US2972550A - Flame plating using detonation reactants - Google Patents
Flame plating using detonation reactants Download PDFInfo
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- US2972550A US2972550A US738283A US73828358A US2972550A US 2972550 A US2972550 A US 2972550A US 738283 A US738283 A US 738283A US 73828358 A US73828358 A US 73828358A US 2972550 A US2972550 A US 2972550A
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- 238000005474 detonation Methods 0.000 title claims description 58
- 238000007747 plating Methods 0.000 title claims description 14
- 239000000376 reactant Substances 0.000 title description 3
- 238000000576 coating method Methods 0.000 claims description 80
- 239000000203 mixture Substances 0.000 claims description 63
- 239000011248 coating agent Substances 0.000 claims description 56
- 238000000034 method Methods 0.000 claims description 41
- 239000007789 gas Substances 0.000 claims description 34
- 239000007800 oxidant agent Substances 0.000 claims description 29
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 21
- 239000001301 oxygen Substances 0.000 claims description 20
- 229910052760 oxygen Inorganic materials 0.000 claims description 20
- 239000000463 material Substances 0.000 claims description 19
- 239000000446 fuel Substances 0.000 claims description 17
- 230000001590 oxidative effect Effects 0.000 claims description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 14
- 229910052799 carbon Inorganic materials 0.000 claims description 14
- 238000007865 diluting Methods 0.000 claims description 10
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 56
- 229910052757 nitrogen Inorganic materials 0.000 description 29
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 17
- 238000002156 mixing Methods 0.000 description 15
- 229910017052 cobalt Inorganic materials 0.000 description 14
- 239000010941 cobalt Substances 0.000 description 14
- 239000008199 coating composition Substances 0.000 description 13
- 239000000843 powder Substances 0.000 description 13
- 239000003085 diluting agent Substances 0.000 description 12
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 11
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 9
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 9
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 9
- 229910052721 tungsten Inorganic materials 0.000 description 9
- 239000010937 tungsten Substances 0.000 description 9
- 239000011261 inert gas Substances 0.000 description 8
- 229910052759 nickel Inorganic materials 0.000 description 8
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 8
- 239000011651 chromium Substances 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 230000001464 adherent effect Effects 0.000 description 6
- XKRFYHLGVUSROY-UHFFFAOYSA-N argon Substances [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 5
- 239000011230 binding agent Substances 0.000 description 5
- 229910052804 chromium Inorganic materials 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- 239000000654 additive Substances 0.000 description 4
- 230000000996 additive effect Effects 0.000 description 4
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 4
- 238000010790 dilution Methods 0.000 description 4
- 239000012895 dilution Substances 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 229910003470 tongbaite Inorganic materials 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 3
- 239000012159 carrier gas Substances 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000003647 oxidation Effects 0.000 description 3
- 238000007254 oxidation reaction Methods 0.000 description 3
- 229910000531 Co alloy Inorganic materials 0.000 description 2
- 229910018487 Ni—Cr Inorganic materials 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- 229910052743 krypton Inorganic materials 0.000 description 2
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 229910052754 neon Inorganic materials 0.000 description 2
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 description 2
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 229910052724 xenon Inorganic materials 0.000 description 2
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910001120 nichrome Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 230000033116 oxidation-reduction process Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
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
- C23C4/08—Metallic material containing only metal elements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
- B05B7/0006—Spraying by means of explosions
-
- 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
-
- 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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/126—Detonation spraying
Definitions
- This invention relates to an improved method of flame plating by means of detonations. More particularly, it relates to such a process wherein improved coatings are obtained by diluting the detonation reactants.
- an improvement over the basic detonation gun flame-plating process which process comprises the steps of introducing desired fuel and oxidant gases into a detonation gun, introducinga comminuted coating material into the gun, and detonating the resultant charge to heat and propel the coating material out of the gun onto an article to be coated.
- the improvement comprises adding an inert diluting gas in an amount between about 25 and 55 percent by volume of the total gas present in the gun.
- the detonation-gun plating process covered in United States Patent No. 2,714,563 is quite useful for applying refractory coatings, such as tungsten carbide associated with or without lower melting point binder metals such as cobalt.
- This process comprises providing a detonable mixture of oxidant and fuel in a detonation gun havinga mixing and ignition chamber and an elongated barrel, introducing a power into the barrel, igniting the detonable mixture and impinging the powder onto a workpiece to form a dense, adherent coating.
- This coating consists of irregularly shaped microscopic leaves or lamellules interlocking and overlapping with each other.
- control of the detonation coating conditions is obtained principally by varying the detonation mixture both in ratio of oxidant to fuel and in use of different combustant materials.
