C22C29/065

Turbine blade coating composition

A composition for a reinforced metal matrix coating, and a method of preparing and coating the composition. The composition includes a plurality of sacrificial metallic binder particles that is anodic with respect to a base substrate, and a plurality of hard particles.

Turbine blade coating composition

A composition for a reinforced metal matrix coating, and a method of preparing and coating the composition. The composition includes a plurality of sacrificial metallic binder particles that is anodic with respect to a base substrate, and a plurality of hard particles.

ENHANCED METAL-METAL-MATRIX COMPOSITE WEAPON BARRELS

A weapon barrel includes an inner core and an outer sleeve. The inner core has a first end, a second end, a bore extending from the first end to the second end, and an external surface extending from the first end to the second end. The inner core includes a material selected from the group consisting of a ferrous alloy, a non-ferrous alloy, a ceramic, a bonded ceramic, and a cemented carbide. The outer sleeve has a first end, a second end, an internal surface extending from the first end to the second end, and an external surface extending from the first end to the second end. The outer sleeve is disposed around and permanently joined to the inner core. The outer sleeve includes a material selected from the group consisting of a metal-matrix composite and a beryllium alloy, the outer sleeve material being located at and between the internal surface and the external surface of the outer sleeve.

Erosion resistant hard composite materials

A hard composite composition may comprise a binder and a polymodal blend of matrix powder. The polymodal blend of matrix powder may have at least one first local maxima at a particle size of about 0.5 nm to about 30 m, at least one second local maxima at a particle size of about 200 m to about 10 mm, and at least one local minima between a particle size of about 30 m to about 200 m that has a value that is less than the first local maxima.

Thixotropic liquid-metal-based fluid and its use in making metal-based structures with or without a mold
09993996 · 2018-06-12 · ·

This invention provides liquid-metal-based thixotropic fluids that, upon solidification with or without a mold, provide metal-matrix composite materials. The fluid is a liquid metal with dispersed solid particles, which can move substantially relative to one another. The liquid is essentially continuous; the solid is substantially discontinuous. The liquid substantially occupies the separation among the solid particles and essentially occupies a portion of the separation. The portion consists of a plurality of regions. Each region is in contact with the surface of a particle. This invention also provides a laminate consisting of metal-matrix composite layers that are essentially parallel and bonded to one another. This invention further provides a method of making a metal-based structure in the absence of a mold, with relevance to three-dimensional metal printing. This method comprises preparing, shaping and depositing the thixotropic fluid on a substrate, and allowing the fluid to cool for complete solidification.

Heterogeneous Composite Bodies With Isolated Cermet Regions Formed By High Temperature, Rapid Consolidation
20180104755 · 2018-04-19 ·

A heterogeneous composite consisting of near-nano ceramic clusters dispersed within a ductile matrix. The composite is formed through the high temperature compaction of a starting powder consisting of a core of ceramic nanoparticles held together with metallic binder. This core is clad with a ductile metal such that when the final powder is consolidated, the ductile metal forms a tough, near-zero contiguity matrix. The material is consolidated using any means that will maintain its heterogeneous structure.

Heterogeneous composite bodies with isolated cermet regions formed by high temperature, rapid consolidation
09943918 · 2018-04-17 · ·

A heterogeneous composite consisting of near-nano ceramic clusters dispersed within a ductile matrix. The composite is formed through the high temperature compaction of a starting powder consisting of a core of ceramic nanoparticles held together with metallic binder. This core is clad with a ductile metal such that when the final powder is consolidated, the ductile metal forms a tough, near-zero contiguity matrix. The material is consolidated using any means that will maintain its heterogeneous structure.

METHOD FOR PRODUCING SILICON CARBIDE COMPOSITE MATERIAL
20180025919 · 2018-01-25 · ·

A silicon carbide composite that is lightweight and has high thermal conductivity as well as a low thermal expansion coefficient close to that of a ceramic substrate, particularly a silicon carbide composite material suitable for heat dissipating components that are required to be particularly free of warping, such as heat sinks. A method for manufacturing a silicon carbide composite obtained by impregnating a porous silicon carbide molded body with a metal having aluminum as a main component, wherein the method for manufacturing a silicon carbide composite material is characterized in that the porous silicon carbide molded article is formed by a wet molding method, and preferably the wet molding method is a wet press method or is a wet casting method.

Heterogeneous composite bodies with isolated cermet regions formed by high temperature, rapid consolidation
12186807 · 2025-01-07 · ·

A heterogeneous composite consisting of near-nano ceramic clusters dispersed within a ductile matrix. The composite is formed through the high temperature compaction of a starting powder consisting of a core of ceramic nanoparticles held together with metallic binder. This core is clad with a ductile metal such that when the final powder is consolidated, the ductile metal forms a tough, near-zero contiguity matrix. The material is consolidated using any means that will maintain its heterogeneous structure.

Heat dissipation member and method of manufacturing the same
12213286 · 2025-01-28 · ·

A plate-shaped heat dissipation member includes a metal-silicon carbide composite containing aluminum or magnesium, in which at least one of two main surfaces of the heat dissipation member is curved to be convex in an outward direction of the heat dissipation member, and when a flatness of the one main surface defined by JIS B 0621 is represented by f.sub.1 and a flatness of the other main surface different from the one main surface defined by JIS B 0621 is represented by f.sub.2, f.sub.2 is less than f.sub.1 by 10 m or more.