A duct for an aircraft or watercraft for influencing fluid flow. The duct comprises a duct section 110, which receives fluid flow, defining a first direction 116 through the duct section from a fluid inlet end 112 to a fluid outlet end 114. The duct section further houses a rotor 120 and vortex generator surface. The vortex generator surface is arranged to induce vortices in the fluid flow through the duct section. The vortex generator may be arranged on one or more rotor blades 124 of the rotor, preferably at the trailing edge of the blade. The vortex generator may be provided on a stator (410, figure 7). The vortex generator may comprise a series of projections 252. The duct section may be a first duct section and the vortex generator surface may be first vortex generator surface wherein the duct further comprises a second duct section 210 having a second vortex generator surface.


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    Title :

    Duct arrangement and method


    Contributors:
    CALLUM STARK (author) / WEICHAO SHI (author)

    Publication date :

    2023-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B63H Schiffsantrieb oder Steuerung der Schiffe , MARINE PROPULSION OR STEERING / B64C AEROPLANES , Flugzeuge / F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten



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