Integrated core-shell investment casting molds that provide tongue or groove structures corresponding, respectively, to groove or tongue structures in the surface of the turbine blade or stator vane, including in locations that are otherwise inaccessible provide a pathway to restrict cooling flow between turbine blades to the flowpath.

Integrated core-shell investment casting molds that provide tongue or groove structures corresponding, respectively, to groove or tongue structures in the surface of the turbine blade or stator vane, including in locations that are otherwise inaccessible provide a pathway to restrict cooling flow between turbine blades to the flowpath.

A method of manufacturing protruding cast in features (10). At least one core insert (12) is manufactured using small particle sizes. A bulk core body is manufactured using large particle sizes. The at least one core insert (12) and bulk core body are fully fired separately. The at least one core insert (12) is bonded with the bulk core body.

A method of manufacturing protruding cast in features (10). At least one core insert (12) is manufactured using small particle sizes. A bulk core body is manufactured using large particle sizes. The at least one core insert (12) and bulk core body are fully fired separately. The at least one core insert (12) is bonded with the bulk core body.

A brake carrier casting and a method of making a brake carrier casting. The brake carrier casting may have a first side portion and a second side portion that may be connected by a first bridge and a second bridge. The first side portion, second side portion, first bridge, and second bridge may define an opening of the brake carrier casting.

A brake carrier casting and a method of making a brake carrier casting. The brake carrier casting may have a first side portion and a second side portion that may be connected by a first bridge and a second bridge. The first side portion, second side portion, first bridge, and second bridge may define an opening of the brake carrier casting.

A casting method is provided that includes a mold, a mixer, and first and second materials. A first pour and a second pour are dispensed from the mixer. The first pour has different proportions of the first and second materials as compared to the second pour. The first pour forms a first layer of a molded part, and the second pour forms a second layer of the molded part.

This caliper body includes a cylinder portion (26) that has a piston disposed therein and is internally provided with a liquid pressure chamber, a bleeder boss portion (29) that communicates with the liquid pressure chamber and includes a bleeder hole configured to discharge air from the liquid pressure chamber, and a plurality of identifiers (112 and 116). At least one identifier (112) of the identifier (112 and 116) is formed in a region hidden by a bleeder plug (131) attached to the bleeder boss portion (29).

A tool for reforming a core pattern. A method of reforming a core pattern comprises opening a core reformer tool. The core reformer tool has a first portion and a second portion facing the first portion. The first portion includes a concave member and a first adjustable pin. The second portion includes a convex member and a second adjustable pin. The method includes positioning the core pattern in the core reformer tool and closing the core reformer tool. The method comprises adjusting at least one of the first adjustable pin and the second adjustable pin to alter a surface of the core pattern. The method includes directing cooling air through the core reformer tool to solidify the core pattern and opening the core reformer tool to remove the core pattern.

A tool for reforming a core pattern. A method of reforming a core pattern comprises opening a core reformer tool. The core reformer tool has a first portion and a second portion facing the first portion. The first portion includes a concave member and a first adjustable pin. The second portion includes a convex member and a second adjustable pin. The method includes positioning the core pattern in the core reformer tool and closing the core reformer tool. The method comprises adjusting at least one of the first adjustable pin and the second adjustable pin to alter a surface of the core pattern. The method includes directing cooling air through the core reformer tool to solidify the core pattern and opening the core reformer tool to remove the core pattern.