A fastening system to couple a first aircraft structure and a second aircraft structure is disclosed. The fastening system (110) includes a fastener (420), a nutplate (400) having a body (402) defining an opening (510) to receive the fastener (420), a flange (404) extending from the body (402) to engage an outer surface of the first structure, and a first sleeve (406) protruding from the flange (404) in a direction away from the body (402), the first sleeve (406) to couple to a first bore formed in the first structure and prevents rotation of the nutplate (400) relative to the first structure.


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    Title :

    FASTENING SYSTEM FOR AIRCRAFT STRUCTURES


    Additional title:

    BEFESTIGUNGSSYSTEM FÜR FLUGZEUGSTRUKTUREN
    SYSTÈME DE FIXATION POUR STRUCTURES D'AÉRONEF


    Contributors:

    Publication date :

    2022-01-05


    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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    BLOCK SAMUEL L / DAVIES JOHN A / SCHROEDER IAN E | European Patent Office | 2022

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