Blade inlet cooling flow deflector apparatus and method

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

Reexamination Certificate

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C416S09600A, C416S09700R

Reexamination Certificate

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06974306

ABSTRACT:
An internally cooled turbine blade including at least one deflector extending into an air cavity generally from a first wall towards a second wall for diverting cooling air away from the first wall and generally towards the second wall to thereby improve cooling flow distribution among a plurality of cooling path inlets.

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