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.
ENGINE MOUNT WAITING FAIL SAFE DETECTION
BELASTUNGSDETEKTION EINER AUSFALLSICHEREN MOTORAUFHÄNGUNG
DÉTECTION DE CHARGE D'UN SUPPORT MOTEUR FAIL-SAFE
2022-06-22
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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