Fuel control for starting a gas turbine engine

A method of controlling fuel flow to a combustor ( 18 ) of a gas turbine engine ( 10 ) during startup of the engine includes determining a relationship between Cv and valve position for a flow control valve (e.g., 24 ) in a fuel supply ( 20 ) to the combustor as a function of at least one real time...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SINGH JATINDER P, KOLLAR JOSEPH L, KOZACHUK DANNY W, GADDE SATISH B, HILDEBRANDT GARY, TEEHAN DAMIEN G
Format:	Patent
Sprache:	eng
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 INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MECHANICAL ENGINEERING WEAPONS
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