An airfoil includes at least one precured composite spar (66, 68) having a web (82, 88) and at least one flange or cap (84, 86, 90, 92) integrated with an end of the web. A precured composite skin (74, 76) is attached to the spar by adhesive bonding the skin to the flange.


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    Title :

    Bonded composite airfoil and fabrication method


    Additional title:

    Tragfläche aus Verbundwerkstoff und Verfahren zu deren Herstellung
    Profil aérodynamique composite et procédé de sa fabrication


    Contributors:

    Publication date :

    2019-07-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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