Methods and systems to facilitate over-speed protection

A method of assembling a gas turbine engine is provided. The method includes coupling a first fuel system interface to a fuel delivery system, coupling a second fuel system interface to the fuel delivery system, coupling a first driver control system in communication with the first and second fuel s...

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Bibliographische Detailangaben
Hauptverfasser:	BERTRAM S NOYES JR, DAVID R VAN VACTOR, PAUL B GOODWIN
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A method of assembling a gas turbine engine is provided. The method includes coupling a first fuel system interface to a fuel delivery system, coupling a second fuel system interface to the fuel delivery system, coupling a first driver control system in communication with the first and second fuel system interfaces, and coupling a second driver control system in communication with the first and second fuel system interfaces.