A structural system for accommodating the thermal expansion of a nacelle lip skin and supporting structure has a lip skin (24) and a first angle element (62) attached to the lip skin (24). The first angle element (62) has a free edge (82) that is scalloped to accommodate thermal stresses. A bulkhead (60) is attached to the first angle element (62).


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    Title :

    METHOD OF ATTACHING NACELLE STRUCTURE TO MINIMIZE FATIGUE LOADING


    Additional title:

    VERFAHREN ZUM ANBRINGEN EINER GONDELSTRUKTUR ZUR MINIMIERUNG VON DAUERBEANSPRUCHUNG
    PROCÉDÉ DE FIXATION DE STRUCTURE DE NACELLE POUR RÉDUIRE UNE CHARGE DE FATIGUE



    Publication date :

    2019-05-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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