Counterflow film cooled wall

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

Reexamination Certificate

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Details

C415S116000, C416S09700R, C416S191000

Reexamination Certificate

active

11224922

ABSTRACT:
A turbine wall includes opposite back and front sides. Film cooling holes are inclined longitudinally through the wall. Adjacent holes are spaced laterally apart and are inclined oppositely for channeling cooling air therethrough in counterflow.

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GE Aircraft Engines, “Turbine Shroud A,” in public use or on sale in US for more than one year before Aug. 2005.
GE Aircraft Engines, “Turbine Shroud B,” in public use or on sale in US for more than one year before Aug. 2005.

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