Methods and apparatuses for gas turbine engines

Details Methods and apparatuses for gas turbine engines Methods and apparatuses for gas turbine engines

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 11/02 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2567940

A gas turbine engine (10) assembly is provided. The gas turbine engine assembly includes a centrifugal compressor (14), a combustor (16) downstream from the centrifugal compressor, a turbine (20) coupled to the compressor, and a seal assembly (40) coupled aft of the centrifugal compressor such that air discharged through the seal assembly facilitates reducing the cavity pressure, and therefore reducing the axial forces induced to an aft side of the centrifugal compressor.

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