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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    Title :

    METHOD AND SYSTEM OF OPERATING AN AIRPLANE ENGINE


    Additional title:

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



    Publication date :

    2023-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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