- This prior art process has shortcomings when used with particular coating mixtures and especially when impact resistant coatings are desired. For example, in protecting compressor blade wear surfaces, a coating is required which is hard enough to give resistance to wear caused by rubbing and also is resilient enoughto withstand impact forces without failure. This latter characteristic is provided by measurable increased modulus of rupture of the coating. Prior detonation-applied coatings have not had sufficient impact resistance.
- Some coating mixtures such as tungsten carbide-chror'nium carbide-nickel as disclosed in application Serial No. 738,300 of J. F. Pelton et al., filed concurrently herewith, and chromium carbide-nickel-chromium as disclosed in application Serial No. 738,299 of I. F. Pelton et al., also filed concurrently herewith, are difficult to apply as dense, adherent coatings by means'of the abovedisclosed detonation process. These coating mixtures are particularly useful in that they result in coatings having improved corrosion and high-temperature oxidation resistance and improved surface finish for precision surfaces, such as those found on gage blocks.
- An improved detonation-plating process has been developed which overcomes the disadvantages of the prior art.
- This process comprises adding between about 25 and 55 percent by volume of the total gas present in the detonation gun as an inert gaseous diluent to the detonation mixture.
- inert is intended to include the chemically inert gases-argon, neon, krypton, xenon, heliumand also other gases such as nitrogen which will not react with the gases forming the detonable mixture nor more than slightly with the coating material. Nitrogen is preferred as the additive since it is relatively inexpensive and is readily available.
- the additive is preferably chemically inert to the coating material under the coating process conditions. There may be a slight nitriding effect when nitrogen is used as the diluent, but the nitride thus formed is quite hard and has good refractory properties.
- This improved process is useful in that it enables increased control to'be obtained over detonation-plating conditions.
- the gaseous diluent reduces or tends to reduce the flame temperature since it does not participate in the detonation reaction.
- Major changes in plating temperatures have been obtained in prior detonation gun processes by varying the mixtures of oxidant and fuel and by using different materials for oxidant and fuel.
- this control was still insufficient to produce acceptable coatings for particular mixtures and.applications.
- the oxidant/fuel ratio is changed, the detonation conditions change to often produce undesirable chemical changes in the coating.
- the present process adds the fine control necessary to enable the detonation-plating process to be used with an increased number of coating compositions and also for new and more widely useful applications based on these resulting coatings.
- Inert carrier gas streams have previously been used with prior detonation-plating processes to introduce coating material into the barrel of a detonation gun.
- the volume of this inert gas in the detonation mixture is relatively small, i.e., less than about 10 volume percent.
- the improved process requires at least about 25 volume percent total inert gas additive before an effective improvement results in the coatings.
- At above about 55 volume percent diluent it is found that the reaction temperature has been lowered to such an extent that inferlor coatings can result.
- These diluent values include any inert gas used as a carrier for injecting coating powder into the detonation gun.
- Different coating compositions have different preferred process diluent amounts, but they all lie within the above limits of 25 and 55 volume percent.
- the inert gas additive can be introduced to the detona tion mixture in any convenient manner. It could be introduced through the fuel line, the oxidant line, or through the coating powder inlet tube. Likewise, a sep' arate line could be used. V
- Tungsten carbide with cobalt binder is'a widely used coating mixture applied by means of the detonation coating process.
- Prior results using no inert gas diluent other than the powder carrier gas resulted in samples having coating modulus of rupture values of about 67,000. psi;
- a preferred addition of about 46 volume percent total nitrogen results in a tungsten carbide-cobalt coating having a modulus of rupture of about 106,000 p.s.i.
- This coating has considerably more impact resistance than similar coatings applied by prior nondiluted detonation processes. This result is believed to be caused in part by retention of higher amounts of cobalt binder in the final coating apparently resulting from lowered flame temperature of the nitrogen-containing detonation mixture.
- Coating mixtures of tungsten carbide-cobalt alloy con taining about 9 weight percent cobalt as applied by prior detonation processes resulted in coatings containing about 7 weight percent cobalt.
- Similar coatings applied by the improved detonation process employing 46 volume percent nitrogen addition contained about 15 weight percent cobalt.
- the cobalt content of the coatings produced by prior art methods has been limited by the raw materials available. It is impractical and almost impossible to obtain a tungsten carbide-cobalt alloy containing more than about 9 weight percent cobalt in powdered form necessary for coating. The higher cobalt content alloys are extremely difficult to pulverize.
- the hardness is decreased somewhat from about 1380 to about 1180 VPN, but the resulting coating is still hard enough to provide desirable wear resistance.
- the tungsten carbide in the form of WC retained in the coating also increased substantially upon use of nitrogen dilution. In prior tungsten carbide-cobalt coatings the final coating contained about 2-3 weight percent WC. In similar coatings obtained by the present invention, the WC content is about 30-40 weight percent. This factor, in combination with increased binder retention, helps to obtain the improved coating properties.
