Turbine airfoil

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

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Reexamination Certificate

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08047789

ABSTRACT:
A turbine airfoil for use in a gas turbine engine, the airfoil formed from a support spar with a leading edge rib having a row of impingement cooling holes, the support spar having an array of modules formed on the pressure side and the suction side of the spar, and a number of cavities separated by ribs extending across the walls of the support spar. Each module is rectangular in shape and includes an impingement compartment and a diffusion compartment separated by a rib with crossover holes to connect the two compartments. Impingement holes connect the impingement compartment to a first cavity, and spent air cooling holes connect the diffusion compartment to a second cavity located downstream from the first cavity.

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