The invention relates to an aerodynamic system (1) comprising a support structure (10) and an aerodynamic component (20) movably coupled to the support structure via first and second coupling units (31, 32) such that the aerodynamic component (20) can be moved relative to the support structure (10). The first and second coupling units (31, 32) can transfer a load from the aerodynamic component (20) to the support structure (10). The system (1) further comprises an auxiliary coupling unit (40) coupled between the aerodynamic component (20) and the support structure (10), and configured to switch from a decoupling state (41) to a coupling state (42), wherein, in the decoupling state (41), a load transfer via the at least one auxiliary coupling unit (40) is prevented, and wherein, in the coupling state (42), a load transfer via the at least one auxiliary coupling unit (40) is enabled.


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    Titel :

    AERODYNAMIC SYSTEM FOR AN AIRCRAFT


    Weitere Titelangaben:

    AERODYNAMISCHES SYSTEM FÜR EIN FLUGZEUG
    SYSTÈME AÉRODYNAMIQUE POUR AÉRONEF


    Beteiligte:
    HENCKE MARC (Autor:in)

    Erscheinungsdatum :

    04.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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