Patent application number | Description | Published |
20090176110 | EROSION AND CORROSION-RESISTANT COATING SYSTEM AND PROCESS THEREFOR - A coating system and process capable of providing erosion and corrosion-resistance to a component, particularly a steel compressor blade of an industrial gas turbine. The coating system includes a metallic sacrificial undercoat on a surface of the component substrate, and a ceramic topcoat deposited by thermal spray on the undercoat. The undercoat contains a metal or metal alloy that is more active in the galvanic series than iron, and electrically contacts the surface of the substrate. The ceramic topcoat consists essentially of a ceramic material chosen from the group consisting of mixtures of alumina and titania, mixtures of chromia and silica, mixtures of chromia and titania, mixtures of chromia, silica, and titania, and mixtures of zirconia, titania, and yttria. | 07-09-2009 |
20090297720 | EROSION AND CORROSION RESISTANT COATINGS, METHODS AND ARTICLES - Disclosed herein is an erosion and corrosion resistant coating comprising a metallic binder, a plurality of hard particles, and a plurality of sacrificial particles. Also disclosed is a method of improving erosion and corrosion resistance of a metal component comprising disposing on a surface of the metal component the foregoing erosion and corrosion resistant coating comprising, and a metal component comprising a metal component surface and the foregoing erosion and corrosion resistant coating comprising a first surface and a second surface opposite the first surface, wherein the first surface is disposed on the metal component surface. | 12-03-2009 |
20110008614 | Electrostatic Powder Coatings - In one embodiment, a protective coating may be electrostatically applied to a rotary machine component. The powder coating includes an electrically conductive sacrificial base coat and a ceramic oxide erosion resistant top coat. | 01-13-2011 |
20120171374 | NOZZLE FOR USE WITH A SPRAY COATING GUN - A nozzle for use with a spray coating gun for applying a coating material to a substrate. The nozzle includes a discharge portion operative to emit the coating material therefrom. The nozzle also includes a material-receiving portion operative to receive feedstock therein. The discharge portion is angled from the material-receiving portion such that the coating material is discharged from the discharge portion and impacts and bonds with a region of the substrate. The discharge portion can be positioned to apply the coating material in various locations. | 07-05-2012 |
20130042456 | SELF-LUBRICATING BRUSH SEAL ASSEMBLY AND METHOD OF REDUCING LEAKAGE - A self-lubricating brush seal assembly, for a power generation system and method of reducing air leakage in a power generation system including a plurality of self-lubricating members is provided. The plurality of self-lubricating members include a plurality of self-lubricating bristles, a plurality of cores sheathed in a self-lubricating braid, a plurality of cores having an outer diameter coated with self-lubricating material and a solid lubricating pack. The lubricating material is selected from graphite, hexagonal-boron nitrite (hBN), molybdenum disulfide (MoS | 02-21-2013 |
20130084399 | COATING COMPOSITION, A PROCESS OF APPLYING A COATING, AND A PROCESS OF FORMING A COATING COMPOSITION - A coating composition, a process of applying a coating having a coating composition, and a process of forming a coating composition are disclosed. The coating composition includes an alloy and an oxide component comprising nickel oxide. The process of applying the coating includes cold spraying the coating onto the article. The process of forming the coating composition includes blending and milling the alloy with the oxide component. | 04-04-2013 |
20130186304 | PROCESS OF FABRICATING A THERMAL BARRIER COATING AND AN ARTICLE HAVING A COLD SPRAYED THERMAL BARRIER COATING - A process of fabricating a thermal barrier coating and an article having a cold sprayed thermal barrier coating are disclosed. The process includes cold spraying ceramic particles and a binder and forming the thermal barrier coating. The binder has a melting point lower than the ceramic particles. The article includes the cold sprayed thermal barrier coating positioned on a substrate of the article and/or a reproducible feature formed by the cold sprayed thermal barrier coating, with the reproducible feature being capable of being replicated without masking. | 07-25-2013 |
20130189441 | PROCESS OF FABRICATING THERMAL BARRIER COATINGS - A process of fabricating a thermal barrier coating is disclosed. The process includes cold spraying a substrate with a feedstock to form a thermal barrier coating and concurrently oxidizing one or more of the substrate, the feedstock, and the thermal barrier coating. The cold spraying is in a region having an oxygen concentration of at least 10%. In another embodiment, the process includes heating a feedstock with a laser and cold spraying a substrate with the feedstock to form a thermal barrier coating. At least a portion of the feedstock is retained in the thermal barrier coating. In another embodiment, the process of fabricating a thermal barrier coating includes heating a substrate with a laser and cold spraying the substrate with a feedstock to form a thermal barrier coating. | 07-25-2013 |
20130323518 | COATING PROCESS, COATING, AND COATED COMPONENT - A coating process, a coating, and a coated component are disclosed. The coating process includes providing a MCrAlY substrate, applying a thermal barrier coating to the MCrAlY substrate, applying a flash layer to the thermal barrier coating, the flash layer including an inert ceramic, applying a reaction product deposition onto the thermal barrier coating, the reaction product deposition including reaction products selected from the group consisting of a magnesium oxide compound, a magnesium orthovanadate compound, a magnesium vanadate compound, a magnesium pyrovanadate compound, a magnesium sulfate compound, and combinations thereof. The reaction products are by-products of a doped fuel. | 12-05-2013 |
