A duct (107) for a ducted-rotor aircraft (101) includes a hub (119), a duct ring (149), and a plurality of stators (121) that extend outward from the hub (119). The hub (119) may be configured to support a motor. The duct ring (149) defines a trailing edge (155). The duct ring (149) is coupled to each of the plurality of stators (121) such that all or substantially all of each of the plurality of stators (121) is located aft of the trailing edge (155) of the duct ring (149).


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    Titel :

    STATORS LOCATED AFT OF DUCT RING


    Weitere Titelangaben:

    HINTER EINEM KANALRING ANGEORDNETE STATOREN
    STATORS SITUÉS À L'ARRIÈRE D'UN ANNEAU DE CONDUIT


    Beteiligte:
    FEELEY ELIZABETH (Autor:in) / SCROEDER KARL (Autor:in)

    Erscheinungsdatum :

    2021-07-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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