In one embodiment, an apparatus may comprise an attachment device (302) configured to be embedded in a structure (308), wherein the attachment device (302) comprises: a body comprising a first flange (306a) and a second flange (306b), wherein the body is configured such that the first flange (306a) and the second flange (306b) are coupled together internally within the body when the attachment device (302) is embedded in the structure (308); an attachment fitting (304) for coupling a component to the structure (308) in which the attachment device (302) is embedded.


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    Title :

    PUCK ATTACHMENT MECHANISM FOR FLEXIBLE AIRCRAFT CONFIGURATION


    Additional title:

    PUCKBEFESTIGUNGSMECHANISMUS FÜR FLEXIBLE FLUGZEUGKONFIGURATION
    MÉCANISME DE FIXATION DE DISQUE POUR UNE CONFIGURATION D'AÉRONEF FLEXIBLE


    Contributors:

    Publication date :

    2020-04-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile



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