Turbine blade with disk rim shield

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means

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416193A, F01D 508

Patent

active

045361290

ABSTRACT:
In a gas turbine engine the turbine blade has protective flanges closely overlying the rim of the rotor to shield the rotor from the hot power gases and to form a path for cooling air. These flanges are spaced radially inward from the flanges on the blade that define the inner wall of the gas path through the turbine.

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