A gas turbine engine (20) includes a control unit (46) to command the gas turbine engine (20) to perform one of a rolling takeoff procedure and an unrestricted takeoff procedure. The control unit (46) is configured to command the gas turbine engine (20) to perform the rolling takeoff procedure when information required to determine whether the unrestricted takeoff procedure can be performed is unavailable to the control unit (46).
TAKEOFF POWER MANAGEMENT SYSTEM AND METHOD FOR GAS TURBINE ENGINES
STARTLEISTUNGSVERWALTUNGSSYSTEM UND -VERFAHREN FÜR GASTURBINENMOTOREN
SYSTÈME DE GESTION DE PUISSANCE AU DÉCOLLAGE ET PROCÉDÉ POUR MOTEURS DE TURBINE À GAZ
2023-01-25
Patent
Elektronische Ressource
Englisch
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