Interturbine vane with multiple air chambers

Details Interturbine vane with multiple air chambers Interturbine vane with multiple air chambers

F - Mech Eng,Light,Heat,Weapons

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F01D 25/28 (2006.01) F01D 5/18 (2006.01) F01D 9/02 (2006.01) F01D 11/00 (2006.01) F01D 25/14 (2006.01) F02C 7/12 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2715594

A gas turbine engine has a mid turbine frame disposed between turbine rotor assemblies. The mid turbine frame includes hollow airfoils radially extending through an annular gas path duct. The airfoils each include a double-walled leading edge structure to define a front chamber separated from a rear chamber defined in the remaining space within the airfoil.

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