- the detonation mixture was ignited about four times per second and the resulting detonation and shock waves impinged the powder onto a metal workpiece to form a dense, adherent, wearresistant coating having improved impact resistance, a modulus of rupture 106,000 p.s.i., and a hardness of 1100 VPN as measured with a 300 gram load.
- EXAMPLE II Tungsten carbide-chromium carbide-nickel coating
- Acetylene at 1.55 c.f.m. and oxygen at 1.55 c.f.m. were introduced to a detonation gun to form a detonable mix ture having an oxygen/carbon atomic ratio of 1.0.
- Nitrogen was introduced through the acetylene line at 1.67 c.f.m.
- Finely divided powder having a composition of about 70 weight percent tungsten carbide (WC and lower carbides)--24 weight percent chromium carbide (Cr C and lower carbides)-6 weight percent nickel was fed into the barrel of the detonation gun by means of a 0.4 c.f.m nitrogen stream.
- the detonation mixture surrounding the coating particles thus contained 40 volume percent nitrogen.
- the detonation mixture was ignited about four times per second and the powder was impinged onto a metal workpiece to form a dense, adherent coating having improved surface finish and corrosion-resistant properties as well as having improved oxidation resistance. It had a hardness of 110 VPN as measured with a 300 gram load. This coating could not be satisfac- EXAMPLE III Chromium carbide-nickel-chromium coating Acetylene at 1.50 c.f.m and oxygen at 1.80 c.f.m. were introduced to a detonation gun to form a detonable mixture having an oxygen/ carbon atomic ratio of 1.2.
- Nitrogen was introduced through the acetylene line at 2.2 c.f.m. Finely divided powder having a composition of about 85 weight percent chromium carbide (Cr C )-15 weight percent nickel-chromium alloy percent nickel-20 percent chromium) was fed into the barrel of the detonation gun by means of a 0.6 c.f.m nitrogen stream. The detonation mixture surrounding the coating particles thus contained 46 volume percent nitrogen. The detonation mixture was ignited about four times per second and the powder was impinged onto a metal workpiece to form a dense, adherent coating having corrosion-resistance and high-temperature oxidation resistance properties and having a hardness between 800 and 850 VPN aspmeasured with a 300 gram load. This coating could likewise not be satisfactorily applied by prior detonation processes.
- the detonation mixture was ignited about four times per second and the resulting detonation and shock waves impinged the nickel powder onto a workpiece to form a dense nickel coating having an acceptable surface finish.
- nitrogen dilution is not used with this material, the resulting coating is unsatisfactory due to lumps and irregularities.
- EXAMPLE V Tungsten carbidc-chromium-nickel coating
- Acetylene at 1.83 c.f.m. and oxygen at 2.02 c.f.m. were introduced to a detonation gun in suflicient quantities to form a detonable mixture having an oxygen/carbon atomic ratio of 1.1.
- Nitrogen at 1.65 c.f.m. was introduced to this detonable mixture so as to constitute about 35 percent by volume.
- Finely divided tungsten carbide powder containing 20 weight percent metal alloy binder (80 percent chromium-2O percent nickel) was fed into the barrel of the detonation gun.
- the detonation mixture was ignited about four times per second and the powder was impinged onto a metal workpiece to form a dense adherent coating having a hardness of 1089 VPN.
- a detonation gun which comprises the steps of introducing desired fuel and oxidant gases into the gun to form a detonatable mixture, introducing a powdered coating material into said detonatable mixture within the gun, and detonating the fuel-oxidant mixture to impinge the coating material onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon atomic ratio between about 1.0 and 1.2 and containing inert diluting gas in an amount between about 25 and 55 percent by volume of the total gas present.
- the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon atomic ratio between about 1.0 and 1.2 and containing between about 25 and 55 percent by volume of the total gas present of a diluting gas composed of one or more of the group consisting of argon, neon, krypton, xenon, helium, and nitrogen.
- the improved process set forth in the inert diluting gas is nitrogen.
- a detonation gun having a mixing and ignition chamber and a barrel portion which comprises introducing desired fuel and oxidant gases into said gun through said mixing and ignition chamber, introducing a comminuted coating material into said barrel portion, and detonating the mixture within said gun to impinge the coating material onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing between about 25 and 55 percent by volume of the total gas present of an inert diluting gas.
- a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about weight percent tungsten carbide, 24 weight percent chromium carbide, and 6 weight percent nickel into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 40 percent of the total gas volume to act as a diluent in the detonable mixture.
- a detonation gun hava ing a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about 85 weight percent of chromium carbide and 15 weight percent of a nickel-chromium alloy percent nickel-20 percent chromium) into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 46 percent of the total gas volume to act as a diluent in the detonable mixture.
- a detonation gun having a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about 80 weight percent tungsten carbide and 20 weight percent of chromium-nickel alloy (80 percent chromium-20 percent nickel) into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 35 percent of the total gas volume to act as a diluent in the detonable mixture.
