GAS TURBINE ENGINE STALL MARGIN MANAGEMENT

A method 300 for operating a gas turbine engine having a starter-electric generator (108) driven by one of a plurality of shafts of the gas turbine engine is provided. The method includes determining 302 a desired amount of thrust to be produced by the gas turbine engine, as well as a desired amount...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GEMIN, Paul Robert, ADIBHATLA, Sridhar, LEAMY, Kevin Richard, RADUN, Arthur Vorwerk
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
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