An aircraft health and usage monitoring system (HUMS) (10) comprising one or more monitoring sensors (30) arranged to be coupled to an aircraft subassembly (102, 104, 106, 108) to monitor the health of one or more parts of the subassembly and a trigger subsystem. The trigger subsystem comprises a sound transducer (20) and a processor (101), the processor being coupled to the sound transducer to receive and process sound signals from the sound transducer to extract sound information and being coupled to the monitoring sensors to provide control commands to the monitoring sensors. The processor is configured to provide a first control command to the monitoring sensors in response to a first criteria having been met, the first criteria comprising registering first sound information.


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    Title :

    AIRCRAFT HEALTH AND USAGE MONITORING SYSTEM AND TRIGGERING METHOD


    Additional title:

    FLUGZEUGGESUNDHEITS- UND -NUTZUNGSÜBERWACHUNGSSYSTEM UND AUSLÖSEVERFAHREN
    SYSTÈME DE SURVEILLANCE DE LA SANTÉ ET DE L'UTILISATION D'UN AÉRONEF ET PROCÉDÉ DE DÉCLENCHEMENT


    Contributors:

    Publication date :

    2024-02-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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