摘要:
A nanocomposite comprising a plurality of nanoparticles dispersed in a metallic alloy matrix, and a structural component formed from such a nanocomposite. The metallic matrix comprises at least one of a nickel-based alloy and an iron-based alloy. The nanocomposite contains a higher volume fraction of nanoparticle dispersoids than those presently available. The structural component include those used in hot gas path assemblies, such as steam turbines, gas turbines, and aircraft turbine. A method of making such nanocomposites is also disclosed.
摘要:
Nano-multilayered structures (10), components and associated methods (30) of manufacture suitable for use in high-temperature applications including a plurality of metallic alloy layers (12), wherein the thickness (16) of each of the plurality of metallic alloy layers (12) is on a nano scale, and a plurality of ceramic oxide layers (14) disposed between the plurality of metallic alloy layers (12) in an alternating manner, wherein the thickness (16) of each of the plurality of ceramic oxide layers (14) is on a nano scale.
摘要:
A mechanical seal includes a pair of opposing seal faces (10), wherein at least one of the pair of seal faces (10) includes a multilayer coating (14) disposed on a substrate (12), wherein the multilayer coating (14) has a periodic repetition of distinct layers, a plurality of layers of a composite wherein no two adjacent layers of the composite comprise an identical ratio of composite constituents, or both. A method of making the seal includes disposing a multilayer coating (14) on a substrate (12) to form at least one of a pair of opposing seal faces (10) of a mechanical seal.
摘要:
A wear resistant coating (116) including a hard backing (118) including a metal alloy matrix dispersed with a plurality of hard particles; and a plurality of nano-layers (120) disposed on the hard backing (118) is provided. The plurality of nano-layers (120) has different characteristics from one another. A method of making a wear resistant coating (116) is provided. The method includes the steps of providing a substrate; disposing a hard backing (118); and disposing a plurality of nano-layers (120) on the hard backing (118).
摘要:
A nanocomposite comprising a plurality of nanoparticles dispersed in a metallic alloy matrix, and a structural component formed from such a nanocomposite. The metallic matrix comprises at least one of a nickel-based alloy and an iron-based alloy. The nanocomposite contains a higher volume fraction of nanoparticle dispersoids than those presently available. The structural component include those used in hot gas path assemblies, such as steam turbines, gas turbines, and aircraft turbine. A method of making such nanocomposites is also disclosed.