Enhanced turbine airfoil cooling

Fluid reaction surfaces (i.e. – impellers) – Method of operation

Reexamination Certificate

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C416S09700R, C415S115000

Reexamination Certificate

active

07901180

ABSTRACT:
The ends of cooling air passages in turbine blades and/or vanes of a gas turbine engine are provided with turbulation promoters to enhance the cooling of such structures as inner and outer shrouds and the like to accommodate thermal loads thereon.

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