The invention relates to a method of manufacturing a stiffened panel (10) comprising a skin (11) and at least one substantially elongate stiffener (12) said stiffener comprising a longitudinal groove (13) forming a cavity (15), said panel comprising at least one means (19) for storing and releasing electrical energy which means is placed inside the cavity, said method involving a step of filling the groove (13) with at least one means (19) of storing and releasing electrical energy; and a step of covering said means with the skin (11) so that the groove of the stiffener and the skin together form the cavity (15). The invention also relates to a stiffened ring (10) derived from such a method.


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    Titel :

    Stiffened panel and method of manufacturing same


    Beteiligte:
    BERMUDEZ MICHEL (Autor:in) / MESNAGE DIDIER (Autor:in) / SMAOUI HICHEM (Autor:in) / FLEURY BENOIT (Autor:in)

    Erscheinungsdatum :

    2015-07-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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