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- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
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- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
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Description
Feb. 21,
J- F. PELTON ACETELENE INERT GAS V OXYGE N/CARBONIC RATIO BETWEEN ABOUT |.o&1.2
INERT GAS ABOUT WC+CO BINDER, CrC,NiCr ALLOY, Ni POWDER,
WC Ni COATING lGNlTlON 25 TO 554 INERT IN RT GAS G55 5 r.Xe,He,N)
INERT GAS MIXING CHAMBER BARREL 4. OXYGEN INVENTOR.
JOHN F. PELTON E ZZWMXVM% A T TORNE Y FLAME PLATING USING DETONATION REACTANTS John F. Pelton, Indianapolis, lind., assignor to Union Carbide Corporation, a corporation of New York Filed May 28, 1953, Ser. No. 738,283 12 Claims. (Cl. 117-21) This invention relates to an improved method of flame plating by means of detonations. More particularly, it relates to such a process wherein improved coatings are obtained by diluting the detonation reactants.
According to this invention there is provided an improvement over the basic detonation gun flame-plating process, which process comprises the steps of introducing desired fuel and oxidant gases into a detonation gun, introducinga comminuted coating material into the gun, and detonating the resultant charge to heat and propel the coating material out of the gun onto an article to be coated. The improvement comprises adding an inert diluting gas in an amount between about 25 and 55 percent by volume of the total gas present in the gun.
As the industrial community has progressed, an increasing demand has resulted for materials and coatings which can withstand severe conditions of erosion, high temperature, and corrosion. For the most part, the desired refractory, wear-resistant compositions could not be applied by known prior art methods. 7
The detonation-gun plating process covered in United States Patent No. 2,714,563 is quite useful for applying refractory coatings, such as tungsten carbide associated with or without lower melting point binder metals such as cobalt. This process comprises providing a detonable mixture of oxidant and fuel in a detonation gun havinga mixing and ignition chamber and an elongated barrel, introducing a power into the barrel, igniting the detonable mixture and impinging the powder onto a workpiece to form a dense, adherent coating. This coating consists of irregularly shaped microscopic leaves or lamellules interlocking and overlapping with each other.
As disclosed in the above patent, control of the detonation coating conditions is obtained principally by varying the detonation mixture both in ratio of oxidant to fuel and in use of different combustant materials. This prior art process has shortcomings when used with particular coating mixtures and especially when impact resistant coatings are desired. For example, in protecting compressor blade wear surfaces, a coating is required which is hard enough to give resistance to wear caused by rubbing and also is resilient enoughto withstand impact forces without failure. This latter characteristic is provided by measurable increased modulus of rupture of the coating. Prior detonation-applied coatings have not had sufficient impact resistance.
Some coating mixtures such as tungsten carbide-chror'nium carbide-nickel as disclosed in application Serial No. 738,300 of J. F. Pelton et al., filed concurrently herewith, and chromium carbide-nickel-chromium as disclosed in application Serial No. 738,299 of I. F. Pelton et al., also filed concurrently herewith, are difficult to apply as dense, adherent coatings by means'of the abovedisclosed detonation process. These coating mixtures are particularly useful in that they result in coatings having improved corrosion and high-temperature oxidation resistance and improved surface finish for precision surfaces, such as those found on gage blocks.
atent O Patented Feb. 21, 1961 It is a principal object of this invention to provide an improved process for the operation of a detonation gun for flame-plating whereby improved coatings may be obtained.
In the drawing the single figure is a diagram of the detonation gun having legends indicating materials used.
An improved detonation-plating process has been developed which overcomes the disadvantages of the prior art. This process comprises adding between about 25 and 55 percent by volume of the total gas present in the detonation gun as an inert gaseous diluent to the detonation mixture. The term inert is intended to include the chemically inert gases-argon, neon, krypton, xenon, heliumand also other gases such as nitrogen which will not react with the gases forming the detonable mixture nor more than slightly with the coating material. Nitrogen is preferred as the additive since it is relatively inexpensive and is readily available. In order not to change the oxidation-reduction potential of the detona tion flame, the additive is preferably chemically inert to the coating material under the coating process conditions. There may be a slight nitriding effect when nitrogen is used as the diluent, but the nitride thus formed is quite hard and has good refractory properties. I I
This improved process is useful in that it enables increased control to'be obtained over detonation-plating conditions. The gaseous diluent reduces or tends to reduce the flame temperature since it does not participate in the detonation reaction. Major changes in plating temperatures have been obtained in prior detonation gun processes by varying the mixtures of oxidant and fuel and by using different materials for oxidant and fuel. However, this control was still insufficient to produce acceptable coatings for particular mixtures and.applications. Also, whenever the oxidant/fuel ratio is changed, the detonation conditions change to often produce undesirable chemical changes in the coating. The present process adds the fine control necessary to enable the detonation-plating process to be used with an increased number of coating compositions and also for new and more widely useful applications based on these resulting coatings.
