The present invention relates to a device for shooting a foundry core which surrounds a free inner space on its outer boundaries, with the device having a mould cavity representing the foundry core, which circulates around an inner slider extending along a longitudinal axis and is delimited on its outer side by an outer slider circulating around the mould cavity, with the clear width of the mould cavity being determined by the distance of the inner surface of the outer slider, assigned to the mould cavity, to the outer surface of the inner slider. The device according to the invention allows for operationally-safe manufacture of foundry cores that are tubular in their base form, but finely-structured in their walls and also on a large scale. This is achieved by the inner slider segments being displaceable between a removal position, in which they are positioned approximated in relation to one another and to the longitudinal axis of the inner slider and the clear width of the mould cavity present between the inner slider and the outer slider is increased, into a shooting position approximating the outer slider, in which the clear width of the mould cavity corresponds to a target specification for the foundry core to be shot.

A deburring method for a casting sand core 40 for removing burrs from a deburring target part 41 in the casting sand core 40 including the deburring target part 41, the deburring target part 41 being at least one of an opening and a cut-out part. The deburring method includes: inserting a bag 13 into the deburring target part 41 of the casting sand core 40; and inflating the bag 13 inserted into the deburring target part 41, and thereby pressing and breaking off burrs 42 formed on a peripheral surface of the deburring target part 41 by the inflated bag 13.

The present disclosure generally relates to partial integrated core-shell investment casting molds that can be assembled into complete molds. Each section of the partial mold may contain both a portion of a core and portion of a shell. Each section can then be assembled into a mold for casting of a metal part. The partial integrated core-shell investment casting molds and the complete molds may be provided with filament structures corresponding to cooling hole patterns on the surface of the turbine blade or the stator vane, which provides a leaching pathway for the core portion after metal casting. The invention also relates to core filaments that can be used to supplement the leaching pathway, for example in a core tip portion of the mold.

The present disclosure generally relates to partial integrated core-shell investment casting molds that can be assembled into complete molds. Each section of the partial mold may contain both a portion of a core and portion of a shell. Each section can then be assembled into a mold for casting of a metal part. The partial integrated core-shell investment casting molds and the complete molds may be provided with filament structures corresponding to cooling hole patterns on the surface of the turbine blade or the stator vane, which provides a leaching pathway for the core portion after metal casting. The invention also relates to core filaments that can be used to supplement the leaching pathway, for example in a core tip portion of the mold.

A core molding method is a method of molding a core using a metal mold that is pressure-fed with mulled sand, and includes heating the metal mold such that the temperature of the metal mold reaches a temperature higher than a predetermined baking temperature, pressure-feeding the heated metal mold with the mulled sand, holding the temperature of the metal mold having been pressure-fed with the mulled sand at the baking temperature, and removing the core from the metal mold after the holding.

A sand core making machine is provided that includes at least one transfer tool by means of which the material for making the core is transferred when said transfer tool is moved to an operating position. The machine also includes a curing tool by means of which the material previously transferred by the transfer tool is hardened and which is arranged in an operating position over the material to perform the hardening once the transfer tool has moved out of its operating position. The machine includes at least one articulated arm for moving the transfer tool and the curing tool to the respective operating position.

A sand core making machine is provided that includes at least one transfer tool by means of which the material for making the core is transferred when said transfer tool is moved to an operating position. The machine also includes a curing tool by means of which the material previously transferred by the transfer tool is hardened and which is arranged in an operating position over the material to perform the hardening once the transfer tool has moved out of its operating position. The machine includes at least one articulated arm for moving the transfer tool and the curing tool to the respective operating position.

A mold assembly for producing a casting core for a cooling jacket of an electric motor has an external mold and an internal mold enclosed by the external mold. The external mold forms an outer wall and the internal mold an inner wall of the core molding cavity fillable with a core material and having a cylindrical shape. The internal mold has two first mold shells and two second mold shells. The two first mold shells and the two second mold shells jointly form the inner wall of the core molding cavity. The second mold shells are arranged between the first mold shells. A first demolding mechanism is arranged between the first mold shells and enables movement of the first mold shells toward one another. A second demolding mechanism is arranged between the second mold shells and enables movement of the second mold shells toward one another.

A mold assembly for producing a casting core for a cooling jacket of an electric motor has an external mold and an internal mold enclosed by the external mold. The external mold forms an outer wall and the internal mold an inner wall of the core molding cavity fillable with a core material and having a cylindrical shape. The internal mold has two first mold shells and two second mold shells. The two first mold shells and the two second mold shells jointly form the inner wall of the core molding cavity. The second mold shells are arranged between the first mold shells. A first demolding mechanism is arranged between the first mold shells and enables movement of the first mold shells toward one another. A second demolding mechanism is arranged between the second mold shells and enables movement of the second mold shells toward one another.

A core structure for a providing a cooling passage in a gas turbine engine includes a core body that has a first cooling passage core. The first cooling passage core has a first width in a chord-wise direction near a first wall. A second width in the chord-wise direction near a second wall. A third width in the chord-wise direction between the first and second walls. The third width being smaller than the first and second widths to form an hourglass shape.