A system for mounting a gas turbine engine to a pylon and for detecting a failure within the system, the gas turbine engine comprising a first case, is disclosed. In various embodiments, the system includes a first mount connecting the first case to the pylon; and a first sensor configured to detect a first relative motion between the first case and the first mount.


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    Titel :

    ENGINE MOUNT WAITING FAIL SAFE DETECTION


    Beteiligte:
    GORMLEY TIMOTHY (Autor:in) / RAMLAOUI JIHAD (Autor:in)

    Erscheinungsdatum :

    2022-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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