Cooling air system for mid turbine frame

Details Cooling air system for mid turbine frame Cooling air system for mid turbine frame

F - Mech Eng,Light,Heat,Weapons

01

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F01D 25/14 (2006.01) F01D 5/18 (2006.01) F01D 25/28 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2715228

A mid turbine frame is disposed between high and low pressure turbine assemblies. A cooling air system defined in the mid turbine frame of a gas turbine engine includes internal cavities for containing pressurized cooling air to cool the inter-turbine duct and the hollow struts, and discharges the used cooling air to further cool respective high and low pressure turbine assemblies.

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