Electrical control system

An example aircraft electrical system includes a generator coupled with a gas turbine engine and a controller operable to distribute power of the generator. The controller includes a first control module positioned at a first location remote from the generator and a second control module positioned...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Bayles, Robert A, Hoegberg, Lon R, Seger, Mark J, Ralph, Wes, Patel, Sunil S
Format: Patent
Sprache:eng
Schlagworte:
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Beschreibung
Zusammenfassung:An example aircraft electrical system includes a generator coupled with a gas turbine engine and a controller operable to distribute power of the generator. The controller includes a first control module positioned at a first location remote from the generator and a second control module positioned at a second location proximate the generator. The first control module is configured to verify at least one output of the generator, detect a fault condition of the generator, and control operation of at least one power bus in communication with the first control module. The second control module is configured to regulate the at least one output of the generator, where the at least one output includes a voltage. An example method of operating an electrical system is also disclosed.