Turbine nozzle airfoil profile
    41.
    发明授权

    公开(公告)号:US08814526B2

    公开(公告)日:2014-08-26

    申请号:US13304732

    申请日:2011-11-28

    CPC classification number: F01D9/02 F05D2250/74

    Abstract: A turbine nozzle is provided including a nozzle airfoil having an airfoil shape, the nozzle airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in inches by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z, the airfoil profile sections at Z distances being joined smoothly with one another to form a complete airfoil shape.

    TURBOMACHINE COMPONENT HAVING A FLOW CONTOUR FEATURE
    42.
    发明申请
    TURBOMACHINE COMPONENT HAVING A FLOW CONTOUR FEATURE 审中-公开
    具有流动特征的涡轮机组件

    公开(公告)号:US20130089430A1

    公开(公告)日:2013-04-11

    申请号:US13270377

    申请日:2011-10-11

    CPC classification number: F01D11/001 F01D5/145

    Abstract: A turbomachine component includes a main body having a gas path surface configured to be exposed to gases passing along a turbomachine gas path, a non gas path surface configured to be arranged in a turbomachine wheelspace outside the turbomachine gas path, and a non-axisymetric flow contour feature extending from the gas path surface to the non gas path surface.

    Abstract translation: 涡轮机械部件包括主体,该主体具有构造成暴露于沿着涡轮机气体通路的气体的气体通路面,构造成布置在涡轮机气路外的涡轮机轮空间中的非气路面,以及非轴测流 轮廓特征从气体路径表面延伸到非气体路径表面。

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