Methods and apparatuses for cooling gas turbine engine rotor...

Details Methods and apparatuses for cooling gas turbine engine rotor... Methods and apparatuses for cooling gas turbine engine rotor...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/12 (2006.01)

Patent

CA 2567938

A turbine mid-frame assembly is provided. The turbine mid-frame assembly includes a turbine mid-frame including at least one of a fastener cover plate and an opening (42) extending through the turbine mid-frame configured to facilitate cooling a turbine (20) coupled downstream from and adjacent to the turbine mid-frame.

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