摘要:
A compressor blade (100) 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 (100) has a blade portion (110), a dovetail portion (120) and a platform portion (130) intermediate the blade portion (110) and the dovetail portion (120), the blade portion (110) terminating in a tip (140) opposite the dovetail portion. A cobalt-based coating overlies at least the blade portion (110) of the compressor blade (100). 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.
摘要:
Nano-structured coating systems (10), components and associated methods of manufacture including a substantially ductile and/or corrosion-resistant binder matrix (14) and a plurality of substantially hard nano-sized ceramic particles (12) or gains disposed within the substantially ductile and/or corrosion resistant binder matrix (14), wherein the mean free spacing between the plurality of nano-sized ceramic particles (12) or gains is on a nano-scale. Optionally, the coating systems (10), components and associated methods of manufacture also including a plurality of substantially hard micron-sized ceramic particles (20) or grains disposed within the substantially ductile and/or corrosion resistant binder matrix (14).
摘要:
A method includes applying a material coating (12) to a surface (14) of a machine component, wherein the material coating (12) is formed from a combination of a hardfacing material (20) and aluminum-containing particles (18). The method also includes thermally treating the material coating (12) to generate an oxide layer (24) comprising aluminum from the aluminum-containing particles (18), wherein the oxide layer (24) is configured to reduce oxidation of the hardfacing material (20).
摘要:
A corrosion monitoring system (110) includes at least one corrosion sensor (100). The corrosion sensor (100) includes a metallic plug (104) having at least one opening, at least one ceramic sheath (106) in the opening of the metallic plug (104), and a plurality of probes (102). Each probe (102) has a central portion with a predetermined cross sectional area extending from the metallic plug (104). The ceramic sheath (106) electrically isolates each first end and each second end of the probes (102) from the metallic plug (104) and the other first ends and second ends. The probes (102) are sized to provide a range of predetermined cross sectional areas of the central portions. Such arrangement permits to extend the lifespan of the system since when one probe has been completely corroded, measurement can be switched to another probe having a higher cross sectional area and which is still operational.The corrosion monitoring system (110) also includes a resistance meter (112) measuring an ohmic resistance for at least one of the probes (102) and a computer (116) determining a corrosion rate by correlating a rate of change of the ohmic resistance to the corrosion rate of the probe (102). The corrosion monitoring system (100) is particularly suitable for real-time corrosion monitoring of components in the hot gas path of turbines.
摘要:
A system includes a turbine combustor (14) and one or more supply circuits configured to supply one or more fluids to the turbine combustor. The one or more supply circuits include at least a liquid fuel supply circuit (88) fluidly coupled to a liquid fuel source (128) and configured to supply a liquid fuel from the liquid fuel source to the turbine combustor. The system also includes a corrosion inhibitor injection system (80) including a magnesium source (98) storing a magnesium-based inhibitor that includes magnesium oxide (MgO) and an yttrium source (100) storing an yttrium-based inhibitor that includes yttrium oxide (Y 2 O 3 ). The corrosion inhibitor injection system (80) is fluidly coupled to the turbine combustor (14) and the one or more supply circuits (88, 90, 92, 94, 96), and is configured to inject the magnesium-based inhibitor and the yttrium-based inhibitor as vanadium corrosion inhibitors into the turbine combustor or the one or more supply circuits.
摘要:
A material (200) is disclosed including a matrix (202) and a plurality of particles (204) dispersed in the matrix (202). The plurality of particles (204) include a plurality of tungsten semicarbide particles (206) constituting at least about 30 vol% of the plurality of particles (204). An article (100) is disclosed including the material (200). A method for forming the article (100) is disclosed, including applying the material (200). Applying the material (200) includes forming the matrix (202) and dispersing a plurality of particles (204) including a plurality of tungsten carbide particles (208) in the matrix (202). The plurality of tungsten carbide particles (208) are at least partially decarburized, transforming at least a portion of the tungsten carbide particles (208) into a plurality of the tungsten semicarbide particles (206) such that the plurality of tungsten semicarbide particles (206) constitute at least about 30 vol% of the plurality of particles (204).