Patent classifications
B28B3/00
Systems and methods for infusion mixing a slurry based electrode
Embodiments described in this application relate generally to a system, an apparatus and/or methods for manufacturing electrodes by infusion electrolyte into compacted electrode materials. In some embodiments, a working electrode materials can be produced using an infusion mixing and manufacturing process. In some embodiments, a single-sided finished electrode can be produced directly from a dry powder mixture using an infusion mixing and manufacturing process. In some embodiments, a double-sided finished electrode can be produced directly from a dry powder mixture using an infusion mixing and manufacturing process. The electrodes produced by an infusion mixing and manufacturing process generally perform better than those produced by non-infusion processes.
Composite substrate, method for producing the same, and electronic device
A composite substrate includes a supporting substrate and a functional substrate that are directly joined together, the supporting substrate being a sintered sialon body.
Composite substrate, method for producing the same, and electronic device
A composite substrate includes a supporting substrate and a functional substrate that are directly joined together, the supporting substrate being a sintered sialon body.
REINFORCED SUPERPLASTIC FORMED AND DIFFUSION BONDED STRUCTURES
An exterior panel is formed of superplastic materials, including an exterior skin of titanium to accommodate high thermal stresses imposed on hypersonic transport vehicles during hypersonic flight. The exterior skin is fixed to an underlying reinforcing skeletal structure consisting of a superplastic formable reinforcement (SFR) layer, for example a titanium, zirconium, and molybdenum (TZM) alloy, which supports the exterior skin whenever the latter may be heated to temperatures exceeding 1200 degrees Fahrenheit. The exterior panel includes a separate interior skin configured for attachment to a frame member such as a rib, stringer, or spar of the hypersonic transport vehicle. A multicellular core is sandwiched between the exterior and interior skins to impart tensile and compressive strength to the exterior panel. In one disclosed method, the core is superplastic formed and diffusion bonded to the exterior and interior skins.
Manufacture of parts using the lost wax method
The invention relates to the making, on a support plate (34), of an annular space (76) in a ceramic paste covering this plate, in order, by successive deposits and firing of layers of said ceramic paste, to create a base of a ceramic shell (40) for the moulding of parts, the base having said annular space (76). For this purpose, between two deposits of said ceramic paste, and on the plate, said deformable annular element (82) will be deformed in order to break the ceramic layer.
FIRING SETTER
A method of manufacturing a furnace setter is disclosed. The method includes placing one or more layers of ceramic tape on a form that has a shape corresponding to a desired shape of the furnace setter. The method further includes applying pressure to the assembly that includes the form and the tape layers. The application of pressure to the assembly compresses the ceramic tape layers together to generate an integrated body having the desired shape of the furnace setter. The method further includes removing the integrated body from the form and applying a heat treatment to the integrated body to generate the furnace setter as a sintered solid body. According to a further embodiment, a furnace setter is disclosed that has a weight to area ratio that is less than 10 g/in.sup.2, less than 5 g/in.sup.2, less than 3 g/in.sup.2, or less than 2 g/in.sup.2.
FIRING SETTER
A method of manufacturing a furnace setter is disclosed. The method includes placing one or more layers of ceramic tape on a form that has a shape corresponding to a desired shape of the furnace setter. The method further includes applying pressure to the assembly that includes the form and the tape layers. The application of pressure to the assembly compresses the ceramic tape layers together to generate an integrated body having the desired shape of the furnace setter. The method further includes removing the integrated body from the form and applying a heat treatment to the integrated body to generate the furnace setter as a sintered solid body. According to a further embodiment, a furnace setter is disclosed that has a weight to area ratio that is less than 10 g/in.sup.2, less than 5 g/in.sup.2, less than 3 g/in.sup.2, or less than 2 g/in.sup.2.
HIGH TOUGHNESS INORGANIC COMPOSITE ARTIFICIAL STONE PANEL AND PREPARATION METHOD THEREOF
A high toughness inorganic composite artificial stone panel and preparation method are disclosed. The panel includes a surface layer, an intermediate metal fiber toughening layer and a substrate toughening layer. The surface layer includes the following components: 40-70 parts of quartz sand, 10-30 parts of quartz powder, 20-45 parts of inorganic active powder, 0.5-4 parts of pigment, 0.3-1 part of water reducer and 3-10 parts of water. The intermediate metal fiber toughening layer includes the following components: 40-60 parts of inorganic active powder, 45-65 parts of sand, 0.8-1.5 parts of water reducer, 6-14 parts of water and 4-8 parts of metal fiber. The substrate toughening layer includes the following components: 30-50 parts of inorganic active powder, 30-55 parts of quartz sand, 15-20 parts of quartz powder, 0.5-1.2 parts of water reducer, 4-8 parts of water and 0.8-2.5 parts of toughening agent.
Inorganic fiber toughened inorganic composite artificial stone panel and preparation method thereof
An inorganic fiber toughened inorganic composite artificial stone panel and a preparation method thereof are disclosed. The panel includes a surface layer and a toughened base layer. The surface layer includes the the following components in parts by weight: 40-70 parts of quartz sand, 10-30 parts of quartz powder, 20-45 parts of inorganic active powder, 0.5-4 parts of pigment, 0.3-1 parts of water reducing agent and 3-10 parts of water. The toughened base layer includes the following components in parts by weight: 40-60 parts of inorganic active powder, 45-65 parts of sand, 0.8-1.5 parts of water reducing agent, 6-14 parts of water, 0.4-2 parts of inorganic fiber and 0.8-2.5 parts of toughener.
Method and plant for manufacturing ceramic products
A method and a plant (i.e., system or assembly) for manufacturing ceramic products comprising the steps of feeding a mixture of ceramic powders so as to obtain a powder material strip; compacting the powder material strip so as to obtain a compacted powder layer; acquiring a surface image of the compacted powder layer that reproduces the respective surface chromatic effects; processing said surface image so as to obtain a graphic decoration to be applied on the surface of the compacted powder layer that is coordinated with the respective chromatic effects in the thickness; and printing the graphic decoration on the surface of the compacted powder layer.