An active flow control system for generating roll control moments for an aircraft during hover flight. The system includes right and left roll 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 roll effectors. 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.


    Access

    Download


    Export, share and cite



    Title :

    Fluidic roll control systems for use in hover



    Publication date :

    2021-11-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Fluidic Roll Control Systems for Use in Hover

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | European Patent Office | 2021

    Free access

    Fluidic Yaw Control Systems for Use in Hover

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | European Patent Office | 2021

    Free access

    Fluidic yaw control systems for use in hover

    ROBERTSON DANIEL BRYAN / GRONINGA KIRK LANDON / LOUIS MATTHEW EDWARD | European Patent Office | 2022

    Free access


    Fluidic emergency roll control system

    Haefner, K. B. / Honda, T. S. | NTRS | 1973