Inert carrier gas streams have previously been used with prior detonation-plating processes to introduce coating material into the barrel of a detonation gun. The volume of this inert gas in the detonation mixture is relatively small, i.e., less than about 10 volume percent.
It thus did not help materially to improve the coating results.
It has been found according to the present invention that the improved process requires at least about 25 volume percent total inert gas additive before an effective improvement results in the coatings. At above about 55 volume percent diluent it is found that the reaction temperature has been lowered to such an extent that inferlor coatings can result. These diluent values include any inert gas used as a carrier for injecting coating powder into the detonation gun. Different coating compositions have different preferred process diluent amounts, but they all lie within the above limits of 25 and 55 volume percent.
The inert gas additive can be introduced to the detona tion mixture in any convenient manner. It could be introduced through the fuel line, the oxidant line, or through the coating powder inlet tube. Likewise, a sep' arate line could be used. V
Tungsten carbide with cobalt binder is'a widely used coating mixture applied by means of the detonation coating process. Prior results using no inert gas diluent other than the powder carrier gas resulted in samples having coating modulus of rupture values of about 67,000. psi; A preferred addition of about 46 volume percent total nitrogen results in a tungsten carbide-cobalt coating having a modulus of rupture of about 106,000 p.s.i. This coating has considerably more impact resistance than similar coatings applied by prior nondiluted detonation processes. This result is believed to be caused in part by retention of higher amounts of cobalt binder in the final coating apparently resulting from lowered flame temperature of the nitrogen-containing detonation mixture. Coating mixtures of tungsten carbide-cobalt alloy con taining about 9 weight percent cobalt as applied by prior detonation processes resulted in coatings containing about 7 weight percent cobalt. Similar coatings applied by the improved detonation process employing 46 volume percent nitrogen addition contained about 15 weight percent cobalt. The cobalt content of the coatings produced by prior art methods has been limited by the raw materials available. It is impractical and almost impossible to obtain a tungsten carbide-cobalt alloy containing more than about 9 weight percent cobalt in powdered form necessary for coating. The higher cobalt content alloys are extremely difficult to pulverize. The hardness is decreased somewhat from about 1380 to about 1180 VPN, but the resulting coating is still hard enough to provide desirable wear resistance. The tungsten carbide in the form of WC retained in the coating also increased substantially upon use of nitrogen dilution. In prior tungsten carbide-cobalt coatings the final coating contained about 2-3 weight percent WC. In similar coatings obtained by the present invention, the WC content is about 30-40 weight percent. This factor, in combination with increased binder retention, helps to obtain the improved coating properties.
The following examples describe the use of this improved process for applying particular coating compositions.
EXAMPLE I Tungsten carbide-cobalt coating Acetylene at 1.65 c.f.m. and oxygen at 1.65 c.f.m. were introduced to a detonation gun to form a detonable mixture having an oxygen/ carbon atomic ratio of 1.0. Nitrogen was introduced through the acetylene line at 2.2 c.f.m. Finely divided (less than 325 mesh) tungsten carbide-cobalt powder containing about 9 weight percent cobalt was fed into the barrel of the detonation gun by means of a 0.6 c.f.m. nitrogen stream. The detonation mixture surrounding the coating particles thus contained 46 volume percent nitrogen. The detonation mixture was ignited about four times per second and the resulting detonation and shock waves impinged the powder onto a metal workpiece to form a dense, adherent, wearresistant coating having improved impact resistance, a modulus of rupture 106,000 p.s.i., and a hardness of 1100 VPN as measured with a 300 gram load.
EXAMPLE II Tungsten carbide-chromium carbide-nickel coating Acetylene at 1.55 c.f.m. and oxygen at 1.55 c.f.m. were introduced to a detonation gun to form a detonable mix ture having an oxygen/carbon atomic ratio of 1.0. Nitrogen was introduced through the acetylene line at 1.67 c.f.m. Finely divided powder having a composition of about 70 weight percent tungsten carbide (WC and lower carbides)--24 weight percent chromium carbide (Cr C and lower carbides)-6 weight percent nickel was fed into the barrel of the detonation gun by means of a 0.4 c.f.m nitrogen stream. The detonation mixture surrounding the coating particles thus contained 40 volume percent nitrogen. The detonation mixture was ignited about four times per second and the powder was impinged onto a metal workpiece to form a dense, adherent coating having improved surface finish and corrosion-resistant properties as well as having improved oxidation resistance. It had a hardness of 110 VPN as measured with a 300 gram load. This coating could not be satisfac- EXAMPLE III Chromium carbide-nickel-chromium coating Acetylene at 1.50 c.f.m and oxygen at 1.80 c.f.m. were introduced to a detonation gun to form a detonable mixture having an oxygen/ carbon atomic ratio of 1.2. Nitrogen was introduced through the acetylene line at 2.2 c.f.m. Finely divided powder having a composition of about 85 weight percent chromium carbide (Cr C )-15 weight percent nickel-chromium alloy percent nickel-20 percent chromium) was fed into the barrel of the detonation gun by means of a 0.6 c.f.m nitrogen stream. The detonation mixture surrounding the coating particles thus contained 46 volume percent nitrogen. The detonation mixture was ignited about four times per second and the powder was impinged onto a metal workpiece to form a dense, adherent coating having corrosion-resistance and high-temperature oxidation resistance properties and having a hardness between 800 and 850 VPN aspmeasured with a 300 gram load. This coating could likewise not be satisfactorily applied by prior detonation processes.
