EP2913421A1 - Coated article and method for production coating - Google Patents
Coated article and method for production coating Download PDFInfo
- Publication number
- EP2913421A1 EP2913421A1 EP15156132.1A EP15156132A EP2913421A1 EP 2913421 A1 EP2913421 A1 EP 2913421A1 EP 15156132 A EP15156132 A EP 15156132A EP 2913421 A1 EP2913421 A1 EP 2913421A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- ceramic
- erosion resistance
- modified
- chromium
- anodic material
- 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.)
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Links
- 238000000576 coating method Methods 0.000 title claims abstract description 44
- 239000011248 coating agent Substances 0.000 title claims abstract description 43
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 7
- 239000000919 ceramic Substances 0.000 claims abstract description 106
- 230000003628 erosive effect Effects 0.000 claims abstract description 58
- 239000002245 particle Substances 0.000 claims abstract description 58
- 239000000758 substrate Substances 0.000 claims abstract description 46
- 239000010405 anode material Substances 0.000 claims abstract description 45
- 239000011159 matrix material Substances 0.000 claims abstract description 24
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 9
- 238000005755 formation reaction Methods 0.000 claims abstract description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 22
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 claims description 16
- CXOWYMLTGOFURZ-UHFFFAOYSA-N azanylidynechromium Chemical compound [Cr]#N CXOWYMLTGOFURZ-UHFFFAOYSA-N 0.000 claims description 13
- 239000011651 chromium Substances 0.000 claims description 13
- 229910003470 tongbaite Inorganic materials 0.000 claims description 13
- 238000000034 method Methods 0.000 claims description 11
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 9
- 229910052804 chromium Inorganic materials 0.000 claims description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 6
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 claims description 6
- 230000003993 interaction Effects 0.000 claims description 4
- 229910000951 Aluminide Inorganic materials 0.000 claims description 3
- SJKRCWUQJZIWQB-UHFFFAOYSA-N azane;chromium Chemical compound N.[Cr] SJKRCWUQJZIWQB-UHFFFAOYSA-N 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 239000002344 surface layer Substances 0.000 claims description 3
- 238000005260 corrosion Methods 0.000 description 14
- 230000007797 corrosion Effects 0.000 description 14
- 239000007921 spray Substances 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 238000000151 deposition Methods 0.000 description 4
- 230000008021 deposition Effects 0.000 description 4
- 239000007789 gas Substances 0.000 description 4
- 230000003746 surface roughness Effects 0.000 description 3
- 238000005229 chemical vapour deposition Methods 0.000 description 2
- 238000005328 electron beam physical vapour deposition Methods 0.000 description 2
- 238000010286 high velocity air fuel Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 238000005054 agglomeration Methods 0.000 description 1
- 230000002776 aggregation Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000003518 caustics Substances 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000007766 curtain coating Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001652 electrophoretic deposition Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000002386 leaching Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000007788 roughening Methods 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000007581 slurry coating method Methods 0.000 description 1
- 238000001694 spray drying Methods 0.000 description 1
- 238000010345 tape casting Methods 0.000 description 1
- 238000001771 vacuum deposition Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
-
- 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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
Definitions
- the present invention is directed to a coated article and a method for producing a coating. More specifically, the present invention is directed to a coated article and a method for producing a coating containing an anodic material and ceramic particles.
- Gas and steam turbine components particularly rear stage gas turbine compressor blades, rear stage gas turbine compressor vanes and centrifugal pump impellers, in addition to pipelines, are subjected to water droplet erosion, particulate deposition and corrosion pitting induced cracking issues caused by on-line water washing.
- the preceding surface degradation mechanisms may also result in undesirable increases in surface roughness.
- Fouling of components may cause corrosion of the components underneath the deposits through a crevice corrosion mechanism. Additionally, particulates in the intake air may cause erosion through foreign object damage to the components thereby causing corrosion.
- Water wash cycles are often performed to remove the particulates that have built up on the components. However, the water wash cycles expose the components to increased amounts of moisture, which may cause corrosion of the components by dissolving and leaching corrosive agents entrapped in the surface deposits, and accelerated corrosion to any portions of the components damaged by foreign object damage.
- the water wash cycles may utilize chemicals to remove complex particulate buildup. These chemicals may increase corrosion of the components and increase maintenance cost of the components.
- Coating systems which require more than one coating layer to address corrosion, oxidation, fouling and/or erosion are undesirable because multiple layers may result in excessive overall thickness of the component so coated. Additionally, multiple coatings may increase the likelihood of undesirable alterations in the aerodynamics or fluid dynamics of the component, or detrimental increases in the weight of the component.
