FUEL DELIVERY SYSTEM FOR GAS TURBINE ENGINE

A fuel delivery system for a gas turbine engine (12) is disclosed which includes a continuously variable drive assembly (14) having a driving portion operatively associated with a gearbox (18) of the gas turbine and a driven portion operatively associated with a fuel pump (22) of the gas turbine, an...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	RIBAROV, Lubomir A, DAVIS, Christopher J, RICKIS, Aaron F, REUTER, Charles E, KOVACH, Brandon T, CARPENTER, Richard J, SCHELONKA, Michael D, HODGE, William D, LE DUC, Zachary Allen Ray
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A fuel delivery system for a gas turbine engine (12) is disclosed which includes a continuously variable drive assembly (14) having a driving portion operatively associated with a gearbox (18) of the gas turbine and a driven portion operatively associated with a fuel pump (22) of the gas turbine, and a governor for controlling a drive ratio of the drive assembly (14) to vary fuel pump flow performance over a range of engine operating conditions.