System (1) and method for interconnecting components (C1, C2) in a vehicle body structure (S), and especially for interconnecting fibre-reinforced composite components in a fuselage structure (F) of an aircraft (A). The system (1) comprises: a first adapter member (10) having a first mating portion (11) configured to substantially conform with a profile (P1) of a first component (C1) of the structure (S) in more than one plane, and a first attachment portion (13) connected to the first mating portion (11); a second adapter member (20) having a second mating portion (21) configured to substantially conform with a profile (P2) of a second component (C2) of the structure (S) in more than one plane, and a second attachment portion (23) connected to the second mating portion (21); and a connector member (30) to securely interconnect the first and second attachment portions (13, 23) of the first and second adapter members (10, 20).


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    Title :

    System and method for interconnecting composite structures


    Additional title:

    System und Verfahren zum Verbinden von Verbundstoffstrukturen miteinander
    Système et procédé pour interconnecter des structures composites


    Contributors:

    Publication date :

    2018-05-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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 / 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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