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.


    Access

    Download


    Export, share and cite



    Title :

    AERODYNAMIC SYSTEM FOR AN AIRCRAFT


    Additional title:

    AERODYNAMISCHES SYSTEM FÜR EIN FLUGZEUG
    SYSTÈME AÉRODYNAMIQUE POUR AÉRONEF


    Contributors:
    HENCKE MARC (author)

    Publication date :

    2024-12-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aerodynamic system for aircraft and aircraft

    HENKE MARC | European Patent Office | 2024

    Free access

    AERODYNAMIC AIRCRAFT

    GRIGORCHUK VLADIMIR STEPANOVICH | European Patent Office | 2017

    Free access

    Aerodynamic System For An Aircraft

    HENCKE MARC | European Patent Office | 2024

    Free access

    AERODYNAMIC SYSTEM FOR AN AIRCRAFT

    DAANDELS DORT / LORENZ FLORIAN / WUNDERLICH SÖNKE | European Patent Office | 2024

    Free access

    AERODYNAMIC AIRCRAFT COMPONENT

    BENSMANN STEFAN | European Patent Office | 2020

    Free access