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).


    Access

    Download


    Export, share and cite



    Title :

    TAKEOFF POWER MANAGEMENT SYSTEM AND METHOD FOR GAS TURBINE ENGINES


    Additional title:

    STARTLEISTUNGSVERWALTUNGSSYSTEM UND -VERFAHREN FÜR GASTURBINENMOTOREN
    SYSTÈME DE GESTION DE PUISSANCE AU DÉCOLLAGE ET PROCÉDÉ POUR MOTEURS DE TURBINE À GAZ


    Contributors:

    Publication date :

    2023-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Takeoff power management system and method for gas turbine engines

    FEULNER MATTHEW R / WALTHER RONALD S | European Patent Office | 2019

    Free access

    TAKEOFF POWER MANAGEMENT SYSTEM AND METHOD FOR GAS TURBINE ENGINES

    FEULNER MATTHEW R / WALTHER RONALD S | European Patent Office | 2017

    Free access


    Vehicle power takeoff parking power takeoff control method and vehicle

    WU XIANGCHAO / SUN WENJU / XIONG YANFENG et al. | European Patent Office | 2023

    Free access

    Power takeoff executing mechanism, power takeoff and vehicle

    ZHANG LIN / ZHONG JIAZONG / ZHAI HENGJUN | European Patent Office | 2023

    Free access