An aircraft airflow modification device, comprising: at least one resiliently deformable base member; and at least one resiliently deformable flap member that extends from the resiliently deformable base member. Deformation of the resiliently deformable base member from a first state to a second state results in corresponding deformation of the resiliently deformable flap member from a first state to a second state.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft airflow modification device and vortex generator arrangement for an aircraft


    Contributors:

    Publication date :

    2020-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT

    ELBRACHT DIRK / STEFES BRUNO | European Patent Office | 2020

    Free access

    AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT

    ELBRACHT DIRK / STEFES BRUNO | European Patent Office | 2018

    Free access

    Vortex generator arrangement for an aircraft

    STEFES BRUNO / EILKEN WOLFGANG / PAUL ERICH | European Patent Office | 2020

    Free access

    VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT

    STEFES BRUNO / EILKEN WOLFGANG / PAUL ERICH | European Patent Office | 2017

    Free access

    VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT

    STEFES BRUNO | European Patent Office | 2019

    Free access