An airfoil includes a proximal end and a distal end opposite the proximal end. The airfoil also includes a distal portion extending adjacent the distal end and an edge extending between the proximal end and the distal end. The airfoil further includes a surface extending between the proximal end and the distal end. The edge and the surface define a sweep and a cahedral through the distal portion and at least a portion of the intermediate portion.


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    Titel :

    AIRFOIL FOR A ROTARY MACHINE INCLUDING A PROPELLOR ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    01.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



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