An end or intermediate casing for a combustion turbine engines includes prefabricated vanes of a first metal. Ends of the prefabricated vanes are then embedded within cast-in place inner and outer, annular-shaped ring castings, formed from a second metal having a lower melting point than the first metal. The respective ends of the prefabricated vanes include first and second shanks, with respective first and second surface features that are oriented transverse to the central axis of the vane are encapsulated in the molten second metal during the inner and outer ring casting. Once the castings harden, the first and second surface features, such as for example circumferential fillets projecting outwardly from the airfoil portion of the vane, inhibit separation of the vanes from the respective inner and outer rings.

An end or intermediate casing for a combustion turbine engines includes prefabricated vanes of a first metal. Ends of the prefabricated vanes are then embedded within cast-in place inner and outer, annular-shaped ring castings, formed from a second metal having a lower melting point than the first metal. The respective ends of the prefabricated vanes include first and second shanks, with respective first and second surface features that are oriented transverse to the central axis of the vane are encapsulated in the molten second metal during the inner and outer ring casting. Once the castings harden, the first and second surface features, such as for example circumferential fillets projecting outwardly from the airfoil portion of the vane, inhibit separation of the vanes from the respective inner and outer rings.

A casting core assembly is disclosed herein. The casting core assembly comprises a casting core and a bumper assembly. The bumper assembly is disposed on an outer surface of the casting core. The bumper assembly comprises a receptacle and a metal apparatus. The metal apparatus may be a pin, a sphere, or the like.

A casting core assembly is disclosed herein. The casting core assembly comprises a casting core and a bumper assembly. The bumper assembly is disposed on an outer surface of the casting core. The bumper assembly comprises a receptacle and a metal apparatus. The metal apparatus may be a pin, a sphere, or the like.

A tool is provided for positioning a core stabilizing pin into a preassigned hole of a plurality of holes formed in an additively manufactured mold. The tool has a main body, a pin cavity, and a standoff. When the tool is used to insert a core stabilizing pin, of a precise, controlled length, into a preassigned hole, and the core stabilizing pin is inserted until the mold engagement end contacts the outer surface of the mold, the angle of the preassigned hole and thickness of the mold precisely positions the core stabilizing pin to engage and stabilize the core.

A tool is provided for positioning a core stabilizing pin into a preassigned hole of a plurality of holes formed in an additively manufactured mold. The tool has a main body, a pin cavity, and a standoff. When the tool is used to insert a core stabilizing pin, of a precise, controlled length, into a preassigned hole, and the core stabilizing pin is inserted until the mold engagement end contacts the outer surface of the mold, the angle of the preassigned hole and thickness of the mold precisely positions the core stabilizing pin to engage and stabilize the core.

A holding device for holding a casting core in a casting mold, especially in a die-casting mold, includes a plurality of clamping sections which are positioned in relation to each other in such a way that a clamping region for a casting core is formed.

A holding device for holding a casting core in a casting mold, especially in a die-casting mold, includes a plurality of clamping sections which are positioned in relation to each other in such a way that a clamping region for a casting core is formed.

Disclosed is a lost-wax method of casting a product, having steps of: attaching temperature control elements to a wax assembly; encasing the wax assembly and the temperature control elements in a ceramic mold; removing the wax assembly from the ceramic mold; filling the ceramic mold with molten material to form a cast part within the ceramic mold; and separating the ceramic mold and the cast part from each other.

An investment casting process for manufacturing a cast component is provided. The investment casting process includes forming a core, casting the cast component about the core such that a core positioning feature provides a location of an anticipated pilot hole in the cast component, removing the core from the cast component once the casting is completed, locating, forming and sizing a pilot hole to form a resized pilot hole that can receive a sealing plug and installing the sealing plug into the resized pilot hole.