EXAMPLE IV Nickel metal coating Acetylene at 1.65 c.f.m. and oxygen at 1.65 c.f.m. were introduced to a detonation gun to form a detonable mixture having an oxygen/ carbon atomic ratio of 1.0. Nitrogen was additionally introduced through the acetylene line at 2.2 c.f.m. Finely divided nickel metal powder was fed into the barrel of the detonation gun by means of a 0.6 c.f.m. nitrogen carrier gas stream. The detonation mixture surrounding the coating particles thus contained about 46 volume percent nitrogen. The detonation mixture was ignited about four times per second and the resulting detonation and shock waves impinged the nickel powder onto a workpiece to form a dense nickel coating having an acceptable surface finish. When nitrogen dilution is not used with this material, the resulting coating is unsatisfactory due to lumps and irregularities.
EXAMPLE V Tungsten carbidc-chromium-nickel coating Acetylene at 1.83 c.f.m. and oxygen at 2.02 c.f.m. were introduced to a detonation gun in suflicient quantities to form a detonable mixture having an oxygen/carbon atomic ratio of 1.1. Nitrogen at 1.65 c.f.m. was introduced to this detonable mixture so as to constitute about 35 percent by volume. Finely divided tungsten carbide powder containing 20 weight percent metal alloy binder (80 percent chromium-2O percent nickel) was fed into the barrel of the detonation gun. The detonation mixture was ignited about four times per second and the powder was impinged onto a metal workpiece to form a dense adherent coating having a hardness of 1089 VPN.
It may be seen from the above examples that the use of the instant process greatly improved previously attained coatings and made possible other coatings that were unsatisfactory when performed by known processes. It will be noticed from Examples I, III, and IV that a nitrogen concentration in the total gas of about 46 volume percent appears to be within an optimum level for a number of different coatings. However, as is evident from Examples Ii and V, the exact dilution for best results should be adjusted according to the compositions employed and the coating properties desired. As stated above, however, this dilution will always be between about 25 and 55 volume percent. The specific examples of coatings applied by the improved process are only illustrative of inherent advantages residing therein and are not intended to be construed as limiting in any manner.
What is claimed is:
1. In the process of flame plating with a detonation gun which comprises the steps of introducing desired fuel and oxidant gases into the gun to form a detonatable mixture, introducing a powdered coating material into said detonatable mixture within the gun, and detonating the fuel-oxidant mixture to impinge the coating material onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon atomic ratio between about 1.0 and 1.2 and containing inert diluting gas in an amount between about 25 and 55 percent by volume of the total gas present.
2. In the process of flame plating with a detonation gun which comprises the steps of introducing desired fuel and oxidant gases into the gun to form a detonatable mixture, introducing a powdered coating material into said detonatable mixture within the gun, and detonating the fuel-oxidant mixture to impinge the coating material onto the article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon atomic ratio between about 1.0 and 1.2 and containing between about 25 and 55 percent by volume of the total gas present of a diluting gas composed of one or more of the group consisting of argon, neon, krypton, xenon, helium, and nitrogen.
3. The improved process set forth in the inert diluting gas is nitrogen.
4. The improved process set forth in claim 1 wherein the inert diluting gas is argon.
5. In the process for operating a detonation gun having a mixing and ignition chamber and a barrel portion which comprises introducing desired fuel and oxidant gases into said gun through said mixing and ignition chamber, introducing a comminuted coating material into said barrel portion, and detonating the mixture within said gun to impinge the coating material onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing between about 25 and 55 percent by volume of the total gas present of an inert diluting gas.
6. The improved process set forth in claim 5 above in which at least part of the inert diluting gas is introduced into the gun as an entraining medium for the comminuted coating material.
7. The improved process set forth in claim 5 above in which at least part of said inert diluting gas is intro duced through the mixing and ignition chamber with the fuel and oxidant gases.
