Flow control ducted fans are disclosed. A disclosed example flow control apparatus for use with an aircraft includes a duct defining an inner cavity with a primary flow path, a fan disposed in the inner cavity, an aperture on an exterior surface of the duct and upstream from the fan, the aperture fluidly coupled to the inner cavity to define a secondary flow path, and a door to control a degree to which the aperture is opened.


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    Titel :

    FLOW CONTROL DUCTED FANS


    Beteiligte:
    NADEL ADAM (Autor:in) / BALTADJIEV NIKOLA (Autor:in) / PRETE ANTHONY (Autor:in) / WHIPPLE BRIAN (Autor:in)

    Erscheinungsdatum :

    25.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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