摘要:
A casting core assembly (140) includes a metallic core (144, 146, 148), a ceramic core (142) having a compartment (186) in which the portion of the metallic core is received, and a ceramic coating (260) at least partially covering the metallic core and the ceramic core.
摘要:
A method for applying a coating (56) to a substrate having a plurality of holes. The method comprises applying a braze material to a substrate having a plurality of holes, heating the substrate to melt the braze material to form a melt, cooling the substrate to solidify the melt to form plugs (90) in the respective holes; applying a coating (56) to the substrate and further heating the substrate to melt the plugs (90) .
摘要:
A combustion system including a transition piece (44) and method of forming the transition piece (44) using a cast nickel-based superalloy is provided. The transition piece (44) includes a body (68) defining a flowpath (72) and enclosure (70), the body (68) having a circular inlet section (60) for receiving combustion product from the combustor (40) and an outlet end (62) for flowing the combustor products into a first stage nozzle of a gas turbine. The transition piece (44) comprises a one-piece single casting construction of the circular inlet section (60), the body (68), and the outlet end (62). The transition piece (44) is formed from a nickel-based superalloy. The transition piece has a thick-to-thin ratio of wall thickness (84) of thick transition (80) to wall thickness (84) of thin transition (82) of about 1.1 to about 2.5.
摘要:
Provided is a method (200) of fabricating an article, including deforming (210) an ingot of a nickel-based superalloy to form an intermediate article, forming a substantially homogeneous dispersion of Laves phase precipitates (240) within the intermediate article by cooling the intermediate article (220) and exposing the intermediate article to a temperature range (230) wherein the Laves phase precipitates are present at a concentration of at least about 0.05 % by volume and the precipitates have a mean diameter of less than one micron. Also provided is a nickel-based superalloy including a substantially homogeneous dispersion of Laves phase precipitates, wherein the intergranular and transgranular Laves phase precipitates are present at a concentration of at least about 0.1 % by volume and wherein the precipitates have a mean diameter of less than one micron. Precipitation of Laves phase may control microstructure during Thermo-mechanical processing and produce superalloys with refined grain size.
摘要:
A blade outer airseal (54) has a body (64) comprising: an inner diameter (ID) surface (52); an outer diameter (OD) surface; a leading end (104); and a trailing end (106). The airseal body (64) has a metallic substrate (56) and a coating system (58) atop the substrate (56) along at least a portion of the inner diameter surface (52). At least over a first area of the inner diameter surface (52), the coating system (58) comprises an abradable layer (128) and a thermal barrier layer (126) between the abradable layer (128) and the substrate (56); and the thermal barrier layer (126) comprises a ceramic and metallic phases (144, 140) within the ceramic.
摘要:
Delamination of thermal barrier coatings (“TBC's”) (276) from superalloy substrates (262) of components (260) for turbine engines (80), such as engine blades (92), vanes (104, 106), or castings in transitions (85), is inhibited during subsequent cooling passage (270) formation. Partially completed cooling passages (264), which have skewed passage paths that end at a terminus (268), which is laterally offset from the passage entrance (266), are formed in the superalloy component (260) prior to application of the TBC layer(s) (276). The skewed, laterally offset path of each partially completed cooling passage (264) establishes an overhanging shield layer (269) of superalloy material that protects the TBC layer (276) during completion of the cooling passage (270).
摘要:
A gamma prime nickel-based superalloy is provided, which can include a combination of Ti and Zr in a total weight amount sufficient to form cellular precipitates located at grain boundaries of the alloy, wherein the cellular precipitates define gamma prime arms that distort the grain boundaries at which they are located. The Hf-containing, gamma prime nickel-based superalloy and/or the gamma prime nickel-based superalloy can include cellular precipitates that are predominantly located at grain boundaries of the alloy such that the cellular precipitates define gamma prime arms that distort the grain boundaries at which they are located. The superalloys can further include finer gamma prime precipitates (e.g., cuboidal or spherical precipitates) than the cellular precipitates.
摘要:
The present disclosure provides a method of preparing superalloy metals having a crystallographic texture controlled micro structure by electron beam melting.