An aircraft structure (10), in particular the fuselage, nacelles or wings, includes, over all or part of an outer surface (21) that may undergo lightning impacts, a layer of flexible polymer (30), a photovoltaic film (40) and a protective layer (50) protecting the photovoltaic film. This aircraft structure primarily has a solar energy capture capacity making it possible to meet the needs of an aircraft as well as an ability to protect against the effects of lightning.


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    Titel :

    AIRCRAFT STRUCTURE WITH SOLAR ENERGY CAPTURE CAPACITY


    Beteiligte:
    RIVES BERTRAND (Autor:in) / PERES GILLES (Autor:in) / PORTE ALAIN (Autor:in)

    Erscheinungsdatum :

    2016-12-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01L Halbleiterbauelemente , SEMICONDUCTOR DEVICES



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