An active flow control system for generating roll control moments for an aircraft during forward flight. The system includes right and left roll effectors disposed on a trailing edge of the wing. A pressurized air system includes a pressurized air source and a plurality of injectors operably associated with the right and left roll effectors that influence the path of airflow across the wing. Based upon which of the injectors is injecting pressurized air, the right and left roll effectors generate no roll control moment, generate a roll right control moment or generate a roll left control moment.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Fluidic Roll Control Systems for Use in Forward Flight


    Beteiligte:

    Erscheinungsdatum :

    30.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Fluidic roll control systems for use in forward flight

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | Europäisches Patentamt | 2021

    Freier Zugriff

    Fluidic pitch control systems for use in forward flight

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | Europäisches Patentamt | 2021

    Freier Zugriff

    Fluidic Pitch Control Systems for Use in Forward Flight

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | Europäisches Patentamt | 2021

    Freier Zugriff

    Fluidic drag rudder systems for yaw control in forward flight

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | Europäisches Patentamt | 2021

    Freier Zugriff

    Fluidic split flap systems for yaw control in forward flight

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | Europäisches Patentamt | 2021

    Freier Zugriff