A method is provided for repairing a structural weakness, preventing or inhibiting the initiation of a structural weakness, or preventing or inhibiting the progression of a structural weakness in an aircraft frame element. The method includes bonding a plurality of particles to the element such that the plurality of metallic particles form a continuous layer over the area of weakness, or the predicted area of weakness. The metallic particles may be applied by a cold spray process such as supersonic particle deposition.


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    Titel :

    METHODS FOR RESTORING AN AIRCRAFT FRAME ELEMENT


    Beteiligte:
    MATTHEWS NEIL (Autor:in) / JONES RHYS (Autor:in)

    Erscheinungsdatum :

    2016-11-24


    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 / B64C AEROPLANES , Flugzeuge / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL



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