The invention relates to a control surface element for an airplane, in particular a spoiler, comprising a composite fiber element that has a surface around which air flows, a mounting device for movably mounting the composite fiber element on a structural component, and a reinforcing structure for reinforcing the composite fiber element. The reinforcing structure comprises at least one reinforcing element which is integrally formed with the composite fiber element. The reinforcing structure comprises a primary reinforcing element which is designed to receive main loads and which is connected to at least one secondary reinforcing element that is designed to receive secondary loads. The composite fiber element comprises a recess for integrally forming the primary reinforcing element.


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    Titel :

    CONTROL SURFACE ELEMENT FOR AN AIRPLANE


    Beteiligte:
    SEIS MICHAEL (Autor:in) / MEINDLHUMER MARTIN (Autor:in)

    Erscheinungsdatum :

    2017-08-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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