An engine vibration monitoring and control system includes an aircraft autopilot and a flight management system (FMS). The FMS is in operable communication with the aircraft autopilot and is configured to determine when the aircraft autopilot is engaged and disengaged. The FMS is also adapted to receive vibration data from an engine vibration data source and is configured, upon determining that the aircraft autopilot is engaged, to: process the vibration data to determine when engine vibrations exceed one or more first thresholds, and when the engine vibrations exceed the one or more first thresholds, supply commands to the autopilot that cause the autopilot to take corrective actions to reduce the engine vibrations below the one or more first thresholds.


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    Titel :

    Automated engine vibration monitoring and control system


    Beteiligte:
    KUMAR ANIL (Autor:in) / S ROHITH (Autor:in) / GUPTA RAJAN (Autor:in) / VAIRAVAN CHAKKARAVARTHY (Autor:in)

    Erscheinungsdatum :

    2023-07-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AUTOMATED ENGINE VIBRATION MONITORING AND CONTROL SYSTEM

    KUMAR ANIL / S ROHITH / GUPTA RAJAN et al. | Europäisches Patentamt | 2022

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