20130340403 | EROSION AND CORROSION RESISTANT COATINGS FOR EXHAUST GAS RECIRCULATION BASED GAS TURBINES - A compressor blade for use in a compressor section of a gas turbine engine, comprising: a martensitic stainless steel compressor blade and an abrasive coating having an anodic component. The compressor blade has a blade portion, a dovetail portion and a platform portion intermediate the blade portion and the dovetail portion, the blade portion terminating in a tip opposite the dovetail portion. A cobalt-based coating overlies at least the blade portion of the compressor blade. The cobalt-based coating comprises a cobalt based material that includes precipitates of tungsten carbide that provide erosion resistance and particles of a sacrificial metal-based material distributed through the cobalt-based coating that provide galvanic corrosion resistance to the system. | 12-26-2013 |
20140086810 | SYSTEM AND METHOD FOR EMPLOYING CATALYTIC REACTOR COATINGS - A system includes a catalytic reactor configured to mount to a combustor. The catalytic reactor includes a catalyst configured to reduce emissions associated with combustion in the combustor. The catalytic reactor also includes a first sacrificial coating disposed over the catalyst prior to mounting of the catalytic reactor into the combustor, wherein the first sacrificial coating is removable while the catalytic reactor is mounted to the combustor without damaging the catalyst. | 03-27-2014 |
20140235426 | CERAMIC POWDERS AND METHODS THEREFOR - A ceramic powder and method of forming the ceramic powder capable of being used in coatings to allow components to survive in high temperatures environments, such as the hostile thermal environment of a gas turbine engine. The ceramic powder includes powder particles each having an inner core formed of a first material and an outer region formed of a second material. The inner core has a lower thermal conductivity than the outer region, and the outer region is more erosion resistance relative to the inner core. | 08-21-2014 |
20140272467 | CALCIUM-MAGNESIUM-ALUMINOSILICATE RESISTANT COATING AND PROCESS OF FORMING A CALCIUM-MAGNESIUM-ALUMINOSILICATE RESISTANT COATING - A process of forming a calcium-magnesium-aluminosilicate (CMAS) penetration resistant coating, and a CMAS penetration resistant coating are disclosed. The process includes providing a thermal barrier coating having a dopant, and exposing the thermal barrier coating to calcium-magnesium-aluminosilicate and gas turbine operating conditions. The exposing forming a calcium-magnesium-aluminosilicate penetration resistant layer. The coating includes a thermal barrier coating composition comprising a dopant selected from the group consisting of rare earth elements, non-rare earth element solutes, and combinations thereof. Additional or alternatively, the coating includes a thermal barrier coating and an impermeable barrier layer or a washable sacrificial layer positioned on an outer surface of the thermal barrier coating. | 09-18-2014 |
20140308479 | ARCHITECTURES FOR HIGH TEMPERATURE TBCs WITH ULTRA LOW THERMAL CONDUCTIVITY AND ABRADABILITY AND METHOD OF MAKING - A method for fabricating thermal barrier coatings. The thermal barrier coatings are produced with a fine grain size by reverse co-precipitation of fine powders. The powders are then sprayed by a solution plasma spray that partially melts the fine powders while producing a fine grain size with dense vertical cracking. The coatings comprise at least one of 45%-65% Yb | 10-16-2014 |
20140312006 | WIRE ARC SPRAY SYSTEM USING COMPOSITE WIRE FOR POROUS COATING, AND RELATED METHOD - A composite wire for use with a wire arc spray system and related methods. The composite wire can include: a low melting point material at a core region thereof and a cladding including a metal surrounding the core region, the low metal point material having a melting point less than that of the metal, wherein the low melting point material includes a polymer in the form of a powder having particles having a size of from approximately 1 nanometer to approximately 100 nanometers. | 10-23-2014 |
20150064451 | COATING, COATING METHOD, AND COATED ARTICLE - A coating method, coated article and coating are provided. The coated article includes a low temperature component, and a graphene coating formed from a graphene derivative applied over the low temperature component. The coating method includes providing a graphene derivative, providing a low temperature component, applying the graphene derivative over the low temperature component, and forming a graphene coating. The graphene coating reduces corrosion and fouling of the low temperature component. The coating includes a graphene derivative, and modified functional groups on the graphene derivative. The modified functional groups increase adherence of the coating on application to a low temperature component. | 03-05-2015 |
20150080282 | CLEANSING AND FILM-FORMING WASHES FOR TURBINE COMPRESSORS - Cleansing washes for compressor sections of turbines include one or more surfactants, one or more corrosion inhibiting dispersants, and one or more balance materials selected from a group consisting of water and solvents. The one or more surfactants and the one or more corrosion inhibiting dispersants combine to comprise from about 1 weight percent to about 20 weight percent, as actives, of the cleansing wash. | 03-19-2015 |