Thermostatic control of turbine cooling air

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

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Details

415116, 416 96A, 416 97R, F01D 500

Patent

active

050228170

ABSTRACT:
A gas turbine engine is provided with hollow guide vanes having thermally responsive actuators mounted within each for individually controlling the cooling air flow therethrough in response to local temperature variations.

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