Combustion turbine with airfoil having enhanced leading edge...

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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C416S09700R

Reexamination Certificate

active

06869268

ABSTRACT:
A combustion turbine20includes a housing22and a plurality of airfoils40within the housing. Each airfoil40has a leading edge surface42and at least one interior cooling passageway44. A plurality of diffusion holes46extend from the at least one interior cooling passageway44to the leading edge surface42. Each diffusion hole46includes a proximal section48having a generally constant cross-sectional shape and a distal tapered section50that extends outwardly from the proximal section, tapering in a radially inward direction.

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