A method includes, while the airplane is on the ground, entering (100) a disking mode including positioning the blades at a disking pitch including rotating each blade around the length, the disking pitch oriented parallel to the plane of rotation, maintaining (102) the blades at the disking pitch, and exiting (104) the disking mode when a disking mode exit condition is met, including rotating each blade around the length, away from the disking pitch.


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    Titel :

    METHOD AND SYSTEM OF OPERATING AN AIRPLANE ENGINE


    Weitere Titelangaben:

    VERFAHREN UND SYSTEM ZUM BETRIEB EINES FLUGZEUGMOTORS
    PROCÉDÉ ET SYSTÈME D'OPÉRATION D'UN MOTEUR D'AVION


    Beteiligte:

    Erscheinungsdatum :

    09.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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