Aspects of the disclosure are directed to a system associated with an engine of an aircraft comprising: a duct, an inlet coupled to the duct, and a fence coupled to the inlet or located upstream of the inlet. In some embodiments, the system further comprises a valve body coupled to the duct. In some embodiments, the valve body includes at least one valve that is configured to rotate between a closed state and an open state.


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    Titel :

    FENCE FOR DUCT TONE MITIGATION


    Beteiligte:
    POST KEITH A (Autor:in) / SHANNON DANIEL W (Autor:in) / ZYSMAN STEVEN H (Autor:in) / ZSURKA MARK (Autor:in) / DE LA RIVA DIEGO H (Autor:in) / KOUSHIK SUDARSHAN N (Autor:in)

    Erscheinungsdatum :

    23.11.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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