An airfoil tip vortex mitigation arrangement comprising one or more flow directors configured and positioned to re-direct freestream air over a low pressure surface of an airfoil in such a way as to displace and weaken a main tip vortex generated at a tip of the airfoil.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Minimally intrusive wingtip vortex wake mitigation using microvane arrays


    Beteiligte:
    DOMEL NEAL D (Autor:in) / CHARLTON ERIC F (Autor:in) / MILLER DANIEL N (Autor:in)

    Erscheinungsdatum :

    2018-02-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Airfoil comprising a minimally intrusive wingtip vortex mitigation device

    WOODEN PERRY / MOOR RUBLE E / CHARLTON ERIC F et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Adhesive panels of microvane arrays for reducing effects of wingtip vortices

    ROSENBERGER BRIAN T / CHARLTON ERIC FREDERICK / MILLER DANIEL N | Europäisches Patentamt | 2020

    Freier Zugriff

    Adhesive panels of microvane arrays for reducing effects of wingtip vortices

    ROSENBERGER BRIAN T / CHARLTON ERIC FREDERICK / MILLER DANIEL N | Europäisches Patentamt | 2018

    Freier Zugriff

    Wingtip vortex turbine

    Patterson, James C., Jr. | NTRS | 1990


    Wingtip Vortex Turbine

    J. C. Patterson | NTIS | 1981