The present invention relates to a drive system for a variable camber aircraft wing having position variable front flaps and/or rear flaps, having drive shafts, which are arranged such that that the flaps undergo a change of position in operation of the drive shafts, and having one or more drive units in driving connection with the drive shafts, wherein at least one switchable coupling is provided via which the drive shafts of two flaps of an aircraft wing can be coupled to one another.


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    Titel :

    Drive system for a variable camber aircraft wing


    Beteiligte:
    CONRAD SUSANNE (Autor:in) / MANGLER WERNER (Autor:in) / BÄR JOSEF (Autor:in) / SCHIEVELBUSCH BERND (Autor:in)

    Erscheinungsdatum :

    16.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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