The chord line increases from a root end towards a tip end of said vane. This vane is fitted pivotably in a turbine engine casing so as to divert a flow of cold air circulating in an annular duct thereof.


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    Titel :

    TURBINE ENGINE STATOR VANE, FAN CASING COMPRISING SUCH A VANE, THRUST REVERSER SYSTEM OF A TURBINE ENGINE EQUIPPED WITH SUCH A VANE AND TURBINE ENGINE EQUIPPED WITH SAID VANE, SAID CASING OR SAID SYSTEM



    Erscheinungsdatum :

    2017-05-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke




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