Active cooling of turbine rotor assembly

Power plants – Combustion products used as motive fluid

Patent

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Details

416 95, 416220R, B64C 1100

Patent

active

053396197

ABSTRACT:
An active cooling mechanism for a turbine disk is disclosed. Various construction details are developed which disclose a turbine section having a rotor assembly, a disk with an attachment means, a radially movable heat shield disposed therebetween, and a cooling passage which directs cooling air over the forward surface and radially outer surface of the attachment means. During operation, rotational forces urge the heat shield radially outward to create a gap between the heat shield and the attachment means, the gap defining a portion of the cooling passage.

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