Turbine airfoil with enhanced cooling
AssigneeSiemens Power Generation, Inc.
InventorGeorge Liang
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AssigneeSiemens Power Generation, Inc.
InventorGeorge Liang
Estimating the term…
An airfoil for a turbine of a gas turbine engine is provided comprising an outer wall structure defining at least one inner cavity adapted to receive a cooling fluid. The wall structure comprises at least one cooling fluid path circuit communicating with the at least one inner cavity. The cooling fluid path circuit comprises: at least one metering opening extending from an inner surface of the wall structure such that the metering opening communicates with the at least one inner cavity; at least one intermediate diffusion region communicating with the metering opening; an intermediate metering opening positioned downstream from the intermediate diffusion region and communicating with the intermediate diffusion region; and, an end diffusion region positioned downstream from the intermediate metering opening for communicating with the intermediate metering opening and extending to an exit in an outer surface of the wall structure.
An airfoil for a turbine of a gas turbine engine comprising:
A vane for a turbine of a gas turbine engine comprising:
An airfoil for a turbine of a gas turbine engine comprising:
Dependencies are inferred from the claim text.