Apparatus and methods to lower peak temperatures and improve performance of aircraft (100) anti-icing systems (200) are described herein. One described example apparatus includes a skin (206) on an inlet side of a nacelle (201) of an aircraft defining an annular chamber (211), a gas delivery system (212) disposed within the annular chamber to provide a first gas to mix with and entrain a second gas in the annular chamber to define a flow through the annular chamber, and a deflector vane (214) disposed within the annular chamber to redirect the flow through the annular chamber. The second gas is at a different temperature from the first gas.


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    Titel :

    Aircraft anti-icing systems having deflector vanes


    Weitere Titelangaben:

    Systeme zur Verhinderung der Flugzeugvereisung mit Umlenkschaufeln
    Systèmes antigivrage d'avion comportant des aubes déflectrices


    Beteiligte:

    Erscheinungsdatum :

    2019-11-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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