Clearance control system

Rotary kinetic fluid motors or pumps – With control means responsive to non-cyclic condition... – Temperature or fluid force responsive member

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415116, 60 3929, F01D 1700

Patent

active

048939838

ABSTRACT:
A method and system for controlling rotor blade tip clearances in a gas turbine engine is disclosed. A flow of heat transfer fluid is supplied to the rotor. The temperature of the flow is controlled as a function of the heat carrying capacity of the fluid.

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