Impingement skin core cooling for gas turbine engine blade

Details Impingement skin core cooling for gas turbine engine blade Impingement skin core cooling for gas turbine engine blade

2007-02-16

2010-11-23

Kershteyn, Igor (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

Changing state mass within or fluid flow through working...

C415S115000

Reexamination Certificate

active

07837441

ABSTRACT:
Turbine components, and in particular turbine blades, are provided with impingement cooling channels. Air is delivered along central channels, and the central channels deliver the air through crossover holes to core channels adjacent both a pressure wall and a suction wall. The air passing through the crossover holes impacts against a wall of the core channels.

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