Cooled turbine blade cast tip recess
AssigneeHoneywell International Inc.
InventorsMark C. Morris, Steve H. Halfmann, Jason C. Smoke
Life of this patent
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AssigneeHoneywell International Inc.
InventorsMark C. Morris, Steve H. Halfmann, Jason C. Smoke
Estimating the term…
A core assembly including two cores is used to manufacture a blade. The first core has an outer surface shaped to complement the tip wall bottom surface. The second core has a tip surface, a side surface, and a protrusion or a depression. The tip surface is shaped to complement at least a portion of the tip wall top surface and is configured to be disposed proximate the first core. The side surface is shaped to complement at least a portion of the side wall, and the protrusion extends from the second core side surface to contact at least a portion of the ceramic mold inner surface. In embodiments employing a depression, the depression is formed in the side surface.
A method of manufacturing an air-cooled turbine blade having an outer surface, side walls and a tip wall, the side walls having tip edges, the tip wall extending between the side walls and recessed a predetermined distance from the tip edges to form a tip recess, the tip wall having a bottom surface and a top surface, the top surface defining a portion of the tip recess, the method comprising the steps of:
A method of manufacturing an air-cooled turbine blade having an outer surface, side walls and a tip wall, the side walls having tip edges, the tip wall extending between the side walls and recessed a predetermined distance from the tip edges to form a tip recess, the tip wall having a bottom surface and a top surface, the top surface defining a portion of the tip recess, the method comprising the steps of
Dependencies are inferred from the claim text.