A structural health monitoring system and method includes a plurality of sensors configured to collect sensed data, a first structural component, and a controller configured to receive the sensed data and detect a first condition based upon the sensed data. The controller is further configured to initiate a first structural interrogation of the first structural component upon detection of the condition.


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    Title :

    AUTOMATED STRUCTURAL INTERROGATION OF AIRCRAFT COMPONENTS


    Contributors:
    CARINI PETER (author) / GANG TRAVIS (author)

    Publication date :

    2018-03-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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