Most commercial aircraft interior panels are constructed of honeycomb cored composite sandwich panels. The panels are conventionally joined using metal brackets fastened with screws. Over the past decade, most major interior fabricators have been in transition to a method of joinery using bonded interlocking joints. This method has recently been adopted by Boeing, and is known here as Tab and Slot Joinery.These interlocking joints are defined and illustrated. The history of the development effort is outlined. Design considerations are developed. Test programs are described, including a designed experiment and a special case fatigue test. Advantages of this new joinery method over the conventional are shown.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Assembly of Interior Composite Panels Utilizing Bonded Interlocking Joints


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    SAE Aerospace Manufacturing Technology Conference & Exposition ; 1997



    Erscheinungsdatum :

    03.06.1997




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Assembly of Interior Composite Panels Utilizing Bonded Interlocking Joints

    Button, S. D. / Hodgman, T. F. / Society of Automotive Engineers | British Library Conference Proceedings | 1997



    Bonded-bolted composite joints

    HART-SMITH, L. | AIAA | 1984


    Bonded-bolted composite joints

    HART-SMITH, L. J. | AIAA | 1985


    Vehicle seat with secure interlocking panels

    SARDO LOUIS | Europäisches Patentamt | 2020

    Freier Zugriff