- Unchecked corrosion, oxidation, fouling and/or erosion of the exposed surfaces of the gas turbine or steam turbine components, or of pipelines, may result in undesirable increases in surface roughness, thereby decreasing the efficiency.
- Coated components and methods for producing coated components that do not suffer from one or more of the above drawbacks would be desirable in the art.
- a method for producing a coating includes providing a substrate defining a substrate surface having a substrate erosion resistance and applying a matrix and ceramic particles to the substrate surface.
- the matrix includes an anodic material having an anodic erosion resistance.
- the ceramic particles include a first ceramic having a first ceramic erosion resistance and a second ceramic having a second ceramic erosion resistance.
- the first ceramic erosion resistance is greater than the second ceramic erosion resistance, greater than the anodic erosion resistance, and greater than the substrate erosion resistance.
- the second ceramic interacts inchoately with the anodic material during the applying to form modified ceramic particles and modified anodic material formations.
- the modified ceramic particles are capable of forming a passive oxide film.
- a coated article in another embodiment, includes a substrate defining a substrate surface having a substrate erosion resistance and a coating on the substrate surface.
- the coating includes a matrix and ceramic particles.
- the matrix includes an anodic material having an anodic erosion resistance.
- the ceramic particles include a first ceramic having a first ceramic erosion resistance and a second ceramic having a second ceramic erosion resistance.
- the coating also includes modified ceramic particles and modified anodic material formations formed by an inchoate interaction between the second ceramic and the anodic material.
- the first ceramic erosion resistance is greater than the second ceramic erosion resistance, greater than the anodic erosion resistance, and greater than the substrate erosion resistance.
- the modified ceramic particles are capable of forming a passive oxide film.
- a coated article and a method for producing a coating are provided.
- Embodiments of the present disclosure in comparison to methods and articles not using one or more of the features disclosed herein, decrease substrate corrosion, decrease substrate oxidation, decrease substrate fouling, decrease substrate erosion, decrease the rate at which the surface roughness of a substrate increases, decrease maintenance costs, increase efficiency, or a combination thereof.
- a coated article 100 is depicted.
- the coated article 100 is any suitable component, for example, a compressor blade 102 (shown), a compressor vane, a centrifugal pump impeller or a pipeline.
- blade as used herein is intended to be synonymous with the term "bucket.”
- the coated article 100 includes a substrate 202 defining a substrate surface 204 having a substrate erosion resistance, and a coating 206 on the substrate surface 204.
- the coating 206 includes a matrix 210 including an anodic material 212 having an anodic erosion resistance, and ceramic particles 214.
- the anodic material 212 may be anodic with respect to the substrate 202.
- the ceramic particles 214 include a first ceramic 216 having a first ceramic erosion resistance and a second ceramic 218 having a second ceramic erosion resistance.
- the coating 206 also includes modified ceramic particles 220 and modified anodic material formations 222 formed from an inchoate interaction between the second ceramic 218 and the anodic material 212.
- the coating 206 defines a coating surface 224 which is exposed to the external environment.
- the first ceramic erosion resistance is greater than the second ceramic erosion resistance, greater than the anodic erosion resistance, and greater than the substrate erosion resistance.
- the anodic material 212 includes Cr 70% Ni 30% (wt%), a mixture of Ni 80 %Al 20 % (wt%) and Ni 95% Al 5% (wt%), cobalt and aluminum particles in a sacrificial metallic undercoat with a ceramic overcoat, a metallurgically bonded aluminide with an aluminum surface layer, NiCrAl, or a combination thereof.
- the anoidic material is Cr 70% Ni 30% (wt%).
- the anodic material 212 is operative to protect the substrate surface 204 from corrosion during downtime, which is endemic in peaking turbine components and not uncommon even in base loaded turbine components.
- the first ceramic 216 is tungsten carbide and the second ceramic 218 is chromium carbide, chromium nitride or a combination of chromium carbide and chromium nitride.
- the anodic material 212 contains chromium and nickel, and the second ceramic interacts inchoately with the chromium and nickel in the anodic material 212 during the applying to form the modified ceramic particles 220 and the modified anodic material formations 222.
- the modified ceramic particles 220 include at least one of modified chromium carbide particles having a range of chromium carbide stoichiometries and modified chromium nitride particles having a range of chromium nitride stoichiometries.
- modified chromium carbide particles having a range of chromium carbide stoichiometries
- modified chromium nitride particles having a range of chromium nitride stoichiometries.
