An aerodynamic system includes a support structure and an aerodynamic component movably coupled to the support structure via first and second coupling units such that the aerodynamic component can be moved relative to the support structure. The first and second coupling units can transfer a load from the aerodynamic component to the support structure. The system further includes an auxiliary coupling unit coupled between the aerodynamic component and the support structure, and configured to switch from a decoupling state to a coupling state, wherein, in the decoupling state, a load transfer via the at least one auxiliary coupling unit is prevented, and wherein, in the coupling state, a load transfer via the at least one auxiliary coupling unit is enabled.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic System For An Aircraft


    Beteiligte:
    HENCKE MARC (Autor:in)

    Erscheinungsdatum :

    05.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aerodynamic system for aircraft and aircraft

    HENKE MARC | Europäisches Patentamt | 2024

    Freier Zugriff

    AERODYNAMIC AIRCRAFT

    GRIGORCHUK VLADIMIR STEPANOVICH | Europäisches Patentamt | 2017

    Freier Zugriff

    AERODYNAMIC SYSTEM FOR AN AIRCRAFT

    HENCKE MARC | Europäisches Patentamt | 2024

    Freier Zugriff

    AERODYNAMIC SYSTEM FOR AN AIRCRAFT

    DAANDELS DORT / LORENZ FLORIAN / WUNDERLICH SÖNKE | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft aerodynamic thermal protection system

    CHEN WEI / ZHANG BIN / FANG HUAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff