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US08876463B2 Interturbine vane with multiple air chambers 有权
具有多个气室的涡轮叶片

Interturbine vane with multiple air chambers
Abstract:
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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