- the coating 206 contains from about 30% to about 60% by weight tungsten carbide, alternatively from about 30% to about 40%, alternatively from about 40% to about 50%, alternatively from about 50% to about 60%. In an additional embodiment, the coating 206 further contains from about 20% to about 50% by weight of one or both of chromium carbide and chromium nitride, alternatively from about 20% to about 30%, alternatively from about 30% to about 40% alternatively from about 40% to about 50%. In a further embodiment, the coating 206 also contain balance essentially anodic material 212.
- the modified ceramic particles 220 are capable of forming a passive oxide film 302.
- the passive oxide film 302 forms under standard rear stage turbine compressor operating conditions.
- Known rear stage turbine compressor operating conditions include, for example, elevated pressures 10-25 times atmospheric pressure, and being subjected to adiabatic heating to 250-677 °C.
- the passive oxide film 302 defines the coating surface 224.
- the passive oxide film 302 resists increases in the roughness of the coating surface 224 caused by oxidation. Without being bound by theory, it is believed that because the passive oxide film 302 include materials which are oxides, these materials will not undergo further oxidation.
- the passive oxide film 302 is uniformly, or substantially uniformly, distributed on the matrix 210.
- the passive oxide film 302 has a thickness of between about 0.1 ⁇ m to about 3 ⁇ m, alternatively between about 0.1 ⁇ m to about 2 ⁇ m, alternatively between about 0.1 ⁇ m to about 1 ⁇ m, alternatively between about 1 ⁇ m to about 2 ⁇ m, alternatively between about 2 ⁇ m to about 3 ⁇ m, alternatively between about 0.1 ⁇ m to about 1.5 ⁇ m, alternatively between about 1.5 ⁇ m to about 3 ⁇ m, alternatively between about 0.1 ⁇ m to about 0.5 ⁇ m, alternatively between about 0.5 ⁇ m to about 1 ⁇ m, alternatively between about 1 ⁇ m to about 1.5 ⁇ m, alternatively between about 1.5 ⁇ m to about 2 ⁇ m.
- the coating 206 is produced by any suitable method.
- a method for applying the coating 206 includes providing the substrate 202 defining the substrate surface 204 and applying the matrix 210 and the ceramic particles 214 to the substrate surface 204. Applying the matrix 210 and the ceramic particles 214 to the substrate surface 204 may be accomplished by any suitable coating techniques, such as, but not limited to, thermal spray, air plasma spray (APS), high velocity oxygen fuel (HVOF) thermal spray, high velocity air fuel spraying (HVAF), vacuum plasma spray (VPS), electron-beam physical vapor deposition (EBPVD), chemical vapor deposition (CVD), ion plasma deposition (IPD), combustion spraying with powder or rod, cold spray, sol gel, electrophoretic deposition, tape casting, polymer derived ceramic coating, slurry coating, dip-application, vacuum-coating application, curtain-coating application, brush-application, roll-coat application, and agglomeration and sintering followed by spray drying.
- suitable coating techniques such as, but not limited to, thermal spray,
- the ceramic particles 214 have an average particle diameter ranging from about 0.3 ⁇ m to about 5 ⁇ m, alternatively from about 0.3 ⁇ m to about 2.5 ⁇ m, alternatively from about 2.5 ⁇ m to about 5 ⁇ m, alternatively from about 0.3 ⁇ m to about 2 ⁇ m, alternatively from about 2 ⁇ m to about 3.5 ⁇ m, alternatively from about 3.5 ⁇ m to about 5 ⁇ m, alternatively from about 0.3 ⁇ m to about 1 ⁇ m, alternatively from about 2 ⁇ m to about 3 ⁇ m, alternatively from about 3 ⁇ m to about 4 ⁇ m, alternatively from about 4 ⁇ m to about 5 ⁇ m.
- the coating 206 has an average distance between the ceramic particles 214 ranging from about 0.2 ⁇ m to about 2 ⁇ m, alternatively from about 0.2 ⁇ m to about 1 ⁇ m, alternatively from about 1 ⁇ m to about 2 ⁇ m, alternatively from about 0.2 ⁇ m to about 0.8 ⁇ m, alternatively from about 0.8 ⁇ m to about 1.4 ⁇ m, alternatively from about 1.4 ⁇ m to about 2 ⁇ m.
