Method and apparatus for testing gas turbine engines

Power plants – Combustion products used as motive fluid – Cooling of auxiliary components

Reexamination Certificate

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C060S806000

Reexamination Certificate

active

07966804

ABSTRACT:
A method for testing a cooling system for use in a gas turbine engine control system is provided. The method includes connecting an inlet of the cooling system to a differential pressure sensor, connecting an outlet of the cooling system to the differential pressure sensor, and determining whether or not a difference in pressure exists between the inlet and outlet, wherein such a pressure difference is indicative of whether cooling fluid is flowing through the cooling system.

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