A flap deployment apparatus and system for a wing of an aircraft that includes a support structure having a first aerodynamic surface. A nose fitting secures the support structure to a forward portion of an aircraft wing and an aft fitting secures the support structure to an aft portion of the wing. A carrier beam having a second aerodynamic surface is coupled to the support structure. The carrier beam is movable between a stowed position and a deployed position. Links guide the carrier between the positions. The first and second aerodynamic surfaces are configured to define a continuous aerodynamic surface when the carrier beam is in the stowed position. The apparatus includes a nose fairing having a third aerodynamic and a mid fairing cover having a fourth aerodynamic surface. The third and fourth aerodynamic surfaces also defines the continuous aerodynamic surface when the carrier beam is in the stowed position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Flap Support Structure


    Beteiligte:

    Erscheinungsdatum :

    2019-12-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aerodynamic flap support structure

    GRUNER BRYAN JACOB | Europäisches Patentamt | 2020

    Freier Zugriff

    AERODYNAMIC MUD FLAP

    MORGAN JUSTIN / BAXTER PARKER / PAN CHINGLIN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    AERODYNAMIC MUD FLAP

    MORGAN JUSTIN / BAXTER PARKER / PAN CHINGLIN et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    AERODYNAMIC MUD FLAP

    BRUIN JAMES / HAWS JAMES D / VELDHUIZEN ROY | Europäisches Patentamt | 2023

    Freier Zugriff

    Aerodynamic mud flap

    MORGAN JUSTIN / BAXTER PARKER / PAN CHINGLIN et al. | Europäisches Patentamt | 2021

    Freier Zugriff