Gas turbine engine component cooling scheme

Details Gas turbine engine component cooling scheme Gas turbine engine component cooling scheme

2011-01-04

2011-01-04

Cuff, Michael (Department: 3741)

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

C060S806000, C415S116000, C416S09700R, C416S09700R

Reexamination Certificate

active

07862291

ABSTRACT:
A gas turbine engine component includes a platform and an airfoil extending from the platform. The platform includes an outer surface. A cover plate is positioned adjacent to the outer surface of the platform. A cooling channel extends between the outer surface and the cover plate and receives cooling air to cool the platform and the airfoil.

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