Aspects of the disclosure are directed to a system (200) associated with an engine (10) of an aircraft comprising a duct (218), an inlet (234) coupled to the duct (218), and a fence (252) coupled to the inlet (234) or located upstream of the inlet (234). In some embodiments, the system further comprises a valve body (226) coupled to the duct (218). In some embodiments, the valve body (226) includes at least one valve (230) that is configured to rotate between a closed state and an open state.


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    Titel :

    FENCE FOR DUCT TONE MITIGATION


    Weitere Titelangaben:

    ZAUN FÜR KANALTONABSCHWÄCHUNG
    CLÔTURE POUR ATTÉNUATION DE TONALITÉ DE CONDUIT


    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 :

    06.03.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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