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Gas turbine engine control systemA control system and method of controlling a gas turbine engine. The control system receives an error signal and processes the error signal to form a primary fuel control signal. The control system also receives at least one anticipatory demand signal and processes the signal to form an anticipatory fuel control signal. The control system adjusts the value of the anticipatory fuel control signal based on the value of the error signal to form an adjusted anticipatory signal and then the adjusted anticipatory fuel control signal and the primary fuel control signal are combined to form a fuel command signal.
Document ID
20080004731
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Idelchik, Michael S.
Date Acquired
August 24, 2013
Publication Date
February 19, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Number: US-PATENT-4,993,221
Patent Application Number: US-PATENT-APPL-SN-287231
Funding Number(s)
CONTRACT_GRANT: NAS3-22752
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,993,221
Patent Application
US-PATENT-APPL-SN-287231

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