B22C9/06

DIRECTIONAL SOLIDIFICATION CASTING ASSEMBLY AND METHOD
20220048099 · 2022-02-17 ·

A directional solidification casting assembly includes a directional solidification mold having an interior chamber with a shape of an object to be cast using directional solidification of molten metal in a growth direction of the mold and a feed line conduit. The conduit is fluidly coupled with a container source of the molten metal and is coupled with the mold at a gating. The feed line conduit conveys the molten metal into the mold through the gating for directional solidification of the object to be cast in the mold. At least a downstream portion of the feed line conduit that is between the intermediate location of the feed line conduit and the second open end of the feed line conduit is located below the gating along the growth direction of the mold.

CONTROLLED NOZZLE COOLING (CNC) CASTING
20220048104 · 2022-02-17 · ·

A process for the casting of metals and their alloys includes the steps of providing at least a mold equipped with a plurality of cooling nozzles, making a layer of coolant permeable materials covering the nozzles and maintaining the materials at desired temperatures, delivering a molten metal into the mold, supplying predetermined amount of coolant to each nozzles to contact the casting at desired rate, time, and duration to achieve an acceptable level of progressive solidification from the distal end of the casting towards the riser until the casting has reached desired temperatures.

CONTROLLED NOZZLE COOLING (CNC) CASTING
20220048104 · 2022-02-17 · ·

A process for the casting of metals and their alloys includes the steps of providing at least a mold equipped with a plurality of cooling nozzles, making a layer of coolant permeable materials covering the nozzles and maintaining the materials at desired temperatures, delivering a molten metal into the mold, supplying predetermined amount of coolant to each nozzles to contact the casting at desired rate, time, and duration to achieve an acceptable level of progressive solidification from the distal end of the casting towards the riser until the casting has reached desired temperatures.

Method and apparatus for controlling variable shell thickness in cast strip

Apparatus and method for continuously casting metal strip includes a pair of casting rolls having casting surfaces with a center portion, edge portions each having average surface roughness between 3 and 7 micrometers Ra, and intermediate portion between each edge portion and the center portion, the center portion average surface roughness between 1.2 and 4.0 times the edge portion surface roughness, and the intermediate portions average surface roughness between that of the edge and center portions. The surface roughness of the center portion is tapered across its width, and may be tapered across its width is in stepped zones. The center portion may have surface roughness varied across the surface to correspond to a desired variation in metal shell thickness across the cast strip. The center portion may be at least 60% of the casting roll width, and each edge portion may be up to 7% of the casting roll width.

Method and apparatus for controlling variable shell thickness in cast strip

Apparatus and method for continuously casting metal strip includes a pair of casting rolls having casting surfaces with a center portion, edge portions each having average surface roughness between 3 and 7 micrometers Ra, and intermediate portion between each edge portion and the center portion, the center portion average surface roughness between 1.2 and 4.0 times the edge portion surface roughness, and the intermediate portions average surface roughness between that of the edge and center portions. The surface roughness of the center portion is tapered across its width, and may be tapered across its width is in stepped zones. The center portion may have surface roughness varied across the surface to correspond to a desired variation in metal shell thickness across the cast strip. The center portion may be at least 60% of the casting roll width, and each edge portion may be up to 7% of the casting roll width.

Mold for forming complex 3D MEMS components

A mold structure having high-precision multi-dimensional components which includes a first oxide layer superimposed on a top of a first semiconductor substrate; a second oxide layer superimposed on a top of a second semiconductor substrate; integrated designs patterned in at least one of the oxide layers; and the first and second semiconductor substrates bonded to one another into a three dimensional (3D) mold such that the first oxide layer only makes partial contact with the second oxide layer such that a portion of the first oxide layer avoids contact with the second oxide layer, the portion of the first oxide layer directly opposite a surface portion of the second semiconductor substrate that is free of the second oxide, the 3D mold selectively filled with a filling material to form a molded high-precision multi-dimensional component.

Mold for forming complex 3D MEMS components

A mold structure having high-precision multi-dimensional components which includes a first oxide layer superimposed on a top of a first semiconductor substrate; a second oxide layer superimposed on a top of a second semiconductor substrate; integrated designs patterned in at least one of the oxide layers; and the first and second semiconductor substrates bonded to one another into a three dimensional (3D) mold such that the first oxide layer only makes partial contact with the second oxide layer such that a portion of the first oxide layer avoids contact with the second oxide layer, the portion of the first oxide layer directly opposite a surface portion of the second semiconductor substrate that is free of the second oxide, the 3D mold selectively filled with a filling material to form a molded high-precision multi-dimensional component.

DIE CAST SYSTEM WITH CERAMIC CASTING MOLD FOR FORMING A COMPONENT USABLE IN A GAS TURBINE ENGINE
20170232506 · 2017-08-17 · ·

A die cast system in which an external shell and an internal core usable to form a component of a gas turbine engine are formed together is disclosed. In at least one embodiment, the external shell and internal core may be formed from at the same time via a selective laser melting process, thus eliminating the need for using the conventional lost-wax casting system. In at least one embodiment, the external shell and internal core may be formed a ceramic material that may support receiving molten metal to form a turbine component. Once formed, the external shell and internal core may be removed to reveal the turbine component.

Core pin for preventing molten metal from flowing into pipe and casting device using the same

A core pin is provided that prevents a molten metal from flowing into a pipe and a casting device using the same is also provided. The core pin specifically contacts a first end of the pipe inserted into a mold to close the end of the pipe, to thus prevent the molten metal from flowing into the pipe.

CASTING MOLD HAVING AT LEAST ONE CAVITY FOR MANUFACTURING AT LEAST ONE CAST ARTICLE

A casting mold having at least one cavity for manufacturing at least one cast article, in which at least some areas of a casting surface of the casting mold delimiting the cavity have a surface texture. The surface texture has multiple elementary cells, wherein each elementary cell has a structure that projects and/or is recessed with respect to the casting surface and ends within the applicable elementary cell. In addition, a cast article produced by the casting mold is provided.