- the coating 206 has a thickness of between about 50 ⁇ m to about 250 ⁇ m, alternatively between about 50 ⁇ m to about 150 ⁇ m, alternatively between about 100 ⁇ m to about 200 ⁇ m, alternatively between about 150 ⁇ m to about 250 ⁇ m, alternatively between about 50 ⁇ m to about 100 ⁇ m, alternatively between about 100 ⁇ m to about 150 ⁇ m, alternatively between about 150 ⁇ m to about 200 ⁇ m, alternatively between about 200 ⁇ m to about 250 ⁇ m.
- the coating 206 consists essentially of a single matrix 210 of anodic material 212 with a plurality of ceramic particles 214 dispersed therein.
- a single matrix 210 of anodic material 212 allows for the thickness of the coating 206 to be minimized.
- the ceramic particles 214 including the first ceramic 216 having a first ceramic erosion resistance are capable of resisting increases in the roughness of the coating surface 224. Without being bound by theory, it is believed that the increased hardness of the first ceramic 216 relative to the hardness of the second ceramic 218 and the anodic material 212 confers resistance to deposition of particles and subsequent corrosion of the coating surface 224.
- the property corresponding to erosion resistance includes erosion of the coating 206 of less than about 76 ⁇ m over about 48,000 hours of operation under standard rear stage turbine compressor operating conditions.
- the anodic material 212 in the matrix 210 is capable of resisting increases in the roughness of the coating surface 224. Without being bound by theory, it is believed that the anodic material 212 protects the substrate 202 from corrosion by undergoing anodic dissolution preferentially as the substrate 202 is placed at a nobler cathodic potential compared to the matrix 210.
- the anodic material 212 is metallic in nature and possesses necessary toughness and ductility.
- the matrix 210 is strengthened by ceramic particles 214.
- the first ceramic 216 in the ceramic particles 214 address erosion resistance.
- the second ceramic 218 in the ceramic particles 214 such as chromium carbide and chromium nitride dissolves during application, such as by thermal spray, to release free chromium, which further augments the anodic nature of the matrix 210.
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- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Ceramic Engineering (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
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Abstract
Description
- The present invention is directed to a coated article and a method for producing a coating. More specifically, the present invention is directed to a coated article and a method for producing a coating containing an anodic material and ceramic particles.
- Gas and steam turbine components, particularly rear stage gas turbine compressor blades, rear stage gas turbine compressor vanes and centrifugal pump impellers, in addition to pipelines, are subjected to water droplet erosion, particulate deposition and corrosion pitting induced cracking issues caused by on-line water washing. The preceding surface degradation mechanisms may also result in undesirable increases in surface roughness.
- Changing the material of the components may improve corrosion resistance but may not improve the roughening effect. Developing alternate alloys may not be cost effective and re-designing components to achieve better overall robustness may not be feasible due to the time and cost involved as well the design constraints imposed by the materials used and the operating requirements.
- Fouling of components may cause corrosion of the components underneath the deposits through a crevice corrosion mechanism. Additionally, particulates in the intake air may cause erosion through foreign object damage to the components thereby causing corrosion. Water wash cycles are often performed to remove the particulates that have built up on the components. However, the water wash cycles expose the components to increased amounts of moisture, which may cause corrosion of the components by dissolving and leaching corrosive agents entrapped in the surface deposits, and accelerated corrosion to any portions of the components damaged by foreign object damage. Furthermore, the water wash cycles may utilize chemicals to remove complex particulate buildup. These chemicals may increase corrosion of the components and increase maintenance cost of the components. Coating systems which require more than one coating layer to address corrosion, oxidation, fouling and/or erosion are undesirable because multiple layers may result in excessive overall thickness of the component so coated. Additionally, multiple coatings may increase the likelihood of undesirable alterations in the aerodynamics or fluid dynamics of the component, or detrimental increases in the weight of the component.
- Unchecked corrosion, oxidation, fouling and/or erosion of the exposed surfaces of the gas turbine or steam turbine components, or of pipelines, may result in undesirable increases in surface roughness, thereby decreasing the efficiency.
- Coated components and methods for producing coated components that do not suffer from one or more of the above drawbacks would be desirable in the art.
- In one embodiment, a method for producing a coating includes providing a substrate defining a substrate surface having a substrate erosion resistance and applying a matrix and ceramic particles to the substrate surface. The matrix includes an anodic material having an anodic erosion resistance. The ceramic particles include a first ceramic having a first ceramic erosion resistance and a second ceramic having a second ceramic erosion resistance. The first ceramic erosion resistance is greater than the second ceramic erosion resistance, greater than the anodic erosion resistance, and greater than the substrate erosion resistance. The second ceramic interacts inchoately with the anodic material during the applying to form modified ceramic particles and modified anodic material formations. The modified ceramic particles are capable of forming a passive oxide film.
