A method of manufacturing a stiffened panel having a skin and at least one substantially elongate stiffener having a longitudinal groove forming a cavity. At least one storage device for storing and releasing electrical energy. The longitudinal groove is filled with at least one storage device for storing and releasing electrical energy. The storage device is covered with a skin which forms the cavity together with the longitudinal groove of the stiffener. A stiffened ring can be derived from the 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 :

    2017-05-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01G Kondensatoren , CAPACITORS



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