An active flow control system for generating yaw control moments for an aircraft during hover flight. The system includes right and left yaw effectors disposed proximate the right and left wingtips of the wing. A pressurized air system includes a pressurized air source and a plurality of injectors operably associated with the right and left yaw effectors. Based upon which of the injectors is injecting pressurized air, the right and left yaw effectors generate no yaw control moment, generate a yaw right control moment or generate a yaw left control moment.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Fluidic yaw control systems for use in hover


    Beteiligte:

    Erscheinungsdatum :

    22.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Fluidic roll control systems for use in hover

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

    Freier Zugriff

    Fluidic Roll Control Systems for Use in Hover

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

    Freier Zugriff

    Fluidic Yaw Control Systems for Use in Hover

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

    Freier Zugriff


    Hover control

    LIU ANG / ZHAO YONGJIAN / ZHOU GUYUE | Europäisches Patentamt | 2020

    Freier Zugriff