- In another embodiment a coated article includes a substrate defining a substrate surface having a substrate erosion resistance and a coating on the substrate surface. The coating includes a matrix and ceramic particles. The matrix includes an anodic material having an anodic erosion resistance. The ceramic particles include a first ceramic having a first ceramic erosion resistance and a second ceramic having a second ceramic erosion resistance. The coating also includes modified ceramic particles and modified anodic material formations formed by an inchoate interaction between the second ceramic and the anodic material. The first ceramic erosion resistance is greater than the second ceramic erosion resistance, greater than the anodic erosion resistance, and greater than the substrate erosion resistance. The modified ceramic particles are capable of forming a passive oxide film.
- Other features and advantages of the present invention will be apparent from the following more detailed description, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
-
-
FIG. 1 is a perspective view of a coated article, according to an embodiment of the disclosure. -
FIG. 2 is a sectional view along lines 2-2 ofFIG. 1 of the coated article, according to an embodiment of the disclosure. -
FIG. 3 is a sectional view of a coated article including a passive oxide film, according to an embodiment of the disclosure. - Wherever possible, the same reference numbers will be used throughout the drawings to represent the same parts.
- Provided are a coated article and a method for producing a coating. Embodiments of the present disclosure, in comparison to methods and articles not using one or more of the features disclosed herein, decrease substrate corrosion, decrease substrate oxidation, decrease substrate fouling, decrease substrate erosion, decrease the rate at which the surface roughness of a substrate increases, decrease maintenance costs, increase efficiency, or a combination thereof.
- Referring to
FIG. 1 , in one embodiment, a coatedarticle 100 is depicted. In one embodiment, the coatedarticle 100 is any suitable component, for example, a compressor blade 102 (shown), a compressor vane, a centrifugal pump impeller or a pipeline. The term "blade" as used herein is intended to be synonymous with the term "bucket." - Referring to
FIG. 2 , in one embodiment the coatedarticle 100 includes asubstrate 202 defining asubstrate surface 204 having a substrate erosion resistance, and acoating 206 on thesubstrate surface 204. Thecoating 206 includes amatrix 210 including ananodic material 212 having an anodic erosion resistance, andceramic particles 214. Theanodic material 212 may be anodic with respect to thesubstrate 202. Theceramic particles 214 include a first ceramic 216 having a first ceramic erosion resistance and a second ceramic 218 having a second ceramic erosion resistance. Thecoating 206 also includes modifiedceramic particles 220 and modifiedanodic material formations 222 formed from an inchoate interaction between the second ceramic 218 and theanodic material 212. Thecoating 206 defines acoating surface 224 which is exposed to the external environment. In a further embodiment, the first ceramic erosion resistance is greater than the second ceramic erosion resistance, greater than the anodic erosion resistance, and greater than the substrate erosion resistance. - In one embodiment, the
anodic material 212 includes Cr70%Ni30% (wt%), a mixture of Ni80%Al20% (wt%) and Ni95%Al5% (wt%), cobalt and aluminum particles in a sacrificial metallic undercoat with a ceramic overcoat, a metallurgically bonded aluminide with an aluminum surface layer, NiCrAl, or a combination thereof. In one embodiment the anoidic material is Cr70%Ni30% (wt%). In a further embodiment, theanodic material 212 is operative to protect thesubstrate surface 204 from corrosion during downtime, which is endemic in peaking turbine components and not uncommon even in base loaded turbine components. - In one embodiment, the first ceramic 216 is tungsten carbide and the second ceramic 218 is chromium carbide, chromium nitride or a combination of chromium carbide and chromium nitride. In a further embodiment, the
anodic material 212 contains chromium and nickel, and the second ceramic interacts inchoately with the chromium and nickel in theanodic material 212 during the applying to form the modifiedceramic particles 220 and the modifiedanodic material formations 222. The modifiedceramic particles 220 include at least one of modified chromium carbide particles having a range of chromium carbide stoichiometries and modified chromium nitride particles having a range of chromium nitride stoichiometries. Without being bound by theory, it is believed that a portion of the second ceramic dissolves during thermal spray processing, releasing free chromium and at least one of carbon and nitrogen. The free chromium may push the electrochemical potential of the matrix toward being more anodic. Nitrogen when dissolved in the matrix may improve pitting resistance of the matrix under corrosive conditions. - In one embodiment, the
