A rotorcraft comprises a fuselage, a tail boom, a rotor system, and a centrifugal blower system. The centrifugal blower system comprises a centrifugal blower configured to generate thrust using an airflow, wherein the centrifugal blower is located within the tail boom. The centrifugal blower system also comprises a plurality of ducts configured to control the thrust generated by the centrifugal blower, wherein the plurality of ducts is located on a portion of the tail boom surrounding the centrifugal blower, and wherein the plurality of ducts comprises one or more adjustable ducts configured to vary a size of an associated duct opening.


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    Titel :

    Rotorcraft anti-torque and directional control using a centrifugal blower


    Beteiligte:
    CARR MATTHEW R (Autor:in) / LOUIS MATTHEW E (Autor:in) / GRONINGA KIRK L (Autor:in) / ROBERTSON DANIEL B (Autor:in) / STAMPS FRANK B (Autor:in) / BRAND ALBERT G (Autor:in) / SINUSAS ERIC A (Autor:in)

    Erscheinungsdatum :

    2020-04-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



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