C22C47/08

High Conductivity Magnesium Alloy
20190338405 · 2019-11-07 ·

A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m-K, and/or ductility exceeding 15-20% elongation to failure.

High Conductivity Magnesium Alloy
20190338405 · 2019-11-07 ·

A castable, moldable, or extrudable magnesium-based alloy that includes one or more insoluble additives. The insoluble additives can be used to enhance the mechanical properties of the structure, such as ductility and/or tensile strength. The final structure can be enhanced by heat treatment, as well as deformation processing such as extrusion, forging, or rolling, to further improve the strength of the final structure as compared to the non-enhanced structure. The magnesium-based composite has improved thermal and mechanical properties by the modification of grain boundary properties through the addition of insoluble nanoparticles to the magnesium alloys. The magnesium-based composite can have a thermal conductivity that is greater than 180 W/m-K, and/or ductility exceeding 15-20% elongation to failure.

ALUMINIUM-ALUMINA COMPOSITE MATERIAL AND ITS METHOD OF PREPARATION
20190304618 · 2019-10-03 ·

The present invention relates to a composite material based on aluminium and alumina, its method of manufacture, and a cable comprising said composite material as an electrical conductor element.

ALUMINIUM-ALUMINA COMPOSITE MATERIAL AND ITS METHOD OF PREPARATION
20190304618 · 2019-10-03 ·

The present invention relates to a composite material based on aluminium and alumina, its method of manufacture, and a cable comprising said composite material as an electrical conductor element.

Turbomachine components manufactured with carbon nanotube composites
10415127 · 2019-09-17 · ·

A turbomachine component and method for fabricating the turbomachine component are provided. The turbomachine component may include a matrix material and carbon nanotubes combined with the matrix material. The matrix material may include a metal or a polymer. The carbon nanotubes may be contacted with the metal to form a metal-based carbon nanotube composite, and the metal-based carbon nanotube composite may be processed to fabricate the turbomachine component.

Turbomachine components manufactured with carbon nanotube composites
10415127 · 2019-09-17 · ·

A turbomachine component and method for fabricating the turbomachine component are provided. The turbomachine component may include a matrix material and carbon nanotubes combined with the matrix material. The matrix material may include a metal or a polymer. The carbon nanotubes may be contacted with the metal to form a metal-based carbon nanotube composite, and the metal-based carbon nanotube composite may be processed to fabricate the turbomachine component.

Process for manufacturing a composite material
10403419 · 2019-09-03 · ·

A process is provided for manufacturing a composite material with functionalized carbon nanotubes and a metal matrix. The arrangement also includes manufacturing an elongated electrically conductive element, and an electrical cable with such an elongated electrically conductive element.

Process for manufacturing a composite material
10403419 · 2019-09-03 · ·

A process is provided for manufacturing a composite material with functionalized carbon nanotubes and a metal matrix. The arrangement also includes manufacturing an elongated electrically conductive element, and an electrical cable with such an elongated electrically conductive element.

Fibre-reinforced metal component for an aircraft or spacecraft and production methods for fibre-reinforced metal components

Production methods for producing a fiber-reinforced metal component having a metal matrix which is penetrated by a plurality of reinforcing fibers are provided. One method includes depositing in layers reinforcing fibers in fiber layers, depositing in layers and liquefying a metal modelling material in matrix material layers, and consolidating in layers the metal modelling material in adjacently deposited matrix material layers to form the metal matrix of the fiber-reinforced metal component. Here, the metal component is formed integrally from alternately deposited matrix material layers and fiber layers. An alternative method includes introducing an open three-dimensional fiberwoven fabric consisting of reinforcing fibers into a casting mold, pouring a liquid metal modelling material into the casting mold and consolidating the metal modelling material to form the metal matrix of the fiber-reinforced metal component. Here, the metal component is formed integrally from the consolidated metal modelling material and the reinforcing fibers.

Fibre-reinforced metal component for an aircraft or spacecraft and production methods for fibre-reinforced metal components

Production methods for producing a fiber-reinforced metal component having a metal matrix which is penetrated by a plurality of reinforcing fibers are provided. One method includes depositing in layers reinforcing fibers in fiber layers, depositing in layers and liquefying a metal modelling material in matrix material layers, and consolidating in layers the metal modelling material in adjacently deposited matrix material layers to form the metal matrix of the fiber-reinforced metal component. Here, the metal component is formed integrally from alternately deposited matrix material layers and fiber layers. An alternative method includes introducing an open three-dimensional fiberwoven fabric consisting of reinforcing fibers into a casting mold, pouring a liquid metal modelling material into the casting mold and consolidating the metal modelling material to form the metal matrix of the fiber-reinforced metal component. Here, the metal component is formed integrally from the consolidated metal modelling material and the reinforcing fibers.