Patent classifications
C22C47/04
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.
COMPONENT FOR A MIRROR ARRAY FOR EUV LITHOGRAPHY
A component for a mirror array for EUV lithography, particularly for use in faceted mirrors in illumination systems of EUV lithography devices. A component (500) for a mirror array for EUV lithography is proposed which is at least partially made from a composite material including matrix material (502) that contains copper and/or aluminium, and reinforcing material in the form of fibers (504). The composite material also includes particles (508) that consist of one or more of the materials from the group: graphite, adamantine carbon, and ceramic.
COMPONENT FOR A MIRROR ARRAY FOR EUV LITHOGRAPHY
A component for a mirror array for EUV lithography, particularly for use in faceted mirrors in illumination systems of EUV lithography devices. A component (500) for a mirror array for EUV lithography is proposed which is at least partially made from a composite material including matrix material (502) that contains copper and/or aluminium, and reinforcing material in the form of fibers (504). The composite material also includes particles (508) that consist of one or more of the materials from the group: graphite, adamantine carbon, and ceramic.
SYSTEM AND PRINT HEAD FOR CONTINUOUSLY MANUFACTURING COMPOSITE STRUCTURE
A print head is disclosed for us with an additive manufacturing system. The print head may include a matrix reservoir configured to hold a supply of matrix, and a flop guide located within the matrix reservoir. The flop guide may be configured to at least partially surround a continuous reinforcement passing through the matrix reservoir. The print head may also include a nozzle connected to an end of the matrix reservoir downstream of the flop guide.
SYSTEM AND PRINT HEAD FOR CONTINUOUSLY MANUFACTURING COMPOSITE STRUCTURE
A system is disclosed for use in additively manufacturing a composite structure. The system may include a head configured to discharge a continuous reinforcement at least partially coated with a matrix. The head may have a matrix reservoir, and a nozzle connected to an end of the matrix reservoir. The system may further include a support configured to move the head during discharging, and a supply of matrix. The system may also include at least one sensor configured to generate a signal indicative of a matrix characteristic inside of the head, and a controller configured to selectively affect the supply of matrix based on the signal.
SYSTEM, PRINT HEAD, AND COMPACTOR FOR CONTINUOUSLY MANUFACTURING COMPOSITE STRUCTURE
A compactor is disclosed for use with an additive manufacturing print head. The compactor may include a housing connectable to the additive manufacturing print head. The compactor may also include a compacting wheel, and at least one spring disposed in the housing and configured to exert an axial force on the compacting wheel. The compactor may further include a piston moveable to adjust a distance between the housing and the compacting wheel.
ALUMINUM-FIBER COMPOSITES CONTAINING INTERMETALLIC PHASE AT THE MATRIX-FIBER INTERFACE
A solid aluminum-fiber composite comprising: (i) an aluminum-containing matrix comprising elemental aluminum; (ii) coated or uncoated fibers embedded within said aluminum-containing matrix, wherein said fibers have a different composition than said aluminum-containing matrix and impart additional strength to said aluminum-containing matrix as compared to said aluminum-containing matrix in the absence of said fibers embedded therein; and (iii) an intermetallic layer present as an interface between each of said fibers and the aluminum-containing matrix, wherein said intermetallic layer has a composition different from said aluminum-containing matrix and said fibers, and said intermetallic layer contains at least one element that is also present in the aluminum-containing matrix and at least one element present in the fibers, whether from the coated or interior portion of the fibers. Methods of producing the above-described composite are also described.
ALUMINUM-FIBER COMPOSITES CONTAINING INTERMETALLIC PHASE AT THE MATRIX-FIBER INTERFACE
A solid aluminum-fiber composite comprising: (i) an aluminum-containing matrix comprising elemental aluminum; (ii) coated or uncoated fibers embedded within said aluminum-containing matrix, wherein said fibers have a different composition than said aluminum-containing matrix and impart additional strength to said aluminum-containing matrix as compared to said aluminum-containing matrix in the absence of said fibers embedded therein; and (iii) an intermetallic layer present as an interface between each of said fibers and the aluminum-containing matrix, wherein said intermetallic layer has a composition different from said aluminum-containing matrix and said fibers, and said intermetallic layer contains at least one element that is also present in the aluminum-containing matrix and at least one element present in the fibers, whether from the coated or interior portion of the fibers. Methods of producing the above-described composite are also described.
Method for Processing and Manufacturing a Metal Structural Material by a Coiling, Sintering and Plastic Working of a Metal Screen Mesh
Provided is a method for processing and manufacturing a metal structural material by knitting metal wires into metal screen mesh strips, tightly coiling the metal screen mesh strips to form a coiled blank body which is coated layer-by-layer and in which an outer-layer material tightly covers an inner-layer material; sintering the coiled blank body; reducing gaps within the coiled blank body material by plastic processing, to reach a porosity that fulfills requirements, and manufacturing mechanical structural parts.