Stringer-less fuselage structures and associated methods of manufacturing are disclosed. In some embodiments, a fuselage structure includes a composite fuselage skin (24) including a plurality of tear straps (32) formed in the composite fuselage skin where each tear strap extends generally along a longitudinal axis of the composite fuselage skin. The fuselage structure also includes a plurality of frames (28) supporting an interior of the composite fuselage skin where the frames are spaced apart along the longitudinal axis of the composite fuselage skin.


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    Title :

    STRINGER-LESS FUSELAGE STRUCTURE AND METHOD OF MANUFACTURE


    Contributors:

    Publication date :

    2018-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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