Method of Making a Combustion Turbine Component Having a Plurality of Surface Cooling Features and Associated Components
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[0037]Referring initially to the flowchart 14 of FIG. 1, a first embodiment of a method of making a combustion turbine component is now described. After the start (Block 15), at Block 16 a plurality of metallic combustion turbine subcomponent greenbodies are assembled together to form a metallic greenbody assembly. The metallic greenbody assembly has a shape closely resembling that of the final combustion turbine component, but has a greater porosity, a lesser density, and a larger size. The plurality of metallic combustion turbine subcomponent greenbodies may be assembled by conventional methods known to those of skill in the art.
[0038]Those of skill in the art will understand that a metallic combustion turbine subcomponent greenbody is an unsintered metallic combustion turbine subcomponent that lacks strength and has both a low density and high porosity compared to a sintered metallic body.
[0039]At Block 17, the metallic greenbody assembly is sintered to thereby form the combustio...
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