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


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    Title :

    Method of attaching nacelle structure to minimize fatigue loading


    Contributors:

    Publication date :

    2017-09-19


    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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