Systems and methods for diagnosing aircraft failure are provided. In one embodiment, a method can include receiving a first set of data from an aircraft in flight indicative of a failure event associated with the aircraft. The first set of data can be indicative of at least one or more conditions associated with the aircraft. The method can include performing one or more computer-based simulations to generate one or more simulated failure events, based at least in part on the conditions. The method can include identifying one or more simulated causes associated with the simulated failure events. The method can include determining one or more potential causes of at least a portion of the failure event, based at least in part on the simulated causes. The method can include communicating a second set of data indicative of at least the potential causes, to the aircraft while it is in flight.


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    Titel :

    Real Time Non-Onboard Diagnostics of Aircraft Failures


    Beteiligte:

    Erscheinungsdatum :

    2017-08-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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