Microcircuit airfoil mainbody

Details Microcircuit airfoil mainbody Microcircuit airfoil mainbody

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F02C 7/18 (2006.01)

Patent

CA 2475885

A cooling circuit disposed within a first wall portion and a second wall portion of a wall for use in a gas turbine engine is provided. The cooling circuit includes a plurality of inlet apertures disposed in the first wall portion to provide a flow path of cooling air into the cooling circuit, a first exit slot disposed in the second wall portion to provide a cooling air flow path out of the cooling circuit, a plurality of pedestals arranged in rows extending within the between the first wall portion and the second wall portion and a first elongated pedestal disposed radially and extending between the first and second wall portions. The first elongated pedestal is positioned between the pedestals and the first exit slot.

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