Methods for controlling an aircraft turbofan engine during icing of a temperature probe and devices for carrying out such methods are described. The methods may comprise: using (46) one or more signals representative of temperature received from a heated temperature probe to generate one or more control signals for use in controlling the engine; determining (44) that an icing condition associated with the probe exists; and using (48) data representing one or more substitute signals in place of signals representative of temperature received from the heated temperature probe to generate the one or more control signals for use in controlling the engine.


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    Titel :

    Aircraft engine control during icing of temperature probe


    Weitere Titelangaben:

    Flugzeugmotorsteuerung mit vereister Temperatursonde
    Contrôle d'un moteur d'avion pendant le givrage d'un capteur de température


    Beteiligte:
    CALANDRA SALVATORE (Autor:in) / GIROUX FREDERIC (Autor:in) / IACOBACCI MARK (Autor:in) / CHABOT MARTIN (Autor:in) / HARTROPP SIMON (Autor:in) / SYED YUSUF (Autor:in) / CHMIEL DARIUSZ (Autor:in) / BALAJ ADRIENNE (Autor:in)

    Erscheinungsdatum :

    2018-10-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / G01K MEASURING TEMPERATURE , Messen der Temperatur



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