A rotor support device includes a plurality of first electrodes, a plurality of second electrodes, a dielectric material, and at least one alternating-current power supply. The dielectric material is disposed between the plurality of first electrodes and the plurality of second electrodes. The at least one AC power supply is configured to apply an alternating-current voltage across the plurality of first electrodes and the plurality of second electrodes and induce flows of gas by causing dielectric barrier discharge between the plurality of first electrodes and the plurality of second electrodes. At least one of the plurality of first electrodes or the plurality of second electrodes is disposed apart from each other in a static system that is stationary with respect to a rotor provided in an aircraft. The static system is adjacent to the rotor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotor support device, rotor, gas turbine engine, and aircraft


    Beteiligte:
    KATO HIROKI (Autor:in) / KIKUCHI MAKI (Autor:in)

    Erscheinungsdatum :

    02.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten



    ROTOR SUPPORT DEVICE, ROTOR, GAS TURBINE ENGINE, AND AIRCRAFT

    KATO HIROKI / KIKUCHI MAKI | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft rotor motor support

    DENG YUNDI | Europäisches Patentamt | 2022

    Freier Zugriff

    Single-engine four-rotor aircraft

    WANG ZHICHENG / SHENG LIHUA | Europäisches Patentamt | 2021

    Freier Zugriff

    Single-engine five-rotor aircraft

    WANG ZHICHENG / HUANG JIASHENG | Europäisches Patentamt | 2021

    Freier Zugriff

    Single-engine three-rotor aircraft

    WANG ZHICHENG / MA WEI | Europäisches Patentamt | 2021

    Freier Zugriff