METHOD AND SYSTEM TO FACILITATE OVER-SPEED PROTECTION

PROBLEM TO BE SOLVED: To provide an over-speed protection system (40) employed in a gas turbine engine (10). SOLUTION: The over-speed protection system (40) includes a first fuel system interface (56), a second fuel system interface (58), a first driver control system (102) coupled in communication...

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Bibliographische Detailangaben
Hauptverfasser:	VAN VACTOR DAVID R, NOYES JR BERTRAM S, GOODWIN PAUL B
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide an over-speed protection system (40) employed in a gas turbine engine (10). SOLUTION: The over-speed protection system (40) includes a first fuel system interface (56), a second fuel system interface (58), a first driver control system (102) coupled in communication with the first fuel system interface and second fuel system interface and equipped with a first driver (106) and a second driver (108) different from the first driver, and a second driver control system (104) coupled in communication with the first fuel system interface and the second fuel system interface and equipped with the first driver (110) and a second driver (112). COPYRIGHT: (C)2010,JPO&INPIT