Flow control ducted fans are disclosed. A disclosed example flow control apparatus for use with an aircraft includes a duct defining an inner cavity (208) with a primary flow path, a fan (110, Figure 1) disposed in the inner cavity (208), an aperture (210) 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 (310) to control a degree to which the aperture is opened.


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    Titel :

    FLOW CONTROL DUCTED FANS


    Weitere Titelangaben:

    KANALGEFÜHRTE DURCHFLUSSREGELUNGSGEBLÄSE
    VENTILATEURS CARÉNÉS DE RÉGULATION D'ÉCOULEMENT


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

    Erscheinungsdatum :

    2024-07-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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