A turbine blade having an airfoil profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, where the X and Y values are in inches and the Z values are non-dimensional values from 0 to 1 and convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form an airfoil shape. The X, Y, and Z distances may be scaled as a function of the same constant number and the X, Y, and Z distances lie within an envelope of approximately +/−0.032 inches in directions normal to the airfoil.


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    Titel :

    IMPROVED SECOND STAGE TURBINE BLADE


    Weitere Titelangaben:

    VERBESSERTE ZWEITSTUFENTURBINENSCHAUFEL
    AUBE DE TURBINE DE SECOND ÉTAGE AMÉLIORÉE


    Beteiligte:
    PARKER DAVID G (Autor:in) / XIAO ZHENHUA (Autor:in) / YU RICHARD (Autor:in) / MARTLING VINCENT C (Autor:in) / HERBER PAUL GREGORY (Autor:in) / STROHL JAMES PAGE (Autor:in)

    Erscheinungsdatum :

    2022-03-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge



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