An aerodynamic system for an aircraft. The aerodynamic system includes a first aerodynamic component configured to be movably coupled to a primary structure of the aircraft, a second aerodynamic component which is movably coupled to the first aerodynamic component and a first panel element coupled to the first aerodynamic component. The first panel element at least partially covers a gap between the first aerodynamic component and the second aerodynamic component. The aerodynamic system further includes a sealing element arranged between the first aerodynamic component and the second aerodynamic component. The sealing element is configured to at least partially block an airflow between the first aerodynamic component and the second aerodynamic component.


    Access

    Download


    Export, share and cite



    Title :

    AERODYNAMIC SYSTEM FOR AN AIRCRAFT


    Contributors:

    Publication date :

    2024-10-17


    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

    HENCKE MARC | European Patent Office | 2024

    Free access

    AERODYNAMIC AIRCRAFT COMPONENT

    BENSMANN STEFAN | European Patent Office | 2020

    Free access