Pre-cooler inlet ducts that utilize active flow-control and systems and methods including the same are disclosed herein. The systems include a pre-cooler inlet duct for a jet engine that is configured to receive a pre-cooler air stream and to direct the pre-cooler air stream into a heat exchanger. The pre-cooler inlet duct includes a flow-directing surface, which defines at least a portion of the pre-cooler inlet duct, and an active flow-control device. The active flow-control device is located to modify a boundary layer fluid flow within a boundary layer adjacent the flow-directing surface to resist separation of the boundary layer from the flow-directing surface when the pre-cooler air stream flows through the pre-cooler inlet duct. The methods include methods of resisting boundary layer separation in the pre-cooler inlet duct by flowing the pre-cooler air stream across the flow-directing surface and modifying the boundary layer with the active flow-control device. (Fig. 6)


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    Titel :

    PRE-COOLER INLET DUCT WITH ACTIVE FLOW-CONTROL AND METHOD INCLUDING THE SAME


    Weitere Titelangaben:

    VORKÜHLERANSAUGKANAL MIT AKTIVSTROMSTEUERUNG SOWIE VERFAHREN DAMIT
    CONDUIT D'ENTRÉE DE PRÉ-REFROIDISSEUR À RÉGULATION DE DÉBIT ACTIVE ET PROCÉDÉ COMPRENANT CELUI-CI


    Beteiligte:
    PACKARD NATHAN O (Autor:in) / WILLIE ROBERT H (Autor:in) / TRETOW PAUL R (Autor:in)

    Erscheinungsdatum :

    25.07.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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