Inventors:
Brent Jerome Brunell - Clifton Park NY, US
Simon Shlomo Lis - Cincinnati OH, US
R. Sheldon Carpenter - Cincinnati OH, US
Samhita Dasgupta - Schenectady NY, US
Sridhar Adibhatla - Glendale OH, US
Scott Douglas Waun - West Chester OH, US
Emad Andarawis Andarawis - Ballston Lake NY, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 9/00
Abstract:
In one embodiment, a gas turbine engine control system includes an engine controller configured to control multiple parameters associated with operation of a gas turbine engine system. The gas turbine engine control system also includes multiple remote interface units communicatively coupled to the engine controller. The remote interface unit is configured to receive an input signal from the engine controller indicative of respective target values of at least one parameter, and the remote interface unit is configured to provide closed-loop control of the at least one parameter based on the input signal and feedback signals indicative of respective measured values of the at least one parameter.
