Example active flow control systems and methods for aircraft are described herein. An example method includes supplying pressurized air to a plurality of nozzles. The nozzles arranged in an array across a control surface of an aircraft, and the nozzles are oriented to eject the pressurized air in a substantially streamwise direction. The method further includes activating the nozzles to eject the pressurized air in sequence to create a wave of air moving in a spanwise direction across the control surface.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ACTIVE FLOW CONTROL SYSTEMS AND METHODS FOR AIRCRAFT


    Beteiligte:
    SHMILOVICH ARVIN (Autor:in) / YADLIN YORAM (Autor:in) / VIJGEN PAUL (Autor:in)

    Erscheinungsdatum :

    2018-02-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    ACTIVE FLOW CONTROL SYSTEMS AND METHODS FOR AIRCRAFT

    SHMILOVICH ARVIN / YADLIN YORAM / VIJGEN PAUL | Europäisches Patentamt | 2019

    Freier Zugriff

    ACTIVE FLOW CONTROL SYSTEMS AND METHODS FOR AIRCRAFT

    RAFFERTY BRADLEY J / BECKMAN MARY E / LEUNG ANDREW et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Active flow control systems and methods for aircraft

    RAFFERTY BRADLEY J / BECKMAN MARY E / LEUNG ANDREW et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Active flow control systems and methods for aircraft

    SHMILOVICH ARVIN / YADLIN YORAM / VIJGEN PAUL | Europäisches Patentamt | 2020

    Freier Zugriff

    ACTIVE FLOW CONTROL SYSTEMS AND METHODS FOR AIRCRAFT

    SHMILOVICH ARVIN / YADLIN YORAM / VIJGEN PAUL | Europäisches Patentamt | 2020

    Freier Zugriff