8. In the process for operating a detonation gun having a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about 91 weight percent of tungsten carbide and 9 weight percent of cobalt into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 46 percent of the total gas volume to act as a diluent in the detonable mixture.
9. In a process for operating a detonation gun having claim 1 wherein a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about weight percent tungsten carbide, 24 weight percent chromium carbide, and 6 weight percent nickel into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 40 percent of the total gas volume to act as a diluent in the detonable mixture.
10. In the process for operating a detonation gun hava ing a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about 85 weight percent of chromium carbide and 15 weight percent of a nickel-chromium alloy percent nickel-20 percent chromium) into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 46 percent of the total gas volume to act as a diluent in the detonable mixture.
11. In the process for operating a detonation gun having a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising finely divided nickel powder into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 46 percent of the total gas volume to act as a diluent in the detonable mixture.
12. In the process for operating a detonation gun having a mixing and ignition chamber and a barrel portion which comprises the steps of introducing desired fuel and oxidant gas through said ignition and mixing chamber, introducing a comminuted coating composition comprising about 80 weight percent tungsten carbide and 20 weight percent of chromium-nickel alloy (80 percent chromium-20 percent nickel) into the barrel portion of the gun and detonating the mixture to propel the coating composition out of the front end of the gun onto an article to be coated, the improvement which comprises using a detonatable fuel-oxidant mixture having an oxygen/carbon ratio between about 1.0 and 1.2 and containing nitrogen at a concentration of about 35 percent of the total gas volume to act as a diluent in the detonable mixture.
References Cited in the file of this patent UNITED STATES PATENTS
Claims (1)
1. IN THE PROCESS OF FLAME PLATING WITH A DETONATION GUN WHICH COMPRISES THE STEPS OF INTRODUCING DESIRED FUEL AND OXIDANT GASES INTO THE GUN TO FORM A DETONATABLE MIXTURE, INTRODUCING A POWDERED COATING MATERIAL INTO SAID DETONATABLE MIXTURE WITHIN THE GUN, AND DETONATING THE FUEL-OXIDANT MIXTURE TO IMPINGE THE COATING MATERIAL ONTO AN ARTICLE TO BE COATED, THE IMPROVEMENT WHICH COMPRISES USING A DETONATABLE FUEL-OXIDANT MIXTURE HAVING AN OXYGEN/CARBON ATOMIC RATIO BETWEEN ABOUT 1.0 AND 1.2 AND CONTAINING INERT DILUTING GAS IN AN AMOUNT BETWEEN ABOUT 25 AND 55 PERCENT BY VOLUME OF THE TOTAL GAS PRESENT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US738283A US2972550A (en) | 1958-05-28 | 1958-05-28 | Flame plating using detonation reactants |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US738283A US2972550A (en) | 1958-05-28 | 1958-05-28 | Flame plating using detonation reactants |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2972550A true US2972550A (en) | 1961-02-21 |
Family
ID=24967348
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US738283A Expired - Lifetime US2972550A (en) | 1958-05-28 | 1958-05-28 | Flame plating using detonation reactants |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2972550A (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3071489A (en) * | 1958-05-28 | 1963-01-01 | Union Carbide Corp | Process of flame spraying a tungsten carbide-chromium carbide-nickel coating, and article produced thereby |
| US3195217A (en) * | 1959-08-14 | 1965-07-20 | Westinghouse Electric Corp | Applying layers of materials to semiconductor bodies |
| US3230097A (en) * | 1962-05-31 | 1966-01-18 | Gen Electric | Coating composition |
| US3326714A (en) * | 1964-01-08 | 1967-06-20 | Union Carbide Corp | Wear and corrosion resistant coating |
| US3915381A (en) * | 1971-11-15 | 1975-10-28 | Southwest Res Inst | Method and apparatus for applying particulate coating material to a work piece |
| US3941903A (en) * | 1972-11-17 | 1976-03-02 | Union Carbide Corporation | Wear-resistant bearing material and a process for making it |
| US4067291A (en) * | 1974-04-08 | 1978-01-10 | H. B. Zachry Company | Coating system using tape encapsulated particulate coating material |
| EP0189053A1 (en) * | 1985-01-17 | 1986-07-30 | Linde Aktiengesellschaft | Method for applying solder |
| US4826734A (en) * | 1988-03-03 | 1989-05-02 | Union Carbide Corporation | Tungsten carbide-cobalt coatings for various articles |
| US4902539A (en) * | 1987-10-21 | 1990-02-20 | Union Carbide Corporation | Fuel-oxidant mixture for detonation gun flame-plating |
