A system for mounting a gas turbine engine to a pylon (202) and for detecting a failure within the system, the gas turbine engine comprising a first case (210), is disclosed. In various embodiments, the system includes a first mount (214) connecting the first case to the pylon; and a first sensor (329) 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


    Weitere Titelangaben:

    BELASTUNGSDETEKTION EINER AUSFALLSICHEREN MOTORAUFHÄNGUNG
    DÉTECTION DE CHARGE D'UN SUPPORT MOTEUR FAIL-SAFE


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

    Erscheinungsdatum :

    2022-06-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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