛り付部品 | |
GB1591593A (en) | Superalloys | |
CN102286744A (zh) | 耐磨和低摩擦涂层以及涂有所述涂层的制品 | |
GB1572320A (en) | Gas turbine blade tip alloy | |
Cameron et al. | Tribaloy Intermetallic Materials: New Wear‐and Corrosion‐Resistant Alloys | |
GB2116211A (en) | Oxidation resistant nickel alloy | |
DE3036206A1 (de) | Verschleissfester, vor oxidation und korrosion schuetzender ueberzug, korrosions- und verschleissfeste ueberzugslegierung, mit einem solchen ueberzug versehener gegenstand und verfahren zum herstellen eines solchen ueberzugs | |
US2711009A (en) | Corrosion resistant sintered stock containing mixed carbides | |
US20050079377A1 (en) | Coatings, method of manufacture, and the articles derived therefrom | |
CA2009599A1 (en) | Material system for high temperature jet engine operation | |
US5837327A (en) | Method for producing a TiB2 -based coating |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: MORGAN GUARANTY TRUST COMPANY OF NEW YORK, AND MOR Free format text: MORTGAGE;ASSIGNORS:UNION CARBIDE CORPORATION, A CORP.,;STP CORPORATION, A CORP. OF DE.,;UNION CARBIDE AGRICULTURAL PRODUCTS CO., INC., A CORP. OF PA.,;AND OTHERS;REEL/FRAME:004547/0001 Effective date: 19860106 |
|
AS | Assignment |
Owner name: UNION CARBIDE CORPORATION, Free format text: RELEASED BY SECURED PARTY;ASSIGNOR:MORGAN BANK (DELAWARE) AS COLLATERAL AGENT;REEL/FRAME:004665/0131 Effective date: 19860925 |
|
STCF | Information on status: patent grant |
Free format text: PATENTED FILE - (OLD CASE ADDED FOR FILE TRACKING PURPOSES) |
|
AS | Assignment |
Owner name: UNION CARBIDE COATINGS SERVICE TECHNOLOGY CORPORAT Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:UNION CARBIDE COATINGS SERVICE CORPORATION;REEL/FRAME:005240/0883 Effective date: 19900102 |