coating 206 contains from about 30% to about 60% by weight tungsten carbide, alternatively from about 30% to about 40%, alternatively from about 40% to about 50%, alternatively from about 50% to about 60%. In an additional embodiment, thecoating 206 further contains from about 20% to about 50% by weight of one or both of chromium carbide and chromium nitride, alternatively from about 20% to about 30%, alternatively from about 30% to about 40% alternatively from about 40% to about 50%. In a further embodiment, thecoating 206 also contain balance essentiallyanodic material 212. - Referring to
FIG. 3 , in one embodiment, the modifiedceramic particles 220 are capable of forming apassive oxide film 302. In a further embodiment, thepassive oxide film 302 forms under standard rear stage turbine compressor operating conditions. Known rear stage turbine compressor operating conditions include, for example, elevated pressures 10-25 times atmospheric pressure, and being subjected to adiabatic heating to 250-677 °C. For example, when formed, thepassive oxide film 302 defines thecoating surface 224. Thepassive oxide film 302 resists increases in the roughness of thecoating surface 224 caused by oxidation. Without being bound by theory, it is believed that because thepassive oxide film 302 include materials which are oxides, these materials will not undergo further oxidation. - In one embodiment, the
passive oxide film 302 is uniformly, or substantially uniformly, distributed on thematrix 210. In another embodiment, thepassive oxide film 302 has a thickness of between about 0.1 µm to about 3 µm, alternatively between about 0.1 µm to about 2 µm, alternatively between about 0.1 µm to about 1 µm, alternatively between about 1 µm to about 2 µm, alternatively between about 2 µm to about 3 µm, alternatively between about 0.1 µm to about 1.5 µm, alternatively between about 1.5 µm to about 3 µm, alternatively between about 0.1 µm to about 0.5 µm, alternatively between about 0.5 µm to about 1 µm, alternatively between about 1 µm to about 1.5 µm, alternatively between about 1.5 µm to about 2 µm. - The
coating 206 is produced by any suitable method. In one embodiment, a method for applying thecoating 206 includes providing thesubstrate 202 defining thesubstrate surface 204 and applying thematrix 210 and theceramic particles 214 to thesubstrate surface 204. Applying thematrix 210 and theceramic particles 214 to thesubstrate surface 204 may be accomplished by any suitable coating techniques, such as, but not limited to, thermal spray, air plasma spray (APS), high velocity oxygen fuel (HVOF) thermal spray, high velocity air fuel spraying (HVAF), vacuum plasma spray (VPS), electron-beam physical vapor deposition (EBPVD), chemical vapor deposition (CVD), ion plasma deposition (IPD), combustion spraying with powder or rod, cold spray, sol gel, electrophoretic deposition, tape casting, polymer derived ceramic coating, slurry coating, dip-application, vacuum-coating application, curtain-coating application, brush-application, roll-coat application, and agglomeration and sintering followed by spray drying. - In one embodiment, the
ceramic particles 214 have an average particle diameter ranging from about 0.3 µm to about 5 µm, alternatively from about 0.3 µm to about 2.5 µm, alternatively from about 2.5 µm to about 5 µm, alternatively from about 0.3 µm to about 2 µm, alternatively from about 2 µm to about 3.5 µm, alternatively from about 3.5 µm to about 5 µm, alternatively from about 0.3 µm to about 1 µm, alternatively from about 2 µm to about 3 µm, alternatively from about 3 µm to about 4 µm, alternatively from about 4 µm to about 5 µm. - In one embodiment, the
coating 206 has an average distance between theceramic particles 214 ranging from about 0.2 µm to about 2 µm, alternatively from about 0.2 µm to about 1 µm, alternatively from about 1 µm to about 2 µm, alternatively from about 0.2 µm to about 0.8 µm, alternatively from about 0.8 µm to about 1.4 µm, alternatively from about 1.4 µm to about 2 µm. - In one embodiment, the
coating 206 has a thickness of between about 50 µm to about 250 µm, alternatively between about 50 µm to about 150 µm, alternatively between about 100 µm to about 200 µm, alternatively between about 150 µm to about 250 µm, alternatively between about 50 µm to about 100 µm, alternatively between about 100 µm to about 150 µm, alternatively between about 150 µm to about 200 µm, alternatively between about 200 µm to about 250 µm. - In one embodiment, the
coating 206 consists essentially of asingle matrix 210 ofanodic material 212 with a plurality ofceramic particles 214 dispersed therein. Asingle matrix 210 ofanodic material 212, as opposed to multiple layers ofanodic material 212, allows for the thickness of thecoating 206 to be minimized. - In one embodiment, the
ceramic particles 214 including the first ceramic 216 having a first ceramic erosion resistance are capable of resisting increases in the roughness of thecoating surface 224. Without being bound by theory, it is believed that the increased hardness of the first ceramic 216 relative to the hardness of the second ceramic 218 and theanodic material 212 confers resistance to deposition of particles and subsequent corrosion of thecoating surface 224. - In one embodiment, wherein the
