Methods and apparatus for cooling gas turbine rotor blades

Details Methods and apparatus for cooling gas turbine rotor blades Methods and apparatus for cooling gas turbine rotor blades

2006-01-10

2006-01-10

Nguyen, Ninh H. (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Rotor having flow confining or deflecting web, shroud or...

Axially extending shroud ring or casing

Reexamination Certificate

active

06984112

ABSTRACT:
A turbine blade is provided. The turbine blade includes a blade platform having an airfoil portion and a root portion extending therefrom, an undercut formed in a first side of the platform and a purge slot formed in a second side of the platform.

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