| US4999255A (en) * | 1989-11-27 | 1991-03-12 | Union Carbide Coatings Service Technology Corporation | Tungsten chromium carbide-nickel coatings for various articles |
| US5075129A (en) * | 1989-11-27 | 1991-12-24 | Union Carbide Coatings Service Technology Corporation | Method of producing tungsten chromium carbide-nickel coatings having particles containing three times by weight more chromium than tungsten |
| US5223332A (en) * | 1990-05-31 | 1993-06-29 | Praxair S.T. Technology, Inc. | Duplex coatings for various substrates |
| EP0688886A1 (en) | 1994-06-24 | 1995-12-27 | Praxair S.T. Technology, Inc. | A process for producing carbide particles dispersed in a MCrAIY-based coating |
| EP0688885A1 (en) | 1994-06-24 | 1995-12-27 | Praxair S.T. Technology, Inc. | A process for producing an oxide dispersed MCrAIY-based coating |
| US6004372A (en) * | 1999-01-28 | 1999-12-21 | Praxair S.T. Technology, Inc. | Thermal spray coating for gates and seats |
| 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 |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2714563A (en) * | 1952-03-07 | 1955-08-02 | Union Carbide & Carbon Corp | Method and apparatus utilizing detonation waves for spraying and other purposes |
-
1958
- 1958-05-28 US US738283A patent/US2972550A/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2714563A (en) * | 1952-03-07 | 1955-08-02 | Union Carbide & Carbon Corp | Method and apparatus utilizing detonation waves for spraying and other purposes |
Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3071489A (en) * | 1958-05-28 | 1963-01-01 | Union Carbide Corp | Process of flame spraying a tungsten carbide-chromium carbide-nickel coating, and article produced thereby |
| US3195217A (en) * | 1959-08-14 | 1965-07-20 | Westinghouse Electric Corp | Applying layers of materials to semiconductor bodies |
| US3230097A (en) * | 1962-05-31 | 1966-01-18 | Gen Electric | Coating composition |
| US3326714A (en) * | 1964-01-08 | 1967-06-20 | Union Carbide Corp | Wear and corrosion resistant coating |
| US3915381A (en) * | 1971-11-15 | 1975-10-28 | Southwest Res Inst | Method and apparatus for applying particulate coating material to a work piece |
| US3941903A (en) * | 1972-11-17 | 1976-03-02 | Union Carbide Corporation | Wear-resistant bearing material and a process for making it |
| US4067291A (en) * | 1974-04-08 | 1978-01-10 | H. B. Zachry Company | Coating system using tape encapsulated particulate coating material |
| EP0189053A1 (en) * | 1985-01-17 | 1986-07-30 | Linde Aktiengesellschaft | Method for applying solder |
| US4902539A (en) * | 1987-10-21 | 1990-02-20 | Union Carbide Corporation | Fuel-oxidant mixture for detonation gun flame-plating |
| EP0331499A1 (en) * | 1988-03-03 | 1989-09-06 | Praxair S.T. Technology, Inc. | Articles with tungsten carbide-cobalt coatings |
| US4826734A (en) * | 1988-03-03 | 1989-05-02 | Union Carbide Corporation | Tungsten carbide-cobalt coatings for various articles |
| US4999255A (en) * | 1989-11-27 | 1991-03-12 | Union Carbide Coatings Service Technology Corporation | Tungsten chromium carbide-nickel coatings for various articles |
| US5075129A (en) * | 1989-11-27 | 1991-12-24 | Union Carbide Coatings Service Technology Corporation | Method of producing tungsten chromium carbide-nickel coatings having particles containing three times by weight more chromium than tungsten |
| AU638182B2 (en) * | 1989-11-27 | 1993-06-17 | Union Carbide Coatings Service Technology Corp. | Process for producing tungsten chromium carbide-nickel coatings for various articles |
| US5223332A (en) * | 1990-05-31 | 1993-06-29 | Praxair S.T. Technology, Inc. | Duplex coatings for various substrates |
| EP0688886A1 (en) | 1994-06-24 | 1995-12-27 | Praxair S.T. Technology, Inc. | A process for producing carbide particles dispersed in a MCrAIY-based coating |
| EP0688885A1 (en) | 1994-06-24 | 1995-12-27 | Praxair S.T. Technology, Inc. | A process for producing an oxide dispersed MCrAIY-based coating |
| US5652028A (en) * | 1994-06-24 | 1997-07-29 | Praxair S.T. Technology, Inc. | Process for producing carbide particles dispersed in a MCrAlY-based coating |
| US5741556A (en) * | 1994-06-24 | 1998-04-21 | Praxair S.T. Technology, Inc. | Process for producing an oxide dispersed MCrAlY-based coating |
| US6004372A (en) * | 1999-01-28 | 1999-12-21 | Praxair S.T. Technology, Inc. | Thermal spray coating for gates and seats |
| 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 |
| EP2767609A1 (en) | 2013-02-14 | 2014-08-20 | Praxair S.T. Technology, Inc. | Selective oxidation of a modified MCrAIY composition loaded with high levels of ceramic acting as a barrier to specific oxide formations |
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