coating 206 has a thickness less than about 250 µm, alternatively less than about 150 µm, the property corresponding to erosion resistance includes erosion of thecoating 206 of less than about 76 µm over about 48,000 hours of operation under standard rear stage turbine compressor operating conditions. - In one embodiment, the
anodic material 212 in thematrix 210 is capable of resisting increases in the roughness of thecoating surface 224. Without being bound by theory, it is believed that theanodic material 212 protects thesubstrate 202 from corrosion by undergoing anodic dissolution preferentially as thesubstrate 202 is placed at a nobler cathodic potential compared to thematrix 210. Theanodic material 212 is metallic in nature and possesses necessary toughness and ductility. However to resist deposition, particulate and water droplet erosion thematrix 210 is strengthened byceramic particles 214. The first ceramic 216 in theceramic particles 214 address erosion resistance. The second ceramic 218 in theceramic particles 214, such as chromium carbide and chromium nitride dissolves during application, such as by thermal spray, to release free chromium, which further augments the anodic nature of thematrix 210. While the invention has been described with reference to one or more embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (15)
- A method for producing a coating, comprising:providing a substrate defining a substrate surface having a substrate erosion resistance; andapplying a matrix and ceramic particles to the substrate surface, wherein:the matrix includes an anodic material having an anodic erosion resistance; andthe ceramic particles include:a first ceramic having a first ceramic erosion resistance; anda second ceramic having a second ceramic erosion resistance,wherein the first ceramic erosion resistance is:greater than the second ceramic erosion resistance;greater than the anodic erosion resistance; andgreater than the substrate erosion resistance,wherein the second ceramic interacts inchoately with the anodic material during the applying to form modified ceramic particles and modified anodic material formations, andwherein the modified ceramic particles are capable of forming a passive oxide film.
- The method of claim 1, wherein the anodic material is selected from a group consisting of Cr70%Ni30% (wt%), a mixture of Ni80%Al20% (wt%) and Ni95%Al5% (wt%), cobalt and aluminum particles in a sacrificial metallic undercoat with a ceramic overcoat, a metallurgically bonded aluminide with an aluminum surface layer, NiCrAl and combinations thereof.
- The method of claim 1 or claim 2, wherein the first ceramic is tungsten carbide and the second ceramic is chromium carbide, chromium nitride or a combination of chromium carbide and chromium nitride.
- The method of any preceding claim, wherein:the anodic material contains chromium and nickel;the second ceramic interacts inchoately with the chromium and nickel in the anodic material during the applying to form the modified ceramic particles and the modified anodic material formations; andthe modified ceramic particles include at least one of modified chromium carbide particles having a range of chromium carbide stoichiometries and modified chromium nitride particles having a range of chromium nitride stoichiometries.
- The method of claim 3 or claim 4, wherein the coating contains from about 30% to about 60% by weight tungsten carbide, from about 20% to about 50% by weight of one or both of chromium carbide and chromium nitride, and balance essentially anodic material.
- The method of any preceding claim, wherein the ceramic particles have an average particle diameter ranging from about 0.3 µm to about 5 µm, and the coating has an average distance between the ceramic particles ranging from about 0.2 µm to about 2 µm.
- The method of any preceding claim, wherein producing the coating consists essentially of applying a single matrix of anodic material with ceramic particles dispersed therein.
- A coated article, comprising:a substrate defining a substrate surface having a substrate erosion resistance; anda coating on the substrate surface, wherein the coating includes:a matrix including an anodic material having an anodic erosion resistance;ceramic particles including:a first ceramic having a first ceramic erosion resistance; anda second ceramic having a second ceramic erosion resistance; andmodified ceramic particles and modified anodic material formations formed by an inchoate interaction between the second ceramic and the anodic material,wherein the first ceramic erosion resistance is:greater than the second ceramic erosion resistance;greater than the anodic erosion resistance; andgreater than the substrate erosion resistance, andwherein the modified ceramic particles are capable of forming a passive oxide film.
- The coated article of claim 8, wherein the anodic material is selected from a group consisting of Cr70%Ni30% (wt%), a mixture of Ni80%Al20% (wt%) and Ni95%Al5% (wt%), cobalt and aluminum particles in a sacrificial metallic undercoat with a ceramic overcoat, a metallurgically bonded aluminide with an aluminum surface layer, NiCrAl, and combinations thereof.
- The coated article of claim 8 or claim 9, wherein the first ceramic is tungsten carbide and the second ceramic is chromium carbide, chromium nitride or a combination of chromium carbide and chromium nitride.
- The coated article of any one of claims 8 to 10, wherein:the anodic material contains chromium and nickel;the modified ceramic particles and the modified anodic material formations are formed by the inchoate interaction of the second ceramic with the chromium and nickel in the anodic material; andthe modified ceramic particles include at least one of modified chromium carbide particles having a range of chromium carbide stoichiometries and modified chromium nitride particles having a range of chromium nitride stoichiometries.
- The coated article of any one of claims 8 to 11, wherein the coating contains from about 30% to about 60% by weight tungsten carbide, from about 20% to about 50% by weight of one or both of chromium carbide and chromium nitride, and balance essentially anodic material.
- The coated article of any one of claims 8 to 12, wherein the ceramic particles have an average particle diameter ranging from about 0.3 µm to about 5 µm, and the coating has an average distance between the ceramic particles ranging from about 0.2 µm to about 2 µm.
- The coated article of any one of claims 8 to 13, wherein the substrate is selected from a group consisting of a compressor blade, a compressor vane, a centrifugal pump impeller, and a pipeline.
- The coated article of any one of claims 8 to 14, wherein the coating consists essentially of a single matrix of anodic material with ceramic particles dispersed therein.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/193,241 US20150247413A1 (en) | 2014-02-28 | 2014-02-28 | Coated article and method for producing coating |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP2913421A1 true EP2913421A1 (en) | 2015-09-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP15156132.1A Withdrawn EP2913421A1 (en) | 2014-02-28 | 2015-02-23 | Coated article and method for production coating |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20150247413A1 (en) |
| EP (1) | EP2913421A1 (en) |
| JP (1) | JP2015165045A (en) |
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| CN112853353B (en) * | 2020-12-31 | 2022-03-15 | 北京科技大学 | A kind of preparation method of nano-filler modified ceramic coating |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1227169A2 (en) * | 2001-01-25 | 2002-07-31 | Fujimi Incorporated | Spray powder and method for its production |
| US20090297720A1 (en) * | 2008-05-29 | 2009-12-03 | General Electric Company | Erosion and corrosion resistant coatings, methods and articles |
| WO2010094256A1 (en) * | 2009-02-21 | 2010-08-26 | Mtu Aero Engines Gmbh | Anti-erosion coating system for gas turbine components |
| EP2226409A2 (en) * | 2009-03-06 | 2010-09-08 | General Electric Company | Erosion and corrosion resistant turbine compressor airfoil and method of making the same |
| EP2395123A1 (en) * | 2010-06-09 | 2011-12-14 | General Electric Company | Composition and method for applying a protective coating |
-
2014
- 2014-02-28 US US14/193,241 patent/US20150247413A1/en not_active Abandoned
-
2015
- 2015-02-20 JP JP2015031186A patent/JP2015165045A/en active Pending
- 2015-02-23 EP EP15156132.1A patent/EP2913421A1/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1227169A2 (en) * | 2001-01-25 | 2002-07-31 | Fujimi Incorporated | Spray powder and method for its production |
| US20090297720A1 (en) * | 2008-05-29 | 2009-12-03 | General Electric Company | Erosion and corrosion resistant coatings, methods and articles |
| WO2010094256A1 (en) * | 2009-02-21 | 2010-08-26 | Mtu Aero Engines Gmbh | Anti-erosion coating system for gas turbine components |
| EP2226409A2 (en) * | 2009-03-06 | 2010-09-08 | General Electric Company | Erosion and corrosion resistant turbine compressor airfoil and method of making the same |
| EP2395123A1 (en) * | 2010-06-09 | 2011-12-14 | General Electric Company | Composition and method for applying a protective coating |
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| Title |
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| FANG W ET AL: "Processing optimization, surface properties and wear behavior of HVOF spraying WC-CrC-Ni coating", JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, ELSEVIER, NL, vol. 209, no. 7, 1 April 2009 (2009-04-01), pages 3561 - 3567, XP026076692, ISSN: 0924-0136, [retrieved on 20080903], DOI: 10.1016/J.JMATPROTEC.2008.08.024 * |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2015165045A (en) | 2015-09-17 |
| US20150247413A1 (en) | 2015-09-03 |
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